- g(SpacecraftState) - Method in class org.orekit.forces.maneuvers.ImpulseManeuver
-
Compute the value of the switching function.
- g(SpacecraftState) - Method in class org.orekit.propagation.events.AbstractDetector
-
Compute the value of the switching function.
- g(SpacecraftState) - Method in class org.orekit.propagation.events.AdapterDetector
-
Compute the value of the switching function.
- g(SpacecraftState) - Method in class org.orekit.propagation.events.AlignmentDetector
-
Compute the value of the switching function.
- g(SpacecraftState) - Method in class org.orekit.propagation.events.AltitudeDetector
-
Compute the value of the switching function.
- g(SpacecraftState) - Method in class org.orekit.propagation.events.AngularSeparationDetector
-
Compute the value of the switching function.
- g(SpacecraftState) - Method in class org.orekit.propagation.events.AngularSeparationFromSatelliteDetector
-
Compute the value of the switching function.
- g(SpacecraftState) - Method in class org.orekit.propagation.events.ApsideDetector
-
Compute the value of the switching function.
- g(SpacecraftState) - Method in class org.orekit.propagation.events.BooleanDetector
-
- g(SpacecraftState) - Method in class org.orekit.propagation.events.DateDetector
-
Compute the value of the switching function.
- g(SpacecraftState) - Method in class org.orekit.propagation.events.EclipseDetector
-
Compute the value of the switching function.
- g(SpacecraftState) - Method in class org.orekit.propagation.events.ElevationDetector
-
Compute the value of the switching function.
- g(SpacecraftState) - Method in class org.orekit.propagation.events.ElevationExtremumDetector
-
Compute the value of the detection function.
- g(SpacecraftState) - Method in interface org.orekit.propagation.events.EventDetector
-
Compute the value of the switching function.
- g(SpacecraftState) - Method in class org.orekit.propagation.events.EventEnablingPredicateFilter
-
Compute the value of the switching function.
- g(SpacecraftState) - Method in class org.orekit.propagation.events.EventShifter
-
Compute the value of the switching function.
- g(SpacecraftState) - Method in class org.orekit.propagation.events.EventSlopeFilter
-
Compute the value of the switching function.
- g(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.events.FieldAbstractDetector
-
Compute the value of the switching function.
- g(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.events.FieldAltitudeDetector
-
Compute the value of the switching function.
- g(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.events.FieldApsideDetector
-
Compute the value of the switching function.
- g(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.events.FieldDateDetector
-
Compute the value of the switching function.
- g(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.events.FieldEclipseDetector
-
Compute the value of the switching function.
- g(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.events.FieldElevationDetector
-
Compute the value of the switching function.
- g(FieldSpacecraftState<T>) - Method in interface org.orekit.propagation.events.FieldEventDetector
-
Compute the value of the switching function.
- g(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.events.FieldFunctionalDetector
-
- g(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.events.FieldLatitudeCrossingDetector
-
Compute the value of the detection function.
- g(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.events.FieldNodeDetector
-
Compute the value of the switching function.
- g(SpacecraftState) - Method in class org.orekit.propagation.events.FieldOfViewDetector
-
Compute the value of the switching function.
- g(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.events.FieldParameterDrivenDateIntervalDetector
-
Compute the value of the switching function.
- g(SpacecraftState) - Method in class org.orekit.propagation.events.FootprintOverlapDetector
-
Compute the value of the switching function.
- g(SpacecraftState) - Method in class org.orekit.propagation.events.FunctionalDetector
-
- g(SpacecraftState) - Method in class org.orekit.propagation.events.GeographicZoneDetector
-
Compute the value of the detection function.
- g(SpacecraftState) - Method in class org.orekit.propagation.events.GroundAtNightDetector
-
Compute the value of the switching function.
- g(SpacecraftState) - Method in class org.orekit.propagation.events.GroundFieldOfViewDetector
-
Compute the value of the switching function.
- g(SpacecraftState) - Method in class org.orekit.propagation.events.HaloXZPlaneCrossingDetector
-
Compute the value of the detection function.
- g(SpacecraftState) - Method in class org.orekit.propagation.events.InterSatDirectViewDetector
-
Compute the value of the switching function.
- g(SpacecraftState) - Method in class org.orekit.propagation.events.LatitudeCrossingDetector
-
Compute the value of the detection function.
- g(SpacecraftState) - Method in class org.orekit.propagation.events.LatitudeExtremumDetector
-
Compute the value of the detection function.
- g(SpacecraftState) - Method in class org.orekit.propagation.events.LongitudeCrossingDetector
-
Compute the value of the detection function.
- g(SpacecraftState) - Method in class org.orekit.propagation.events.LongitudeExtremumDetector
-
Compute the value of the detection function.
- g(SpacecraftState) - Method in class org.orekit.propagation.events.MagneticFieldDetector
-
Compute the value of the detection function.
- g(SpacecraftState) - Method in class org.orekit.propagation.events.NegateDetector
-
- g(SpacecraftState) - Method in class org.orekit.propagation.events.NodeDetector
-
Compute the value of the switching function.
- g(SpacecraftState) - Method in class org.orekit.propagation.events.ParameterDrivenDateIntervalDetector
-
Compute the value of the switching function.
- g(SpacecraftState) - Method in class org.orekit.propagation.events.PositionAngleDetector
-
Compute the value of the detection function.
- G0_STANDARD_GRAVITY - Static variable in interface org.orekit.utils.Constants
-
Standard gravity constant, used in maneuvers definition: 9.80665 m/s².
- Galileo - Class in org.orekit.gnss.attitude
-
Attitude providers for Galileo navigation satellites.
- Galileo(double, AbsoluteDate, AbsoluteDate, ExtendedPVCoordinatesProvider, Frame) - Constructor for class org.orekit.gnss.attitude.Galileo
-
Simple constructor.
- GALILEO_AV - Static variable in interface org.orekit.propagation.analytical.gnss.data.GNSSConstants
-
Value of the earth's rotation rate in rad/s for Galileo user.
- GALILEO_EPOCH - Static variable in class org.orekit.time.AbsoluteDate
-
Reference epoch for Galileo System Time: 1999-08-22T00:00:00 GST.
- GALILEO_EPOCH - Static variable in class org.orekit.time.DateComponents
-
Reference epoch for Galileo System Time: 1999-08-22.
- GALILEO_MU - Static variable in interface org.orekit.propagation.analytical.gnss.data.GNSSConstants
-
Earth's universal gravitational parameter for Galileo user in m³/s².
- GALILEO_WEEK_NB - Static variable in interface org.orekit.propagation.analytical.gnss.data.GNSSConstants
-
Number of weeks in the Galileo cycle.
- GalileoAlmanac - Class in org.orekit.propagation.analytical.gnss.data
-
Class for Galileo almanac.
- GalileoAlmanac() - Constructor for class org.orekit.propagation.analytical.gnss.data.GalileoAlmanac
-
Build a new almanac.
- GalileoNavigationMessage - Class in org.orekit.propagation.analytical.gnss.data
-
Container for data contained in a Galileo navigation message.
- GalileoNavigationMessage() - Constructor for class org.orekit.propagation.analytical.gnss.data.GalileoNavigationMessage
-
Constructor.
- GalileoScale - Class in org.orekit.time
-
Galileo system time scale.
- GammaMnsFunction - Class in org.orekit.propagation.semianalytical.dsst.utilities
-
Compute the Γmn,s(γ) function from equation 2.7.1-(13).
- GammaMnsFunction(int, double, int) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.GammaMnsFunction
-
Simple constructor.
- generate(List<OrekitStepInterpolator>) - Method in class org.orekit.estimation.measurements.generation.ContinuousScheduler
-
Generate a sequence of measurements.
- generate(List<OrekitStepInterpolator>) - Method in class org.orekit.estimation.measurements.generation.EventBasedScheduler
-
Generate a sequence of measurements.
- generate(AbsoluteDate, AbsoluteDate) - Method in class org.orekit.estimation.measurements.generation.Generator
-
Generate measurements.
- generate(List<OrekitStepInterpolator>) - Method in interface org.orekit.estimation.measurements.generation.Scheduler
-
Generate a sequence of measurements.
- generate(AbsoluteDate, AbsoluteDate) - Method in class org.orekit.frames.FieldTransformGenerator
-
Generate a chronologically sorted list of entries to be cached.
- generate(AbsoluteDate, AbsoluteDate) - Method in class org.orekit.frames.TransformGenerator
-
Generate a chronologically sorted list of entries to be cached.
- generate(AbsoluteDate, AbsoluteDate) - Method in interface org.orekit.utils.TimeStampedGenerator
-
Generate a chronologically sorted list of entries to be cached.
- generateCartesianOrbit() - Method in class org.orekit.files.ccsds.ndm.odm.opm.Opm
-
Generate a Cartesian orbit.
- generateException(Exception) - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken
-
Generate a parse exception for this entry.
- generateKeplerianOrbit(Frame) - Method in class org.orekit.files.ccsds.ndm.odm.KeplerianElements
-
Generate a keplerian orbit.
- generateKeplerianOrbit() - Method in class org.orekit.files.ccsds.ndm.odm.omm.Omm
-
Generate a keplerian orbit.
- generateKeplerianOrbit() - Method in class org.orekit.files.ccsds.ndm.odm.opm.Opm
-
Generate a keplerian orbit.
- generateSpacecraftState() - Method in class org.orekit.files.ccsds.ndm.odm.omm.Omm
-
Generate spacecraft state from the
CartesianOrbit
generated by generateCartesianOrbit.
- generateSpacecraftState() - Method in class org.orekit.files.ccsds.ndm.odm.opm.Opm
-
Generate spacecraft state from the
CartesianOrbit
generated by generateCartesianOrbit.
- generateTLE() - Method in class org.orekit.files.ccsds.ndm.odm.omm.Omm
-
Generate TLE from OMM file.
- Generator - Class in org.orekit.estimation.measurements.generation
-
- Generator() - Constructor for class org.orekit.estimation.measurements.generation.Generator
-
Build a generator with no sequences generator.
- Generator - Interface in org.orekit.files.ccsds.utils.generation
-
Generation interface for CCSDS messages.
- GenericGNSS - Class in org.orekit.gnss.attitude
-
Attitude providers for navigation satellites for which no specialized model is known.
- GenericGNSS(AbsoluteDate, AbsoluteDate, ExtendedPVCoordinatesProvider, Frame) - Constructor for class org.orekit.gnss.attitude.GenericGNSS
-
Simple constructor.
- GenericTimeStampedCache<T extends TimeStamped> - Class in org.orekit.utils
-
- GenericTimeStampedCache(int, int, double, double, TimeStampedGenerator<T>) - Constructor for class org.orekit.utils.GenericTimeStampedCache
-
Simple constructor.
- GeodeticPoint - Class in org.orekit.bodies
-
Point location relative to a 2D body surface.
- GeodeticPoint(double, double, double) - Constructor for class org.orekit.bodies.GeodeticPoint
-
Build a new instance.
- GeographicZoneDetector - Class in org.orekit.propagation.events
-
Detector for entry/exit of a zone defined by geographic boundaries.
- GeographicZoneDetector(BodyShape, SphericalPolygonsSet, double) - Constructor for class org.orekit.propagation.events.GeographicZoneDetector
-
Build a new detector.
- GeographicZoneDetector(double, double, BodyShape, SphericalPolygonsSet, double) - Constructor for class org.orekit.propagation.events.GeographicZoneDetector
-
Build a detector.
- Geoid - Class in org.orekit.models.earth
-
A geoid is a level surface of the gravity potential of a body.
- Geoid(NormalizedSphericalHarmonicsProvider, ReferenceEllipsoid) - Constructor for class org.orekit.models.earth.Geoid
-
Creates a geoid from the given geopotential, reference ellipsoid and the
assumptions in the comment for
Geoid
.
- GeoMagneticElements - Class in org.orekit.models.earth
-
Contains the elements to represent a magnetic field at a single point.
- GeoMagneticElements(Vector3D) - Constructor for class org.orekit.models.earth.GeoMagneticElements
-
Construct a new element with the given field vector.
- GeoMagneticField - Class in org.orekit.models.earth
-
Used to calculate the geomagnetic field at a given geodetic point on earth.
- GeoMagneticField(String, double, int, int, double, double) - Constructor for class org.orekit.models.earth.GeoMagneticField
-
Create a new geomagnetic field model with the given parameters.
- GeoMagneticFieldFactory - Class in org.orekit.models.earth
-
- GeoMagneticFieldFactory.FieldModel - Enum in org.orekit.models.earth
-
The currently supported geomagnetic field models.
- GeoMagneticFields - Interface in org.orekit.models.earth
-
Methods for obtaining geomagnetic fields.
- GeoMagneticModelLoader - Class in org.orekit.models.earth
-
Loads geomagnetic field models from a given input stream.
- GeoMagneticModelLoader() - Constructor for class org.orekit.models.earth.GeoMagneticModelLoader
-
- GeometryFreeCombination - Class in org.orekit.estimation.measurements.gnss
-
Geometry-free combination.
- GeometryFreeCycleSlipDetector - Class in org.orekit.estimation.measurements.gnss
-
Geometry free cycle slip detectors.
- GeometryFreeCycleSlipDetector(double, double, int) - Constructor for class org.orekit.estimation.measurements.gnss.GeometryFreeCycleSlipDetector
-
Constructor.
- get(String) - Method in class org.orekit.utils.DoubleArrayDictionary
-
Get the value corresponding to a key.
- get(String) - Method in class org.orekit.utils.FieldArrayDictionary
-
Get the value corresponding to a key.
- get(FieldAbsoluteDate<D>) - Method in class org.orekit.utils.FieldTimeSpanMap
-
Get the entry valid at a specified date.
- get(AbsoluteDate) - Method in class org.orekit.utils.TimeSpanMap
-
Get the entry valid at a specified date.
- get24HoursKp(AbsoluteDate) - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherData
-
Get the last 24H mean geomagnetic index.
- get24HoursKp(AbsoluteDate) - Method in class org.orekit.models.earth.atmosphere.data.MarshallSolarActivityFutureEstimation
-
The Kp index is derived from the Ap index.
- get24HoursKp(AbsoluteDate) - Method in interface org.orekit.models.earth.atmosphere.DTM2000InputParameters
-
Get the last 24H mean geomagnetic index.
- getA() - Method in class org.orekit.bodies.Ellipse
-
Get the semi major axis.
- getA() - Method in class org.orekit.bodies.Ellipsoid
-
Get the length of the first semi-axis.
- getA() - Method in class org.orekit.files.ccsds.ndm.odm.KeplerianElements
-
Get the orbit semi-major axis.
- getA() - Method in class org.orekit.models.earth.troposphere.ViennaModelCoefficientsLoader
-
Returns the a coefficients array.
- getA() - Method in class org.orekit.models.earth.weather.GlobalPressureTemperature2Model
-
Returns the a coefficients array.
- getA() - Method in class org.orekit.orbits.CartesianOrbit
-
Get the semi-major axis.
- getA() - Method in class org.orekit.orbits.CircularOrbit
-
Get the semi-major axis.
- getA() - Method in class org.orekit.orbits.EquinoctialOrbit
-
Get the semi-major axis.
- getA() - Method in class org.orekit.orbits.FieldCartesianOrbit
-
Get the semi-major axis.
- getA() - Method in class org.orekit.orbits.FieldCircularOrbit
-
Get the semi-major axis.
- getA() - Method in class org.orekit.orbits.FieldEquinoctialOrbit
-
Get the semi-major axis.
- getA() - Method in class org.orekit.orbits.FieldKeplerianOrbit
-
Get the semi-major axis.
- getA() - Method in class org.orekit.orbits.FieldOrbit
-
Get the semi-major axis.
- getA() - Method in class org.orekit.orbits.KeplerianOrbit
-
Get the semi-major axis.
- getA() - Method in class org.orekit.orbits.Orbit
-
Get the semi-major axis.
- getA() - Method in class org.orekit.propagation.FieldSpacecraftState
-
Get the semi-major axis.
- getA() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBodyContext
-
Get A = sqrt(μ * a).
- getA() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldAbstractGaussianContributionContext
-
Get A = sqrt(μ * a).
- getA() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTThirdBodyContext
-
Get A = sqrt(μ * a).
- getA() - Method in class org.orekit.propagation.SpacecraftState
-
Get the semi-major axis.
- getAbscissaGrid() - Method in class org.orekit.utils.InterpolationTableLoader
-
Returns a copy of the abscissa grid for the interpolation function.
- getAbsoluteDate() - Method in class org.orekit.utils.FieldTimeSpanMap.Transition
-
Get the transition field absolute date.
- getAbsPVA() - Method in class org.orekit.propagation.FieldSpacecraftState
-
Get the absolute position-velocity-acceleration.
- getAbsPVA() - Method in class org.orekit.propagation.SpacecraftState
-
Get the absolute position-velocity-acceleration.
- getAcceleration() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Maneuver
-
Get acceleration.
- getAcceleration(SpacecraftState, Attitude, double[]) - Method in interface org.orekit.forces.maneuvers.propulsion.PropulsionModel
-
Get the acceleration of the spacecraft during maneuver and in maneuver frame.
- getAcceleration(FieldSpacecraftState<T>, FieldAttitude<T>, T[]) - Method in interface org.orekit.forces.maneuvers.propulsion.PropulsionModel
-
Get the acceleration of the spacecraft during maneuver and in maneuver frame.
- getAcceleration(SpacecraftState, Attitude, double[]) - Method in interface org.orekit.forces.maneuvers.propulsion.ThrustPropulsionModel
-
Get the acceleration of the spacecraft during maneuver and in maneuver frame.
- getAcceleration(FieldSpacecraftState<T>, FieldAttitude<T>, T[]) - Method in interface org.orekit.forces.maneuvers.propulsion.ThrustPropulsionModel
-
Get the acceleration of the spacecraft during maneuver and in maneuver frame.
- getAcceleration() - Method in class org.orekit.frames.FieldTransform
-
Get the second time derivative of the translation.
- getAcceleration() - Method in class org.orekit.frames.Transform
-
Get the second time derivative of the translation.
- getAcceleration() - Method in class org.orekit.utils.FieldPVCoordinates
-
Gets the acceleration.
- getAcceleration() - Method in class org.orekit.utils.PVCoordinates
-
Gets the acceleration.
- getAccelerationDirectionSigma() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Maneuver
-
Get one σ angular off-nominal acceleration direction.
- getAccelerationInterpolation() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Maneuver
-
Get interpolation mode between current and next acceleration line.
- getAccelerationMagnitudeSigma() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Maneuver
-
Get one σ percent error on acceleration magnitude.
- getAccelerationModel(AbsoluteDate) - Method in class org.orekit.forces.empirical.TimeSpanParametricAcceleration
-
- getAccelerationModelSpan(AbsoluteDate) - Method in class org.orekit.forces.empirical.TimeSpanParametricAcceleration
-
- getAccuracy(int) - Method in class org.orekit.files.sp3.SP3
-
Get the formal accuracy for a satellite.
- getAccuracy() - Method in class org.orekit.files.sp3.SP3.SP3Ephemeris
-
Get the formal accuracy for this satellite.
- getAccuracy() - Method in interface org.orekit.gnss.metric.messages.rtcm.ephemeris.utils.AccuracyProvider
-
Get the accuracy of the ephemeris data from an accuracy index.
- getAccuracy() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.utils.GlonassUserRangeAccuracy
-
Get the accuracy of the ephemeris data from an accuracy index.
- getAccuracy() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.utils.SignalInSpaceAccuracy
-
Get the accuracy of the ephemeris data from an accuracy index.
- getAccuracy() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.utils.UserRangeAccuracy
-
Get the accuracy of the ephemeris data from an accuracy index.
- getAccuracyProvider() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.RtcmEphemerisData
-
Get the accuracy provider of the ephemeris message.
- getAction() - Method in class org.orekit.propagation.events.EventState.EventOccurrence
-
Get the user requested action.
- getAction() - Method in class org.orekit.propagation.events.FieldEventState.EventOccurrence
-
Get the user requested action.
- getActualOdSpan() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
-
Get actual time span used for the OD of the object.
- getAdaptedPropagator() - Method in class org.orekit.propagation.conversion.AbstractPropagatorConverter
-
Get the adapted propagator.
- getAdditionalDerivativesProviders() - Method in class org.orekit.propagation.conversion.AbstractPropagatorBuilder
-
Get the list of additional equations.
- getAdditionalDerivativesProviders() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
-
Get an unmodifiable list of providers for additional derivatives.
- getAdditionalDerivativesProviders() - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator
-
Get an unmodifiable list of providers for additional derivatives.
- getAdditionalEquations() - Method in class org.orekit.propagation.conversion.AbstractPropagatorBuilder
-
- getAdditionalState(SpacecraftState) - Method in class org.orekit.forces.maneuvers.jacobians.Duration
-
Get the additional state.
- getAdditionalState(SpacecraftState) - Method in class org.orekit.forces.maneuvers.jacobians.MedianDate
-
Get the additional state.
- getAdditionalState(SpacecraftState) - Method in class org.orekit.forces.maneuvers.jacobians.TriggerDate
-
Get the additional state.
- getAdditionalState(SpacecraftState) - Method in interface org.orekit.propagation.AdditionalStateProvider
-
Get the additional state.
- getAdditionalState(SpacecraftState) - Method in class org.orekit.propagation.analytical.gnss.ClockCorrectionsProvider
-
Get the additional state.
- getAdditionalState(FieldSpacecraftState<T>) - Method in interface org.orekit.propagation.FieldAdditionalStateProvider
-
Get the additional state.
- getAdditionalState(String) - Method in class org.orekit.propagation.FieldSpacecraftState
-
Get an additional state.
- getAdditionalState(String) - Method in class org.orekit.propagation.SpacecraftState
-
Get an additional state.
- getAdditionalStateDerivative(String) - Method in class org.orekit.propagation.FieldSpacecraftState
-
Get an additional state derivative.
- getAdditionalStateDerivative(String) - Method in class org.orekit.propagation.SpacecraftState
-
Get an additional state derivative.
- getAdditionalStateDimension() - Method in class org.orekit.propagation.integration.AbstractJacobiansMapper
-
Compute the length of the one-dimensional additional state array needed.
- getAdditionalStateProviders() - Method in class org.orekit.propagation.AbstractPropagator
-
Get an unmodifiable list of providers for additional state.
- getAdditionalStateProviders() - Method in class org.orekit.propagation.FieldAbstractPropagator
-
Get an unmodifiable list of providers for additional state.
- getAdditionalStateProviders() - Method in interface org.orekit.propagation.FieldPropagator
-
Get an unmodifiable list of providers for additional state.
- getAdditionalStateProviders() - Method in interface org.orekit.propagation.Propagator
-
Get an unmodifiable list of providers for additional state.
- getAdditionalStates() - Method in class org.orekit.propagation.FieldSpacecraftState
-
- getAdditionalStates() - Method in class org.orekit.propagation.SpacecraftState
-
- getAdditionalStatesDerivatives() - Method in class org.orekit.propagation.FieldSpacecraftState
-
Get an unmodifiable map of additional states derivatives.
- getAdditionalStatesDerivatives() - Method in class org.orekit.propagation.SpacecraftState
-
Get an unmodifiable map of additional states derivatives.
- getAdditionalStatesValues() - Method in class org.orekit.propagation.FieldSpacecraftState
-
Get an unmodifiable map of additional states.
- getAdditionalStatesValues() - Method in class org.orekit.propagation.SpacecraftState
-
Get an unmodifiable map of additional states.
- getAdmMessageLink() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
-
Get the Unique identifier of Attitude Data Message linked to this Orbit Data Message.
- getADot() - Method in class org.orekit.orbits.CartesianOrbit
-
Get the semi-major axis derivative.
- getADot() - Method in class org.orekit.orbits.CircularOrbit
-
Get the semi-major axis derivative.
- getADot() - Method in class org.orekit.orbits.EquinoctialOrbit
-
Get the semi-major axis derivative.
- getADot() - Method in class org.orekit.orbits.FieldCartesianOrbit
-
Get the semi-major axis derivative.
- getADot() - Method in class org.orekit.orbits.FieldCircularOrbit
-
Get the semi-major axis derivative.
- getADot() - Method in class org.orekit.orbits.FieldEquinoctialOrbit
-
Get the semi-major axis derivative.
- getADot() - Method in class org.orekit.orbits.FieldKeplerianOrbit
-
Get the semi-major axis derivative.
- getADot() - Method in class org.orekit.orbits.FieldOrbit
-
Get the semi-major axis derivative.
- getADot() - Method in class org.orekit.orbits.KeplerianOrbit
-
Get the semi-major axis derivative.
- getADot() - Method in class org.orekit.orbits.Orbit
-
Get the semi-major axis derivative.
- getAe() - Method in class org.orekit.forces.gravity.potential.CachedNormalizedSphericalHarmonicsProvider
-
Get the value of the central body reference radius.
- getAe() - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
-
Get the central body reference radius.
- getAe() - Method in interface org.orekit.forces.gravity.potential.SphericalHarmonicsProvider
-
Get the value of the central body reference radius.
- getAf0() - Method in class org.orekit.propagation.analytical.gnss.data.CommonGnssData
-
Getter for the the SV Clock Bias Correction Coefficient.
- getAf0() - Method in interface org.orekit.propagation.analytical.gnss.data.GNSSClockElements
-
Gets the Zeroth Order Clock Correction.
- getAf1() - Method in class org.orekit.propagation.analytical.gnss.data.CommonGnssData
-
Getter for the SV Clock Drift Correction Coefficient.
- getAf1() - Method in interface org.orekit.propagation.analytical.gnss.data.GNSSClockElements
-
Gets the First Order Clock Correction.
- getAf2() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractAlmanac
-
Getter for the Drift Rate Correction Coefficient.
- getAf2() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractNavigationMessage
-
Getter for the Drift Rate Correction Coefficient.
- getAf2() - Method in interface org.orekit.propagation.analytical.gnss.data.GNSSClockElements
-
Gets the Second Order Clock Correction.
- getAfter() - Method in class org.orekit.utils.FieldTimeSpanMap.Transition
-
Get the entry valid after transition.
- getAfter() - Method in class org.orekit.utils.TimeSpanMap.Transition
-
Get the entry valid after transition.
- getAgency() - Method in class org.orekit.files.sp3.SP3
-
Returns the agency that prepared this SP3 file.
- getAgencyName() - Method in class org.orekit.gnss.clock.RinexClock
-
Getter for the agency name.
- getAgencyName() - Method in class org.orekit.gnss.navigation.RinexNavigation
-
Getter for the agency name.
- getAgencyName() - Method in class org.orekit.gnss.RinexObservationHeader
-
Get name of the agency.
- getAGf0() - Method in class org.orekit.propagation.analytical.gnss.data.SBASNavigationMessage
-
Gets the Zeroth Order Clock Correction.
- getAGf0() - Method in interface org.orekit.propagation.analytical.gnss.data.SBASOrbitalElements
-
Gets the Zeroth Order Clock Correction.
- getAGf1() - Method in class org.orekit.propagation.analytical.gnss.data.SBASNavigationMessage
-
Gets the First Order Clock Correction.
- getAGf1() - Method in interface org.orekit.propagation.analytical.gnss.data.SBASOrbitalElements
-
Gets the First Order Clock Correction.
- getAlbedoGridSize() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
-
Get albedo grid size.
- getAlbedoModel() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
-
Get albedo model.
- getAlignAngle() - Method in class org.orekit.propagation.events.AlignmentDetector
-
Get the alignment angle (rad).
- getAll() - Method in class org.orekit.utils.ImmutableTimeStampedCache
-
Get all of the data in this cache.
- getAllAmbiguityDrivers() - Method in class org.orekit.estimation.measurements.gnss.AmbiguitySolver
-
Get all the ambiguity parameters drivers.
- getAllForceModels() - Method in class org.orekit.propagation.conversion.DSSTPropagatorBuilder
-
Get the list of all force models.
- getAllForceModels() - Method in class org.orekit.propagation.conversion.NumericalPropagatorBuilder
-
Get the list of all force models.
- getAllForceModels() - Method in class org.orekit.propagation.numerical.FieldNumericalPropagator
-
Get all the force models, perturbing forces and Newtonian attraction included.
- getAllForceModels() - Method in class org.orekit.propagation.numerical.NumericalPropagator
-
Get all the force models, perturbing forces and Newtonian attraction included.
- getAllForceModels() - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator
-
Get all the force models, perturbing forces and Newtonian attraction included.
- getAllForceModels() - Method in class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator
-
Get all the force models, perturbing forces and Newtonian attraction included.
- getAlmanacs() - Method in class org.orekit.gnss.SEMParser
-
- getAlmanacs() - Method in class org.orekit.gnss.YUMAParser
-
- getAlpha() - Method in class org.orekit.models.earth.ionosphere.KlobucharIonoCoefficientsLoader
-
Returns the alpha coefficients array.
- getAlpha(PositionAngle) - Method in class org.orekit.orbits.CircularOrbit
-
Get the latitude argument.
- getAlpha(PositionAngle) - Method in class org.orekit.orbits.FieldCircularOrbit
-
Get the latitude argument.
- getAlpha() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBodyContext
-
Get direction cosine α for central body.
- getAlpha() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTThirdBodyContext
-
Get direction cosine α for central body.
- getAlpha() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
-
Get direction cosine α for central body.
- getAlpha() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldAuxiliaryElements
-
Get direction cosine α for central body.
- getAlphaDot(PositionAngle) - Method in class org.orekit.orbits.CircularOrbit
-
Get the latitude argument derivative.
- getAlphaDot(PositionAngle) - Method in class org.orekit.orbits.FieldCircularOrbit
-
Get the latitude argument derivative.
- getAlphaE() - Method in class org.orekit.orbits.CircularOrbit
-
Get the eccentric latitude argument.
- getAlphaE() - Method in class org.orekit.orbits.FieldCircularOrbit
-
Get the eccentric latitude argument.
- getAlphaEDot() - Method in class org.orekit.orbits.CircularOrbit
-
Get the eccentric latitude argument derivative.
- getAlphaEDot() - Method in class org.orekit.orbits.FieldCircularOrbit
-
Get the eccentric latitude argument derivative.
- getAlphaM() - Method in class org.orekit.orbits.CircularOrbit
-
Get the mean latitude argument.
- getAlphaM() - Method in class org.orekit.orbits.FieldCircularOrbit
-
Get the mean latitude argument.
- getAlphaMDot() - Method in class org.orekit.orbits.CircularOrbit
-
Get the mean latitude argument derivative.
- getAlphaMDot() - Method in class org.orekit.orbits.FieldCircularOrbit
-
Get the mean latitude argument derivative.
- getAlphaV() - Method in class org.orekit.orbits.CircularOrbit
-
Get the true latitude argument.
- getAlphaV() - Method in class org.orekit.orbits.FieldCircularOrbit
-
Get the true latitude argument.
- getAlphaVDot() - Method in class org.orekit.orbits.CircularOrbit
-
Get the true latitude argument derivative.
- getAlphaVDot() - Method in class org.orekit.orbits.FieldCircularOrbit
-
Get the true latitude argument derivative.
- getAlternateNames() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
-
Get the alternate names for this space object.
- getAltitude() - Method in class org.orekit.bodies.FieldGeodeticPoint
-
Get the altitude.
- getAltitude() - Method in class org.orekit.bodies.GeodeticPoint
-
Get the altitude.
- getAltitude() - Method in class org.orekit.propagation.events.AltitudeDetector
-
Get the threshold altitude value.
- getAltitude() - Method in class org.orekit.propagation.events.FieldAltitudeDetector
-
Get the threshold altitude value.
- getAmbiguityDriver() - Method in class org.orekit.estimation.measurements.gnss.InterSatellitesPhase
-
Get the driver for phase ambiguity.
- getAmbiguityDriver() - Method in class org.orekit.estimation.measurements.gnss.OneWayGNSSPhase
-
Get the driver for phase ambiguity.
- getAmbiguityDriver() - Method in class org.orekit.estimation.measurements.gnss.Phase
-
Get the driver for phase ambiguity.
- getAmplifierBandwidth() - Method in class org.orekit.files.ilrs.CRDConfiguration.DetectorConfiguration
-
Get the amplifier bandwidth.
- getAmplifierGain() - Method in class org.orekit.files.ilrs.CRDConfiguration.DetectorConfiguration
-
Get the amplifier gain.
- getAmplifierInUse() - Method in class org.orekit.files.ilrs.CRDConfiguration.DetectorConfiguration
-
Get the amplifier in use.
- getAnalysisCenterID() - Method in class org.orekit.gnss.clock.RinexClock
-
Getter for the analysis center ID.
- getAnalysisCenterName() - Method in class org.orekit.gnss.clock.RinexClock
-
Getter for the analysis center name.
- getAncestor(int) - Method in class org.orekit.frames.Frame
-
Get the nth ancestor of the frame.
- getAngle() - Method in class org.orekit.propagation.events.PositionAngleDetector
-
Get the fixed angle to be crossed (radians).
- getAngle() - Method in class org.orekit.utils.units.Unit
-
Get the angle exponent.
- getAnglesData() - Method in class org.orekit.files.ilrs.CRD.CRDDataBlock
-
Get the angles data for the data block.
- getAngleType() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
-
Getter for angleType.
- getAngular() - Method in class org.orekit.frames.FieldTransform
-
Get the underlying elementary angular part.
- getAngular() - Method in class org.orekit.frames.Transform
-
Get the underlying elementary angular part.
- getAngularCoordinates() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemData
-
Get an unmodifiable view of the data points.
- getAngularCoordinates() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemSegment
-
Get an unmodifiable list of attitude data lines.
- getAngularCoordinates() - Method in interface org.orekit.files.general.AttitudeEphemerisFile.AttitudeEphemerisSegment
-
Get an unmodifiable list of attitude data lines.
- getAngularCoordinates() - Method in class org.orekit.files.general.OrekitAttitudeEphemerisFile.OrekitAttitudeEphemerisSegment
-
Get an unmodifiable list of attitude data lines.
- getAngularDerivativesFilter() - Method in enum org.orekit.files.ccsds.ndm.adm.AttitudeType
-
Get the angular derivative filter corresponding to the attitude data.
- getAngularVelocity() - Method in class org.orekit.propagation.analytical.gnss.data.CommonGnssData
-
Getter for the mean angular velocity of the Earth for the GNSS model.
- getAngularVelocity() - Method in interface org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElements
-
Gets the mean angular velocity of the Earth of the GNSS model.
- getAngularVelocity() - Method in class org.orekit.utils.FieldPVCoordinates
-
Get the angular velocity (spin) of this point as seen from the origin.
- getAngularVelocity() - Method in class org.orekit.utils.PVCoordinates
-
Get the angular velocity (spin) of this point as seen from the origin.
- getAnomaly() - Method in class org.orekit.files.ccsds.ndm.odm.KeplerianElements
-
Get the orbit anomaly.
- getAnomaly(PositionAngle) - Method in class org.orekit.orbits.FieldKeplerianOrbit
-
Get the anomaly.
- getAnomaly(PositionAngle) - Method in class org.orekit.orbits.KeplerianOrbit
-
Get the anomaly.
- getAnomalyDot(PositionAngle) - Method in class org.orekit.orbits.FieldKeplerianOrbit
-
Get the anomaly derivative.
- getAnomalyDot(PositionAngle) - Method in class org.orekit.orbits.KeplerianOrbit
-
Get the anomaly derivative.
- getAnomalyType() - Method in class org.orekit.files.ccsds.ndm.odm.KeplerianElements
-
Get the type of anomaly (true or mean).
- getAntennaAzimuth() - Method in class org.orekit.gnss.RinexObservationHeader
-
Get the azimuth of the zero direction of a fixed antenna.
- getAntennaBSight() - Method in class org.orekit.gnss.RinexObservationHeader
-
Get the antenna B.Sight.
- getAntennaHeight() - Method in class org.orekit.gnss.RinexObservationHeader
-
Get the antenna height.
- getAntennaNumber() - Method in class org.orekit.gnss.RinexObservationHeader
-
Get the number of the antenna.
- getAntennaPhaseCenter() - Method in class org.orekit.gnss.RinexObservationHeader
-
Get the antenna phasecenter.
- getAntennaReferencePoint() - Method in class org.orekit.gnss.RinexObservationHeader
-
Get the position of antenna reference point for antenna on vehicle.
- getAntennaType() - Method in class org.orekit.gnss.RinexObservationHeader
-
Get the type of the antenna.
- getAntennaZeroDirection() - Method in class org.orekit.gnss.RinexObservationHeader
-
Get the zero direction of antenna.
- getAODC() - Method in class org.orekit.propagation.analytical.gnss.data.BeidouNavigationMessage
-
Getter for the Age Of Data Clock (AODC).
- getAODE() - Method in class org.orekit.propagation.analytical.gnss.data.BeidouNavigationMessage
-
Getter for the Age Of Data Ephemeris (AODE).
- getAoR3Pow() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBodyContext
-
Get the value of a / R3 up to power maxAR3Pow.
- getAoR3Pow() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTThirdBodyContext
-
Get the value of a / R3 up to power maxAR3Pow.
- getAp(AbsoluteDate) - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherData
-
Get the Ap geomagnetic indices.
- getAp(AbsoluteDate) - Method in class org.orekit.models.earth.atmosphere.data.MarshallSolarActivityFutureEstimation
-
Get the Ap geomagnetic indices.
- getAp(AbsoluteDate) - Method in interface org.orekit.models.earth.atmosphere.NRLMSISE00InputParameters
-
Get the Ap geomagnetic indices.
- getApAvg() - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherDataLoader.LineParameters
-
Gets the arithmetic average of all eight Ap indices for the current entry.
- getApplicableWavelength() - Method in class org.orekit.files.ilrs.CRDConfiguration.DetectorConfiguration
-
Get the applicable wavelength.
- getAppliedVoltage() - Method in class org.orekit.files.ilrs.CRDConfiguration.DetectorConfiguration
-
Get the applied voltage.
- getApproxPos() - Method in class org.orekit.gnss.RinexObservationHeader
-
Get the Approximate Marker Position.
- getArbitraryEpoch(Field<T>) - Static method in class org.orekit.time.FieldAbsoluteDate
-
Get an arbitrary date.
- getArea() - Method in class org.orekit.forces.BoxAndSolarArraySpacecraft.Facet
-
Get facet area.
- getAstronomicalAmplitudesMap() - Method in class org.orekit.forces.gravity.potential.AstronomicalAmplitudeReader
-
Get astronomical amplitudes map.
- getAtmosphere() - Method in class org.orekit.forces.drag.DragForce
-
Get the atmospheric model.
- getAtmosphere() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTAtmosphericDrag
-
Get the atmospheric model.
- getAtmosphericModel() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
-
Get name of atmospheric model.
- getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.AggregateBoundedAttitudeProvider
-
Compute the attitude corresponding to an orbital state.
- getAttitude(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.AggregateBoundedAttitudeProvider
-
Compute the attitude corresponding to an orbital state.
- getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in interface org.orekit.attitudes.AttitudeProvider
-
Compute the attitude corresponding to an orbital state.
- getAttitude(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in interface org.orekit.attitudes.AttitudeProvider
-
Compute the attitude corresponding to an orbital state.
- getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.AttitudesSequence
-
Compute the attitude corresponding to an orbital state.
- getAttitude(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.AttitudesSequence
-
Compute the attitude corresponding to an orbital state.
- getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.CelestialBodyPointed
-
Compute the attitude corresponding to an orbital state.
- getAttitude(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.CelestialBodyPointed
-
Compute the attitude corresponding to an orbital state.
- getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.FixedRate
-
Compute the attitude corresponding to an orbital state.
- getAttitude(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.FixedRate
-
Compute the attitude corresponding to an orbital state.
- getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.GroundPointing
-
Compute the attitude corresponding to an orbital state.
- getAttitude(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.GroundPointing
-
Compute the attitude corresponding to an orbital state.
- getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.InertialProvider
-
Compute the attitude corresponding to an orbital state.
- getAttitude(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.InertialProvider
-
Compute the attitude corresponding to an orbital state.
- getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.LofOffset
-
Compute the attitude corresponding to an orbital state.
- getAttitude(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.LofOffset
-
Compute the attitude corresponding to an orbital state.
- getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.LofOffsetPointing
-
Compute the attitude corresponding to an orbital state.
- getAttitude(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.LofOffsetPointing
-
Compute the attitude corresponding to an orbital state.
- getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.SpinStabilized
-
Compute the attitude corresponding to an orbital state.
- getAttitude(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.SpinStabilized
-
Compute the attitude corresponding to an orbital state.
- getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.TabulatedLofOffset
-
Compute the attitude corresponding to an orbital state.
- getAttitude(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.TabulatedLofOffset
-
Compute the attitude corresponding to an orbital state.
- getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.TabulatedProvider
-
Compute the attitude corresponding to an orbital state.
- getAttitude(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.TabulatedProvider
-
Compute the attitude corresponding to an orbital state.
- getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.YawCompensation
-
Compute the attitude corresponding to an orbital state.
- getAttitude(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.YawCompensation
-
Compute the attitude corresponding to an orbital state.
- getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.YawSteering
-
Compute the attitude corresponding to an orbital state.
- getAttitude(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.YawSteering
-
Compute the attitude corresponding to an orbital state.
- getAttitude(Frame, PVCoordinatesProvider) - Method in class org.orekit.files.ccsds.ndm.adm.apm.Apm
-
Get the attitude.
- getAttitude(Frame, PVCoordinatesProvider) - Method in class org.orekit.files.ccsds.ndm.adm.apm.ApmQuaternion
-
Get the attitude.
- getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.forces.maneuvers.propulsion.ThrustDirectionAndAttitudeProvider
-
Compute the attitude corresponding to an orbital state.
- getAttitude(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.forces.maneuvers.propulsion.ThrustDirectionAndAttitudeProvider
-
Compute the attitude corresponding to an orbital state.
- getAttitude() - Method in class org.orekit.propagation.FieldSpacecraftState
-
Get the attitude.
- getAttitude() - Method in class org.orekit.propagation.SpacecraftState
-
Get the attitude.
- getAttitudeActuatorType() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
-
Get the type of actuator for attitude control.
- getAttitudeControlAccuracy() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
-
Get the accuracy of attitude control.
- getAttitudeControlMode() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
-
Get the attitude control mode.
- getAttitudeFromFrame(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.forces.maneuvers.propulsion.ThrustDirectionAndAttitudeProvider
-
Compute the attitude for DIRECTION_IN_FRAME or DIRECTION_IN_LOF types.
- getAttitudeKnowledgeAccuracy() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
-
Get the accuracy of attitude knowledge.
- getAttitudeOverride() - Method in class org.orekit.forces.maneuvers.ImpulseManeuver
-
Get the Attitude Provider to use during maneuver.
- getAttitudeOverride() - Method in class org.orekit.forces.maneuvers.Maneuver
-
Get the attitude override used for the maneuver.
- getAttitudePointingAccuracy() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
-
Get the overall accuracy of spacecraft to maintain attitude.
- getAttitudeProvider() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemSegment
-
Get the attitude provider for this attitude ephemeris segment.
- getAttitudeProvider() - Method in interface org.orekit.files.general.AttitudeEphemerisFile.AttitudeEphemerisSegment
-
Get the attitude provider for this attitude ephemeris segment.
- getAttitudeProvider() - Method in interface org.orekit.files.general.AttitudeEphemerisFile.SatelliteAttitudeEphemeris
-
Get the attitude provider corresponding to this ephemeris, combining data from all
segments
.
- getAttitudeProvider() - Method in class org.orekit.files.general.OrekitAttitudeEphemerisFile.OrekitAttitudeEphemerisSegment
-
Get the attitude provider for this attitude ephemeris segment.
- getAttitudeProvider() - Method in class org.orekit.propagation.AbstractPropagator
-
Get attitude provider.
- getAttitudeProvider() - Method in class org.orekit.propagation.conversion.AbstractPropagatorBuilder
-
Get the attitude provider.
- getAttitudeProvider() - Method in class org.orekit.propagation.FieldAbstractPropagator
-
Get attitude provider.
- getAttitudeProvider() - Method in interface org.orekit.propagation.FieldPropagator
-
Get attitude provider.
- getAttitudeProvider() - Method in class org.orekit.propagation.integration.FieldStateMapper
-
Get the attitude provider.
- getAttitudeProvider() - Method in class org.orekit.propagation.integration.StateMapper
-
Get the attitude provider.
- getAttitudeProvider() - Method in interface org.orekit.propagation.Propagator
-
Get attitude provider.
- getAttitudeType() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemMetadata
-
Get the format of the data lines in the message.
- getAugmentedInitialState(int) - Method in class org.orekit.propagation.numerical.cr3bp.CR3BPMultipleShooter
-
Compute the additional state from the additionalEquations.
- getAugmentedInitialState(SpacecraftState, AdditionalEquations) - Method in class org.orekit.utils.AbstractMultipleShooting
-
- getAugmentedInitialState(int) - Method in class org.orekit.utils.AbstractMultipleShooting
-
Compute the additional state from the additionalEquations.
- getAugmentedInitialState(int) - Method in class org.orekit.utils.MultipleShooter
-
Compute the additional state from the additionalEquations.
- getAuthentication(String) - Static method in enum org.orekit.gnss.metric.ntrip.Authentication
-
Get the authentication type corresponding to a keyword.
- getAuthentication() - Method in class org.orekit.gnss.metric.ntrip.DataStreamRecord
-
Get the authentication method.
- getAuthentication() - Method in class org.orekit.gnss.metric.ntrip.NetworkRecord
-
Get the authentication method.
- getAuxiliaryElements() - Method in class org.orekit.propagation.semianalytical.dsst.forces.ForceModelContext
-
- getAvailableDerivatives() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemSegment
-
Get which derivatives of angular data are available in this attitude ephemeris segment.
- getAvailableDerivatives() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryState
-
Get which derivatives of position are available in this state.
- getAvailableDerivatives() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistory
-
Get which derivatives of position are available in this ephemeris segment.
- getAvailableDerivatives() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemData
-
Get the derivatives available in the block.
- getAvailableDerivatives() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemSegment
-
Get which derivatives of position are available in this ephemeris segment.
- getAvailableDerivatives() - Method in interface org.orekit.files.general.AttitudeEphemerisFile.AttitudeEphemerisSegment
-
Get which derivatives of angular data are available in this attitude ephemeris segment.
- getAvailableDerivatives() - Method in interface org.orekit.files.general.EphemerisFile.EphemerisSegment
-
Get which derivatives of position are available in this ephemeris segment.
- getAvailableDerivatives() - Method in class org.orekit.files.general.OrekitAttitudeEphemerisFile.OrekitAttitudeEphemerisSegment
-
Get which derivatives of angular data are available in this attitude ephemeris segment.
- getAvailableDerivatives() - Method in class org.orekit.files.general.OrekitEphemerisFile.OrekitEphemerisSegment
-
Get which derivatives of position are available in this ephemeris segment.
- getAvailableDerivatives() - Method in class org.orekit.files.ilrs.CPF.CPFEphemeris
-
Get which derivatives of position are available in this ephemeris segment.
- getAvailableDerivatives() - Method in class org.orekit.files.sp3.SP3.SP3Ephemeris
-
- getAverageFlux(AbsoluteDate) - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherData
-
Get the value of the 81 day average of F10.7 solar flux centered on current day.
- getAverageFlux(AbsoluteDate) - Method in class org.orekit.models.earth.atmosphere.data.MarshallSolarActivityFutureEstimation
-
Get the value of the 81 day average of F10.7 solar flux centered on current day.
- getAverageFlux(AbsoluteDate) - Method in interface org.orekit.models.earth.atmosphere.NRLMSISE00InputParameters
-
Get the value of the 81 day average of F10.7 solar flux centered on current day.
- getAx2oA() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseralContext
-
Get ax2oA = 2 * a / A .
- getAx2oA() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTTesseralContext
-
Get ax2oA = 2 * a / A .
- getAzimuth() - Method in class org.orekit.files.ilrs.CRD.AnglesMeasurement
-
Get the azimuth angle.
- getAzimuth(Vector3D, Frame, AbsoluteDate) - Method in class org.orekit.frames.TopocentricFrame
-
Get the azimuth of a point with regards to the topocentric frame center point.
- getAzimuth(FieldVector3D<T>, Frame, FieldAbsoluteDate<T>) - Method in class org.orekit.frames.TopocentricFrame
-
Get the azimuth of a point with regards to the topocentric frame center point.
- getAzimuthRate() - Method in class org.orekit.files.ilrs.CRD.AnglesMeasurement
-
Get the azimuth rate.
- getB() - Method in class org.orekit.bodies.Ellipse
-
Get the semi minor axis.
- getB() - Method in class org.orekit.bodies.Ellipsoid
-
Get the length of the second semi-axis.
- getb() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBodyContext
-
Get b = 1 / (1 + sqrt(1 - e²)) = 1 / (1 + B).
- getb() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTThirdBodyContext
-
Get b = 1 / (1 + sqrt(1 - e²)) = 1 / (1 + B).
- getB() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
-
Get B = sqrt(1 - e²).
- getB() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldAuxiliaryElements
-
Get B = sqrt(1 - e²).
- getB1() - Method in class org.orekit.propagation.semianalytical.dsst.DSSTHarvester
-
Get the Jacobian matrix B1 (B1 = ∂εη/∂Y).
- getB2(SpacecraftState) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTHarvester
-
Get the Jacobian matrix B2 (B2 = ∂Y/∂Y₀).
- getB3(SpacecraftState) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTHarvester
-
Get the Jacobian matrix B3 (B3 = ∂Y/∂P).
- getB4() - Method in class org.orekit.propagation.semianalytical.dsst.DSSTHarvester
-
Get the Jacobian matrix B4 (B4 = ∂εη/∂c).
- getBase() - Method in class org.orekit.utils.units.PowerTerm
-
Get the base term.
- getBaseDate() - Method in class org.orekit.utils.DateDriver
-
Get the base (unshifted) date.
- getBaseEquipment() - Method in class org.orekit.files.ccsds.definitions.SpacecraftBodyFrame
-
Get the quipment on which the frame is located.
- getBaseFrame() - Method in class org.orekit.estimation.measurements.GroundStation
-
Get the base frame associated with the station.
- getBaseName(T) - Method in class org.orekit.data.AbstractListCrawler
-
Get the base name of an input.
- getBaseName(File) - Method in class org.orekit.data.FilesListCrawler
-
Get the base name of an input.
- getBaseName(URL) - Method in class org.orekit.data.NetworkCrawler
-
Get the base name of an input.
- getBaseProvider(boolean, int, int) - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
-
Get a time-independent provider containing base harmonics coefficients.
- getBaseState(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.YawCompensation
-
Compute the base system state at given date, without compensation.
- getBaseState(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.YawCompensation
-
Compute the base system state at given date, without compensation.
- getBaseState(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.YawSteering
-
Compute the base system state at given date, without compensation.
- getBaseState(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.YawSteering
-
Compute the base system state at given date, without compensation.
- getBaseWeight() - Method in class org.orekit.estimation.measurements.AbstractMeasurement
-
Get the base weight associated with the measurement
- getBaseWeight() - Method in class org.orekit.estimation.measurements.generation.AbstractMeasurementBuilder
-
Get the base weight associated with the measurement
- getBaseWeight() - Method in interface org.orekit.estimation.measurements.ObservedMeasurement
-
Get the base weight associated with the measurement
- getBasicDimension() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
-
Get state vector dimension without additional parameters.
- getBasicDimension() - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator
-
Get state vector dimension without additional parameters.
- getBB() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBodyContext
-
Get B².
- getBB() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonalContext
-
Get B * B.
- getBB() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTThirdBodyContext
-
Get B².
- getBB() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTZonalContext
-
Get B * B.
- getBBB() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBodyContext
-
Get B³.
- getBBB() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTThirdBodyContext
-
Get B³.
- getBDT() - Method in class org.orekit.time.LazyLoadedTimeScales
-
- getBDT() - Method in interface org.orekit.time.TimeScales
-
Get the BeiDou Navigation Satellite System time scale.
- getBDT() - Static method in class org.orekit.time.TimeScalesFactory
-
Get the BeiDou Navigation Satellite System time scale.
- getBeacon() - Method in class org.orekit.propagation.events.AngularSeparationDetector
-
Get the beacon at the center of the proximity zone.
- getBeamDivergence() - Method in class org.orekit.files.ilrs.CRDConfiguration.LaserConfiguration
-
Get the beam divergence.
- getBefore() - Method in class org.orekit.utils.FieldTimeSpanMap.Transition
-
Get the entry valid before transition.
- getBefore() - Method in class org.orekit.utils.TimeSpanMap.Transition
-
Get the entry valid before transition.
- getBeginDate(Frequency) - Method in class org.orekit.estimation.measurements.gnss.CycleSlipDetectorResults
-
Return the date of validity beginning of the detector.
- getBeidouEpoch() - Method in class org.orekit.time.AbstractTimeScales
-
- getBeidouEpoch() - Method in interface org.orekit.time.TimeScales
-
Reference epoch for BeiDou weeks: 2006-01-01T00:00:00 UTC.
- getBeidouNavigationMessage() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1042Data
-
Get the Beidou navigation message corresponding to the current RTCM data.
- getBeidouNavigationMessage(TimeScales) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1042Data
-
Get the Beidou navigation message corresponding to the current RTCM data.
- getBeidouNavigationMessages() - Method in class org.orekit.gnss.navigation.RinexNavigation
-
Get all the Beidou navigation messages contained in the file.
- getBeidouNavigationMessages(String) - Method in class org.orekit.gnss.navigation.RinexNavigation
-
Get the Beidou navigation messages for the given satellite Id.
- getBeidouToc() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1042Data
-
Get the Beidou time of clock.
- getBeta() - Method in class org.orekit.models.earth.ionosphere.KlobucharIonoCoefficientsLoader
-
Returns the beta coefficients array.
- getBeta() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBodyContext
-
Get direction cosine β for central body.
- getBeta() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTThirdBodyContext
-
Get direction cosine β for central body.
- getBeta() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
-
Get direction cosine β for central body.
- getBeta() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldAuxiliaryElements
-
Get direction cosine β for central body.
- getBGDE1E5a() - Method in class org.orekit.propagation.analytical.gnss.data.GalileoNavigationMessage
-
Getter for the E1/E5a broadcast group delay.
- getBGDE5bE1() - Method in class org.orekit.propagation.analytical.gnss.data.GalileoNavigationMessage
-
Getter for the the Broadcast Group Delay E5b/E1.
- getBitRate() - Method in class org.orekit.gnss.metric.ntrip.DataStreamRecord
-
Get the bit rate.
- getBN() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data
-
Get the GLONASS Bn Word.
- getBoA() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseralContext
-
Get B / A.
- getBoA() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBodyContext
-
Get B / A.
- getBoA() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonalContext
-
Get B / A.
- getBoA() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTTesseralContext
-
Get B / A.
- getBoA() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTThirdBodyContext
-
Get B / A.
- getBoA() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTZonalContext
-
Get B / A.
- getBoABpo() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseralContext
-
Get BoABpo = B / A(1 + B).
- getBoABpo() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBodyContext
-
Get BoABpo = B / A(1 + B).
- getBoABpo() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonalContext
-
Get BoABpo = B / A(1 + B).
- getBoABpo() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTTesseralContext
-
Get BoABpo = B / A(1 + B).
- getBoABpo() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTThirdBodyContext
-
Get BoABpo = B / A(1 + B).
- getBoABpo() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTZonalContext
-
Get BoABpo = B / A(1 + B).
- getBody(String) - Method in interface org.orekit.bodies.CelestialBodies
-
Get a celestial body.
- getBody(String) - Static method in class org.orekit.bodies.CelestialBodyFactory
-
Get a celestial body.
- getBody(String) - Method in class org.orekit.bodies.LazyLoadedCelestialBodies
-
Get a celestial body.
- getBody() - Method in class org.orekit.files.ccsds.definitions.BodyFacade
-
Get the celestial body.
- getBody() - Method in class org.orekit.propagation.events.FieldLatitudeCrossingDetector
-
Get the body on which the geographic zone is defined.
- getBody() - Method in class org.orekit.propagation.events.FootprintOverlapDetector
-
Get the body on which the geographic zone is defined.
- getBody() - Method in class org.orekit.propagation.events.GeographicZoneDetector
-
Get the body on which the geographic zone is defined.
- getBody() - Method in class org.orekit.propagation.events.LatitudeCrossingDetector
-
Get the body on which the geographic zone is defined.
- getBody() - Method in class org.orekit.propagation.events.LatitudeExtremumDetector
-
Get the body on which the geographic zone is defined.
- getBody() - Method in class org.orekit.propagation.events.LongitudeCrossingDetector
-
Get the body on which the geographic zone is defined.
- getBody() - Method in class org.orekit.propagation.events.LongitudeExtremumDetector
-
Get the body on which the geographic zone is defined.
- getBody() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBody
-
Get third body.
- getBodyFrame() - Method in class org.orekit.attitudes.GroundPointing
-
Get the body frame.
- getBodyFrame() - Method in interface org.orekit.bodies.BodyShape
-
Get body frame related to body shape.
- getBodyFrame() - Method in class org.orekit.bodies.OneAxisEllipsoid
-
Get body frame related to body shape.
- getBodyFrame() - Method in class org.orekit.models.earth.Geoid
-
- getBodyOrientedFrame() - Method in interface org.orekit.bodies.CelestialBody
-
Get a body oriented, body centered frame.
- getBodyShape() - Method in class org.orekit.propagation.events.AltitudeDetector
-
Get the body shape.
- getBodyShape() - Method in class org.orekit.propagation.events.FieldAltitudeDetector
-
Get the body shape.
- getBolDv() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
-
Get the total ΔV capability at beginning of life.
- getBStar() - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmTle
-
Get the SGP/SGP4 drag-like coefficient.
- getBStar() - Method in class org.orekit.propagation.analytical.tle.FieldTLE
-
Get the ballistic coefficient.
- getBStar() - Method in class org.orekit.propagation.analytical.tle.TLE
-
Get the ballistic coefficient.
- getBuilder() - Method in class org.orekit.estimation.measurements.generation.AbstractScheduler
-
Get the measurements builder.
- getBuilders() - Method in class org.orekit.estimation.sequential.AbstractKalmanModel
-
Getter for the propagators.
- getBusModel() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
-
Get the bus model name.
- getC() - Method in class org.orekit.bodies.Ellipsoid
-
Get the length of the third semi-axis.
- getC() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
-
Get C = 1 + p² + q².
- getC() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldAuxiliaryElements
-
Get C = 1 + p² + q².
- getC2n0(int) - Method in class org.orekit.models.earth.ReferenceEllipsoid
-
Get the fully normalized coefficient C2n,0 for the normal
gravity potential.
- getCacheSlotsNumber() - Static method in class org.orekit.utils.OrekitConfiguration
-
Get the number of slots to use in caches.
- getCalendarWeek() - Method in class org.orekit.time.DateComponents
-
Get the calendar week number.
- getCalls() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
-
Get the number of calls to the differential equations computation method.
- getCalls() - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator
-
Get the number of calls to the differential equations computation method.
- getCapitalizedAbbreviation() - Method in enum org.orekit.time.Month
-
Get the capitalized three letters abbreviation.
- getCapitalizedName() - Method in enum org.orekit.time.Month
-
Get the capitalized full name.
- getCarrierPhase(String) - Static method in enum org.orekit.gnss.metric.ntrip.CarrierPhase
-
Get the carrier phase corresponding to a code.
- getCarrierPhase() - Method in class org.orekit.gnss.metric.ntrip.DataStreamRecord
-
Get the carrier phase.
- getCartesian() - Method in class org.orekit.frames.FieldTransform
-
Get the underlying elementary Cartesian part.
- getCartesian() - Method in class org.orekit.frames.Transform
-
Get the underlying elementary Cartesian part.
- getCartesianIntersectionPoint(Line, Vector3D, Frame, AbsoluteDate) - Method in class org.orekit.bodies.OneAxisEllipsoid
-
Get the intersection point of a line with the surface of the body.
- getCartesianIntersectionPoint(FieldLine<T>, FieldVector3D<T>, Frame, FieldAbsoluteDate<T>) - Method in class org.orekit.bodies.OneAxisEllipsoid
-
Get the intersection point of a line with the surface of the body.
- getCasters() - Method in class org.orekit.gnss.metric.ntrip.SourceTable
-
Get the casters records.
- getCatalogName() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
-
Get the specification of satellite catalog source.
- getCcsdsEpoch() - Method in class org.orekit.time.AbstractTimeScales
-
- getCCSDSEpoch(Field<T>) - Static method in class org.orekit.time.FieldAbsoluteDate
-
Reference epoch for CCSDS Time Code Format (CCSDS 301.0-B-4):
- getCcsdsEpoch() - Method in interface org.orekit.time.TimeScales
-
Reference epoch for CCSDS Time Code Format (CCSDS 301.0-B-4): 1958-01-01T00:00:00
International Atomic Time (not UTC).
- getCdmMessageLink() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
-
Get the Unique identifier of Conjunction Data Message linked to this Orbit Data Message.
- getCelestialBodies() - Static method in class org.orekit.bodies.CelestialBodyFactory
-
Get the instance of
CelestialBodies
that is called by the static methods in
this class.
- getCelestialBodies() - Method in class org.orekit.data.CompositeDataContext
-
- getCelestialBodies() - Method in interface org.orekit.data.DataContext
-
Get a factory constructing
CelestialBody
s based on the auxiliary data in
this context.
- getCelestialBodies() - Method in class org.orekit.data.ExceptionalDataContext
-
- getCelestialBodies() - Method in class org.orekit.data.LazyLoadedDataContext
-
- getCelestialBody() - Method in enum org.orekit.files.ccsds.definitions.CenterName
-
Get the celestial body corresponding to the CCSDS constant.
- getCelestialBody(CelestialBodies) - Method in enum org.orekit.files.ccsds.definitions.CenterName
-
Get the celestial body corresponding to the CCSDS constant.
- getCelestialSource() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
-
Get the source and version of celestial body (e.g.
- getCenter() - Method in class org.orekit.bodies.Ellipse
-
Get the center of the 2D ellipse.
- getCenter() - Method in class org.orekit.files.ccsds.ndm.adm.AdmMetadata
-
Get the body at origin of reference frame.
- getCenter() - Method in class org.orekit.files.ccsds.ndm.odm.CommonMetadata
-
Get the origin of reference frame.
- getCenter() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata
-
Get the origin of reference frame.
- getCenter() - Method in class org.orekit.geometry.fov.SmoothFieldOfView
-
Get the direction of the FOV center, in spacecraft frame.
- getCenter() - Method in class org.orekit.models.earth.tessellation.Tile
-
Get the center point.
- getCenterMass() - Method in class org.orekit.gnss.RinexObservationHeader
-
Get the current center of mass of vehicle in body fixed coordinate system.
- getCenterName() - Method in class org.orekit.files.ccsds.definitions.ModifiedFrame
-
Get the CCSDS center name.
- getCenterOfCurvature(Vector2D) - Method in class org.orekit.bodies.Ellipse
-
Find the center of curvature (point on the evolute) at the nadir of a point.
- getCenterOfMassOffset() - Method in class org.orekit.files.ilrs.CPFHeader
-
Get the approximate center of mass to reflector offset.
- getCentralBody() - Method in class org.orekit.propagation.events.InterSatDirectViewDetector
-
Get the central body.
- getCentralBodyRotation() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
-
Get central body angular rotation rate.
- getChi() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseralContext
-
Get Χ = 1 / sqrt(1 - e²) = 1 / B.
- getChi() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTTesseralContext
-
Get Χ = 1 / sqrt(1 - e²) = 1 / B.
- getChi2() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseralContext
-
Get Χ².
- getChi2() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTTesseralContext
-
Get Χ².
- getChildren() - Method in class org.orekit.frames.OrphanFrame
-
Get all children of the instance.
- getCic() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractAlmanac
-
Getter for the Cic parameter.
- getCic() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractNavigationMessage
-
Getter for the Cic parameter.
- getCic() - Method in interface org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElements
-
Gets the Amplitude of the Cosine Harmonic Correction Term to the Angle of Inclination.
- getCij(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution.FieldFourierCjSjCoefficients
-
Get the coefficient Cij.
- getCij(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution.FourierCjSjCoefficients
-
Get the coefficient Cij.
- getCircularEx() - Method in class org.orekit.orbits.CircularOrbit
-
Get the first component of the circular eccentricity vector.
- getCircularEx() - Method in class org.orekit.orbits.FieldCircularOrbit
-
Get the first component of the circular eccentricity vector.
- getCircularExDot() - Method in class org.orekit.orbits.CircularOrbit
-
Get the first component of the circular eccentricity vector derivative.
- getCircularExDot() - Method in class org.orekit.orbits.FieldCircularOrbit
-
Get the first component of the circular eccentricity vector derivative.
- getCircularEy() - Method in class org.orekit.orbits.CircularOrbit
-
Get the second component of the circular eccentricity vector.
- getCircularEy() - Method in class org.orekit.orbits.FieldCircularOrbit
-
Get the second component of the circular eccentricity vector.
- getCircularEyDot() - Method in class org.orekit.orbits.CircularOrbit
-
Get the second component of the circular eccentricity vector derivative.
- getCircularEyDot() - Method in class org.orekit.orbits.FieldCircularOrbit
-
Get the second component of the circular eccentricity vector derivative.
- getCIRF(IERSConventions, boolean) - Method in class org.orekit.frames.AbstractFrames
-
- getCIRF(IERSConventions, boolean) - Method in interface org.orekit.frames.Frames
-
Get the CIRF2000 reference frame.
- getCIRF(IERSConventions, boolean) - Static method in class org.orekit.frames.FramesFactory
-
Get the CIRF2000 reference frame.
- getCis() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractAlmanac
-
Getter for the Cis parameter.
- getCis() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractNavigationMessage
-
Getter for the Cis parameter.
- getCis() - Method in interface org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElements
-
Gets the Amplitude of the Sine Harmonic Correction Term to the Angle of Inclination.
- getCj(int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.CjSjCoefficient
-
Get the Cj coefficient.
- getCj(int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldCjSjCoefficient
-
Get the Cj coefficient.
- getCk0() - Method in class org.orekit.propagation.analytical.BrouwerLyddanePropagator
-
Get the un-normalized zonal coefficients.
- getCk0() - Method in class org.orekit.propagation.analytical.EcksteinHechlerPropagator
-
Get the un-normalized zonal coefficients.
- getClassification() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
-
Get the message classification.
- getClassification() - Method in class org.orekit.propagation.analytical.tle.FieldTLE
-
Get the classification.
- getClassification() - Method in class org.orekit.propagation.analytical.tle.TLE
-
Get the classification.
- getClassificationType() - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmTle
-
Get the classification type.
- getClkOffset() - Method in class org.orekit.gnss.RinexObservationHeader
-
Get the realtime-derived receiver clock offset.
- getClockAcceleration() - Method in class org.orekit.gnss.clock.RinexClock.ClockDataLine
-
Getter for the clock acceleration.
- getClockAccelerationSigma() - Method in class org.orekit.gnss.clock.RinexClock.ClockDataLine
-
Getter for the clock acceleration sigma.
- getClockBias() - Method in class org.orekit.gnss.clock.RinexClock.ClockDataLine
-
Getter for the clock bias.
- getClockBiasSigma() - Method in class org.orekit.gnss.clock.RinexClock.ClockDataLine
-
Getter for the clock bias sigma.
- getClockConstraint() - Method in class org.orekit.gnss.clock.RinexClock.ReferenceClock
-
Getter for the clock constraint.
- getClockCorrection() - Method in class org.orekit.files.sp3.SP3.SP3Coordinate
-
Returns the clock correction value.
- getClockCorrection() - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm02Data
-
Get the clock correction data.
- getClockCorrection() - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm03Data
-
Get the clock correction data.
- getClockCount() - Method in class org.orekit.files.ccsds.utils.ContextBinding
-
Get clock count.
- getClockData() - Method in class org.orekit.gnss.clock.RinexClock
-
Getter for an unmodifiable map of clock data.
- getClockDataTypes() - Method in class org.orekit.gnss.clock.RinexClock
-
Getter for the different clock data types.
- getClockDriftDriver() - Method in class org.orekit.estimation.measurements.GroundStation
-
Get a driver allowing to change station clock drift (which is related to measurement date).
- getClockDriftDriver() - Method in class org.orekit.estimation.measurements.ObservableSatellite
-
Get the clock drift parameter driver.
- getClockID() - Method in class org.orekit.gnss.clock.RinexClock.ReferenceClock
-
Getter for the clock ID.
- getClockOffsetDriver() - Method in class org.orekit.estimation.measurements.GroundStation
-
Get a driver allowing to change station clock (which is related to measurement date).
- getClockOffsetDriver() - Method in class org.orekit.estimation.measurements.ObservableSatellite
-
Get the clock offset parameter driver.
- getClockRate() - Method in class org.orekit.files.ccsds.utils.ContextBinding
-
Get clock rate.
- getClockRate() - Method in class org.orekit.gnss.clock.RinexClock.ClockDataLine
-
Getter for the clock rate.
- getClockRateChange() - Method in class org.orekit.files.sp3.SP3.SP3Coordinate
-
Returns the clock rate.
- getClockRateSigma() - Method in class org.orekit.gnss.clock.RinexClock.ClockDataLine
-
Getter for the clock rate sigma.
- getCnm() - Method in class org.orekit.gnss.metric.messages.ssr.subtype.SsrIm201Data
-
Get the cosine parameters of spherical harmonics expansion of degree N and order M.
- getCo2AB() - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContributionContext
-
Get co2AB = C / 2AB.
- getCo2AB() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseralContext
-
Get Co2AB = C / 2AB.
- getCo2AB() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldAbstractGaussianContributionContext
-
Get co2AB = C / 2AB.
- getCo2AB() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTTesseralContext
-
Get Co2AB = C / 2AB.
- getCodeBias() - Method in class org.orekit.gnss.metric.messages.ssr.igm.CodeBias
-
Get the code bias associated to the signal ID.
- getCodeBias(int) - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm05Data
-
Get the code bias for a given signal ID.
- getCodeBiases() - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm05Data
-
Get the code biases for the current satellite.
- getCoefficients() - Method in enum org.orekit.forces.gravity.potential.OceanLoadDeformationCoefficients
-
Get the load deformation coefficients for ocean tides.
- getCoefficients(String) - Method in class org.orekit.models.earth.displacement.OceanLoadingCoefficientsBLQFactory
-
Get the coefficients for a given site.
- getCoefficients(FieldAbsoluteDate<T>, Set<String>) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution.FieldGaussianShortPeriodicCoefficients
-
Computes the coefficients involved in the contributions.
- getCoefficients(AbsoluteDate, Set<String>) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution.GaussianShortPeriodicCoefficients
-
Computes the coefficients involved in the contributions.
- getCoefficients(FieldAbsoluteDate<T>, Set<String>) - Method in interface org.orekit.propagation.semianalytical.dsst.forces.FieldShortPeriodTerms
-
Computes the coefficients involved in the contributions.
- getCoefficients(AbsoluteDate, Set<String>) - Method in interface org.orekit.propagation.semianalytical.dsst.forces.ShortPeriodTerms
-
Computes the coefficients involved in the contributions.
- getCoefficientsKeyPrefix() - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution.FieldGaussianShortPeriodicCoefficients
-
Get the prefix for short period coefficients keys.
- getCoefficientsKeyPrefix() - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution.GaussianShortPeriodicCoefficients
-
Get the prefix for short period coefficients keys.
- getCoefficientsKeyPrefix() - Method in interface org.orekit.propagation.semianalytical.dsst.forces.FieldShortPeriodTerms
-
Get the prefix for short period coefficients keys.
- getCoefficientsKeyPrefix() - Method in interface org.orekit.propagation.semianalytical.dsst.forces.ShortPeriodTerms
-
Get the prefix for short period coefficients keys.
- getCombinationType() - Method in class org.orekit.gnss.CombinedObservationData
-
Get the type of the combination of measurements used to build the instance.
- getCombinedFrequency(Frequency, Frequency) - Method in class org.orekit.estimation.measurements.gnss.AbstractDualFrequencyCombination
-
Get the combined frequency of two measurements.
- getCombinedFrequency(Frequency, Frequency) - Method in class org.orekit.estimation.measurements.gnss.GeometryFreeCombination
-
Get the combined frequency of two measurements.
- getCombinedFrequency(Frequency, Frequency) - Method in class org.orekit.estimation.measurements.gnss.IonosphereFreeCombination
-
Get the combined frequency of two measurements.
- getCombinedFrequency(Frequency, Frequency) - Method in class org.orekit.estimation.measurements.gnss.NarrowLaneCombination
-
Get the combined frequency of two measurements.
- getCombinedFrequency(Frequency, Frequency) - Method in class org.orekit.estimation.measurements.gnss.WideLaneCombination
-
Get the combined frequency of two measurements.
- getCombinedMHzFrequency() - Method in class org.orekit.gnss.CombinedObservationData
-
Get the value of the combined frequency in MHz.
- getCombinedProvider(TransformProvider, TransformProvider) - Static method in class org.orekit.frames.TransformProviderUtils
-
Combine two transform providers.
- getCombinedValue(double, Frequency, double, Frequency) - Method in class org.orekit.estimation.measurements.gnss.AbstractDualFrequencyCombination
-
Get the combined observed value of two measurements.
- getCombinedValue(double, double) - Method in class org.orekit.estimation.measurements.gnss.AbstractSingleFrequencyCombination
-
Get the combined observed value of two measurements.
- getCombinedValue(double, Frequency, double, Frequency) - Method in class org.orekit.estimation.measurements.gnss.GeometryFreeCombination
-
Get the combined observed value of two measurements.
- getCombinedValue(double, double) - Method in class org.orekit.estimation.measurements.gnss.GRAPHICCombination
-
Get the combined observed value of two measurements.
- getCombinedValue(double, Frequency, double, Frequency) - Method in class org.orekit.estimation.measurements.gnss.IonosphereFreeCombination
-
Get the combined observed value of two measurements.
- getCombinedValue(double, Frequency, double, Frequency) - Method in class org.orekit.estimation.measurements.gnss.NarrowLaneCombination
-
Get the combined observed value of two measurements.
- getCombinedValue(double, double) - Method in class org.orekit.estimation.measurements.gnss.PhaseMinusCodeCombination
-
Get the combined observed value of two measurements.
- getCombinedValue(double, Frequency, double, Frequency) - Method in class org.orekit.estimation.measurements.gnss.WideLaneCombination
-
Get the combined observed value of two measurements.
- getComments() - Method in class org.orekit.files.ccsds.ndm.adm.apm.ApmData
-
Get the comments.
- getComments() - Method in class org.orekit.files.ccsds.ndm.Ndm
-
Get an unmodifiable view of the comments.
- getComments() - Method in class org.orekit.files.ccsds.section.CommentsContainer
-
Get the comments.
- getComments() - Method in class org.orekit.files.ilrs.CPF
-
Get the comments contained in the file.
- getComments() - Method in class org.orekit.files.ilrs.CRD
-
Get the comments contained in the file.
- getComments() - Method in class org.orekit.gnss.clock.RinexClock
-
Getter for the comments.
- getComments() - Method in class org.orekit.gnss.navigation.RinexNavigation
-
Getter for the comments.
- getCompleteName(T) - Method in class org.orekit.data.AbstractListCrawler
-
Get the complete name of a input.
- getCompleteName(File) - Method in class org.orekit.data.FilesListCrawler
-
Get the complete name of a input.
- getCompleteName(URL) - Method in class org.orekit.data.NetworkCrawler
-
Get the complete name of a input.
- getComponents(TimeScale) - Method in class org.orekit.time.AbsoluteDate
-
Split the instance into date/time components.
- getComponents(int) - Method in class org.orekit.time.AbsoluteDate
-
Split the instance into date/time components for a local time.
- getComponents(int, TimeScale) - Method in class org.orekit.time.AbsoluteDate
-
Split the instance into date/time components for a local time.
- getComponents(TimeZone) - Method in class org.orekit.time.AbsoluteDate
-
Split the instance into date/time components for a time zone.
- getComponents(TimeZone, TimeScale) - Method in class org.orekit.time.AbsoluteDate
-
Split the instance into date/time components for a time zone.
- getComponents(TimeScale) - Method in class org.orekit.time.FieldAbsoluteDate
-
Split the instance into date/time components.
- getComponents(int) - Method in class org.orekit.time.FieldAbsoluteDate
-
Split the instance into date/time components for a local time.
- getComponents(int, TimeScale) - Method in class org.orekit.time.FieldAbsoluteDate
-
Split the instance into date/time components for a local time.
- getComponents(TimeZone) - Method in class org.orekit.time.FieldAbsoluteDate
-
Split the instance into date/time components for a time zone.
- getComponents(TimeZone, TimeScale) - Method in class org.orekit.time.FieldAbsoluteDate
-
Split the instance into date/time components for a time zone.
- getCompressionEncryption() - Method in class org.orekit.gnss.metric.ntrip.DataStreamRecord
-
Get the compression/encryption algorithm applied.
- getConfidence() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
-
Get confidence metric.
- getConfiguration(String, int) - Method in class org.orekit.frames.ITRFVersionLoader
-
- getConfiguration(String, int) - Method in interface org.orekit.frames.ItrfVersionProvider
-
Get the ITRF version configuration defined by a given file at specified date.
- getConfigurationRecords() - Method in class org.orekit.files.ilrs.CRD.CRDDataBlock
-
Get the system configuration records.
- getConsiderN() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
-
Get number of consider parameters.
- getConsiderParameters() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
-
Get description of consider parameters.
- getConstantNormalizedProvider(int, int) - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory
-
Get the constant gravity field coefficients provider from the first supported file.
- getConstantNormalizedProvider(int, int) - Method in interface org.orekit.forces.gravity.potential.GravityFields
-
Get a constant gravity field normalized coefficients provider.
- getConstantNormalizedProvider(int, int) - Method in class org.orekit.forces.gravity.potential.LazyLoadedGravityFields
-
Get a constant gravity field normalized coefficients provider.
- getConstantProvider(boolean, int, int) - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
-
- getConstantUnnormalizedProvider(int, int) - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory
-
Get the constant gravity field coefficients provider from the first supported file.
- getConstantUnnormalizedProvider(int, int) - Method in interface org.orekit.forces.gravity.potential.GravityFields
-
Get a constant gravity field unnormalized coefficients provider.
- getConstantUnnormalizedProvider(int, int) - Method in class org.orekit.forces.gravity.potential.LazyLoadedGravityFields
-
Get a constant gravity field unnormalized coefficients provider.
- getConstellation() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
-
Get the name of the constellation this space object belongs to.
- getConstituents() - Method in class org.orekit.files.ccsds.ndm.Ndm
-
Get an unmodifiable view of the constituents.
- getConstraintsMap() - Method in class org.orekit.utils.AbstractMultipleShooting
-
Get the map of patch points components which are constrained.
- getContentAsBoolean() - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken
-
Get the content of the entry as a boolean.
- getContentAsDouble() - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken
-
Get the content of the entry as a double.
- getContentAsEnum(Class<T>) - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken
-
Get the content of the entry as an enum.
- getContentAsEnumList(Class<T>) - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken
-
Get the content of the entry as a list of enum.
- getContentAsInt() - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken
-
Get the content of the entry as an integer.
- getContentAsNormalizedList() - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken
-
Get the content of the entry as a list of free-text strings.
- getContentAsNormalizedString() - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken
-
Get the content of the entry.
- getContentAsUppercaseCharacter() - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken
-
Get the content of the entry as an uppercase character.
- getContentAsUppercaseList() - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken
-
Get the content of the entry as a list of normalized and uppercased strings.
- getContentAsUppercaseString() - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken
-
Get the content of the entry as normalized and uppercased.
- getContentAsVector() - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken
-
Get the content of the entry as a vector.
- getContext() - Method in class org.orekit.files.ccsds.utils.generation.AbstractMessageWriter
-
Get the current context.
- getConventions() - Method in class org.orekit.files.ccsds.ndm.AbstractBuilder
-
Get the IERS conventions.
- getConventions() - Method in class org.orekit.files.ccsds.ndm.NdmConstituent
-
Get IERS conventions.
- getConventions() - Method in class org.orekit.files.ccsds.utils.ContextBinding
-
Get IERS conventions.
- getConventions() - Method in class org.orekit.files.ccsds.utils.parsing.AbstractConstituentParser
-
Get IERS conventions.
- getConventions() - Method in class org.orekit.frames.EOPHistory
-
Get the IERS conventions to which these EOP apply.
- getConversionJacobian(SpacecraftState) - Method in class org.orekit.propagation.AbstractMatricesHarvester
-
Get the conversion Jacobian between state parameters and parameters used for derivatives.
- getConversionJacobian(SpacecraftState) - Method in class org.orekit.propagation.numerical.AbsoluteJacobiansMapper
-
Get the conversion Jacobian between state parameters and parameters used for derivatives.
- getConversionJacobian(SpacecraftState) - Method in class org.orekit.propagation.numerical.JacobiansMapper
-
Get the conversion Jacobian between state parameters and parameters used for derivatives.
- getConverter(ContextBinding) - Method in enum org.orekit.files.ccsds.definitions.TimeSystem
-
- getConverter(ITRFVersion, ITRFVersion) - Static method in enum org.orekit.frames.ITRFVersion
-
Find a converter between specified ITRF frames.
- getConverter(ITRFVersion, ITRFVersion, TimeScale) - Static method in enum org.orekit.frames.ITRFVersion
-
Find a converter between specified ITRF frames.
- getCoordinates(SpacecraftState, int, int) - Static method in class org.orekit.estimation.measurements.AbstractMeasurement
-
Get Cartesian coordinates as derivatives.
- getCoordinates() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistory
-
- getCoordinates() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemData
-
Get an unmodifiable view of the data points.
- getCoordinates() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemSegment
-
- getCoordinates() - Method in interface org.orekit.files.general.EphemerisFile.EphemerisSegment
-
- getCoordinates() - Method in class org.orekit.files.general.OrekitEphemerisFile.OrekitEphemerisSegment
-
- getCoordinates() - Method in class org.orekit.files.ilrs.CPF.CPFEphemeris
-
- getCoordinates() - Method in class org.orekit.files.sp3.SP3.SP3Ephemeris
-
- getCoordinateSystem() - Method in class org.orekit.files.sp3.SP3
-
Returns the coordinate system of the entries in this orbit file.
- getCorrectedMeasurement() - Method in class org.orekit.estimation.sequential.AbstractKalmanModel
-
Get the estimated measurement.
- getCorrectedMeasurement() - Method in interface org.orekit.estimation.sequential.KalmanEstimation
-
Get the estimated measurement.
- getCorrectedMeasurement() - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanModel
-
Get the estimated measurement.
- getCorrectedSpacecraftStates() - Method in class org.orekit.estimation.sequential.AbstractKalmanModel
-
Get the corrected spacecraft states.
- getCorrectedSpacecraftStates() - Method in interface org.orekit.estimation.sequential.KalmanEstimation
-
Get the corrected spacecraft states.
- getCorrectedSpacecraftStates() - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanModel
-
Get the corrected spacecraft states.
- getCorrection() - Method in class org.orekit.gnss.RinexObservationLoader.Parser.PhaseShiftCorrection
-
Get the Phase Shift Corrections.
- getCorrection() - Method in class org.orekit.gnss.RinexObservationLoader.Parser.ScaleFactorCorrection
-
Get the Scale Factor.
- getCorrectionAberrationDiurnal() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
-
Getter for the diurnal aberration correction.
- getCorrectionAberrationYearly() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
-
Getter for the yearly aberration correction.
- getCorrectionAngle1() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
-
Getter for the correctionAngle1.
- getCorrectionAngle2() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
-
Getter for the correctionAngle2.
- getCorrectionDoppler() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
-
Getter for the correctionDoppler.
- getCorrectionMagnitude() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
-
Getter for the magnitude correction.
- getCorrectionRange(RangeUnitsConverter) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
-
Getter for the raw correction for range in meters.
- getCorrectionRcs() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
-
Getter for the radar cross section correction.
- getCorrectionReceive() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
-
Getter for the correctionReceive.
- getCorrectionsApplied() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
-
Getter for the correctionApplied.
- getCorrectionTransmit() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
-
Getter for the correctionTransmit.
- getCorrelationCoefficientsMatrix() - Method in class org.orekit.estimation.measurements.Position
-
Get the correlation coefficients matrix.
- getCorrelationCoefficientsMatrix() - Method in class org.orekit.estimation.measurements.PV
-
Get the correlation coefficients matrix.
- getCosparID() - Method in class org.orekit.gnss.antenna.SatelliteAntenna
-
Get COSPAR ID.
- getCount() - Method in class org.orekit.estimation.measurements.EstimatedMeasurement
-
Get the evaluations counter.
- getCountry() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
-
Get the name of the country where the space object owner is based.
- getCountry() - Method in class org.orekit.gnss.metric.ntrip.CasterRecord
-
Get the country.
- getCountry() - Method in class org.orekit.gnss.metric.ntrip.DataStreamRecord
-
Get the country.
- getCovariance() - Method in class org.orekit.estimation.sequential.MeasurementDecorator
- getCovarianceBlock() - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmData
-
Get the covariance matrix logical block.
- getCovarianceBlock() - Method in class org.orekit.files.ccsds.ndm.odm.opm.OpmData
-
Get the covariance matrix logical block.
- getCovarianceBlocks() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmData
-
Get covariance logical blocks.
- getCovarianceMatrices() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemData
-
Get an unmodifiable view of Covariance Matrices.
- getCovarianceMatrices() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemSegment
-
Get an unmodifiable view of Covariance Matrices.
- getCovarianceMatrix() - Method in class org.orekit.estimation.measurements.Position
-
Get the covariance matrix.
- getCovarianceMatrix() - Method in class org.orekit.estimation.measurements.PV
-
Get the covariance matrix.
- getCovarianceMatrix() - Method in class org.orekit.files.ccsds.ndm.odm.CartesianCovariance
-
Get the Position/Velocity covariance matrix.
- getCovariances() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.CovarianceHistory
-
Get the covariances.
- getCovBasis() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.CovarianceHistoryMetadata
-
Get basis of this covariance time history data.
- getCovBasisID() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.CovarianceHistoryMetadata
-
Get identification number of the orbit determination or simulation upon which this covariance is based.
- getCovConfidence() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.CovarianceHistoryMetadata
-
Get the measure of confidence in covariance error matching reality.
- getCovFrameEpoch() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.CovarianceHistoryMetadata
-
- getCovID() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.CovarianceHistoryMetadata
-
Get covariance identification number.
- getCovNextID() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.CovarianceHistoryMetadata
-
Get identification number of next covariance.
- getCovOrdering() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.CovarianceHistoryMetadata
-
Get covariance ordering.
- getCovPrevID() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.CovarianceHistoryMetadata
-
Get identification number of previous covariance.
- getCovReferenceFrame() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.CovarianceHistoryMetadata
-
Get reference frame of the covariance.
- getCovScaleMax() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.CovarianceHistoryMetadata
-
Get the maximum scale factor to apply to achieve realism.
- getCovScaleMin() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.CovarianceHistoryMetadata
-
Get the minimum scale factor to apply to achieve realism.
- getCovType() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.CovarianceHistoryMetadata
-
Get covariance element set type.
- getCovUnits() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.CovarianceHistoryMetadata
-
Get covariance element set units.
- getCr3bpSystem() - Method in class org.orekit.orbits.RichardsonExpansion
-
Get the considered CR3BP system.
- getCrc() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractAlmanac
-
Getter for the Crc parameter.
- getCrc() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractNavigationMessage
-
Getter for the Crc parameter.
- getCrc() - Method in interface org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElements
-
Gets the Amplitude of the Cosine Harmonic Correction Term to the Orbit Radius.
- getCreationDate() - Method in class org.orekit.files.ccsds.section.Header
-
Get the file creation date and time in UTC.
- getCreationDate() - Method in class org.orekit.gnss.clock.RinexClock
-
Getter for the creation date.
- getCreationDate() - Method in class org.orekit.gnss.navigation.RinexNavigation
-
Getter for the creation date.
- getCreationDateString() - Method in class org.orekit.gnss.clock.RinexClock
-
Getter for the creation date of the file as a string.
- getCreationDateString() - Method in class org.orekit.gnss.navigation.RinexNavigation
-
Getter for the creation date of the file as a string.
- getCreationTimeString() - Method in class org.orekit.gnss.clock.RinexClock
-
Getter for the creation time of the file as a string.
- getCreationTimeString() - Method in class org.orekit.gnss.navigation.RinexNavigation
-
Getter for the creation time of the file as a string.
- getCreationTimeZoneString() - Method in class org.orekit.gnss.clock.RinexClock
-
Getter for the creation time zone of the file as a string.
- getCreationTimeZoneString() - Method in class org.orekit.gnss.navigation.RinexNavigation
-
Getter for the creation time zone of the file as a string.
- getCrs() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractAlmanac
-
Getter for the Crs parameter.
- getCrs() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractNavigationMessage
-
Getter for the Crs parameter.
- getCrs() - Method in interface org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElements
-
Gets the Amplitude of the Sine Harmonic Correction Term to the Orbit Radius.
- getCrsIndicator() - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm01Header
-
Get the Global/Regional CRS Indicator.
- getCrsIndicator() - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm03Header
-
Get the Global/Regional CRS Indicator.
- getCtr81Adj() - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherDataLoader.LineParameters
-
Gets the centered 81-day arithmetic average of F10.7 (adjusted).
- getCtr81Obs() - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherDataLoader.LineParameters
-
Gets the centered 81-day arithmetic average of F10.7 (observed).
- getCuc() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractAlmanac
-
Getter for the Cuc parameter.
- getCuc() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractNavigationMessage
-
Getter for the Cuc parameter.
- getCuc() - Method in interface org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElements
-
Gets the Amplitude of the Cosine Harmonic Correction Term to the Argument of Latitude.
- getCurrent() - Method in class org.orekit.files.ccsds.utils.parsing.AbstractMessageParser
-
Get the current processing state.
- getCurrent() - Method in class org.orekit.utils.units.Unit
-
Get the current exponent.
- getCurrentDate() - Method in class org.orekit.estimation.sequential.AbstractKalmanModel
-
Get the current date.
- getCurrentDate() - Method in interface org.orekit.estimation.sequential.KalmanEstimation
-
Get the current date.
- getCurrentDate() - Method in class org.orekit.estimation.sequential.KalmanEstimator
-
Get the current date.
- getCurrentDate() - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanEstimator
-
Get the current date.
- getCurrentDate() - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanModel
-
Get the current date.
- getCurrentMeasurementNumber() - Method in class org.orekit.estimation.sequential.AbstractKalmanModel
-
Get the current measurement number.
- getCurrentMeasurementNumber() - Method in interface org.orekit.estimation.sequential.KalmanEstimation
-
Get the current measurement number.
- getCurrentMeasurementNumber() - Method in class org.orekit.estimation.sequential.KalmanEstimator
-
Get the current measurement number.
- getCurrentMeasurementNumber() - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanEstimator
-
Get the current measurement number.
- getCurrentMeasurementNumber() - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanModel
-
Get the current measurement number.
- getCurrentState() - Method in interface org.orekit.propagation.sampling.FieldOrekitStepInterpolator
-
Get the state at previous grid point date.
- getCurrentState() - Method in interface org.orekit.propagation.sampling.OrekitStepInterpolator
-
Get the state at current grid point date.
- getCus() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractAlmanac
-
Getter for the Cus parameter.
- getCus() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractNavigationMessage
-
Getter for the Cus parameter.
- getCus() - Method in interface org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElements
-
Gets the Amplitude of the Sine Harmonic Correction Term to the Argument of Latitude.
- getCXO2N2A2() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonalContext
-
Get (C * χ) / ( 2 * n² * a² ).
- getCXO2N2A2() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTZonalContext
-
Get (C * χ) / ( 2 * n² * a² ).
- getCycleDuration() - Method in class org.orekit.propagation.analytical.gnss.data.CommonGnssData
-
Getter for the duration of the GNSS cycle in seconds.
- getCycleDuration() - Method in interface org.orekit.propagation.analytical.gnss.data.GNSSClockElements
-
Gets the duration of the GNSS cycle in seconds.
- getCycleDuration() - Method in interface org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElements
-
Gets the duration of the GNSS cycle in seconds.
- getCycleSlipMap() - Method in class org.orekit.estimation.measurements.gnss.CycleSlipDetectorResults
-
Get the cycle slip Map with contains the results.
- getD() - Method in class org.orekit.data.DelaunayArguments
-
Get the mean elongation of the Moon from the Sun.
- getD() - Method in class org.orekit.data.FieldDelaunayArguments
-
Get the mean elongation of the Moon from the Sun.
- getDailyFlux(AbsoluteDate) - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherData
-
Get the value of the daily F10.7 solar flux for previous day.
- getDailyFlux(AbsoluteDate) - Method in class org.orekit.models.earth.atmosphere.data.MarshallSolarActivityFutureEstimation
-
Get the value of the daily F10.7 solar flux for previous day.
- getDailyFlux(AbsoluteDate) - Method in interface org.orekit.models.earth.atmosphere.NRLMSISE00InputParameters
-
Get the value of the daily F10.7 solar flux for previous day.
- getDarkCount() - Method in class org.orekit.files.ilrs.CRDConfiguration.DetectorConfiguration
-
Get the dark count.
- getData() - Method in class org.orekit.files.ccsds.ndm.adm.apm.Apm
-
Get the file data.
- getData() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Ocm
-
Get the data from the single
segment
.
- getData() - Method in class org.orekit.files.ccsds.ndm.odm.omm.Omm
-
Get the file data.
- getData() - Method in class org.orekit.files.ccsds.ndm.odm.opm.Opm
-
Get the file data.
- getData() - Method in class org.orekit.files.ccsds.section.Segment
-
Get the segment data.
- getData() - Method in class org.orekit.files.ilrs.CRD.Meteo
-
Get an unmodifiable view of the tabulated meteorological data.
- getData() - Method in class org.orekit.gnss.metric.messages.rtcm.RtcmMessage
-
Get the data.
- getData() - Method in class org.orekit.gnss.metric.messages.ssr.SsrMessage
-
Get the data.
- getData() - Method in class org.orekit.utils.DoubleArrayDictionary
-
Get an unmodifiable view of the dictionary entries.
- getData() - Method in class org.orekit.utils.FieldArrayDictionary
-
Get an unmodifiable view of the dictionary entries.
- getData() - Method in class org.orekit.utils.TimeSpanMap.Span
-
Get the data valid during this time span.
- getDataBlocks() - Method in class org.orekit.files.ilrs.CRD
-
Get the data blocks contain in the file.
- getDataContext() - Method in class org.orekit.files.ccsds.ndm.AbstractBuilder
-
Get the data context.
- getDataContext() - Method in class org.orekit.files.ccsds.ndm.NdmConstituent
-
Get the data context.
- getDataContext() - Method in class org.orekit.files.ccsds.utils.ContextBinding
-
Get the data context used for getting frames, time scales, and celestial bodies.
- getDataContext() - Method in class org.orekit.files.ccsds.utils.parsing.AbstractConstituentParser
-
Get the data context used for getting frames, time scales, and celestial bodies.
- getDataFormat(String) - Static method in enum org.orekit.gnss.metric.ntrip.DataFormat
-
Get the message type corresponding to a keyword.
- getDataProvidersManager() - Method in class org.orekit.data.AbstractSelfFeedingLoader
-
Get the data provider manager.
- getDataProvidersManager() - Method in class org.orekit.data.LazyLoadedDataContext
-
Get the provider of auxiliary data for this data context.
- getDataProvidersManager() - Method in class org.orekit.frames.LazyLoadedEop
-
Get the data providers manager for this instance.
- getDataQuality() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
-
Getter for the dataQuality.
- getDataReleaseFlag() - Method in class org.orekit.files.ilrs.CRDHeader
-
Get the flag indicating the data release.
- getDataSet() - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherDataLoader
-
Getter for the data set.
- getDataStreams() - Method in class org.orekit.gnss.metric.ntrip.SourceTable
-
Get the data streams records.
- getDataType() - Method in class org.orekit.files.ilrs.CRDHeader
-
Get the data type.
- getDataType() - Method in class org.orekit.gnss.clock.RinexClock.ClockDataLine
-
Getter for the clock data type.
- getDataTypes() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
-
Get observation data types used.
- getDataTypes() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
-
Getter for the data types in the data section.
- getDataUsed() - Method in class org.orekit.files.sp3.SP3
-
Returns the data used indicator from the SP3 file.
- getDate() - Method in class org.orekit.attitudes.Attitude
-
Get the date of attitude parameters.
- getDate() - Method in class org.orekit.attitudes.FieldAttitude
-
Get the date of attitude parameters.
- getDate() - Method in class org.orekit.data.DelaunayArguments
-
Get the date.
- getDate() - Method in class org.orekit.data.FieldDelaunayArguments
-
Get the date.
- getDate() - Method in class org.orekit.estimation.measurements.AbstractMeasurement
-
Get the date.
- getDate() - Method in class org.orekit.estimation.measurements.EstimatedMeasurement
-
Get the date.
- getDate() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Covariance
-
Get the date.
- getDate() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Maneuver
-
Get the date.
- getDate() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryState
-
Get the date.
- getDate() - Method in class org.orekit.files.ccsds.ndm.odm.omm.Omm
-
Get the date.
- getDate() - Method in class org.orekit.files.ccsds.ndm.odm.opm.Opm
-
Get the date.
- getDate() - Method in class org.orekit.files.ilrs.CRD.AnglesMeasurement
-
Get the date.
- getDate() - Method in class org.orekit.files.ilrs.CRD.MeteorologicalMeasurement
-
Get the date.
- getDate() - Method in class org.orekit.files.ilrs.CRD.RangeMeasurement
-
Get the date.
- getDate() - Method in class org.orekit.forces.maneuvers.SmallManeuverAnalyticalModel
-
Get the date of the maneuver.
- getDate() - Method in class org.orekit.frames.EOPEntry
-
Get the date.
- getDate() - Method in class org.orekit.frames.FieldTransform
-
Get the date.
- getDate() - Method in class org.orekit.frames.Transform
-
Get the date.
- getDate() - Method in class org.orekit.gnss.CombinedObservationDataSet
-
Get the date.
- getDate() - Method in class org.orekit.gnss.DOP
-
Gets the calculation date of the DOP.
- getDate() - Method in class org.orekit.gnss.ObservationDataSet
-
Get the date.
- getDate() - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherDataLoader.LineParameters
-
- getDate() - Method in class org.orekit.orbits.FieldOrbit
-
Get the date of orbital parameters.
- getDate() - Method in class org.orekit.orbits.Orbit
-
Get the date of orbital parameters.
- getDate() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractEphemerisMessage
-
Getter for the reference date of the ephemeris.
- getDate() - Method in class org.orekit.propagation.analytical.gnss.data.CommonGnssData
-
Getter for the ephemeris reference date.
- getDate() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSAlmanac
-
- getDate() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSEphemeris
-
- getDate() - Method in class org.orekit.propagation.analytical.tle.FieldTLE
-
Get the TLE current date.
- getDate() - Method in class org.orekit.propagation.analytical.tle.TLE
-
Get the TLE current date.
- getDate() - Method in class org.orekit.propagation.events.DateDetector
-
Get the current event date according to the propagator.
- getDate() - Method in class org.orekit.propagation.events.EventsLogger.LoggedEvent
-
Get the date.
- getDate() - Method in class org.orekit.propagation.events.FieldDateDetector
-
Get the current event date according to the propagator.
- getDate() - Method in class org.orekit.propagation.FieldSpacecraftState
-
Get the date.
- getDate() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
-
Get the date of the orbit.
- getDate() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldAuxiliaryElements
-
Get the date of the orbit.
- getDate() - Method in class org.orekit.propagation.SpacecraftState
-
Get the date.
- getDate() - Method in class org.orekit.time.AbsoluteDate
-
Get the date.
- getDate() - Method in class org.orekit.time.DateTimeComponents
-
Get the date component.
- getDate() - Method in class org.orekit.time.FieldAbsoluteDate
-
Get the date.
- getDate() - Method in interface org.orekit.time.FieldTimeStamped
-
Get the date.
- getDate() - Method in class org.orekit.time.GLONASSDate
-
- getDate() - Method in class org.orekit.time.GNSSDate
-
Get the date.
- getDate() - Method in interface org.orekit.time.TimeStamped
-
Get the date.
- getDate() - Method in class org.orekit.time.UTCTAIOffset
-
Get the date of the start of the leap.
- getDate() - Method in class org.orekit.utils.DateDriver
-
Get the shifted date.
- getDate() - Method in class org.orekit.utils.FieldTimeSpanMap.Transition
-
Get the transition absolute date.
- getDate() - Method in class org.orekit.utils.TimeSpanMap.Transition
-
Get the transition date.
- getDate() - Method in class org.orekit.utils.TimeStampedAngularCoordinates
-
Get the date.
- getDate() - Method in class org.orekit.utils.TimeStampedFieldAngularCoordinates
-
Get the date.
- getDate() - Method in class org.orekit.utils.TimeStampedFieldPVCoordinates
-
Get the date.
- getDate() - Method in class org.orekit.utils.TimeStampedPVCoordinates
-
Get the date.
- getDateAndTime() - Method in class org.orekit.files.ilrs.CRDHeader
-
Get the date and time as the string value.
- getDates() - Method in class org.orekit.propagation.events.DateDetector
-
Get all event dates currently managed, in chronological order.
- getDay() - Method in class org.orekit.time.DateComponents
-
Get the day.
- getDayFraction() - Method in class org.orekit.files.sp3.SP3
-
Returns the day fraction for this SP3 file.
- getDayNumber() - Method in class org.orekit.time.GLONASSDate
-
Get the number of the current day in a four year interval.
- getDayOfWeek() - Method in class org.orekit.time.DateComponents
-
Get the day of week.
- getDayOfYear() - Method in class org.orekit.time.DateComponents
-
Get the day number in year.
- getDcBodyFrame() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata
-
- getDcBodyTrigger() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata
-
Get direction in
body frame
for triggering duty cycle.
- getDcExecStart() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata
-
Get the start time of initial duty cycle-based maneuver execution.
- getDcExecStop() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata
-
Get the end time of final duty cycle-based maneuver execution.
- getDcjDh(int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.CjSjCoefficient
-
Get the dCj / dh coefficient.
- getDcjDh(int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldCjSjCoefficient
-
Get the dCj / dh coefficient.
- getDcjDk(int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.CjSjCoefficient
-
Get the dCj / dk coefficient.
- getDcjDk(int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldCjSjCoefficient
-
Get the dCj / dk coefficient.
- getDcMaxCycles() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata
-
Get the maximum number of "ON" duty cycles.
- getDcMinCycles() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata
-
Get the minimum number of "ON" duty cycles.
- getDcPhaseStartAngle() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata
-
Get phase angle of pulse start.
- getDcPhaseStopAngle() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata
-
Get phase angle of pulse stop.
- getDcRefDir() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata
-
Get reference direction for triggering duty cycle.
- getDcRefTime() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata
-
Get duty cycle thrust reference time.
- getDcTimePulseDuration() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata
-
Get duty cycle pulse "ON" duration.
- getDcTimePulsePeriod() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata
-
Get duty cycle elapsed time between start of a pulse and start of next pulse.
- getDcType() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata
-
Get type of duty cycle.
- getDcWindowClose() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata
-
Get the end time of duty cycle-based maneuver window.
- getDcWindowOpen() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata
-
Get the start time of duty cycle-based maneuver window.
- getDdEps() - Method in class org.orekit.frames.EOPEntry
-
Get the correction for nutation in obliquity δΔε.
- getDdim() - Method in class org.orekit.bodies.CR3BPSystem
-
Get the CR3BP distance between the two bodies.
- getDDot() - Method in class org.orekit.data.DelaunayArguments
-
Get the mean elongation of the Moon from the Sun time derivative.
- getDDot() - Method in class org.orekit.data.FieldDelaunayArguments
-
Get the mean elongation of the Moon from the Sun time derivative.
- getDdPsi() - Method in class org.orekit.frames.EOPEntry
-
Get the correction for nutation in longitude δΔΨ.
- getDecimalYear(int, int, int) - Static method in class org.orekit.models.earth.GeoMagneticField
-
Utility function to get a decimal year for a given day.
- getDeclination() - Method in class org.orekit.models.earth.GeoMagneticElements
-
Returns the declination of the magnetic field in radians.
- getDecorrelatedReference() - Method in class org.orekit.estimation.measurements.gnss.AbstractLambdaMethod
-
Get the reference decorrelated ambiguities.
- getDecreasingTimeShift() - Method in class org.orekit.propagation.events.EventShifter
-
Get the decreasing events time shift.
- getDefault() - Static method in interface org.orekit.data.DataContext
-
Get the default data context that is used to implement the static factories (
TimeScalesFactory
,
FramesFactory
, etc) and loaders that feed themselves
(e.g.
- getDefaultInterpolationDegree() - Method in class org.orekit.files.ccsds.ndm.ParserBuilder
-
Get the default interpolation degree.
- getDefaultLaw(Frames) - Static method in interface org.orekit.propagation.Propagator
-
Get a default law using the given frames.
- getDefaultMass() - Method in class org.orekit.files.ccsds.ndm.ParserBuilder
-
Get the default mass.
- getDefaultModel() - Static method in class org.orekit.models.earth.troposphere.FixedTroposphericDelay
-
Returns the default model, loading delay values from the file
"tropospheric-delay.txt" via the
default data
context
.
- getDefaultTimeSystem(TimeScales) - Method in enum org.orekit.gnss.SatelliteSystem
-
Get default time scale for satellite system.
- getDefaultVersion() - Method in class org.orekit.files.ccsds.utils.generation.AbstractMessageWriter
-
Get the default format version.
- getDefaultYawRate(int) - Static method in class org.orekit.gnss.attitude.GPSBlockIIA
-
Get the default yaw rate for a satellite.
- getDelaunayMultipliers() - Method in class org.orekit.models.earth.displacement.Tide
-
Get the multipliers for Delaunay arguments (l, l', F, D, Ω).
- getDeltaClockC0() - Method in class org.orekit.gnss.metric.messages.ssr.igm.ClockCorrection
-
Get the delta clock C0.
- getDeltaClockC1() - Method in class org.orekit.gnss.metric.messages.ssr.igm.ClockCorrection
-
Get the delta clock C1.
- getDeltaClockC2() - Method in class org.orekit.gnss.metric.messages.ssr.igm.ClockCorrection
-
Get the delta clock C2.
- getDeltaI() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSAlmanac
-
- getDeltaI() - Method in interface org.orekit.propagation.analytical.gnss.data.GLONASSOrbitalElements
-
Get the correction to the mean value of inclination.
- getDeltaMass() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Maneuver
-
Get mass change.
- getDeltaMass() - Method in class org.orekit.files.ccsds.ndm.odm.opm.Maneuver
-
Get mass change during maneuver (value is < 0).
- getDeltaOrbitAlongTrack() - Method in class org.orekit.gnss.metric.messages.ssr.igm.OrbitCorrection
-
Get the along-track orbit correction for broadcast ephemeris.
- getDeltaOrbitCrossTrack() - Method in class org.orekit.gnss.metric.messages.ssr.igm.OrbitCorrection
-
Get the cross-track orbit correction for broadcast ephemeris.
- getDeltaOrbitRadial() - Method in class org.orekit.gnss.metric.messages.ssr.igm.OrbitCorrection
-
Get the radial orbit correction for broadcast ephemeris.
- getDeltaT() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSAlmanac
-
- getDeltaT() - Method in interface org.orekit.propagation.analytical.gnss.data.GLONASSOrbitalElements
-
Get the correction to the mean value of Draconian period.
- getDeltaTDot() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSAlmanac
-
- getDeltaTDot() - Method in interface org.orekit.propagation.analytical.gnss.data.GLONASSOrbitalElements
-
Get the rate of change of Draconian period.
- getDeltaTN() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data
-
Get the deltaTauN value.
- getDeltaVSat() - Method in class org.orekit.forces.maneuvers.ImpulseManeuver
-
Get the velocity increment in satellite frame.
- getDensity(AbsoluteDate, Vector3D, Frame) - Method in interface org.orekit.models.earth.atmosphere.Atmosphere
-
Get the local density.
- getDensity(FieldAbsoluteDate<T>, FieldVector3D<T>, Frame) - Method in interface org.orekit.models.earth.atmosphere.Atmosphere
-
Get the local density.
- getDensity(int, double, double, double, double, double, double, double, double) - Method in class org.orekit.models.earth.atmosphere.DTM2000
-
Get the local density with initial entries.
- getDensity(int, T, T, T, T, double, double, double, double) - Method in class org.orekit.models.earth.atmosphere.DTM2000
-
Get the local density with initial entries.
- getDensity(AbsoluteDate, Vector3D, Frame) - Method in class org.orekit.models.earth.atmosphere.DTM2000
-
Get the local density.
- getDensity(FieldAbsoluteDate<T>, FieldVector3D<T>, Frame) - Method in class org.orekit.models.earth.atmosphere.DTM2000
-
Get the local density.
- getDensity(Vector3D, Vector3D) - Method in class org.orekit.models.earth.atmosphere.HarrisPriester
-
Get the local density.
- getDensity(Vector3D, FieldVector3D<T>) - Method in class org.orekit.models.earth.atmosphere.HarrisPriester
-
Get the local density.
- getDensity(AbsoluteDate, Vector3D, Frame) - Method in class org.orekit.models.earth.atmosphere.HarrisPriester
-
Get the local density at some position.
- getDensity(FieldAbsoluteDate<T>, FieldVector3D<T>, Frame) - Method in class org.orekit.models.earth.atmosphere.HarrisPriester
-
Get the local density at some position.
- getDensity(double, double, double, double, double, double, double, double, double, double, double, double, double, double, double) - Method in class org.orekit.models.earth.atmosphere.JB2008
-
Get the local density with initial entries.
- getDensity(T, T, T, T, T, T, double, double, double, double, double, double, double, double, double) - Method in class org.orekit.models.earth.atmosphere.JB2008
-
Get the local density with initial entries.
- getDensity(AbsoluteDate, Vector3D, Frame) - Method in class org.orekit.models.earth.atmosphere.JB2008
-
Get the local density.
- getDensity(FieldAbsoluteDate<T>, FieldVector3D<T>, Frame) - Method in class org.orekit.models.earth.atmosphere.JB2008
-
Get the local density.
- getDensity(int) - Method in class org.orekit.models.earth.atmosphere.NRLMSISE00.FieldOutput
-
Get one of the stored densities.
- getDensity(AbsoluteDate, Vector3D, Frame) - Method in class org.orekit.models.earth.atmosphere.NRLMSISE00
-
Get the local density.
- getDensity(FieldAbsoluteDate<T>, FieldVector3D<T>, Frame) - Method in class org.orekit.models.earth.atmosphere.NRLMSISE00
-
Get the local density.
- getDensity(AbsoluteDate, Vector3D, Frame) - Method in class org.orekit.models.earth.atmosphere.SimpleExponentialAtmosphere
-
Get the local density.
- getDensity(FieldAbsoluteDate<T>, FieldVector3D<T>, Frame) - Method in class org.orekit.models.earth.atmosphere.SimpleExponentialAtmosphere
-
- getDeployDirSigma() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Maneuver
-
Get one σ angular off-nominal deployment vector direction.
- getDeployDv() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Maneuver
-
Get velocity increment of deployed "child" object.
- getDeployDvCda() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Maneuver
-
Get typical (50th percentile) product of drag coefficient times cross-sectional area of deployed "child" object.
- getDeployDvRatio() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Maneuver
-
Get ratio of child-to-host ΔV vectors.
- getDeployDvSigma() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Maneuver
-
Get one σ percent error on deployment ΔV magnitude.
- getDeployId() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Maneuver
-
Get identifier of resulting "child" object deployed from this host.
- getDeployMass() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Maneuver
-
Get decrement in host mass as a result of deployment.
- getDepth() - Method in class org.orekit.frames.Frame
-
Get the depth of the frame.
- getDerivative(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGammaMnsFunction
-
Get Γ function derivative.
- getDerivative(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GammaMnsFunction
-
Get Γ function derivative.
- getDerivative(int, T) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.FieldHansenTesseralLinear
-
Compute the value of the derivative dKj-n-1, s / de².
- getDerivative(int, T) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.FieldHansenThirdBodyLinear
-
Compute the value of the Hansen coefficient dK₀n, s / dΧ.
- getDerivative(int, T) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.FieldHansenZonalLinear
-
Get the dK₀-n-1,s / dΧ coefficient derivative.
- getDerivative(int, double) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenTesseralLinear
-
Compute the value of the derivative dKj-n-1, s / de².
- getDerivative(int, double) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenThirdBodyLinear
-
Compute the value of the Hansen coefficient dK₀n, s / dΧ.
- getDerivative(int, double) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenZonalLinear
-
Get the dK₀-n-1,s / dΧ coefficient derivative.
- getDerivativesDrivers() - Method in class org.orekit.estimation.measurements.EstimatedMeasurement
-
Get all the drivers with set derivatives.
- getDerivativesToEpoch(SpacecraftState, double[]) - Method in class org.orekit.forces.gravity.ThirdBodyAttractionEpoch
-
Compute derivatives of the state w.r.t epoch.
- getDesignator() - Method in class org.orekit.gnss.clock.RinexClock.Receiver
-
Getter for the designator.
- getDestination() - Method in enum org.orekit.frames.HelmertTransformation.Predefined
-
Get the destination ITRF.
- getDestination() - Method in class org.orekit.frames.ITRFVersion.Converter
-
Get the destination ITRF.
- getDetector() - Method in class org.orekit.propagation.events.AdapterDetector
-
Get the wrapped detector.
- getDetector() - Method in class org.orekit.propagation.events.EventEnablingPredicateFilter
-
Get the wrapped raw detector.
- getDetector() - Method in class org.orekit.propagation.events.EventShifter
-
Get the detector for the raw unshifted event.
- getDetector() - Method in class org.orekit.propagation.events.EventSlopeFilter
-
Get the wrapped raw detector.
- getDetector() - Method in class org.orekit.propagation.events.handlers.FieldRecordAndContinue.Event
-
Get the detector.
- getDetector() - Method in class org.orekit.propagation.events.handlers.RecordAndContinue.Event
-
Get the detector.
- getDetectorId() - Method in class org.orekit.files.ilrs.CRDConfiguration.DetectorConfiguration
-
Get the detector configuration ID.
- getDetectorRecord() - Method in class org.orekit.files.ilrs.CRDConfiguration
-
Get the detector configuration record.
- getDetectors() - Method in class org.orekit.propagation.events.BooleanDetector
-
Get the list of original detectors.
- getDetectorType() - Method in class org.orekit.files.ilrs.CRDConfiguration.DetectorConfiguration
-
Get the detector type.
- getdGjsdAlpha(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHIJjsPolynomials
-
Get the dGjs / dα coefficient.
- getdGjsdAlpha(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
-
Get the dGjs / dα coefficient.
- getdGjsdBeta(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHIJjsPolynomials
-
Get the dGjs / dβ coefficient.
- getdGjsdBeta(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
-
Get the dGjs / dβ coefficient.
- getdGjsdh(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHIJjsPolynomials
-
Get the dGjs / dh coefficient.
- getdGjsdh(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
-
Get the dGjs / dh coefficient.
- getdGjsdk(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHIJjsPolynomials
-
Get the dGjs / dk coefficient.
- getdGjsdk(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
-
Get the dGjs / dk coefficient.
- getdGmsdAlpha(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHmsjPolynomials
-
Get the dGmsj / dα coefficient.
- getdGmsdAlpha(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHmsjPolynomials
-
Get the dGmsj / dα coefficient.
- getdGmsdBeta(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHmsjPolynomials
-
Get the dGmsj / dβ coefficient.
- getdGmsdBeta(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHmsjPolynomials
-
Get the dGmsj / dβ coefficient.
- getdGmsdh(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHmsjPolynomials
-
Get the dGmsj / dh coefficient.
- getdGmsdh(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHmsjPolynomials
-
Get the dGmsj / dh coefficient.
- getdGmsdk(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHmsjPolynomials
-
Get the dGmsj / dk coefficient.
- getdGmsdk(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHmsjPolynomials
-
Get the dGmsj / dk coefficient.
- getdHjsdAlpha(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHIJjsPolynomials
-
Get the dHjs / dα coefficient.
- getdHjsdAlpha(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
-
Get the dHjs / dα coefficient.
- getdHjsdBeta(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHIJjsPolynomials
-
Get the dHjs / dβ coefficient.
- getdHjsdBeta(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
-
Get the dHjs / dβ coefficient.
- getdHjsdh(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHIJjsPolynomials
-
Get the dHjs / dh coefficient.
- getdHjsdh(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
-
Get the dHjs / dh coefficient.
- getdHjsdk(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHIJjsPolynomials
-
Get the dHjs / dk coefficient.
- getdHjsdk(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
-
Get the dHjs / dk coefficient.
- getdHmsdAlpha(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHmsjPolynomials
-
Get the dHmsj / dα coefficient.
- getdHmsdAlpha(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHmsjPolynomials
-
Get the dHmsj / dα coefficient.
- getdHmsdBeta(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHmsjPolynomials
-
Get the dHmsj / dβ coefficient.
- getdHmsdBeta(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHmsjPolynomials
-
Get the dHmsj / dβ coefficient.
- getdHmsdh(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHmsjPolynomials
-
Get the dHmsj / dh coefficient.
- getdHmsdh(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHmsjPolynomials
-
Get the dHmsj / dh coefficient.
- getdHmsdk(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHmsjPolynomials
-
Get the dHmsj / dk coefficient.
- getdHmsdk(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHmsjPolynomials
-
Get the dHmsj / dk coefficient.
- getDiagReference() - Method in class org.orekit.estimation.measurements.gnss.AbstractLambdaMethod
-
Get a reference to the diagonal matrix of the decomposition.
- getdIjsdAlpha(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHIJjsPolynomials
-
Get the dIjs / dα coefficient.
- getdIjsdAlpha(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
-
Get the dIjs / dα coefficient.
- getdIjsdBeta(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHIJjsPolynomials
-
Get the dIjs / dβ coefficient.
- getdIjsdBeta(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
-
Get the dIjs / dβ coefficient.
- getdIjsdh(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHIJjsPolynomials
-
Get the dIjs / dh coefficient.
- getdIjsdh(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
-
Get the dIjs / dh coefficient.
- getdIjsdk(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHIJjsPolynomials
-
Get the dIjs / dk coefficient.
- getdIjsdk(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
-
Get the dIjs / dk coefficient.
- getDimension() - Method in class org.orekit.estimation.measurements.AbstractMeasurement
-
Get the dimension of the measurement.
- getDimension() - Method in interface org.orekit.estimation.measurements.ObservedMeasurement
-
Get the dimension of the measurement.
- getDimension() - Method in class org.orekit.forces.maneuvers.jacobians.MassDepletionDelay
-
Get the dimension of the generated column.
- getDimension() - Method in interface org.orekit.propagation.integration.AdditionalDerivativesProvider
-
Get the dimension of the generated derivative.
- getDimension() - Method in class org.orekit.propagation.integration.AdditionalEquationsAdapter
-
Deprecated.
Get the dimension of the generated derivative.
- getDimension() - Method in interface org.orekit.propagation.integration.FieldAdditionalDerivativesProvider
-
Get the dimension of the generated derivative.
- getDimension() - Method in class org.orekit.propagation.integration.FieldAdditionalEquationsAdapter
-
Deprecated.
Get the dimension of the generated derivative.
- getDimension() - Method in class org.orekit.propagation.numerical.cr3bp.STMEquations
-
Get the dimension of the generated derivative.
- getDimension() - Method in class org.orekit.propagation.numerical.EpochDerivativesEquations
-
Get the dimension of the generated derivative.
- getDimension() - Method in class org.orekit.propagation.numerical.PartialDerivativesEquations
-
Deprecated.
Get the dimension of the generated derivative.
- getDimension() - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPartialDerivativesEquations
-
Deprecated.
Get the dimension of the generated derivative.
- getDirection() - Method in class org.orekit.forces.maneuvers.ConstantThrustManeuver
-
Get the direction.
- getDirection() - Method in class org.orekit.forces.maneuvers.propulsion.AbstractConstantThrustPropulsionModel
-
Get the thrust direction in S/C frame.
- getDirection(SpacecraftState) - Method in interface org.orekit.forces.maneuvers.propulsion.ThrustPropulsionModel
-
Get the thrust direction in spacecraft frame.
- getDirectionFlag() - Method in class org.orekit.files.ilrs.CRD.AnglesMeasurement
-
Get the direction flag (0 = transmit & receive ; 1 = transmit ; 2 = receive).
- getDiscontinuityCounter() - Method in class org.orekit.gnss.metric.messages.ssr.igm.PhaseBias
-
Get the signal phase discontinuity counter.
- getDisplacements() - Method in class org.orekit.estimation.measurements.GroundStation
-
Get the displacement models.
- getdJjsdAlpha(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHIJjsPolynomials
-
Get the dJjs / dα coefficient.
- getdJjsdAlpha(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
-
Get the dJjs / dα coefficient.
- getdJjsdBeta(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHIJjsPolynomials
-
Get the dJjs / dβ coefficient.
- getdJjsdBeta(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
-
Get the dJjs / dβ coefficient.
- getdJjsdh(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHIJjsPolynomials
-
Get the dJjs / dh coefficient.
- getdJjsdh(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
-
Get the dJjs / dh coefficient.
- getdJjsdk(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHIJjsPolynomials
-
Get the dJjs / dk coefficient.
- getdJjsdk(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
-
Get the dJjs / dk coefficient.
- getdLnsdGamma(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldLnsCoefficients
-
Get the value of dLns / dγ (γ).
- getdLnsdGamma(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.LnsCoefficients
-
Get the value of dLns / dγ (γ).
- getDnl(double, double, int, int) - Static method in class org.orekit.propagation.semianalytical.dsst.utilities.UpperBounds
-
Get the upper bound value Dnl(Χ).
- getDnl(T, T, int, int) - Static method in class org.orekit.propagation.semianalytical.dsst.utilities.UpperBounds
-
Get the upper bound value Dnl(Χ).
- getDockedWith() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
-
Get the other space objects this object is docked to.
- getDomes() - Method in class org.orekit.files.sinex.Station
-
Get the site DOMES number.
- getDoodson() - Method in class org.orekit.forces.gravity.potential.OceanTidesWave
-
Get the Doodson number for the wave.
- getDoodsonMultipliers() - Method in class org.orekit.models.earth.displacement.Tide
-
Get the multipliers for Doodson arguments (τ, s, h, p, N', ps).
- getDoodsonNumber() - Method in class org.orekit.models.earth.displacement.Tide
-
Get the Doodson number.
- getDopplerCountBias() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
-
Get the Doppler count bias.
- getDopplerCountScale() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
-
Get the Doppler count scale.
- getDotOrbitDeltaAlongTrack() - Method in class org.orekit.gnss.metric.messages.ssr.igm.OrbitCorrection
-
Get the velocity of along-track orbit correction for broadcast ephemeris.
- getDotOrbitDeltaCrossTrack() - Method in class org.orekit.gnss.metric.messages.ssr.igm.OrbitCorrection
-
Get the velocity of cross-track orbit correction for broadcast ephemeris.
- getDotOrbitDeltaRadial() - Method in class org.orekit.gnss.metric.messages.ssr.igm.OrbitCorrection
-
Get the velocity of radial orbit correction for broadcast ephemeris.
- getDrag() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTAtmosphericDrag
-
Get drag force.
- getDragArea() - Method in class org.orekit.files.ccsds.ndm.odm.SpacecraftParameters
-
Get the drag area.
- getDragCoeff() - Method in class org.orekit.files.ccsds.ndm.odm.SpacecraftParameters
-
Get the drag coefficient.
- getDragCoefficient() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
-
Get the nominal drag coefficient.
- getDragConstantArea() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
-
Get the attitude-independent drag cross-sectional area, not already into attitude-dependent area along OEB.
- getDragParametersDrivers() - Method in class org.orekit.forces.BoxAndSolarArraySpacecraft
-
Get the drivers for supported parameters.
- getDragParametersDrivers() - Method in interface org.orekit.forces.drag.DragSensitive
-
Get the drivers for supported parameters.
- getDragParametersDrivers() - Method in class org.orekit.forces.drag.IsotropicDrag
-
Get the drivers for supported parameters.
- getDragSensitive(AbsoluteDate) - Method in class org.orekit.forces.drag.TimeSpanDragForce
-
- getDragSensitiveSpan(AbsoluteDate) - Method in class org.orekit.forces.drag.TimeSpanDragForce
-
- getDragUncertainty() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
-
Get the drag coefficient 1σ uncertainty.
- getDrivers() - Method in class org.orekit.estimation.measurements.modifiers.AbstractAmbiguityModifier
-
Get the drivers for this modifier.
- getDrivers(double, Orbit, PositionAngle) - Method in enum org.orekit.orbits.OrbitType
-
Get parameters drivers initialized from a reference orbit.
- getDrivers() - Method in class org.orekit.utils.ParameterDriversList
-
Get delegating drivers for all parameters.
- getDryMass() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
-
Get the mass without propellant.
- getDSDensityWrtStateUsingFiniteDifferences(AbsoluteDate, Frame, FieldVector3D<DerivativeStructure>) - Method in class org.orekit.forces.drag.AbstractDragForceModel
-
Compute density and its derivatives.
- getDsjDh(int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.CjSjCoefficient
-
Get the dSj / dh coefficient.
- getDsjDh(int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldCjSjCoefficient
-
Get the dSj / dh coefficient.
- getDsjDk(int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.CjSjCoefficient
-
Get the dSj / dk coefficient.
- getDsjDk(int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldCjSjCoefficient
-
Get the dSj / dk coefficient.
- getDSTDTC(AbsoluteDate) - Method in interface org.orekit.models.earth.atmosphere.JB2008InputParameters
-
Get the temperature change computed from Dst index.
- getDuration() - Method in class org.orekit.files.ccsds.ndm.adm.apm.Maneuver
-
Get duration (value is 0 for impulsive maneuver).
- getDuration() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Maneuver
-
Get duration.
- getDuration() - Method in class org.orekit.files.ccsds.ndm.odm.opm.Maneuver
-
Get duration (value is 0 for impulsive maneuver).
- getDuration() - Method in class org.orekit.forces.maneuvers.ConstantThrustManeuver
-
Get the duration of the maneuver (s).
- getDuration() - Method in class org.orekit.forces.maneuvers.trigger.DateBasedManeuverTriggers
-
Get the duration of the maneuver (s).
- getDurationDriver() - Method in class org.orekit.propagation.events.FieldParameterDrivenDateIntervalDetector
-
Get the driver for duration.
- getDurationDriver() - Method in class org.orekit.propagation.events.ParameterDrivenDateIntervalDetector
-
Get the driver for duration.
- getDv() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Maneuver
-
Get velocity increment.
- getDV() - Method in class org.orekit.files.ccsds.ndm.odm.opm.Maneuver
-
Get velocity increment.
- getDvDirSigma() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Maneuver
-
Get one σ angular off-nominal ΔV direction.
- getDvMagSigma() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Maneuver
-
Get one σ percent error on ΔV magnitude.
- getDx() - Method in class org.orekit.frames.EOPEntry
-
Get the correction for Celestial Intermediate Pole (CIP) coordinates.
- getDy() - Method in class org.orekit.frames.EOPEntry
-
Get the correction for Celestial Intermediate Pole (CIP) coordinates.
- getE() - Method in class org.orekit.files.ccsds.ndm.odm.KeplerianElements
-
Get the orbit eccentricity.
- getE() - Method in class org.orekit.orbits.CartesianOrbit
-
Get the eccentricity.
- getE() - Method in class org.orekit.orbits.CircularOrbit
-
Get the eccentricity.
- getE() - Method in class org.orekit.orbits.EquinoctialOrbit
-
Get the eccentricity.
- getE() - Method in class org.orekit.orbits.FieldCartesianOrbit
-
Get the eccentricity.
- getE() - Method in class org.orekit.orbits.FieldCircularOrbit
-
Get the eccentricity.
- getE() - Method in class org.orekit.orbits.FieldEquinoctialOrbit
-
Get the eccentricity.
- getE() - Method in class org.orekit.orbits.FieldKeplerianOrbit
-
Get the eccentricity.
- getE() - Method in class org.orekit.orbits.FieldOrbit
-
Get the eccentricity.
- getE() - Method in class org.orekit.orbits.KeplerianOrbit
-
Get the eccentricity.
- getE() - Method in class org.orekit.orbits.Orbit
-
Get the eccentricity.
- getE() - Method in class org.orekit.propagation.analytical.gnss.data.CommonGnssData
-
Getter for the eccentricity.
- getE() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSAlmanac
-
- getE() - Method in interface org.orekit.propagation.analytical.gnss.data.GLONASSOrbitalElements
-
Get the Eccentricity.
- getE() - Method in interface org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElements
-
Gets the Eccentricity.
- getE() - Method in class org.orekit.propagation.analytical.tle.FieldTLE
-
Get the eccentricity.
- getE() - Method in class org.orekit.propagation.analytical.tle.TLE
-
Get the eccentricity.
- getE() - Method in class org.orekit.propagation.FieldSpacecraftState
-
Get the eccentricity.
- getE() - Method in class org.orekit.propagation.SpacecraftState
-
Get the eccentricity.
- getE2() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseralContext
-
Get ecc².
- getE2() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTTesseralContext
-
Get ecc².
- getEarliest() - Method in class org.orekit.utils.GenericTimeStampedCache
-
Get the earliest cached entry.
- getEarliest() - Method in class org.orekit.utils.ImmutableTimeStampedCache
-
Get the earliest entry in this cache.
- getEarliest() - Method in interface org.orekit.utils.TimeStampedCache
-
Get the earliest entry in this cache.
- getEarth() - Method in interface org.orekit.bodies.CelestialBodies
-
Get the Earth singleton body.
- getEarth() - Static method in class org.orekit.bodies.CelestialBodyFactory
-
Get the Earth singleton body.
- getEarth() - Method in class org.orekit.bodies.LazyLoadedCelestialBodies
-
- getEarth() - Method in class org.orekit.forces.gravity.DeSitterRelativity
-
Get the Earth model used to compute De Sitter effect.
- getEarthMoonBarycenter() - Method in interface org.orekit.bodies.CelestialBodies
-
Get the Earth-Moon barycenter singleton bodies pair.
- getEarthMoonBarycenter() - Static method in class org.orekit.bodies.CelestialBodyFactory
-
Get the Earth-Moon barycenter singleton bodies pair.
- getEarthMoonBarycenter() - Method in class org.orekit.bodies.LazyLoadedCelestialBodies
-
- getEarthMoonBarycenterSemiMajorAxis(AbsoluteDate, TimeScale) - Static method in class org.orekit.propagation.numerical.cr3bp.CR3BPConstants
-
Get the Earth-Moon barycenter semi-major axis.
- getEarthMoonCR3BP() - Static method in class org.orekit.bodies.CR3BPFactory
-
Get the Earth-Moon CR3BP singleton bodies pair.
- getEarthOrientationAngleFunction(TimeScale) - Method in enum org.orekit.utils.IERSConventions
-
Get the function computing the raw Earth Orientation Angle.
- getEarthOrientationAngleFunction(TimeScale, TimeScale) - Method in enum org.orekit.utils.IERSConventions
-
Get the function computing the raw Earth Orientation Angle.
- getEast() - Method in class org.orekit.bodies.FieldGeodeticPoint
-
Get the direction to the east of point, expressed in parent shape frame.
- getEast() - Method in class org.orekit.bodies.GeodeticPoint
-
Get the direction to the east of point, expressed in parent shape frame.
- getEast() - Method in class org.orekit.frames.TopocentricFrame
-
Get the east direction of topocentric frame, expressed in parent shape frame.
- getEastOffsetDriver() - Method in class org.orekit.estimation.measurements.GroundStation
-
Get a driver allowing to change station position along East axis.
- getEcc() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
-
Get the eccentricity.
- getEcc() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldAuxiliaryElements
-
Get the eccentricity.
- getEccentricAnomaly() - Method in class org.orekit.orbits.FieldKeplerianOrbit
-
Get the eccentric anomaly.
- getEccentricAnomaly() - Method in class org.orekit.orbits.KeplerianOrbit
-
Get the eccentric anomaly.
- getEccentricAnomalyDot() - Method in class org.orekit.orbits.FieldKeplerianOrbit
-
Get the eccentric anomaly derivative.
- getEccentricAnomalyDot() - Method in class org.orekit.orbits.KeplerianOrbit
-
Get the eccentric anomaly derivative.
- getEccentricities() - Method in class org.orekit.files.sinex.Station
-
Get the last known station antenna eccentricities.
- getEccentricities(AbsoluteDate) - Method in class org.orekit.files.sinex.Station
-
Get the station antenna eccentricities for the given epoch.
- getEccentricities(Frequency) - Method in class org.orekit.gnss.antenna.Antenna
-
Get the phase center eccentricities.
- getEccentricities() - Method in class org.orekit.gnss.antenna.FrequencyPattern
-
Get the phase center eccentricities.
- getEccentricities() - Method in class org.orekit.gnss.RinexObservationHeader
-
Get the eccentricities of antenna center.
- getEccentricitiesTimeSpanMap() - Method in class org.orekit.files.sinex.Station
-
Get the TimeSpanMap of site antenna eccentricities.
- getEccRefSystem() - Method in class org.orekit.files.sinex.Station
-
Get the reference system used to define the eccentricity vector (local or cartesian).
- getEccRefSystem(String) - Static method in enum org.orekit.files.sinex.Station.ReferenceSystem
-
Get the eccentricity reference system corresponding to the given value.
- getECEF() - Method in class org.orekit.propagation.analytical.gnss.GLONASSAnalyticalPropagator
-
Gets the Earth Centered Earth Fixed frame used to propagate GLONASS orbits.
- getECEF() - Method in class org.orekit.propagation.analytical.gnss.GNSSPropagator
-
Gets the Earth Centered Earth Fixed frame used to propagate GNSS orbits according to the
Interface Control Document.
- getECEF() - Method in class org.orekit.propagation.analytical.gnss.SBASPropagator
-
Gets the Earth Centered Earth Fixed frame used to propagate GNSS orbits.
- getECI() - Method in class org.orekit.propagation.analytical.gnss.GLONASSAnalyticalPropagator
-
Gets the Earth Centered Inertial frame used to propagate the orbit.
- getECI() - Method in class org.orekit.propagation.analytical.gnss.GNSSPropagator
-
Gets the Earth Centered Inertial frame used to propagate the orbit.
- getECI() - Method in class org.orekit.propagation.analytical.gnss.SBASPropagator
-
Gets the Earth Centered Inertial frame used to propagate the orbit.
- getEclipseAngles(Vector3D, Vector3D) - Method in class org.orekit.forces.radiation.AbstractRadiationForceModel
-
Get the useful angles for eclipse computation.
- getEclipseAngles(FieldVector3D<T>, FieldVector3D<T>) - Method in class org.orekit.forces.radiation.AbstractRadiationForceModel
-
Get the useful angles for eclipse computation.
- getEcliptic(IERSConventions) - Method in class org.orekit.frames.AbstractFrames
-
- getEcliptic(IERSConventions) - Method in interface org.orekit.frames.Frames
-
Get the ecliptic frame.
- getEcliptic(IERSConventions) - Static method in class org.orekit.frames.FramesFactory
-
Get the ecliptic frame.
- getEDot() - Method in class org.orekit.orbits.CartesianOrbit
-
Get the eccentricity derivative.
- getEDot() - Method in class org.orekit.orbits.CircularOrbit
-
Get the eccentricity derivative.
- getEDot() - Method in class org.orekit.orbits.EquinoctialOrbit
-
Get the eccentricity derivative.
- getEDot() - Method in class org.orekit.orbits.FieldCartesianOrbit
-
Get the eccentricity derivative.
- getEDot() - Method in class org.orekit.orbits.FieldCircularOrbit
-
Get the eccentricity derivative.
- getEDot() - Method in class org.orekit.orbits.FieldEquinoctialOrbit
-
Get the eccentricity derivative.
- getEDot() - Method in class org.orekit.orbits.FieldKeplerianOrbit
-
Get the eccentricity derivative.
- getEDot() - Method in class org.orekit.orbits.FieldOrbit
-
Get the eccentricity derivative.
- getEDot() - Method in class org.orekit.orbits.KeplerianOrbit
-
Get the eccentricity derivative.
- getEDot() - Method in class org.orekit.orbits.Orbit
-
Get the eccentricity derivative.
- getEffects() - Method in class org.orekit.propagation.analytical.AdapterPropagator
-
Get the differential effects.
- getElem(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.PolynomialFunctionMatrix
-
Get the value of an element.
- getElementNumber() - Method in class org.orekit.propagation.analytical.tle.FieldTLE
-
Get the element number.
- getElementNumber() - Method in class org.orekit.propagation.analytical.tle.TLE
-
Get the element number.
- getElements() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryState
-
Get trajectory elements.
- getElementSetNumber() - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmTle
-
Get the element set number for this satellite.
- getElevation() - Method in class org.orekit.files.ilrs.CRD.AnglesMeasurement
-
Get the elevation angle.
- getElevation(Vector3D, Frame, AbsoluteDate) - Method in class org.orekit.frames.TopocentricFrame
-
Get the elevation of a point with regards to the local point.
- getElevation(FieldVector3D<T>, Frame, FieldAbsoluteDate<T>) - Method in class org.orekit.frames.TopocentricFrame
-
Get the elevation of a point with regards to the local point.
- getElevation(SpacecraftState) - Method in class org.orekit.propagation.events.ElevationExtremumDetector
-
Get the elevation value.
- getElevation(double) - Method in class org.orekit.utils.ElevationMask
-
Get the interpolated elevation for a given azimuth according to the mask.
- getElevationMask() - Method in class org.orekit.gnss.DOPComputer
-
Get the elevation mask.
- getElevationMask() - Method in class org.orekit.propagation.events.ElevationDetector
-
Returns the currently configured elevation mask.
- getElevationMask() - Method in class org.orekit.propagation.events.FieldElevationDetector
-
Returns the currently configured elevation mask.
- getElevationRate() - Method in class org.orekit.files.ilrs.CRD.AnglesMeasurement
-
Get the elevation rate.
- getEllipsoid() - Method in interface org.orekit.models.earth.EarthShape
-
Get the underlying ellipsoid model that defines latitude and longitude.
- getEllipsoid() - Method in class org.orekit.models.earth.Geoid
-
- getEllipsoid() - Method in class org.orekit.models.earth.ReferenceEllipsoid
-
- getEME2000() - Method in class org.orekit.frames.AbstractFrames
-
- getEME2000() - Method in interface org.orekit.frames.Frames
-
Get the unique EME2000 frame.
- getEME2000() - Static method in class org.orekit.frames.FramesFactory
-
Get the unique EME2000 frame.
- getEn() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data
-
Get the GLONASS En Word.
- getEnd() - Method in class org.orekit.estimation.measurements.generation.AbstractMeasurementBuilder
-
Get the end of the measurements time span.
- getEnd() - Method in class org.orekit.utils.TimeSpanMap.Span
-
Get the end of this time span.
- getEndDate(Frequency) - Method in class org.orekit.estimation.measurements.gnss.CycleSlipDetectorResults
-
Return the end date at the given frequency.
- getEndDate() - Method in class org.orekit.forces.maneuvers.ConstantThrustManeuver
-
Get the end date.
- getEndDate() - Method in class org.orekit.forces.maneuvers.trigger.DateBasedManeuverTriggers
-
Get the end date.
- getEndDate() - Method in class org.orekit.frames.EOPHistory
-
Get the date of the last available Earth Orientation Parameters.
- getEndDate() - Method in class org.orekit.gnss.clock.RinexClock.ReferenceClock
-
Getter for the validity period end date.
- getEndEpoch() - Method in class org.orekit.files.ilrs.ILRSHeader
-
Get the ending epoch (UTC).
- getEndpoints() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemMetadata
-
Get the endpoints (i.e.
- getEndpoints() - Method in class org.orekit.files.ccsds.ndm.adm.apm.ApmQuaternion
-
Get the endpoints (i.e.
- getEndpoints() - Method in class org.orekit.files.ccsds.ndm.adm.apm.Euler
-
Get the endpoints (i.e.
- getEndpoints() - Method in class org.orekit.files.ccsds.ndm.adm.apm.SpinStabilized
-
Get the endpoints (i.e.
- getEndTransition() - Method in class org.orekit.utils.TimeSpanMap.Span
-
Get the transition at end of this time span.
- getEntries() - Method in class org.orekit.frames.EOPHistory
-
Get a non-modifiable view of the EOP entries.
- getEntries() - Method in class org.orekit.utils.GenericTimeStampedCache
-
Get the total number of entries cached.
- getEntry(String) - Method in class org.orekit.utils.DoubleArrayDictionary
-
Get a complete entry.
- getEntry(String) - Method in class org.orekit.utils.FieldArrayDictionary
-
Get a complete entry.
- getEOPHistory() - Method in interface org.orekit.frames.EOPBasedTransformProvider
-
Get the EOP history.
- getEOPHistory(IERSConventions, boolean) - Method in interface org.orekit.frames.Frames
-
Get Earth Orientation Parameters history.
- getEOPHistory(IERSConventions, boolean) - Static method in class org.orekit.frames.FramesFactory
-
Get Earth Orientation Parameters history.
- getEOPHistory() - Method in class org.orekit.frames.GTODProvider
-
Get the EOP history.
- getEOPHistory(IERSConventions, boolean, TimeScales) - Method in class org.orekit.frames.LazyLoadedEop
-
Get Earth Orientation Parameters history.
- getEOPHistory(IERSConventions, boolean) - Method in class org.orekit.frames.LazyLoadedFrames
-
Get Earth Orientation Parameters history.
- getEopHistory(IERSConventions, boolean) - Method in class org.orekit.time.AbstractTimeScales
-
Get the EOP history for the given conventions.
- getEopHistory(IERSConventions, boolean) - Method in class org.orekit.time.LazyLoadedTimeScales
-
- getEOPHistory() - Method in class org.orekit.time.UT1Scale
-
Get the EOP history.
- getEopSource() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
-
Get the source and version of Earth Orientation Parameters.
- getEOPTidalCorrection() - Method in enum org.orekit.utils.IERSConventions
-
Get the function computing tidal corrections for Earth Orientation Parameters.
- getEOPTidalCorrection(TimeScales) - Method in enum org.orekit.utils.IERSConventions
-
Get the function computing tidal corrections for Earth Orientation Parameters.
- getEphemeridesDataLines() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemData
-
Get the list of Ephemerides data lines.
- getEphemeridesDataLines() - Method in class org.orekit.files.ilrs.CPF.CPFEphemeris
-
Get the list of Ephemerides data lines.
- getEphemerisData() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.RtcmEphemerisMessage
-
Get the ephemeris data contain in the ephemeris message.
- getEphemerisGenerator() - Method in class org.orekit.propagation.analytical.AbstractAnalyticalPropagator
-
Set up an ephemeris generator that will monitor the propagation for building
an ephemeris from it once completed.
- getEphemerisGenerator() - Method in class org.orekit.propagation.analytical.FieldAbstractAnalyticalPropagator
-
Set up an ephemeris generator that will monitor the propagation for building
an ephemeris from it once completed.
- getEphemerisGenerator() - Method in interface org.orekit.propagation.FieldPropagator
-
Set up an ephemeris generator that will monitor the propagation for building
an ephemeris from it once completed.
- getEphemerisGenerator() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
-
Set up an ephemeris generator that will monitor the propagation for building
an ephemeris from it once completed.
- getEphemerisGenerator() - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator
-
Set up an ephemeris generator that will monitor the propagation for building
an ephemeris from it once completed.
- getEphemerisGenerator() - Method in interface org.orekit.propagation.Propagator
-
Set up an ephemeris generator that will monitor the propagation for building
an ephemeris from it once completed.
- getEphemerisNames() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
-
Getter for external ephemeris names for participants.
- getEphemerisType() - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmTle
-
Get the ephemeris type.
- getEphemerisType() - Method in class org.orekit.propagation.analytical.tle.FieldTLE
-
Get the type of ephemeris.
- getEphemerisType() - Method in class org.orekit.propagation.analytical.tle.TLE
-
Get the type of ephemeris.
- getEpoch() - Method in class org.orekit.files.ccsds.ndm.adm.apm.ApmQuaternion
-
Get the epoch of the data.
- getEpoch() - Method in class org.orekit.files.ccsds.ndm.odm.CartesianCovariance
-
Get matrix epoch.
- getEpoch() - Method in class org.orekit.files.ccsds.ndm.odm.KeplerianElements
-
Get epoch of state vector, Keplerian elements and covariance matrix data.
- getEpoch() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
-
Get time tag for orbit determination solved-for state.
- getEpoch() - Method in class org.orekit.files.ccsds.ndm.odm.StateVector
-
Get epoch of state vector, Keplerian elements and covariance matrix data.
- getEpoch() - Method in class org.orekit.files.ccsds.ndm.tdm.Observation
-
Getter for the epoch.
- getEpoch() - Method in class org.orekit.files.sinex.Station
-
Get the coordinates reference epoch.
- getEpoch() - Method in class org.orekit.files.sp3.SP3
-
Returns the start epoch of the orbit file.
- getEpoch() - Method in class org.orekit.frames.HelmertTransformation
-
Get the reference epoch of the transform.
- getEpoch() - Method in class org.orekit.gnss.clock.RinexClock.ClockDataLine
-
Get data line epoch.
- getEpoch(TimeScale) - Method in class org.orekit.gnss.clock.RinexClock.ClockDataLine
-
Get data line epoch.
- getEpoch() - Method in class org.orekit.models.earth.GeoMagneticField
-
Returns the epoch for this magnetic field model.
- getEpochDelayCorrection() - Method in class org.orekit.files.ilrs.CRDConfiguration.TimingSystemConfiguration
-
Get the epoch delay correction.
- getEpochEigenMaj() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
-
Get positional error ellipsoid 1σ major eigenvalue at the epoch of OD.
- getEpochEigenMed() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
-
Get positional error ellipsoid 1σ intermediate eigenvalue at the epoch of OD.
- getEpochEigenMin() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
-
Get positional error ellipsoid 1σ minor eigenvalue at the epoch of OD.
- getEpochEvent() - Method in class org.orekit.files.ilrs.CRD.RangeMeasurement
-
Get the indicator for the time event reference.
- getEpochIdentifier() - Method in class org.orekit.files.ilrs.CRDHeader
-
Get the epoch identifier.
- getEpochIgnition() - Method in class org.orekit.files.ccsds.ndm.odm.opm.Maneuver
-
Get epoch ignition.
- getEpochInterval() - Method in class org.orekit.files.sp3.SP3
-
Returns the time interval between epochs (in seconds).
- getEpochStart() - Method in class org.orekit.files.ccsds.ndm.adm.apm.Maneuver
-
Get epoch start.
- getEpochT0() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
-
Get the epoch to which all relative times are referenced in data blocks.
- getEpochToc() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractEphemerisMessage
-
Getter for the time of clock epoch.
- getEpochToc() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractNavigationMessage
-
Getter for the time of clock epoch.
- getEquatorialRadius() - Method in class org.orekit.bodies.OneAxisEllipsoid
-
Get the equatorial radius of the body.
- getEquatorialRadius() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
-
Get oblate spheroid equatorial radius of central body.
- getEquatorialRadius() - Method in class org.orekit.forces.radiation.AbstractRadiationForceModel
-
Getter for equatorial radius.
- getEquatorialRadius() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTSolarRadiationPressure
-
Get the central body equatorial radius.
- getEquinoctialEx() - Method in class org.orekit.orbits.CartesianOrbit
-
Get the first component of the equinoctial eccentricity vector derivative.
- getEquinoctialEx() - Method in class org.orekit.orbits.CircularOrbit
-
Get the first component of the equinoctial eccentricity vector derivative.
- getEquinoctialEx() - Method in class org.orekit.orbits.EquinoctialOrbit
-
Get the first component of the equinoctial eccentricity vector derivative.
- getEquinoctialEx() - Method in class org.orekit.orbits.FieldCartesianOrbit
-
Get the first component of the equinoctial eccentricity vector.
- getEquinoctialEx() - Method in class org.orekit.orbits.FieldCircularOrbit
-
Get the first component of the equinoctial eccentricity vector.
- getEquinoctialEx() - Method in class org.orekit.orbits.FieldEquinoctialOrbit
-
Get the first component of the equinoctial eccentricity vector.
- getEquinoctialEx() - Method in class org.orekit.orbits.FieldKeplerianOrbit
-
Get the first component of the equinoctial eccentricity vector.
- getEquinoctialEx() - Method in class org.orekit.orbits.FieldOrbit
-
Get the first component of the equinoctial eccentricity vector.
- getEquinoctialEx() - Method in class org.orekit.orbits.KeplerianOrbit
-
Get the first component of the equinoctial eccentricity vector derivative.
- getEquinoctialEx() - Method in class org.orekit.orbits.Orbit
-
Get the first component of the equinoctial eccentricity vector derivative.
- getEquinoctialEx() - Method in class org.orekit.propagation.FieldSpacecraftState
-
Get the first component of the eccentricity vector (as per equinoctial parameters).
- getEquinoctialEx() - Method in class org.orekit.propagation.SpacecraftState
-
Get the first component of the eccentricity vector (as per equinoctial parameters).
- getEquinoctialExDot() - Method in class org.orekit.orbits.CartesianOrbit
-
Get the first component of the equinoctial eccentricity vector.
- getEquinoctialExDot() - Method in class org.orekit.orbits.CircularOrbit
-
Get the first component of the equinoctial eccentricity vector.
- getEquinoctialExDot() - Method in class org.orekit.orbits.EquinoctialOrbit
-
Get the first component of the equinoctial eccentricity vector.
- getEquinoctialExDot() - Method in class org.orekit.orbits.FieldCartesianOrbit
-
Get the first component of the equinoctial eccentricity vector.
- getEquinoctialExDot() - Method in class org.orekit.orbits.FieldCircularOrbit
-
Get the first component of the equinoctial eccentricity vector.
- getEquinoctialExDot() - Method in class org.orekit.orbits.FieldEquinoctialOrbit
-
Get the first component of the equinoctial eccentricity vector.
- getEquinoctialExDot() - Method in class org.orekit.orbits.FieldKeplerianOrbit
-
Get the first component of the equinoctial eccentricity vector.
- getEquinoctialExDot() - Method in class org.orekit.orbits.FieldOrbit
-
Get the first component of the equinoctial eccentricity vector.
- getEquinoctialExDot() - Method in class org.orekit.orbits.KeplerianOrbit
-
Get the first component of the equinoctial eccentricity vector.
- getEquinoctialExDot() - Method in class org.orekit.orbits.Orbit
-
Get the first component of the equinoctial eccentricity vector.
- getEquinoctialEy() - Method in class org.orekit.orbits.CartesianOrbit
-
Get the second component of the equinoctial eccentricity vector derivative.
- getEquinoctialEy() - Method in class org.orekit.orbits.CircularOrbit
-
Get the second component of the equinoctial eccentricity vector derivative.
- getEquinoctialEy() - Method in class org.orekit.orbits.EquinoctialOrbit
-
Get the second component of the equinoctial eccentricity vector derivative.
- getEquinoctialEy() - Method in class org.orekit.orbits.FieldCartesianOrbit
-
Get the second component of the equinoctial eccentricity vector.
- getEquinoctialEy() - Method in class org.orekit.orbits.FieldCircularOrbit
-
Get the second component of the equinoctial eccentricity vector.
- getEquinoctialEy() - Method in class org.orekit.orbits.FieldEquinoctialOrbit
-
Get the second component of the equinoctial eccentricity vector.
- getEquinoctialEy() - Method in class org.orekit.orbits.FieldKeplerianOrbit
-
Get the second component of the equinoctial eccentricity vector.
- getEquinoctialEy() - Method in class org.orekit.orbits.FieldOrbit
-
Get the second component of the equinoctial eccentricity vector.
- getEquinoctialEy() - Method in class org.orekit.orbits.KeplerianOrbit
-
Get the second component of the equinoctial eccentricity vector derivative.
- getEquinoctialEy() - Method in class org.orekit.orbits.Orbit
-
Get the second component of the equinoctial eccentricity vector derivative.
- getEquinoctialEy() - Method in class org.orekit.propagation.FieldSpacecraftState
-
Get the second component of the eccentricity vector (as per equinoctial parameters).
- getEquinoctialEy() - Method in class org.orekit.propagation.SpacecraftState
-
Get the second component of the eccentricity vector (as per equinoctial parameters).
- getEquinoctialEyDot() - Method in class org.orekit.orbits.CartesianOrbit
-
Get the second component of the equinoctial eccentricity vector.
- getEquinoctialEyDot() - Method in class org.orekit.orbits.CircularOrbit
-
Get the second component of the equinoctial eccentricity vector.
- getEquinoctialEyDot() - Method in class org.orekit.orbits.EquinoctialOrbit
-
Get the second component of the equinoctial eccentricity vector.
- getEquinoctialEyDot() - Method in class org.orekit.orbits.FieldCartesianOrbit
-
Get the second component of the equinoctial eccentricity vector.
- getEquinoctialEyDot() - Method in class org.orekit.orbits.FieldCircularOrbit
-
Get the second component of the equinoctial eccentricity vector.
- getEquinoctialEyDot() - Method in class org.orekit.orbits.FieldEquinoctialOrbit
-
Get the second component of the equinoctial eccentricity vector.
- getEquinoctialEyDot() - Method in class org.orekit.orbits.FieldKeplerianOrbit
-
Get the second component of the equinoctial eccentricity vector.
- getEquinoctialEyDot() - Method in class org.orekit.orbits.FieldOrbit
-
Get the second component of the equinoctial eccentricity vector.
- getEquinoctialEyDot() - Method in class org.orekit.orbits.KeplerianOrbit
-
Get the second component of the equinoctial eccentricity vector.
- getEquinoctialEyDot() - Method in class org.orekit.orbits.Orbit
-
Get the second component of the equinoctial eccentricity vector.
- getEquinoxNutationCorrection(AbsoluteDate) - Method in class org.orekit.frames.EOPHistory
-
Get the correction to the nutation parameters for equinox-based paradigm.
- getEquinoxNutationCorrection(FieldAbsoluteDate<T>) - Method in class org.orekit.frames.EOPHistory
-
Get the correction to the nutation parameters for equinox-based paradigm.
- getEstimate() - Method in class org.orekit.estimation.sequential.AbstractKalmanModel
-
Get the current corrected estimate.
- getEstimate() - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanModel
-
Get the current corrected estimate.
- getEstimatedEarthFrame() - Method in class org.orekit.estimation.measurements.GroundStation
-
Get the estimated Earth frame, including the estimated linear models for pole and prime meridian.
- getEstimatedMeasurement(int) - Method in interface org.orekit.estimation.measurements.EstimationsProvider
-
Get one estimated measurement.
- getEstimatedMeasurements() - Method in class org.orekit.estimation.measurements.MultiplexedMeasurement
-
Get the underlying estimated measurements.
- getEstimatedMeasurementsParameters() - Method in class org.orekit.estimation.sequential.AbstractKalmanModel
-
Get the list of estimated measurements parameters.
- getEstimatedMeasurementsParameters() - Method in interface org.orekit.estimation.sequential.KalmanEstimation
-
Get the list of estimated measurements parameters.
- getEstimatedMeasurementsParameters() - Method in class org.orekit.estimation.sequential.KalmanEstimator
-
Get the list of estimated measurements parameters.
- getEstimatedMeasurementsParameters() - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanEstimator
-
Get the list of estimated measurements parameters.
- getEstimatedMeasurementsParameters() - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanModel
-
Get the list of estimated measurements parameters.
- getEstimatedOrbitalParameters() - Method in class org.orekit.estimation.sequential.AbstractKalmanModel
-
Get the list of estimated orbital parameters.
- getEstimatedOrbitalParameters() - Method in interface org.orekit.estimation.sequential.KalmanEstimation
-
Get the list of estimated orbital parameters.
- getEstimatedOrbitalParameters() - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanModel
-
Get the list of estimated orbital parameters.
- getEstimatedPropagationParameters() - Method in class org.orekit.estimation.sequential.AbstractKalmanModel
-
Get the list of estimated propagation parameters.
- getEstimatedPropagationParameters() - Method in interface org.orekit.estimation.sequential.KalmanEstimation
-
Get the list of estimated propagation parameters.
- getEstimatedPropagationParameters() - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanModel
-
Get the list of estimated propagation parameters.
- getEstimatedPropagator() - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanModel
-
Get the propagator estimated with the values set in the propagator builder.
- getEstimatedPropagators() - Method in class org.orekit.estimation.sequential.AbstractKalmanModel
-
Get the propagators estimated with the values set in the propagators builders.
- getEstimatedUT1() - Method in class org.orekit.estimation.measurements.EstimatedEarthFrameProvider
-
Get the estimated UT1 time scale.
- getEstimatedUT1() - Method in class org.orekit.estimation.measurements.GroundStation
-
Get the estimated UT1 scale, including the estimated linear models for prime meridian.
- getEstimatedValue() - Method in class org.orekit.estimation.measurements.EstimatedMeasurement
-
Get the estimated value.
- getEulerBlock() - Method in class org.orekit.files.ccsds.ndm.adm.apm.ApmData
-
Get the Euler angles logical block.
- getEulerRotSeq() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemMetadata
-
Get the rotation order of Euler angles.
- getEulerRotSeq() - Method in class org.orekit.files.ccsds.ndm.adm.apm.Euler
-
Get the rotation order of Euler angles.
- getEvaluations() - Method in class org.orekit.propagation.conversion.AbstractPropagatorConverter
-
Get the number of objective function evaluations.
- getEvaluationsCount() - Method in class org.orekit.estimation.leastsquares.AbstractBatchLSModel
-
Get the evaluations count.
- getEvaluationsCount() - Method in class org.orekit.estimation.leastsquares.BatchLSEstimator
-
Get the number of evaluations used for last estimation.
- getEventDate() - Method in class org.orekit.propagation.events.EventState
-
Get the occurrence time of the event triggered in the current
step.
- getEventDate() - Method in class org.orekit.propagation.events.FieldEventState
-
Get the occurrence time of the event triggered in the current
step.
- getEventDetector() - Method in class org.orekit.propagation.events.EventsLogger.LoggedEvent
-
Get the event detector triggered.
- getEventDetector() - Method in class org.orekit.propagation.events.EventState
-
Get the underlying event detector.
- getEventDetector() - Method in class org.orekit.propagation.events.FieldEventsLogger.FieldLoggedEvent
-
Get the event detector triggered.
- getEventDetector() - Method in class org.orekit.propagation.events.FieldEventState
-
Get the underlying event detector.
- getEvents() - Method in class org.orekit.propagation.events.handlers.FieldRecordAndContinue
-
Get the events passed to this handler.
- getEvents() - Method in class org.orekit.propagation.events.handlers.RecordAndContinue
-
Get the events passed to this handler.
- getEventsDetectors() - Method in class org.orekit.forces.drag.DragForce
-
Get the discrete events related to the model.
- getEventsDetectors() - Method in class org.orekit.forces.drag.TimeSpanDragForce
-
Get the discrete events related to the model.
- getEventsDetectors() - Method in class org.orekit.forces.empirical.ParametricAcceleration
-
Get the discrete events related to the model.
- getEventsDetectors() - Method in class org.orekit.forces.empirical.TimeSpanParametricAcceleration
-
Get the discrete events related to the model.
- getEventsDetectors() - Method in interface org.orekit.forces.ForceModel
-
Get the discrete events related to the model.
- getEventsDetectors() - Method in class org.orekit.forces.gravity.DeSitterRelativity
-
Get the discrete events related to the model.
- getEventsDetectors() - Method in class org.orekit.forces.gravity.HolmesFeatherstoneAttractionModel
-
Get the discrete events related to the model.
- getEventsDetectors() - Method in class org.orekit.forces.gravity.LenseThirringRelativity
-
Get the discrete events related to the model.
- getEventsDetectors() - Method in class org.orekit.forces.gravity.NewtonianAttraction
-
Get the discrete events related to the model.
- getEventsDetectors() - Method in class org.orekit.forces.gravity.OceanTides
-
Get the discrete events related to the model.
- getEventsDetectors() - Method in class org.orekit.forces.gravity.Relativity
-
Get the discrete events related to the model.
- getEventsDetectors() - Method in class org.orekit.forces.gravity.SingleBodyAbsoluteAttraction
-
Get the discrete events related to the model.
- getEventsDetectors() - Method in class org.orekit.forces.gravity.SingleBodyRelativeAttraction
-
Get the discrete events related to the model.
- getEventsDetectors() - Method in class org.orekit.forces.gravity.SolidTides
-
Get the discrete events related to the model.
- getEventsDetectors() - Method in class org.orekit.forces.gravity.ThirdBodyAttraction
-
Get the discrete events related to the model.
- getEventsDetectors() - Method in class org.orekit.forces.inertia.InertialForces
-
Get the discrete events related to the model.
- getEventsDetectors() - Method in class org.orekit.forces.maneuvers.Maneuver
-
Get the discrete events related to the model.
- getEventsDetectors() - Method in class org.orekit.forces.maneuvers.trigger.EventBasedManeuverTriggers
-
Get the event detectors associated with the triggers.
- getEventsDetectors() - Method in class org.orekit.forces.maneuvers.trigger.IntervalEventTrigger
-
Get the event detectors associated with the triggers.
- getEventsDetectors() - Method in interface org.orekit.forces.maneuvers.trigger.ManeuverTriggers
-
Get the event detectors associated with the triggers.
- getEventsDetectors() - Method in class org.orekit.forces.maneuvers.trigger.StartStopEventsTrigger
-
Get the event detectors associated with the triggers.
- getEventsDetectors() - Method in class org.orekit.forces.radiation.AbstractRadiationForceModel
-
Get the discrete events related to the model.
- getEventsDetectors() - Method in class org.orekit.forces.radiation.KnockeRediffusedForceModel
-
Get the discrete events related to the model.
- getEventsDetectors() - Method in class org.orekit.propagation.analytical.AbstractAnalyticalPropagator
-
Get all the events detectors that have been added.
- getEventsDetectors() - Method in class org.orekit.propagation.analytical.FieldAbstractAnalyticalPropagator
-
Get all the events detectors that have been added.
- getEventsDetectors() - Method in interface org.orekit.propagation.FieldPropagator
-
Get all the events detectors that have been added.
- getEventsDetectors() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
-
Get all the events detectors that have been added.
- getEventsDetectors() - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator
-
Get all the events detectors that have been added.
- getEventsDetectors() - Method in class org.orekit.propagation.numerical.cr3bp.CR3BPForceModel
-
Get the discrete events related to the model.
- getEventsDetectors() - Method in interface org.orekit.propagation.Propagator
-
Get all the events detectors that have been added.
- getEventsDetectors() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTAtmosphericDrag
-
Get the discrete events related to the model.
- getEventsDetectors() - Method in interface org.orekit.propagation.semianalytical.dsst.forces.DSSTForceModel
-
Get the discrete events related to the model.
- getEventsDetectors() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTNewtonianAttraction
-
Get the discrete events related to the model.
- getEventsDetectors() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTSolarRadiationPressure
-
Get the discrete events related to the model.
- getEventsDetectors() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseral
-
Get the discrete events related to the model.
- getEventsDetectors() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBody
-
Get the discrete events related to the model.
- getEventsDetectors() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonal
-
Get the discrete events related to the model.
- getEvolution(double, RealVector, MeasurementDecorator) - Method in class org.orekit.estimation.sequential.AbstractKalmanModel
- getEvolution(double, RealVector, MeasurementDecorator) - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanModel
- getException() - Method in class org.orekit.gnss.metric.ntrip.StreamMonitor
-
Retrieve exception caught during monitoring.
- getExponent() - Method in class org.orekit.utils.units.PowerTerm
-
Get the fractional exponent.
- getExternalClockReference() - Method in class org.orekit.gnss.clock.RinexClock
-
Getter for the external clock reference.
- getExternalFrame() - Method in class org.orekit.files.ccsds.ndm.adm.AttitudeEndoints
-
Get the external frame.
- getExternalSignalProcessing() - Method in class org.orekit.files.ilrs.CRDConfiguration.DetectorConfiguration
-
Get the external signal processing.
- getExtrapolationThreshold() - Method in class org.orekit.propagation.analytical.Ephemeris
-
Get the maximum timespan outside of the stored ephemeris that is allowed
for extrapolation.
- getF() - Method in class org.orekit.data.DelaunayArguments
-
Get L - Ω where L is the mean longitude of the Moon.
- getF() - Method in class org.orekit.data.FieldDelaunayArguments
-
Get L - Ω where L is the mean longitude of the Moon.
- getF10(AbsoluteDate) - Method in interface org.orekit.models.earth.atmosphere.JB2008InputParameters
-
Get the value of the instantaneous solar flux index
(1e-22*Watt/(m²*Hertz)).
- getF107Adj() - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherDataLoader.LineParameters
-
Gets the 10.7-cm Solar Radio Flux (F10.7) Adjusted to 1 AU.
- getF107Obs() - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherDataLoader.LineParameters
-
Gets the observed (unadjusted) value of F10.7.
- getF10B(AbsoluteDate) - Method in interface org.orekit.models.earth.atmosphere.JB2008InputParameters
-
Get the value of the mean solar flux.
- getFactoryKey() - Method in class org.orekit.frames.FactoryManagedFrame
-
Get the key of the frame within the factory.
- getFallbackHostOrIPAddress() - Method in class org.orekit.gnss.metric.ntrip.CasterRecord
-
Get the fallback host or IP address.
- getFallbackPort() - Method in class org.orekit.gnss.metric.ntrip.CasterRecord
-
Get the fallback port number.
- getFDot() - Method in class org.orekit.data.DelaunayArguments
-
Get L - Ω where L is the mean longitude of the Moon time derivative.
- getFDot() - Method in class org.orekit.data.FieldDelaunayArguments
-
Get L - Ω where L is the mean longitude of the Moon time derivative.
- getField(int) - Method in class org.orekit.gnss.metric.ntrip.Record
-
Get one field from the parsed sourcetable.
- getField(GeoMagneticFieldFactory.FieldModel, double) - Static method in class org.orekit.models.earth.GeoMagneticFieldFactory
-
- getField(GeoMagneticFieldFactory.FieldModel, double) - Method in interface org.orekit.models.earth.GeoMagneticFields
-
- getField(GeoMagneticFieldFactory.FieldModel, double) - Method in class org.orekit.models.earth.LazyLoadedGeoMagneticFields
-
- getField() - Method in class org.orekit.propagation.FieldAbstractPropagator
-
Field getter.
- getField() - Method in class org.orekit.time.FieldAbsoluteDate
-
Get the field.
- getField() - Method in class org.orekit.utils.FieldArrayDictionary
-
Get the field to which elements belong.
- getFieldAuxiliaryElements() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldForceModelContext
-
- getFieldDate() - Method in class org.orekit.frames.FieldTransform
-
Get the date.
- getFieldEventsDetectors(Field<T>) - Method in class org.orekit.forces.drag.DragForce
-
Get the discrete events related to the model.
- getFieldEventsDetectors(Field<T>) - Method in class org.orekit.forces.drag.TimeSpanDragForce
-
Get the discrete events related to the model.
- getFieldEventsDetectors(Field<T>) - Method in class org.orekit.forces.empirical.ParametricAcceleration
-
Get the discrete events related to the model.
- getFieldEventsDetectors(Field<T>) - Method in class org.orekit.forces.empirical.TimeSpanParametricAcceleration
-
Get the discrete events related to the model.
- getFieldEventsDetectors(Field<T>) - Method in interface org.orekit.forces.ForceModel
-
Get the discrete events related to the model.
- getFieldEventsDetectors(Field<T>) - Method in class org.orekit.forces.gravity.DeSitterRelativity
-
Get the discrete events related to the model.
- getFieldEventsDetectors(Field<T>) - Method in class org.orekit.forces.gravity.HolmesFeatherstoneAttractionModel
-
- getFieldEventsDetectors(Field<T>) - Method in class org.orekit.forces.gravity.LenseThirringRelativity
-
Get the discrete events related to the model.
- getFieldEventsDetectors(Field<T>) - Method in class org.orekit.forces.gravity.NewtonianAttraction
-
Get the discrete events related to the model.
- getFieldEventsDetectors(Field<T>) - Method in class org.orekit.forces.gravity.OceanTides
-
Get the discrete events related to the model.
- getFieldEventsDetectors(Field<T>) - Method in class org.orekit.forces.gravity.Relativity
-
Get the discrete events related to the model.
- getFieldEventsDetectors(Field<T>) - Method in class org.orekit.forces.gravity.SingleBodyAbsoluteAttraction
-
- getFieldEventsDetectors(Field<T>) - Method in class org.orekit.forces.gravity.SingleBodyRelativeAttraction
-
- getFieldEventsDetectors(Field<T>) - Method in class org.orekit.forces.gravity.SolidTides
-
Get the discrete events related to the model.
- getFieldEventsDetectors(Field<T>) - Method in class org.orekit.forces.gravity.ThirdBodyAttraction
-
Get the discrete events related to the model.
- getFieldEventsDetectors(Field<T>) - Method in class org.orekit.forces.inertia.InertialForces
-
Get the discrete events related to the model.
- getFieldEventsDetectors(Field<T>) - Method in class org.orekit.forces.maneuvers.Maneuver
-
Get the discrete events related to the model.
- getFieldEventsDetectors(Field<T>) - Method in class org.orekit.forces.maneuvers.trigger.EventBasedManeuverTriggers
-
Get the event detectors associated with the triggers.
- getFieldEventsDetectors(Field<S>) - Method in class org.orekit.forces.maneuvers.trigger.IntervalEventTrigger
-
Get the event detectors associated with the triggers.
- getFieldEventsDetectors(Field<T>) - Method in interface org.orekit.forces.maneuvers.trigger.ManeuverTriggers
-
Get the event detectors associated with the triggers.
- getFieldEventsDetectors(Field<S>) - Method in class org.orekit.forces.maneuvers.trigger.StartStopEventsTrigger
-
Get the event detectors associated with the triggers.
- getFieldEventsDetectors(Field<T>) - Method in class org.orekit.forces.radiation.AbstractRadiationForceModel
-
Get the discrete events related to the model.
- getFieldEventsDetectors(Field<T>) - Method in class org.orekit.forces.radiation.KnockeRediffusedForceModel
-
Get the discrete events related to the model.
- getFieldEventsDetectors(Field<T>) - Method in class org.orekit.propagation.numerical.cr3bp.CR3BPForceModel
-
- getFieldEventsDetectors(Field<T>) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTAtmosphericDrag
-
Get the discrete events related to the model.
- getFieldEventsDetectors(Field<T>) - Method in interface org.orekit.propagation.semianalytical.dsst.forces.DSSTForceModel
-
Get the discrete events related to the model.
- getFieldEventsDetectors(Field<T>) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTNewtonianAttraction
-
Get the discrete events related to the model.
- getFieldEventsDetectors(Field<T>) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTSolarRadiationPressure
-
Get the discrete events related to the model.
- getFieldEventsDetectors(Field<T>) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseral
-
Get the discrete events related to the model.
- getFieldEventsDetectors(Field<T>) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBody
-
Get the discrete events related to the model.
- getFieldEventsDetectors(Field<T>) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonal
-
Get the discrete events related to the model.
- getFieldsNumber() - Method in class org.orekit.gnss.metric.ntrip.Record
-
Get the number of fields.
- getFieldVector() - Method in class org.orekit.models.earth.GeoMagneticElements
-
Returns the magnetic field vector in nTesla.
- getFiftiesEpoch() - Method in class org.orekit.time.AbstractTimeScales
-
- getFiftiesEpoch(Field<T>) - Static method in class org.orekit.time.FieldAbsoluteDate
-
Reference epoch for 1950 dates: 1950-01-01T00:00:00 Terrestrial Time.
- getFiftiesEpoch() - Method in interface org.orekit.time.TimeScales
-
Reference epoch for 1950 dates: 1950-01-01T00:00:00 Terrestrial Time.
- getFileDate(AbsoluteDate) - Method in class org.orekit.models.earth.atmosphere.data.MarshallSolarActivityFutureEstimation
-
Get the date of the file from which data at the specified date comes from.
- getFileFormat() - Method in class org.orekit.files.ccsds.utils.parsing.AbstractMessageParser
-
Get the file format.
- getFileName() - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken
-
Get the name of the file.
- getFileType() - Method in class org.orekit.gnss.navigation.RinexNavigation
-
Get the file type.
- getFilter(int) - Static method in enum org.orekit.utils.AngularDerivativesFilter
-
Get the filter corresponding to a maximum derivation order.
- getFilter(int) - Static method in enum org.orekit.utils.CartesianDerivativesFilter
-
Get the filter corresponding to a maximum derivation order.
- getFiltersManager() - Method in class org.orekit.data.DataProvidersManager
-
Get the manager for filters.
- getFiringIntervalDetector() - Method in class org.orekit.forces.maneuvers.trigger.IntervalEventTrigger
-
Getter for the firing interval detector.
- getFirings() - Method in class org.orekit.forces.maneuvers.trigger.AbstractManeuverTriggers
-
Get the firings detected during last propagation.
- getFirstKnownLeapSecond() - Method in class org.orekit.time.UTCScale
-
Get the date of the first known leap second.
- getFirstSpan() - Method in class org.orekit.forces.drag.TimeSpanDragForce
-
Get the first
time span
of the drag sensitive time span map.
- getFirstSpan() - Method in class org.orekit.forces.empirical.TimeSpanParametricAcceleration
-
Get the first
time span
of the acceleration model time span map.
- getFirstSpan() - Method in class org.orekit.models.earth.troposphere.TimeSpanEstimatedTroposphericModel
-
Get the first
time span
of the tropospheric model time span map.
- getFirstSpan() - Method in class org.orekit.utils.TimeSpanMap
-
Get the first (earliest) span.
- getFirstTransition() - Method in class org.orekit.utils.TimeSpanMap
-
Get the first (earliest) transition.
- getFittedParameters() - Method in class org.orekit.utils.SecularAndHarmonic
-
Get a copy of the last fitted parameters.
- getFixedF10P7() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
-
Get fixed (time invariant) value of the Solar Flux Unit daily proxy F10.7.
- getFixedF10P7Mean() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
-
Get fixed (time invariant) value of the Solar Flux Unit 81-day running center-average proxy F10.7.
- getFixedGeomagneticAp() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
-
Get fixed (time invariant) value of the planetary 3-hour-range geomagnetic index aₚ.
- getFixedGeomagneticDst() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
-
Get fixed (time invariant) value of the planetary 1-hour-range geomagnetic index Dst.
- getFixedGeomagneticKp() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
-
Get fixed (time invariant) value of the planetary 3-hour-range geomagnetic index Kₚ.
- getFixedM10P7() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
-
Get fixed (time invariant) value of the Solar Flux daily proxy M10.7.
- getFixedM10P7Mean() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
-
Get fixed (time invariant) value of the Solar Flux 81-day running center-average proxy M10.7.
- getFixedS10P7() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
-
Get fixed (time invariant) value of the Solar Flux daily proxy S10.7.
- getFixedS10P7Mean() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
-
Get fixed (time invariant) value of the Solar Flux 81-day running center-average proxy S10.7.
- getFixedStepHandler() - Method in class org.orekit.propagation.sampling.FieldOrekitStepNormalizer
-
Get the underlying fixed step handler.
- getFixedStepHandler() - Method in class org.orekit.propagation.sampling.OrekitStepNormalizer
-
Get the underlying fixed step handler.
- getFixedTimeStep() - Method in class org.orekit.propagation.sampling.FieldOrekitStepNormalizer
-
Get the fixed time step.
- getFixedTimeStep() - Method in class org.orekit.propagation.sampling.OrekitStepNormalizer
-
Get the fixed time step.
- getFixedY10P7() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
-
Get fixed (time invariant) value of the Solar Flux daily proxy Y10.7.
- getFixedY10P7Mean() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
-
Get fixed (time invariant) value of the Solar Flux 81-day running center-average proxy Y10.7.
- getFlattening() - Method in class org.orekit.bodies.OneAxisEllipsoid
-
Get the flattening of the body: f = (a-b)/a.
- getFlowRate() - Method in class org.orekit.forces.maneuvers.ConstantThrustManeuver
-
Get the flow rate.
- getFlowRate(SpacecraftState) - Method in class org.orekit.forces.maneuvers.propulsion.AbstractConstantThrustPropulsionModel
-
Get the flow rate (kg/s).
- getFlowRate(SpacecraftState, double[]) - Method in class org.orekit.forces.maneuvers.propulsion.AbstractConstantThrustPropulsionModel
-
Get the flow rate (kg/s).
- getFlowRate(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.maneuvers.propulsion.AbstractConstantThrustPropulsionModel
-
Get the flow rate (kg/s).
- getFlowRate() - Method in class org.orekit.forces.maneuvers.propulsion.AbstractConstantThrustPropulsionModel
-
Get the flow rate (kg/s).
- getFlowRate(double[]) - Method in class org.orekit.forces.maneuvers.propulsion.AbstractConstantThrustPropulsionModel
-
Get the flow rate (kg/s).
- getFlowRate(T[]) - Method in class org.orekit.forces.maneuvers.propulsion.AbstractConstantThrustPropulsionModel
-
Get the flow rate (kg/s).
- getFlowRate() - Method in class org.orekit.forces.maneuvers.propulsion.BasicConstantThrustPropulsionModel
-
Get the flow rate (kg/s).
- getFlowRate(double[]) - Method in class org.orekit.forces.maneuvers.propulsion.BasicConstantThrustPropulsionModel
-
Get the flow rate (kg/s).
- getFlowRate(T[]) - Method in class org.orekit.forces.maneuvers.propulsion.BasicConstantThrustPropulsionModel
-
Get the flow rate (kg/s).
- getFlowRate() - Method in class org.orekit.forces.maneuvers.propulsion.ScaledConstantThrustPropulsionModel
-
Get the flow rate (kg/s).
- getFlowRate(double[]) - Method in class org.orekit.forces.maneuvers.propulsion.ScaledConstantThrustPropulsionModel
-
Get the flow rate (kg/s).
- getFlowRate(T[]) - Method in class org.orekit.forces.maneuvers.propulsion.ScaledConstantThrustPropulsionModel
-
Get the flow rate (kg/s).
- getFlowRate(SpacecraftState) - Method in interface org.orekit.forces.maneuvers.propulsion.ThrustPropulsionModel
-
Get the flow rate (kg/s).
- getFlowRate(SpacecraftState, double[]) - Method in interface org.orekit.forces.maneuvers.propulsion.ThrustPropulsionModel
-
Get the flow rate (kg/s).
- getFlowRate(FieldSpacecraftState<T>, T[]) - Method in interface org.orekit.forces.maneuvers.propulsion.ThrustPropulsionModel
-
Get the flow rate (kg/s).
- getFluxQualifier() - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherDataLoader.LineParameters
-
Gets the Flux Qualifier.
- getFocus1() - Method in class org.orekit.geometry.fov.EllipticalFieldOfView
-
Get first focus in spacecraft frame.
- getFocus2() - Method in class org.orekit.geometry.fov.EllipticalFieldOfView
-
Get second focus in spacecraft frame.
- getFootprint(Transform, OneAxisEllipsoid, double) - Method in interface org.orekit.geometry.fov.FieldOfView
-
Get the footprint of the Field Of View on ground.
- getFootprint(Transform, OneAxisEllipsoid, double) - Method in class org.orekit.geometry.fov.PolygonalFieldOfView
-
Get the footprint of the Field Of View on ground.
- getFootprint(Transform, OneAxisEllipsoid, double) - Method in class org.orekit.geometry.fov.SmoothFieldOfView
-
Get the footprint of the Field Of View on ground.
- getFormat() - Method in interface org.orekit.files.ccsds.utils.generation.Generator
-
Get the generated file format.
- getFormat() - Method in class org.orekit.files.ccsds.utils.generation.KvnGenerator
-
Get the generated file format.
- getFormat() - Method in class org.orekit.files.ccsds.utils.generation.XmlGenerator
-
Get the generated file format.
- getFormat() - Method in class org.orekit.files.ilrs.ILRSHeader
-
Get the file format.
- getFormat() - Method in class org.orekit.gnss.metric.ntrip.DataStreamRecord
-
Get the data format.
- getFormatDetails() - Method in class org.orekit.gnss.metric.ntrip.DataStreamRecord
-
Get the format details.
- getFormatVersion() - Method in class org.orekit.files.ccsds.section.Header
-
Get the CCSDS NDM (ADM, ODM or TDM) format version.
- getFormatVersion() - Method in class org.orekit.gnss.clock.RinexClock
-
Getter for the format version.
- getFormatVersion() - Method in class org.orekit.gnss.navigation.RinexNavigation
-
Getter for the format version.
- getFormatVersionKey() - Method in interface org.orekit.files.ccsds.utils.lexical.MessageParser
-
Get the key for format version.
- getFormatVersionKey() - Method in class org.orekit.files.ccsds.utils.parsing.AbstractMessageParser
-
Get the key for format version.
- getFOV() - Method in class org.orekit.propagation.events.FieldOfViewDetector
-
Get the Field Of View.
- getFOV() - Method in class org.orekit.propagation.events.FootprintOverlapDetector
-
Get the Field Of View.
- getFOV() - Method in class org.orekit.propagation.events.GroundFieldOfViewDetector
-
Get the Field Of View.
- getFrame() - Method in class org.orekit.bodies.Ellipse
-
Get the defining frame.
- getFrame() - Method in class org.orekit.bodies.Ellipsoid
-
Get the ellipsoid central frame.
- getFrame(IERSConventions, boolean, DataContext) - Method in enum org.orekit.files.ccsds.definitions.CelestialBodyFrame
-
Get the frame corresponding to the CCSDS constant.
- getFrame() - Method in class org.orekit.files.ccsds.ndm.odm.CommonMetadata
-
Get the reference frame in which data are given: used for state vector and
Keplerian elements data (and for the covariance reference frame if none is given).
- getFrame() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistory
-
Get the reference frame for this ephemeris segment.
- getFrame() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemSegment
-
Get the reference frame for this ephemeris segment.
- getFrame() - Method in interface org.orekit.files.general.EphemerisFile.EphemerisSegment
-
Get the reference frame for this ephemeris segment.
- getFrame() - Method in class org.orekit.files.general.OrekitEphemerisFile.OrekitEphemerisSegment
-
Get the reference frame for this ephemeris segment.
- getFrame() - Method in class org.orekit.files.ilrs.CPF.CPFEphemeris
-
Get the reference frame for this ephemeris segment.
- getFrame() - Method in class org.orekit.files.sp3.SP3.SP3Ephemeris
-
- getFrame(Predefined) - Method in class org.orekit.frames.AbstractFrames
-
- getFrame(Predefined) - Method in interface org.orekit.frames.Frames
-
Get one of the predefined frames.
- getFrame(Predefined) - Static method in class org.orekit.frames.FramesFactory
-
Get one of the predefined frames.
- getFrame() - Method in class org.orekit.frames.OrphanFrame
-
Get the associated
frame
.
- getFrame() - Method in class org.orekit.gnss.clock.RinexClock
-
Get the reference frame for the station positions.
- getFrame() - Method in interface org.orekit.models.earth.atmosphere.Atmosphere
-
Get the frame of the central body.
- getFrame() - Method in class org.orekit.models.earth.atmosphere.DTM2000
-
Get the frame of the central body.
- getFrame() - Method in class org.orekit.models.earth.atmosphere.HarrisPriester
-
Get the frame of the central body.
- getFrame() - Method in class org.orekit.models.earth.atmosphere.JB2008
-
Get the frame of the central body.
- getFrame() - Method in class org.orekit.models.earth.atmosphere.NRLMSISE00
-
Get the frame of the central body.
- getFrame() - Method in class org.orekit.models.earth.atmosphere.SimpleExponentialAtmosphere
-
Get the frame of the central body.
- getFrame() - Method in class org.orekit.orbits.FieldOrbit
-
Get the frame in which the orbital parameters are defined.
- getFrame() - Method in class org.orekit.orbits.Orbit
-
Get the frame in which the orbital parameters are defined.
- getFrame() - Method in class org.orekit.propagation.AbstractPropagator
-
Get the frame in which the orbit is propagated.
- getFrame() - Method in class org.orekit.propagation.analytical.Ephemeris
-
- getFrame() - Method in class org.orekit.propagation.analytical.gnss.GLONASSAnalyticalPropagator
-
Get the frame in which the orbit is propagated.
- getFrame() - Method in class org.orekit.propagation.analytical.gnss.GNSSPropagator
-
Get the frame in which the orbit is propagated.
- getFrame() - Method in class org.orekit.propagation.analytical.gnss.SBASPropagator
-
Get the frame in which the orbit is propagated.
- getFrame() - Method in class org.orekit.propagation.analytical.tle.FieldTLEPropagator
-
Get the frame in which the orbit is propagated.
- getFrame() - Method in class org.orekit.propagation.analytical.tle.TLEPropagator
-
Get the frame in which the orbit is propagated.
- getFrame() - Method in class org.orekit.propagation.conversion.AbstractPropagatorBuilder
-
Get the frame in which the orbit is propagated.
- getFrame() - Method in class org.orekit.propagation.conversion.AbstractPropagatorConverter
-
Get the frame of the initial state.
- getFrame() - Method in interface org.orekit.propagation.conversion.PropagatorBuilder
-
Get the frame in which the orbit is propagated.
- getFrame() - Method in class org.orekit.propagation.events.FieldNodeDetector
-
Get the frame in which the equator is defined.
- getFrame() - Method in class org.orekit.propagation.events.GroundFieldOfViewDetector
-
Get the sensor reference frame.
- getFrame() - Method in class org.orekit.propagation.events.NodeDetector
-
Get the frame in which the equator is defined.
- getFrame() - Method in class org.orekit.propagation.FieldAbstractPropagator
-
Get the frame in which the orbit is propagated.
- getFrame() - Method in interface org.orekit.propagation.FieldPropagator
-
Get the frame in which the orbit is propagated.
- getFrame() - Method in class org.orekit.propagation.FieldSpacecraftState
-
Get the defining frame.
- getFrame() - Method in class org.orekit.propagation.integration.FieldIntegratedEphemeris
-
- getFrame() - Method in class org.orekit.propagation.integration.FieldStateMapper
-
Get the inertial frame.
- getFrame() - Method in class org.orekit.propagation.integration.IntegratedEphemeris
-
- getFrame() - Method in class org.orekit.propagation.integration.StateMapper
-
Get the inertial frame.
- getFrame() - Method in interface org.orekit.propagation.Propagator
-
Get the frame in which the orbit is propagated.
- getFrame() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
-
Get the definition frame of the orbit.
- getFrame() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldAuxiliaryElements
-
Get the definition frame of the orbit.
- getFrame() - Method in class org.orekit.propagation.SpacecraftState
-
Get the defining frame.
- getFrame() - Method in class org.orekit.utils.AbsolutePVCoordinates
-
Get the frame in which the coordinates are defined.
- getFrame() - Method in class org.orekit.utils.FieldAbsolutePVCoordinates
-
Get the frame in which the coordinates are defined.
- getFrameA() - Method in class org.orekit.files.ccsds.ndm.adm.AttitudeEndoints
-
Get frame A.
- getFrameB() - Method in class org.orekit.files.ccsds.ndm.adm.AttitudeEndoints
-
Get frame B.
- getFrameEpoch() - Method in class org.orekit.files.ccsds.ndm.odm.CommonMetadata
-
Get epoch of reference frame, if not intrinsic to the definition of the
reference frame.
- getFrameName() - Method in class org.orekit.gnss.clock.RinexClock
-
Getter for the frame name.
- getFrames() - Method in class org.orekit.data.CompositeDataContext
-
- getFrames() - Method in interface org.orekit.data.DataContext
-
Get a factory constructing
Frame
s based on the auxiliary data in this
context.
- getFrames() - Method in class org.orekit.data.ExceptionalDataContext
-
- getFrames() - Method in class org.orekit.data.LazyLoadedDataContext
-
- getFrames() - Static method in class org.orekit.frames.FramesFactory
-
Get the instance of
Frames
that is called by the static methods in this
class.
- getFreeAmbiguityDrivers() - Method in class org.orekit.estimation.measurements.gnss.AmbiguitySolver
-
Get the ambiguity parameters drivers that have not been fixed yet.
- getFreeAmbiguityIndirection(int, List<ParameterDriver>) - Method in class org.orekit.estimation.measurements.gnss.AmbiguitySolver
-
Get ambiguity indirection array for ambiguity parameters drivers that have not been fixed yet.
- getFreeEpochMap() - Method in class org.orekit.utils.AbstractMultipleShooting
-
Get the flags representing the free epoch of patch points.
- getFreePatchPointMap() - Method in class org.orekit.utils.AbstractMultipleShooting
-
Get the flags representing the free components of patch points.
- getFreeStateParameters() - Method in class org.orekit.estimation.measurements.modifiers.IonosphericGradientConverter
-
Get the number of free state parameters.
- getFreeStateParameters() - Method in class org.orekit.estimation.measurements.modifiers.TroposphericGradientConverter
-
Get the number of free state parameters.
- getFreeStateParameters() - Method in class org.orekit.propagation.integration.AbstractGradientConverter
-
Get the number of free state parameters.
- getFreqOffset() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
-
Getter for the freqOffset.
- getFrequencies() - Method in class org.orekit.gnss.antenna.Antenna
-
Get supported frequencies.
- getFrequency(SatelliteSystem) - Method in enum org.orekit.gnss.ObservationType
-
Get the frequency for a specified satellite system.
- getFrequencyChannel() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSAlmanac
-
Get the frequency channel.
- getFrequencyNumber() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSNavigationMessage
-
Getter for the frequency number.
- getFrequencySource() - Method in class org.orekit.files.ilrs.CRDConfiguration.TimingSystemConfiguration
-
Get the frequency source.
- getFrom() - Method in class org.orekit.utils.units.UnitsConverter
-
Get the source unit.
- getFrozenFrame(Frame, AbsoluteDate, String) - Method in class org.orekit.frames.Frame
-
Get a new version of the instance, frozen with respect to a reference frame.
- getFT() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data
-
Get the GLONASS FT Word.
- getFunction() - Method in class org.orekit.propagation.events.FieldFunctionalDetector
-
Get the switching function.
- getFunction() - Method in class org.orekit.propagation.events.FunctionalDetector
-
Get the switching function.
- getFutureInfinity() - Method in class org.orekit.time.AbstractTimeScales
-
- getFutureInfinity(Field<T>) - Static method in class org.orekit.time.FieldAbsoluteDate
-
Dummy date at infinity in the future direction.
- getFutureInfinity() - Method in interface org.orekit.time.TimeScales
-
Dummy date at infinity in the future direction.
- getGalileoDataValidityStatus() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1045Data
-
Get the Galileo data validity status.
- getGalileoEpoch() - Method in class org.orekit.time.AbstractTimeScales
-
- getGalileoEpoch(Field<T>) - Static method in class org.orekit.time.FieldAbsoluteDate
-
Reference epoch for Galileo System Time: 1999-08-22T00:00:00 UTC.
- getGalileoEpoch() - Method in interface org.orekit.time.TimeScales
-
Reference epoch for Galileo System Time: 1999-08-22T00:00:00 GST.
- getGalileoNavigationMessage() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1045Data
-
Get the Galileo navigation message corresponding to the current RTCM data.
- getGalileoNavigationMessage(TimeScales) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1045Data
-
Get the Galileo navigation message corresponding to the current RTCM data.
- getGalileoNavigationMessages() - Method in class org.orekit.gnss.navigation.RinexNavigation
-
Get all the Galileo navigation messages contained in the file.
- getGalileoNavigationMessages(String) - Method in class org.orekit.gnss.navigation.RinexNavigation
-
Get the Galileo navigation messages for the given satellite Id.
- getGalileoToc() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1045Data
-
Get the Galileo time of clock.
- getGamma(LagrangianPoints) - Method in class org.orekit.bodies.CR3BPSystem
-
Get the position of the Lagrangian point in the CR3BP Rotating frame.
- getGamma() - Method in class org.orekit.data.DelaunayArguments
-
Get the tide parameter γ = GMST + π.
- getGamma() - Method in class org.orekit.data.FieldDelaunayArguments
-
Get the tide parameter γ = GMST + π.
- getGamma() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBodyContext
-
Get direction cosine γ for central body.
- getGamma() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTThirdBodyContext
-
Get direction cosine γ for central body.
- getGamma() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
-
Get direction cosine γ for central body.
- getGamma() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldAuxiliaryElements
-
Get direction cosine γ for central body.
- getGammaDot() - Method in class org.orekit.data.DelaunayArguments
-
Get the tide parameter γ = GMST + π time derivative.
- getGammaDot() - Method in class org.orekit.data.FieldDelaunayArguments
-
Get the tide parameter γ = GMST + π time derivative.
- getGammaN() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSNavigationMessage
-
Get the relative deviation of predicted satellite carrier frequency from nominal value.
- getGammaN() - Method in interface org.orekit.propagation.analytical.gnss.data.GLONASSOrbitalElements
-
Get the relative deviation of predicted satellite carrier frequency from nominal value.
- getGASTFunction(TimeScale, EOPHistory) - Method in enum org.orekit.utils.IERSConventions
-
Get the function computing Greenwich apparent sidereal time, in radians.
- getGASTFunction(TimeScale, EOPHistory, TimeScales) - Method in enum org.orekit.utils.IERSConventions
-
Get the function computing Greenwich apparent sidereal time, in radians.
- getGCRF() - Method in class org.orekit.frames.AbstractFrames
-
- getGCRF() - Method in interface org.orekit.frames.Frames
-
Get the unique GCRF frame.
- getGCRF() - Static method in class org.orekit.frames.FramesFactory
-
Get the unique GCRF frame.
- getGdop() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
-
Get generalize Dilution Of Precision.
- getGdop() - Method in class org.orekit.gnss.DOP
-
Gets the geometric dilution of precision.
- getGeneralEclipseAngles(Vector3D, Vector3D, double, Vector3D, double) - Method in class org.orekit.forces.radiation.AbstractRadiationForceModel
-
Get the useful angles for eclipse computation.
- getGeneralEclipseAngles(FieldVector3D<T>, FieldVector3D<T>, T, FieldVector3D<T>, T) - Method in class org.orekit.forces.radiation.AbstractRadiationForceModel
-
Get the useful angles for eclipse computation.
- getGeneralEclipseRatio(Vector3D, Vector3D, double, Vector3D, double) - Method in class org.orekit.forces.radiation.SolarRadiationPressure
-
Get eclipse ratio between to bodies seen from a specific object.
- getGeneralEclipseRatio(FieldVector3D<T>, FieldVector3D<T>, T, FieldVector3D<T>, T) - Method in class org.orekit.forces.radiation.SolarRadiationPressure
-
Get eclipse ratio between to bodies seen from a specific object.
- getGenerateCalls() - Method in class org.orekit.utils.GenericTimeStampedCache
-
Get the number of calls to the generate method.
- getGeneratedEphemeris() - Method in interface org.orekit.propagation.EphemerisGenerator
-
Get the ephemeris generated during the propagation.
- getGeneratedEphemeris() - Method in interface org.orekit.propagation.FieldEphemerisGenerator
-
Get the ephemeris generated during the propagation.
- getGenerator() - Method in class org.orekit.gnss.metric.ntrip.DataStreamRecord
-
Get the hardware or software generator.
- getGenerator() - Method in class org.orekit.utils.GenericTimeStampedCache
-
Get the generator.
- getGeoMagneticFields() - Method in class org.orekit.data.CompositeDataContext
-
- getGeoMagneticFields() - Method in interface org.orekit.data.DataContext
-
Get a factory constructing
GeoMagneticField
s based on the auxiliary
data in this context.
- getGeoMagneticFields() - Method in class org.orekit.data.ExceptionalDataContext
-
- getGeoMagneticFields() - Method in class org.orekit.data.LazyLoadedDataContext
-
- getGeoMagneticFields() - Static method in class org.orekit.models.earth.GeoMagneticFieldFactory
-
- getGeometryFreeCombination(SatelliteSystem) - Static method in class org.orekit.estimation.measurements.gnss.MeasurementCombinationFactory
-
Get the Geometry-Free combination of measurements.
- getGetNeighborsCalls() - Method in class org.orekit.utils.GenericTimeStampedCache
-
- getGjs(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHIJjsPolynomials
-
Get the Gjs coefficient.
- getGjs(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
-
Get the Gjs coefficient.
- getGlo2UTC() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSAlmanac
-
Get the correction from GLONASS to UTC.
- getGLONASS() - Method in class org.orekit.time.LazyLoadedTimeScales
-
- getGLONASS() - Method in interface org.orekit.time.TimeScales
-
Get the GLObal NAvigation Satellite System time scale.
- getGLONASS() - Static method in class org.orekit.time.TimeScalesFactory
-
Get the GLObal NAvigation Satellite System time scale.
- getGlonassEpoch() - Method in class org.orekit.time.AbstractTimeScales
-
- getGlonassEpoch() - Method in interface org.orekit.time.TimeScales
-
Reference epoch for GLONASS four-year interval number: 1996-01-01T00:00:00 GLONASS
time.
- getGlonassNavigationMessage() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data
-
Get the Glonass navigation message corresponding to the current RTCM data.
- getGlonassNavigationMessage(TimeScales) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data
-
Get the Glonass navigation message corresponding to the current RTCM data.
- getGlonassNavigationMessages() - Method in class org.orekit.gnss.navigation.RinexNavigation
-
Get all the Glonass navigation messages contained in the file.
- getGlonassNavigationMessages(String) - Method in class org.orekit.gnss.navigation.RinexNavigation
-
Get the Glonass navigation messages for the given satellite Id.
- getGLONASSOrbitalElements() - Method in class org.orekit.propagation.analytical.gnss.GLONASSAnalyticalPropagator
-
Gets the underlying GLONASS orbital elements.
- getGLONASSOrbitalElements() - Method in class org.orekit.propagation.numerical.GLONASSNumericalPropagator
-
Gets the underlying GLONASS orbital elements.
- getGloOffset() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSAlmanac
-
Get the correction of time relative to GLONASS system time.
- getGM() - Method in interface org.orekit.bodies.CelestialBody
-
Get the attraction coefficient of the body.
- getGm() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
-
Get gravitational coefficient of attracting body.
- getGM() - Method in class org.orekit.models.earth.ReferenceEllipsoid
-
Gets the gravitational parameter that is part of the definition of the
reference ellipsoid.
- getGM() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTNewtonianAttractionContext
-
Get standard gravitational parameter μ for the body in m³/s².
- getGM() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTNewtonianAttractionContext
-
Get standard gravitational parameter μ for the body in m³/s².
- getGmsj(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHmsjPolynomials
-
Get the Gmsj coefficient.
- getGmsj(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHmsjPolynomials
-
Get the Gmsj coefficient.
- getGMST(IERSConventions, boolean) - Method in class org.orekit.time.AbstractTimeScales
-
- getGMST() - Method in class org.orekit.time.GLONASSDate
-
Get the Greenwich Mean Sidereal Time.
- getGMST(IERSConventions, boolean) - Method in class org.orekit.time.LazyLoadedTimeScales
-
- getGMST(IERSConventions, boolean) - Method in interface org.orekit.time.TimeScales
-
Get the Greenwich Mean Sidereal Time scale.
- getGMST(IERSConventions, boolean) - Static method in class org.orekit.time.TimeScalesFactory
-
Get the Greenwich Mean Sidereal Time scale.
- getGMSTFunction(TimeScale) - Method in enum org.orekit.utils.IERSConventions
-
Get the function computing Greenwich mean sidereal time, in radians.
- getGMSTFunction(TimeScale, TimeScales) - Method in enum org.orekit.utils.IERSConventions
-
Get the function computing Greenwich mean sidereal time, in radians.
- getGMSTRateFunction(TimeScale) - Method in enum org.orekit.utils.IERSConventions
-
Get the function computing Greenwich mean sidereal time rate, in radians per second.
- getGMSTRateFunction(TimeScale, TimeScales) - Method in enum org.orekit.utils.IERSConventions
-
Get the function computing Greenwich mean sidereal time rate, in radians per
second.
- getGnssIod() - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm01Data
-
Get the GNSS IOD.
- getGnssIod() - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm03Data
-
Get the GNSS IOD.
- getGnssNb() - Method in class org.orekit.gnss.DOP
-
Gets the number of GNSS satellites taken into account for DOP computation.
- getGPS() - Method in class org.orekit.time.LazyLoadedTimeScales
-
- getGPS() - Method in interface org.orekit.time.TimeScales
-
Get the Global Positioning System scale.
- getGPS() - Static method in class org.orekit.time.TimeScalesFactory
-
Get the Global Positioning System scale.
- getGPS2Glo() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSAlmanac
-
Get the correction to GPS time relative GLONASS.
- getGpsCodeOnL2() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1019Data
-
Get the GPS code on L2.
- getGpsEpoch() - Method in class org.orekit.time.AbstractTimeScales
-
- getGPSEpoch(Field<T>) - Static method in class org.orekit.time.FieldAbsoluteDate
-
Reference epoch for GPS weeks: 1980-01-06T00:00:00 GPS time.
- getGpsEpoch() - Method in interface org.orekit.time.TimeScales
-
Reference epoch for GPS weeks: 1980-01-06T00:00:00 GPS time.
- getGpsFitInterval() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1019Data
-
Get the GPS fit interval.
- getGpsL2PDataFlag() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1019Data
-
Get the GPS L2 P-Code data flag.
- getGpsNavigationMessage() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1019Data
-
Get the GPS navigation message corresponding to the current RTCM data.
- getGpsNavigationMessage(TimeScales) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1019Data
-
Get the GPS navigation message corresponding to the current RTCM data.
- getGPSNavigationMessages() - Method in class org.orekit.gnss.navigation.RinexNavigation
-
Get all the GPS navigation messages contained in the file.
- getGPSNavigationMessages(String) - Method in class org.orekit.gnss.navigation.RinexNavigation
-
Get the GPS navigation messages for the given satellite Id.
- getGpsToc() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1019Data
-
Get the GPS time of clock.
- getGpsWeek() - Method in class org.orekit.files.sp3.SP3
-
Returns the GPS week as contained in the SP3 file.
- getGradientConverter() - Method in class org.orekit.propagation.analytical.AbstractAnalyticalMatricesHarvester
-
Get the gradient converter related to the analytical orbit propagator.
- getGradientDensityWrtStateUsingFiniteDifferences(AbsoluteDate, Frame, FieldVector3D<Gradient>) - Method in class org.orekit.forces.drag.AbstractDragForceModel
-
Compute density and its derivatives.
- getGRAPHICCombination(SatelliteSystem) - Static method in class org.orekit.estimation.measurements.gnss.MeasurementCombinationFactory
-
Get the GRAPHIC combination of measurements.
- getGravitationalAssist() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata
-
Get the origin of gravitational assist.
- getGravityDegree() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
-
Get degree of the gravity model.
- getGravityFields() - Method in class org.orekit.data.CompositeDataContext
-
- getGravityFields() - Method in interface org.orekit.data.DataContext
-
Get a factory constructing gravity fields based on the auxiliary data in this
context.
- getGravityFields() - Method in class org.orekit.data.ExceptionalDataContext
-
- getGravityFields() - Method in class org.orekit.data.LazyLoadedDataContext
-
- getGravityFields() - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory
-
Get the instance of
GravityFields
that is called by the static methods of
this class.
- getGravityModel() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
-
Get gravity model name.
- getGravityOrder() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
-
Get order of the gravity model.
- getGridPoints() - Method in class org.orekit.frames.InterpolatingTransformProvider
-
Get the number of interpolation grid points.
- getGridPoints() - Method in class org.orekit.frames.ShiftingTransformProvider
-
Get the number of interpolation grid points.
- getGridPoints(T, T) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldFixedNumberInterpolationGrid
-
Get grid points that are within the current step.
- getGridPoints(T, T) - Method in interface org.orekit.propagation.semianalytical.dsst.utilities.FieldInterpolationGrid
-
Get grid points that are within the current step.
- getGridPoints(T, T) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldMaxGapInterpolationGrid
-
Get grid points that are within the current step.
- getGridPoints(double, double) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FixedNumberInterpolationGrid
-
Get grid points that are within the current step.
- getGridPoints(double, double) - Method in interface org.orekit.propagation.semianalytical.dsst.utilities.InterpolationGrid
-
Get grid points that are within the current step.
- getGridPoints(double, double) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.MaxGapInterpolationGrid
-
Get grid points that are within the current step.
- getGrs80(Frame) - Static method in class org.orekit.models.earth.ReferenceEllipsoid
-
Get the GRS80 ellipsoid, attached to the given body frame.
- getGST() - Method in class org.orekit.time.LazyLoadedTimeScales
-
- getGST() - Method in interface org.orekit.time.TimeScales
-
Get the Galileo System Time scale.
- getGST() - Static method in class org.orekit.time.TimeScalesFactory
-
Get the Galileo System Time scale.
- getGTOD(boolean) - Method in class org.orekit.frames.AbstractFrames
-
- getGTOD(IERSConventions, boolean) - Method in class org.orekit.frames.AbstractFrames
-
- getGTOD(boolean) - Method in interface org.orekit.frames.Frames
-
Get the GTOD reference frame.
- getGTOD(IERSConventions, boolean) - Method in interface org.orekit.frames.Frames
-
Get the GTOD reference frame.
- getGTOD(boolean) - Static method in class org.orekit.frames.FramesFactory
-
Get the GTOD reference frame.
- getGTOD(IERSConventions, boolean) - Static method in class org.orekit.frames.FramesFactory
-
Get the GTOD reference frame.
- getH() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
-
Get the y component of eccentricity vector.
- getH() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldAuxiliaryElements
-
Get the y component of eccentricity vector.
- getHalfAperture() - Method in class org.orekit.geometry.fov.CircularFieldOfView
-
get the FOV half aperture angle.
- getHalfApertureAlongX() - Method in class org.orekit.geometry.fov.EllipticalFieldOfView
-
get the FOV half aperture angle for spreading along Xell (i.e.
- getHalfApertureAlongY() - Method in class org.orekit.geometry.fov.EllipticalFieldOfView
-
get the FOV half aperture angle for spreading along Yell (i.e.
- getHaloOrbitalPeriod(double) - Method in class org.orekit.orbits.RichardsonExpansion
-
Return the orbital period of the Halo Orbit.
- getHandler() - Method in class org.orekit.propagation.events.AbstractDetector
-
Get the handler.
- getHandler() - Method in class org.orekit.propagation.events.FieldAbstractDetector
-
Get the handler.
- getHandlers() - Method in class org.orekit.propagation.events.handlers.EventMultipleHandler
-
Retrieve managed handlers list.
- getHandlers() - Method in class org.orekit.propagation.sampling.FieldStepHandlerMultiplexer
-
Get an unmodifiable view of all handlers.
- getHandlers() - Method in class org.orekit.propagation.sampling.StepHandlerMultiplexer
-
Get an unmodifiable view of all handlers.
- getHarmonicAmplitude() - Method in class org.orekit.utils.SecularAndHarmonic
-
Get an upper bound of the fitted harmonic amplitude.
- getHarvester() - Method in class org.orekit.propagation.AbstractPropagator
-
Get the harvester.
- getHasCreatableBody() - Method in class org.orekit.files.ccsds.ndm.adm.AdmMetadata
-
Get boolean testing whether the body corresponding to the centerName
attribute can be created through the
CelestialBodies
.
- getHdop() - Method in class org.orekit.gnss.DOP
-
Gets the horizontal dilution of precision.
- getHeader() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemParser
-
Get file header to fill.
- getHeader() - Method in class org.orekit.files.ccsds.ndm.adm.apm.ApmParser
-
Get file header to fill.
- getHeader() - Method in class org.orekit.files.ccsds.ndm.NdmConstituent
-
Get the header.
- getHeader() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmParser
-
Get file header to fill.
- getHeader() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemParser
-
Get file header to fill.
- getHeader() - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmParser
-
Get file header to fill.
- getHeader() - Method in class org.orekit.files.ccsds.ndm.odm.opm.OpmParser
-
Get file header to fill.
- getHeader() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmParser
-
Get file header to fill.
- getHeader() - Method in class org.orekit.files.ccsds.utils.parsing.AbstractConstituentParser
-
Get file header to fill.
- getHeader() - Method in class org.orekit.files.ilrs.CPF
-
Get the CPF file header.
- getHeader() - Method in class org.orekit.files.ilrs.CRD.CRDDataBlock
-
Get the header of the current data block.
- getHeader() - Method in class org.orekit.gnss.CombinedObservationDataSet
-
Get the Rinex header associated with this data set.
- getHeader() - Method in class org.orekit.gnss.metric.messages.ssr.SsrMessage
-
Get the header.
- getHeader() - Method in class org.orekit.gnss.ObservationDataSet
-
Get the Rinex header associated with this data set.
- getHealth() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractEphemerisMessage
-
Getter for the health status.
- getHealth() - Method in class org.orekit.propagation.analytical.gnss.data.BeidouAlmanac
-
Gets the Health status.
- getHealth() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSAlmanac
-
Get the Health status.
- getHealth() - Method in class org.orekit.propagation.analytical.gnss.data.GPSAlmanac
-
Gets the Health status.
- getHealth() - Method in class org.orekit.propagation.analytical.gnss.data.QZSSAlmanac
-
Gets the Health status.
- getHealthE1() - Method in class org.orekit.propagation.analytical.gnss.data.GalileoAlmanac
-
Gets the E1-B/C signal health status.
- getHealthE5a() - Method in class org.orekit.propagation.analytical.gnss.data.GalileoAlmanac
-
Gets the E5a signal health status.
- getHealthE5b() - Method in class org.orekit.propagation.analytical.gnss.data.GalileoAlmanac
-
Gets the E5b signal health status.
- getHeightIonosphericLayer() - Method in class org.orekit.gnss.metric.messages.ssr.subtype.SsrIm201Data
-
Get the height of the ionospheric layer.
- getHighRateClockCorrection() - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm04Data
-
Get the high rate clock correction to be added to the polynomial clock correction.
- getHjs(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHIJjsPolynomials
-
Get the Hjs coefficient.
- getHjs(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
-
Get the Hjs coefficient.
- getHK() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonalContext
-
Get h * k.
- getHK() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTZonalContext
-
Get h * k.
- getHmsj(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHmsjPolynomials
-
Get the Hmsj coefficient.
- getHmsj(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHmsjPolynomials
-
Get the Hmsj coefficient.
- getHorizontalIntensity() - Method in class org.orekit.models.earth.GeoMagneticElements
-
Returns the horizontal intensity of the magnetic field (= norm of the
vector in the plane spanned by the x/y components of the field vector).
- getHost() - Method in class org.orekit.gnss.metric.ntrip.NtripClient
-
Get the caster host.
- getHostOrIPAddress() - Method in class org.orekit.gnss.metric.ntrip.CasterRecord
-
Get the host or IP address.
- getHour() - Method in class org.orekit.time.TimeComponents
-
Get the hour number.
- getHumidity() - Method in class org.orekit.files.ilrs.CRD.MeteorologicalMeasurement
-
Get the relative humidity at the surface.
- getHumiSensorManufacturer() - Method in class org.orekit.files.ilrs.CRDConfiguration.MeteorologicalConfiguration
-
Get the humidity sensor manufacturer.
- getHumiSensorModel() - Method in class org.orekit.files.ilrs.CRDConfiguration.MeteorologicalConfiguration
-
Get the humidity sensor model.
- getHumiSensorSerialNumber() - Method in class org.orekit.files.ilrs.CRDConfiguration.MeteorologicalConfiguration
-
Get the humidity sensor serial number.
- getHx() - Method in class org.orekit.orbits.CartesianOrbit
-
Get the first component of the inclination vector.
- getHx() - Method in class org.orekit.orbits.CircularOrbit
-
Get the first component of the inclination vector.
- getHx() - Method in class org.orekit.orbits.EquinoctialOrbit
-
Get the first component of the inclination vector.
- getHx() - Method in class org.orekit.orbits.FieldCartesianOrbit
-
Get the first component of the inclination vector.
- getHx() - Method in class org.orekit.orbits.FieldCircularOrbit
-
Get the first component of the inclination vector.
- getHx() - Method in class org.orekit.orbits.FieldEquinoctialOrbit
-
Get the first component of the inclination vector.
- getHx() - Method in class org.orekit.orbits.FieldKeplerianOrbit
-
Get the first component of the inclination vector.
- getHx() - Method in class org.orekit.orbits.FieldOrbit
-
Get the first component of the inclination vector.
- getHx() - Method in class org.orekit.orbits.KeplerianOrbit
-
Get the first component of the inclination vector.
- getHx() - Method in class org.orekit.orbits.Orbit
-
Get the first component of the inclination vector.
- getHx() - Method in class org.orekit.propagation.FieldSpacecraftState
-
Get the first component of the inclination vector (as per equinoctial parameters).
- getHx() - Method in class org.orekit.propagation.SpacecraftState
-
Get the first component of the inclination vector (as per equinoctial parameters).
- getHxDot() - Method in class org.orekit.orbits.CartesianOrbit
-
Get the first component of the inclination vector derivative.
- getHxDot() - Method in class org.orekit.orbits.CircularOrbit
-
Get the first component of the inclination vector derivative.
- getHxDot() - Method in class org.orekit.orbits.EquinoctialOrbit
-
Get the first component of the inclination vector derivative.
- getHxDot() - Method in class org.orekit.orbits.FieldCartesianOrbit
-
Get the first component of the inclination vector derivative.
- getHxDot() - Method in class org.orekit.orbits.FieldCircularOrbit
-
Get the first component of the inclination vector derivative.
- getHxDot() - Method in class org.orekit.orbits.FieldEquinoctialOrbit
-
Get the first component of the inclination vector derivative.
- getHxDot() - Method in class org.orekit.orbits.FieldKeplerianOrbit
-
Get the first component of the inclination vector derivative.
- getHxDot() - Method in class org.orekit.orbits.FieldOrbit
-
Get the first component of the inclination vector derivative.
- getHxDot() - Method in class org.orekit.orbits.KeplerianOrbit
-
Get the first component of the inclination vector derivative.
- getHxDot() - Method in class org.orekit.orbits.Orbit
-
Get the first component of the inclination vector derivative.
- getHXXX() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBodyContext
-
Get hXXX = h * Χ³.
- getHXXX() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTThirdBodyContext
-
Get hXXX = h * Χ³.
- getHy() - Method in class org.orekit.orbits.CartesianOrbit
-
Get the second component of the inclination vector.
- getHy() - Method in class org.orekit.orbits.CircularOrbit
-
Get the second component of the inclination vector.
- getHy() - Method in class org.orekit.orbits.EquinoctialOrbit
-
Get the second component of the inclination vector.
- getHy() - Method in class org.orekit.orbits.FieldCartesianOrbit
-
Get the second component of the inclination vector.
- getHy() - Method in class org.orekit.orbits.FieldCircularOrbit
-
Get the second component of the inclination vector.
- getHy() - Method in class org.orekit.orbits.FieldEquinoctialOrbit
-
Get the second component of the inclination vector.
- getHy() - Method in class org.orekit.orbits.FieldKeplerianOrbit
-
Get the second component of the inclination vector.
- getHy() - Method in class org.orekit.orbits.FieldOrbit
-
Get the second component of the inclination vector.
- getHy() - Method in class org.orekit.orbits.KeplerianOrbit
-
Get the second component of the inclination vector.
- getHy() - Method in class org.orekit.orbits.Orbit
-
Get the second component of the inclination vector.
- getHy() - Method in class org.orekit.propagation.FieldSpacecraftState
-
Get the second component of the inclination vector (as per equinoctial parameters).
- getHy() - Method in class org.orekit.propagation.SpacecraftState
-
Get the second component of the inclination vector (as per equinoctial parameters).
- getHyDot() - Method in class org.orekit.orbits.CartesianOrbit
-
Get the second component of the inclination vector derivative.
- getHyDot() - Method in class org.orekit.orbits.CircularOrbit
-
Get the second component of the inclination vector derivative.
- getHyDot() - Method in class org.orekit.orbits.EquinoctialOrbit
-
Get the second component of the inclination vector derivative.
- getHyDot() - Method in class org.orekit.orbits.FieldCartesianOrbit
-
Get the second component of the inclination vector derivative.
- getHyDot() - Method in class org.orekit.orbits.FieldCircularOrbit
-
Get the second component of the inclination vector derivative.
- getHyDot() - Method in class org.orekit.orbits.FieldEquinoctialOrbit
-
Get the second component of the inclination vector derivative.
- getHyDot() - Method in class org.orekit.orbits.FieldKeplerianOrbit
-
Get the second component of the inclination vector derivative.
- getHyDot() - Method in class org.orekit.orbits.FieldOrbit
-
Get the second component of the inclination vector derivative.
- getHyDot() - Method in class org.orekit.orbits.KeplerianOrbit
-
Get the second component of the inclination vector derivative.
- getHyDot() - Method in class org.orekit.orbits.Orbit
-
Get the second component of the inclination vector derivative.
- getI() - Method in class org.orekit.files.ccsds.ndm.odm.KeplerianElements
-
Get the orbit inclination.
- getI() - Method in class org.orekit.orbits.CartesianOrbit
-
Get the inclination.
- getI() - Method in class org.orekit.orbits.CircularOrbit
-
Get the inclination.
- getI() - Method in class org.orekit.orbits.EquinoctialOrbit
-
Get the inclination.
- getI() - Method in class org.orekit.orbits.FieldCartesianOrbit
-
Get the inclination.
- getI() - Method in class org.orekit.orbits.FieldCircularOrbit
-
Get the inclination.
- getI() - Method in class org.orekit.orbits.FieldEquinoctialOrbit
-
Get the inclination.
- getI() - Method in class org.orekit.orbits.FieldKeplerianOrbit
-
Get the inclination.
- getI() - Method in class org.orekit.orbits.FieldOrbit
-
Get the inclination.
- getI() - Method in class org.orekit.orbits.KeplerianOrbit
-
Get the inclination.
- getI() - Method in class org.orekit.orbits.Orbit
-
Get the inclination.
- getI() - Method in class org.orekit.propagation.analytical.tle.FieldTLE
-
Get the inclination.
- getI() - Method in class org.orekit.propagation.analytical.tle.TLE
-
Get the inclination.
- getI() - Method in class org.orekit.propagation.FieldSpacecraftState
-
Get the inclination.
- getI() - Method in class org.orekit.propagation.SpacecraftState
-
Get the inclination.
- getI0() - Method in class org.orekit.propagation.analytical.gnss.data.CommonGnssData
-
Getter for the inclination angle at reference time.
- getI0() - Method in interface org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElements
-
Gets the Inclination Angle at Reference Time.
- getI11() - Method in class org.orekit.files.ccsds.ndm.adm.apm.SpacecraftParameters
-
Get the moment of Inertia about the 1-axis (N.m²).
- getI12() - Method in class org.orekit.files.ccsds.ndm.adm.apm.SpacecraftParameters
-
Get the moment of Inertia about the 1 and 2 axes (N.m²).
- getI13() - Method in class org.orekit.files.ccsds.ndm.adm.apm.SpacecraftParameters
-
Get the moment of Inertia about the 1 and 3 axes (N.m²).
- getI22() - Method in class org.orekit.files.ccsds.ndm.adm.apm.SpacecraftParameters
-
Get the moment of Inertia about the 2-axis (N.m²).
- getI23() - Method in class org.orekit.files.ccsds.ndm.adm.apm.SpacecraftParameters
-
Get the moment of Inertia about the 2 and 3 axes (N.m²).
- getI33() - Method in class org.orekit.files.ccsds.ndm.adm.apm.SpacecraftParameters
-
Get the moment of Inertia about the 3-axis (N.m²).
- getICRF() - Method in class org.orekit.frames.AbstractFrames
-
- getICRF() - Method in interface org.orekit.frames.Frames
-
Get the unique ICRF frame.
- getICRF() - Static method in class org.orekit.frames.FramesFactory
-
Get the unique ICRF frame.
- getId() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemSatelliteEphemeris
-
Get the satellite ID.
- getId() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmSatelliteEphemeris
-
Get the satellite ID.
- getId() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
-
Get identification number.
- getId() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemSatelliteEphemeris
-
Get the satellite ID.
- getId() - Method in interface org.orekit.files.general.AttitudeEphemerisFile.SatelliteAttitudeEphemeris
-
Get the satellite ID.
- getId() - Method in interface org.orekit.files.general.EphemerisFile.SatelliteEphemeris
-
Get the satellite ID.
- getId() - Method in class org.orekit.files.general.OrekitAttitudeEphemerisFile.OrekitSatelliteAttitudeEphemeris
-
Get the satellite ID.
- getId() - Method in class org.orekit.files.general.OrekitEphemerisFile.OrekitSatelliteEphemeris
-
Get the satellite ID.
- getId() - Method in class org.orekit.files.ilrs.CPF.CPFEphemeris
-
Get the satellite ID.
- getId() - Method in class org.orekit.files.sp3.SP3.SP3Ephemeris
-
- getId() - Method in class org.orekit.gnss.metric.ntrip.StreamedMessage
-
Get message id.
- getIdentifier() - Method in enum org.orekit.files.ilrs.StreamingCpfWriter.HeaderLineWriter
-
Get the regular expression for identifying line.
- getIdentity(Field<T>) - Static method in class org.orekit.frames.FieldTransform
-
Get the identity transform.
- getIdentity(Field<T>) - Static method in class org.orekit.utils.FieldAngularCoordinates
-
Fixed orientation parallel with reference frame
(identity rotation, zero rotation rate and acceleration).
- getIDot() - Method in class org.orekit.orbits.CartesianOrbit
-
Get the inclination derivative.
- getIDot() - Method in class org.orekit.orbits.CircularOrbit
-
Get the inclination derivative.
- getIDot() - Method in class org.orekit.orbits.EquinoctialOrbit
-
Get the inclination derivative.
- getIDot() - Method in class org.orekit.orbits.FieldCartesianOrbit
-
Get the inclination derivative.
- getIDot() - Method in class org.orekit.orbits.FieldCircularOrbit
-
Get the inclination derivative.
- getIDot() - Method in class org.orekit.orbits.FieldEquinoctialOrbit
-
Get the inclination derivative.
- getIDot() - Method in class org.orekit.orbits.FieldKeplerianOrbit
-
Get the inclination derivative.
- getIDot() - Method in class org.orekit.orbits.FieldOrbit
-
Get the inclination derivative.
- getIDot() - Method in class org.orekit.orbits.KeplerianOrbit
-
Get the inclination derivative.
- getIDot() - Method in class org.orekit.orbits.Orbit
-
Get the inclination derivative.
- getIDot() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractAlmanac
-
Getter for the rate of inclination angle.
- getIDot() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractNavigationMessage
-
Getter for the rate of inclination angle.
- getIDot() - Method in interface org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElements
-
Gets the Rate of Inclination Angle.
- getIers2003(Frame) - Static method in class org.orekit.models.earth.ReferenceEllipsoid
-
Get the IERS2003 ellipsoid, attached to the given body frame.
- getIers2010(Frame) - Static method in class org.orekit.models.earth.ReferenceEllipsoid
-
Get the IERS2010 ellipsoid, attached to the given body frame.
- getIers96(Frame) - Static method in class org.orekit.models.earth.ReferenceEllipsoid
-
Get the IERS96 ellipsoid, attached to the given body frame.
- getIGRF(double) - Static method in class org.orekit.models.earth.GeoMagneticFieldFactory
-
Get the IGRF model for the given year.
- getIGRF(double) - Method in interface org.orekit.models.earth.GeoMagneticFields
-
Get the IGRF model for the given year.
- getIGRF(double) - Method in class org.orekit.models.earth.LazyLoadedGeoMagneticFields
-
- getIjs(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHIJjsPolynomials
-
Get the Ijs coefficient.
- getIjs(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
-
Get the Ijs coefficient.
- getIlrsSatelliteId() - Method in class org.orekit.files.ilrs.ILRSHeader
-
Get the IRLS satellite ID (based on COSPAR ID).
- getImaginary(int, int) - Method in class org.orekit.utils.LoveNumbers
-
Get the imaginary part of a nominal Love numbers.
- getInclination() - Method in class org.orekit.models.earth.GeoMagneticElements
-
Returns the inclination of the magnetic field in radians.
- getIncreasingTimeShift() - Method in class org.orekit.propagation.events.EventShifter
-
Get the increasing events time shift.
- getIndicator() - Method in enum org.orekit.files.ilrs.CRDHeader.RangeType
-
Get the range type indicator.
- getInertialDV() - Method in class org.orekit.forces.maneuvers.SmallManeuverAnalyticalModel
-
Get the inertial velocity increment of the maneuver.
- getInertialFrame() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemSegment
-
Get the inertial reference frame for this ephemeris segment.
- getInertialFrame() - Method in interface org.orekit.files.general.EphemerisFile.EphemerisSegment
-
Get the inertial reference frame for this ephemeris segment.
- getInertialFrame() - Method in class org.orekit.files.general.OrekitEphemerisFile.OrekitEphemerisSegment
-
Get the inertial reference frame for this ephemeris segment.
- getInertialFrame() - Method in class org.orekit.forces.maneuvers.SmallManeuverAnalyticalModel
-
Get the inertial frame in which the velocity increment is defined.
- getInertiallyOrientedFrame() - Method in interface org.orekit.bodies.CelestialBody
-
Get an inertially oriented, body centered frame.
- getInertiaMatrix() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
-
Get the inertia matrix.
- getInertiaReferenceFrame() - Method in class org.orekit.files.ccsds.ndm.adm.apm.SpacecraftParameters
-
Get the coordinate system for the inertia tensor.
- getInitialCovarianceMatrix(SpacecraftState) - Method in class org.orekit.estimation.sequential.AbstractCovarianceMatrixProvider
-
Get the initial covariance matrix.
- getInitialCovarianceMatrix(SpacecraftState) - Method in interface org.orekit.estimation.sequential.CovarianceMatrixProvider
-
Get the initial covariance matrix.
- getInitialFlowrate() - Method in class org.orekit.forces.maneuvers.propulsion.AbstractConstantThrustPropulsionModel
-
- getInitialIntegrationState() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
-
Get the initial state for integration.
- getInitialIntegrationState() - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator
-
Get the initial state for integration.
- getInitialIntegrationState() - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator
-
Get the initial state for integration.
- getInitialIntegrationState() - Method in class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator
-
Get the initial state for integration.
- getInitialJacobianColumn(String) - Method in class org.orekit.propagation.AbstractMatricesHarvester
-
Get the initial column of Jacobian matrix with respect to named parameter.
- getInitialOrbitDate() - Method in class org.orekit.propagation.conversion.AbstractPropagatorBuilder
-
Get the date of the initial orbit.
- getInitialOrbitDate() - Method in interface org.orekit.propagation.conversion.PropagatorBuilder
-
Get the date of the initial orbit.
- getInitialPV() - Method in class org.orekit.orbits.LibrationOrbit
-
Return the initialPV on the libration orbit.
- getInitialState() - Method in class org.orekit.propagation.AbstractPropagator
-
Get the propagator initial state.
- getInitialState() - Method in class org.orekit.propagation.analytical.AdapterPropagator
-
Get the propagator initial state.
- getInitialState() - Method in class org.orekit.propagation.analytical.AggregateBoundedPropagator
-
- getInitialState() - Method in class org.orekit.propagation.analytical.Ephemeris
-
Get the propagator initial state.
- getInitialState() - Method in class org.orekit.propagation.FieldAbstractPropagator
-
Get the propagator initial state.
- getInitialState() - Method in interface org.orekit.propagation.FieldPropagator
-
Get the propagator initial state.
- getInitialState() - Method in class org.orekit.propagation.integration.FieldIntegratedEphemeris
-
Get the propagator initial state.
- getInitialState() - Method in class org.orekit.propagation.integration.IntegratedEphemeris
-
Get the propagator initial state.
- getInitialState() - Method in interface org.orekit.propagation.Propagator
-
Get the propagator initial state.
- getInitialStateTransitionMatrix() - Method in class org.orekit.propagation.AbstractMatricesHarvester
-
Get the initial State Transition Matrix.
- getInitialThrustVector() - Method in class org.orekit.forces.maneuvers.propulsion.AbstractConstantThrustPropulsionModel
-
- getInitialWetMass() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
-
Get the total mass at beginning of life.
- getInnovation(MeasurementDecorator, NonLinearEvolution, RealMatrix) - Method in class org.orekit.estimation.sequential.AbstractKalmanModel
- getInnovation(MeasurementDecorator, NonLinearEvolution, RealMatrix) - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanModel
- getInputs() - Method in class org.orekit.data.AbstractListCrawler
-
Get the list of inputs supported by the instance.
- getInstantFlux(AbsoluteDate) - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherData
-
Get the value of the instantaneous solar flux.
- getInstantFlux(AbsoluteDate) - Method in class org.orekit.models.earth.atmosphere.data.MarshallSolarActivityFutureEstimation
-
Get the value of the instantaneous solar flux.
- getInstantFlux(AbsoluteDate) - Method in interface org.orekit.models.earth.atmosphere.DTM2000InputParameters
-
Get the value of the instantaneous solar flux.
- getIntegrationInterval() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
-
Getter for the integrationInterval.
- getIntegrationRef() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
-
Getter for the integrationRef.
- getIntegrator() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
-
Get the integrator used by the propagator.
- getIntegrator() - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator
-
Get the integrator used by the propagator.
- getIntegratorBuilder() - Method in class org.orekit.propagation.conversion.DSSTPropagatorBuilder
-
Get the integrator builder.
- getIntegratorBuilder() - Method in class org.orekit.propagation.conversion.NumericalPropagatorBuilder
-
Get the integrator builder.
- getInternationalDesignator() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
-
Get the international designator for the object.
- getInterpMethodEOP() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
-
Get the interpolation method for Earth Orientation Parameters.
- getInterpMethodSW() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
-
Get the interpolation method for Space Weather data.
- getInterpolatedPoint(double, double) - Method in class org.orekit.models.earth.tessellation.Tile
-
Get an interpolated point inside the tile.
- getInterpolatedState(FieldAbsoluteDate<T>) - Method in interface org.orekit.propagation.sampling.FieldOrekitStepInterpolator
-
Get the state at interpolated date.
- getInterpolatedState(AbsoluteDate) - Method in interface org.orekit.propagation.sampling.OrekitStepInterpolator
-
Get the state at interpolated date.
- getInterpolationDegree() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemMetadata
-
Get the interpolation degree.
- getInterpolationDegree() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata
-
Get the interpolation degree.
- getInterpolationDegree() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemMetadata
-
Get the interpolation degree.
- getInterpolationDegree() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
-
Get the interpolation degree.
- getInterpolationMethod() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemMetadata
-
Get the interpolation method to be used.
- getInterpolationMethod() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemSegment
-
Get the interpolation method to be used.
- getInterpolationMethod() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata
-
Get the interpolation method to be used.
- getInterpolationMethod() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemMetadata
-
Get the interpolation method to be used.
- getInterpolationMethod() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
-
Get the interpolation method to be used.
- getInterpolationMethod() - Method in interface org.orekit.files.general.AttitudeEphemerisFile.AttitudeEphemerisSegment
-
Get the interpolation method to be used.
- getInterpolationMethod() - Method in class org.orekit.files.general.OrekitAttitudeEphemerisFile.OrekitAttitudeEphemerisSegment
-
Get the interpolation method to be used.
- getInterpolationSamples() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemMetadata
-
Get the number of samples to use in interpolation.
- getInterpolationSamples() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemSegment
-
Get the number of samples to use in interpolation.
- getInterpolationSamples() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistory
-
Get the number of samples to use in interpolation.
- getInterpolationSamples() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemSegment
-
Get the number of samples to use in interpolation.
- getInterpolationSamples() - Method in interface org.orekit.files.general.AttitudeEphemerisFile.AttitudeEphemerisSegment
-
Get the number of samples to use in interpolation.
- getInterpolationSamples() - Method in interface org.orekit.files.general.EphemerisFile.EphemerisSegment
-
Get the number of samples to use in interpolation.
- getInterpolationSamples() - Method in class org.orekit.files.general.OrekitAttitudeEphemerisFile.OrekitAttitudeEphemerisSegment
-
Get the number of samples to use in interpolation.
- getInterpolationSamples() - Method in class org.orekit.files.general.OrekitEphemerisFile.OrekitEphemerisSegment
-
Get the number of samples to use in interpolation.
- getInterpolationSamples() - Method in class org.orekit.files.ilrs.CPF.CPFEphemeris
-
Get the number of samples to use in interpolation.
- getInterpolationSamples() - Method in class org.orekit.files.sp3.SP3.SP3Ephemeris
-
- getIntersectionPoint(Line, Vector3D, Frame, AbsoluteDate) - Method in interface org.orekit.bodies.BodyShape
-
Get the intersection point of a line with the surface of the body.
- getIntersectionPoint(FieldLine<T>, FieldVector3D<T>, Frame, FieldAbsoluteDate<T>) - Method in interface org.orekit.bodies.BodyShape
-
Get the intersection point of a line with the surface of the body.
- getIntersectionPoint(Line, Vector3D, Frame, AbsoluteDate) - Method in class org.orekit.bodies.OneAxisEllipsoid
-
Get the intersection point of a line with the surface of the body.
- getIntersectionPoint(FieldLine<T>, FieldVector3D<T>, Frame, FieldAbsoluteDate<T>) - Method in class org.orekit.bodies.OneAxisEllipsoid
-
Get the intersection point of a line with the surface of the body.
- getIntersectionPoint(Line, Vector3D, Frame, AbsoluteDate) - Method in class org.orekit.models.earth.Geoid
-
Get the intersection point of a line with the surface of the body.
- getIntersectionPoint(FieldLine<T>, FieldVector3D<T>, Frame, FieldAbsoluteDate<T>) - Method in class org.orekit.models.earth.Geoid
-
Get the intersection point of a line with the surface of the body.
- getInterval() - Method in class org.orekit.gnss.RinexObservationHeader
-
Get the observation interval in seconds.
- getIntervalNumber() - Method in class org.orekit.time.GLONASSDate
-
Get the number of the current four year interval.
- getInverse() - Method in class org.orekit.frames.FieldTransform
-
Get the inverse transform of the instance.
- getInverse() - Method in class org.orekit.frames.Transform
-
Get the inverse transform of the instance.
- getIOD() - Method in class org.orekit.propagation.analytical.gnss.data.GalileoAlmanac
-
Gets the Issue of Data (IOD).
- getIOD() - Method in interface org.orekit.propagation.analytical.gnss.data.GLONASSOrbitalElements
-
Gets the GLONASS Issue Of Data (IOD).
- getIODC() - Method in class org.orekit.propagation.analytical.gnss.data.GPSNavigationMessage
-
Getter for the Issue Of Data Clock (IODC).
- getIODC() - Method in class org.orekit.propagation.analytical.gnss.data.QZSSNavigationMessage
-
Getter for the Issue Of Data Clock (IODC).
- getIODE() - Method in class org.orekit.propagation.analytical.gnss.data.GPSNavigationMessage
-
Getter for the Issue Of Data Ephemeris (IODE).
- getIODE() - Method in class org.orekit.propagation.analytical.gnss.data.QZSSNavigationMessage
-
Getter for the Issue Of Data Ephemeris (IODE).
- getIODEC() - Method in class org.orekit.propagation.analytical.gnss.data.IRNSSNavigationMessage
-
Getter for the Issue Of Data Ephemeris and Clock (IODEC).
- getIODN() - Method in class org.orekit.propagation.analytical.gnss.data.SBASNavigationMessage
-
Gets the Issue Of Data Navigation (IODN).
- getIODN() - Method in interface org.orekit.propagation.analytical.gnss.data.SBASOrbitalElements
-
Gets the Issue Of Data Navigation (IODN).
- getIODNav() - Method in class org.orekit.propagation.analytical.gnss.data.GalileoNavigationMessage
-
Getter for the the Issue Of Data (IOD).
- getIodSsr() - Method in class org.orekit.gnss.metric.messages.ssr.SsrHeader
-
Get the IOD SSR.
- getIonosphereFreeCombination(SatelliteSystem) - Static method in class org.orekit.estimation.measurements.gnss.MeasurementCombinationFactory
-
Get the Ionosphere-Free combination of measurements.
- getIonosphericCorrectionType() - Method in class org.orekit.gnss.navigation.RinexNavigation
-
Getter for the ionospheric correction type.
- getIonosphericModel() - Method in class org.orekit.gnss.metric.messages.ssr.subtype.SsrIm201
-
Get the ionospheric model adapted to the current IM201 message.
- getIRNSS() - Method in class org.orekit.time.LazyLoadedTimeScales
-
- getIRNSS() - Method in interface org.orekit.time.TimeScales
-
Get the Indian Regional Navigation Satellite System time scale.
- getIRNSS() - Static method in class org.orekit.time.TimeScalesFactory
-
Get the Indian Regional Navigation Satellite System time scale.
- getIrnssEpoch() - Method in class org.orekit.time.AbstractTimeScales
-
- getIrnssEpoch() - Method in interface org.orekit.time.TimeScales
-
Reference epoch for IRNSS weeks: 1999-08-22T00:00:00 IRNSS time.
- getIRNSSNavigationMessages() - Method in class org.orekit.gnss.navigation.RinexNavigation
-
Get all the IRNSS navigation messages contained in the file.
- getIRNSSNavigationMessages(String) - Method in class org.orekit.gnss.navigation.RinexNavigation
-
Get the IRNSS navigation messages for the given satellite Id.
- getISP() - Method in class org.orekit.forces.maneuvers.ConfigurableLowThrustManeuver
-
Get the specific impulse.
- getISP() - Method in class org.orekit.forces.maneuvers.ConstantThrustManeuver
-
Get the specific impulse.
- getIsp() - Method in class org.orekit.forces.maneuvers.ImpulseManeuver
-
Get the specific impulse.
- getIsp() - Method in class org.orekit.forces.maneuvers.propulsion.AbstractConstantThrustPropulsionModel
-
Get the specific impulse.
- getIsp(SpacecraftState) - Method in interface org.orekit.forces.maneuvers.propulsion.ThrustPropulsionModel
-
Get the specific impulse (s).
- getIteration() - Method in class org.orekit.estimation.measurements.EstimatedMeasurement
-
Get the iteration number.
- getIterationsCount() - Method in class org.orekit.estimation.leastsquares.AbstractBatchLSModel
-
Get the iterations count.
- getIterationsCount() - Method in class org.orekit.estimation.leastsquares.BatchLSEstimator
-
Get the number of iterations used for last estimation.
- getITRF(IERSConventions, boolean) - Method in class org.orekit.frames.AbstractFrames
-
- getITRF(ITRFVersion, IERSConventions, boolean) - Method in class org.orekit.frames.AbstractFrames
-
- getITRF(IERSConventions, boolean) - Method in interface org.orekit.frames.Frames
-
Get an unspecified International Terrestrial Reference Frame.
- getITRF(ITRFVersion, IERSConventions, boolean) - Method in interface org.orekit.frames.Frames
-
Get an specific International Terrestrial Reference Frame.
- getITRF(IERSConventions, boolean) - Static method in class org.orekit.frames.FramesFactory
-
Get an unspecified International Terrestrial Reference Frame.
- getITRF(ITRFVersion, IERSConventions, boolean) - Static method in class org.orekit.frames.FramesFactory
-
Get an specific International Terrestrial Reference Frame.
- getITRFEquinox(IERSConventions, boolean) - Method in class org.orekit.frames.AbstractFrames
-
- getITRFEquinox(IERSConventions, boolean) - Method in interface org.orekit.frames.Frames
-
Get the equinox-based ITRF reference frame.
- getITRFEquinox(IERSConventions, boolean) - Static method in class org.orekit.frames.FramesFactory
-
Get the equinox-based ITRF reference frame.
- getITRFType() - Method in class org.orekit.frames.EOPEntry
-
Get the ITRF version this entry defines.
- getITRFVersion(AbsoluteDate) - Method in class org.orekit.frames.EOPHistory
-
Get the ITRF version.
- getITRFVersion(int) - Static method in enum org.orekit.frames.ITRFVersion
-
Find an ITRF version from its reference year.
- getITRFVersion(String) - Static method in enum org.orekit.frames.ITRFVersion
-
Find an ITRF version from its name.
- getITRFVersion() - Method in class org.orekit.frames.VersionedITRF
-
Get the ITRF version.
- getJ2000Day() - Method in class org.orekit.time.DateComponents
-
Get the day number with respect to J2000 epoch.
- getJ2000Epoch() - Method in class org.orekit.time.AbstractTimeScales
-
- getJ2000Epoch(Field<T>) - Static method in class org.orekit.time.FieldAbsoluteDate
-
J2000.0 Reference epoch: 2000-01-01T12:00:00 Terrestrial Time (not UTC).
- getJ2000Epoch() - Method in interface org.orekit.time.TimeScales
-
J2000.0 Reference epoch: 2000-01-01T12:00:00 Terrestrial Time (not UTC).
- getJacobian(Orbit, PositionAngle, double[][]) - Method in class org.orekit.forces.maneuvers.SmallManeuverAnalyticalModel
-
Compute the Jacobian of the orbit with respect to maneuver parameters.
- getJacobian(CartesianDerivativesFilter, T[][]) - Method in class org.orekit.frames.FieldTransform
-
- getJacobian(CartesianDerivativesFilter, double[][]) - Method in class org.orekit.frames.Transform
-
- getJacobiansColumnsNames() - Method in class org.orekit.propagation.analytical.AbstractAnalyticalMatricesHarvester
-
- getJacobiansColumnsNames() - Method in class org.orekit.propagation.analytical.AbstractAnalyticalPropagator
-
- getJacobiansColumnsNames() - Method in class org.orekit.propagation.analytical.BrouwerLyddanePropagator
-
- getJacobiansColumnsNames() - Method in class org.orekit.propagation.analytical.tle.TLEPropagator
-
- getJacobiansColumnsNames() - Method in class org.orekit.propagation.integration.AbstractJacobiansMapper
-
- getJacobiansColumnsNames() - Method in interface org.orekit.propagation.MatricesHarvester
-
- getJacobiansColumnsNames() - Method in class org.orekit.propagation.semianalytical.dsst.DSSTHarvester
-
- getJacobiansColumnsNames() - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator
-
- getJacobianWrtCartesian(PositionAngle, T[][]) - Method in class org.orekit.orbits.FieldOrbit
-
Compute the Jacobian of the orbital parameters with respect to the Cartesian parameters.
- getJacobianWrtCartesian(PositionAngle, double[][]) - Method in class org.orekit.orbits.Orbit
-
Compute the Jacobian of the orbital parameters with respect to the Cartesian parameters.
- getJacobianWrtParameters(PositionAngle, T[][]) - Method in class org.orekit.orbits.FieldOrbit
-
Compute the Jacobian of the Cartesian parameters with respect to the orbital parameters.
- getJacobianWrtParameters(PositionAngle, double[][]) - Method in class org.orekit.orbits.Orbit
-
Compute the Jacobian of the Cartesian parameters with respect to the orbital parameters.
- getJavaEpoch() - Method in class org.orekit.time.AbstractTimeScales
-
- getJavaEpoch(Field<T>) - Static method in class org.orekit.time.FieldAbsoluteDate
-
Java Reference epoch: 1970-01-01T00:00:00 Universal Time Coordinate.
- getJavaEpoch() - Method in interface org.orekit.time.TimeScales
-
Java Reference epoch: 1970-01-01T00:00:00 Universal Time Coordinate.
- getJD0() - Method in class org.orekit.time.GLONASSDate
-
Get the current Julian date JD0.
- getJjs(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHIJjsPolynomials
-
Get the Jjs coefficient.
- getJjs(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
-
Get the Jjs coefficient.
- getJulianDay() - Method in class org.orekit.files.sp3.SP3
-
Returns the julian day for this SP3 file.
- getJulianEpoch() - Method in class org.orekit.time.AbstractTimeScales
-
- getJulianEpoch(Field<T>) - Static method in class org.orekit.time.FieldAbsoluteDate
-
Reference epoch for julian dates: -4712-01-01T12:00:00 Terrestrial Time.
- getJulianEpoch() - Method in interface org.orekit.time.TimeScales
-
Reference epoch for julian dates: -4712-01-01T12:00:00 Terrestrial Time.
- getJupiter() - Method in interface org.orekit.bodies.CelestialBodies
-
Get the Jupiter singleton body.
- getJupiter() - Static method in class org.orekit.bodies.CelestialBodyFactory
-
Get the Jupiter singleton body.
- getJupiter() - Method in class org.orekit.bodies.LazyLoadedCelestialBodies
-
- getJupiterSemiMajorAxis(AbsoluteDate, TimeScale) - Static method in class org.orekit.propagation.numerical.cr3bp.CR3BPConstants
-
Get the Jupiter semi-major axis.
- getK() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
-
Get the x component of eccentricity vector.
- getK() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldAuxiliaryElements
-
Get the x component of eccentricity vector.
- getK2MH2() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonalContext
-
Get k² - h².
- getK2MH2() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTZonalContext
-
Get k² - h².
- getK2MH2O2() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonalContext
-
Get (k² - h²) / 2.
- getK2MH2O2() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTZonalContext
-
Get (k² - h²) / 2.
- getKeplerianElementsBlock() - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmData
-
Get the Keplerian elements logical block.
- getKeplerianElementsBlock() - Method in class org.orekit.files.ccsds.ndm.odm.opm.OpmData
-
Get the Keplerian elements logical block.
- getKeplerianMeanMotion() - Method in class org.orekit.orbits.FieldOrbit
-
Get the Keplerian mean motion.
- getKeplerianMeanMotion() - Method in class org.orekit.orbits.Orbit
-
Get the Keplerian mean motion.
- getKeplerianMeanMotion() - Method in class org.orekit.propagation.FieldSpacecraftState
-
Get the Keplerian mean motion.
- getKeplerianMeanMotion() - Method in class org.orekit.propagation.SpacecraftState
-
Get the Keplerian mean motion.
- getKeplerianPeriod() - Method in class org.orekit.orbits.FieldOrbit
-
Get the Keplerian period.
- getKeplerianPeriod() - Method in class org.orekit.orbits.Orbit
-
Get the Keplerian period.
- getKeplerianPeriod() - Method in class org.orekit.propagation.FieldSpacecraftState
-
Get the Keplerian period.
- getKeplerianPeriod() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
-
Get the Keplerian period.
- getKeplerianPeriod() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldAuxiliaryElements
-
Get the Keplerian period.
- getKeplerianPeriod() - Method in class org.orekit.propagation.SpacecraftState
-
Get the Keplerian period.
- getKey() - Method in enum org.orekit.gnss.clock.RinexClock.ClockDataType
-
Get the key for the system.
- getKey() - Method in enum org.orekit.gnss.SatelliteSystem
-
Get the key for the system.
- getKey() - Method in enum org.orekit.gnss.TimeSystem
-
Get the key for the system.
- getKey() - Method in class org.orekit.utils.DoubleArrayDictionary.Entry
-
Get the entry key.
- getKey() - Method in class org.orekit.utils.FieldArrayDictionary.Entry
-
Get the entry key.
- getKlobucharAlpha() - Method in class org.orekit.gnss.navigation.RinexNavigation
-
Get the "alpha" ionospheric parameters.
- getKlobucharBeta() - Method in class org.orekit.gnss.navigation.RinexNavigation
-
Get the "beta" ionospheric parameters.
- getKpSum() - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherDataLoader.LineParameters
-
Gets the sum of all eight Kp indices for the current entry.
- getKXXX() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBodyContext
-
Get kXXX = h * Χ³.
- getKXXX() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTThirdBodyContext
-
Get kXXX = h * Χ³.
- getL() - Method in class org.orekit.data.DelaunayArguments
-
Get the mean anomaly of the Moon.
- getL() - Method in class org.orekit.data.FieldDelaunayArguments
-
Get the mean anomaly of the Moon.
- getL(PositionAngle) - Method in class org.orekit.orbits.EquinoctialOrbit
-
Get the longitude argument.
- getL(PositionAngle) - Method in class org.orekit.orbits.FieldEquinoctialOrbit
-
Get the longitude argument.
- getLabel() - Method in class org.orekit.files.ccsds.definitions.SpacecraftBodyFrame
-
Get the frame label.
- getLagrangianPoint() - Method in class org.orekit.orbits.RichardsonExpansion
-
Get the considered lagrangian point.
- getLambda() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSAlmanac
-
- getLambda() - Method in interface org.orekit.propagation.analytical.gnss.data.GLONASSOrbitalElements
-
Get the longitude of ascending node of orbit.
- getLaserId() - Method in class org.orekit.files.ilrs.CRDConfiguration.LaserConfiguration
-
Get the laser configuration ID.
- getLaserRecord() - Method in class org.orekit.files.ilrs.CRDConfiguration
-
Get the laser configuration record.
- getLaserType() - Method in class org.orekit.files.ilrs.CRDConfiguration.LaserConfiguration
-
Get the laser type.
- getLastDailyPredictedDate() - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherDataLoader
-
Gets the day (at data start) of the last daily data entry.
- getLastEstimations() - Method in class org.orekit.estimation.leastsquares.BatchLSEstimator
-
Get the last estimations performed.
- getLastKnownLeapSecond() - Method in class org.orekit.time.UTCScale
-
Get the date of the last known leap second.
- getLastObservedDate() - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherDataLoader
-
Gets the day (at data start) of the last observed data entry.
- getLastSpan() - Method in class org.orekit.utils.TimeSpanMap
-
Get the last (latest) span.
- getLastTransition() - Method in class org.orekit.utils.TimeSpanMap
-
Get the last (latest) transition.
- getLatest() - Method in class org.orekit.utils.GenericTimeStampedCache
-
Get the latest cached entry.
- getLatest() - Method in class org.orekit.utils.ImmutableTimeStampedCache
-
Get the latest entry in this cache.
- getLatest() - Method in interface org.orekit.utils.TimeStampedCache
-
Get the latest entry in this cache.
- getLatitude() - Method in class org.orekit.bodies.FieldGeodeticPoint
-
Get the latitude.
- getLatitude() - Method in class org.orekit.bodies.GeodeticPoint
-
Get the latitude.
- getLatitude() - Method in class org.orekit.gnss.metric.ntrip.CasterRecord
-
Get the latitude.
- getLatitude() - Method in class org.orekit.gnss.metric.ntrip.DataStreamRecord
-
Get the latitude.
- getLatitude() - Method in class org.orekit.propagation.events.FieldLatitudeCrossingDetector
-
Get the fixed latitude to be crossed (radians).
- getLatitude() - Method in class org.orekit.propagation.events.LatitudeCrossingDetector
-
Get the fixed latitude to be crossed (radians).
- getLaunchNumber() - Method in class org.orekit.files.ccsds.ndm.adm.AdmMetadata
-
Get the launch number.
- getLaunchNumber() - Method in class org.orekit.files.ccsds.ndm.odm.CommonMetadata
-
Get the launch number.
- getLaunchNumber(String) - Method in class org.orekit.files.ccsds.section.Metadata
-
Get the launch number.
- getLaunchNumber() - Method in class org.orekit.propagation.analytical.tle.FieldTLE
-
Get the launch number.
- getLaunchNumber() - Method in class org.orekit.propagation.analytical.tle.TLE
-
Get the launch number.
- getLaunchPiece() - Method in class org.orekit.files.ccsds.ndm.adm.AdmMetadata
-
Get the piece of launch.
- getLaunchPiece() - Method in class org.orekit.files.ccsds.ndm.odm.CommonMetadata
-
Get the piece of launch.
- getLaunchPiece(String) - Method in class org.orekit.files.ccsds.section.Metadata
-
Get the piece of launch.
- getLaunchPiece() - Method in class org.orekit.propagation.analytical.tle.FieldTLE
-
Get the launch piece.
- getLaunchPiece() - Method in class org.orekit.propagation.analytical.tle.TLE
-
Get the launch piece.
- getLaunchYear() - Method in class org.orekit.files.ccsds.ndm.adm.AdmMetadata
-
Get the launch year.
- getLaunchYear() - Method in class org.orekit.files.ccsds.ndm.odm.CommonMetadata
-
Get the launch year.
- getLaunchYear(String) - Method in class org.orekit.files.ccsds.section.Metadata
-
Get the launch year.
- getLaunchYear() - Method in class org.orekit.propagation.analytical.tle.FieldTLE
-
Get the launch year.
- getLaunchYear() - Method in class org.orekit.propagation.analytical.tle.TLE
-
Get the launch year.
- getLDot() - Method in class org.orekit.data.DelaunayArguments
-
Get the mean anomaly of the Moon time derivative.
- getLDot() - Method in class org.orekit.data.FieldDelaunayArguments
-
Get the mean anomaly of the Moon time derivative.
- getLDot(PositionAngle) - Method in class org.orekit.orbits.EquinoctialOrbit
-
Get the longitude argument derivative.
- getLDot(PositionAngle) - Method in class org.orekit.orbits.FieldEquinoctialOrbit
-
Get the longitude argument derivative.
- getLE() - Method in class org.orekit.data.BodiesElements
-
Get the mean Earth longitude.
- getLE() - Method in class org.orekit.data.FieldBodiesElements
-
Get the mean Earth longitude.
- getLE() - Method in class org.orekit.orbits.CartesianOrbit
-
Get the eccentric longitude argument.
- getLE() - Method in class org.orekit.orbits.CircularOrbit
-
Get the eccentric longitude argument.
- getLE() - Method in class org.orekit.orbits.EquinoctialOrbit
-
Get the eccentric longitude argument.
- getLE() - Method in class org.orekit.orbits.FieldCartesianOrbit
-
Get the eccentric longitude argument.
- getLE() - Method in class org.orekit.orbits.FieldCircularOrbit
-
Get the eccentric longitude argument.
- getLE() - Method in class org.orekit.orbits.FieldEquinoctialOrbit
-
Get the eccentric longitude argument.
- getLE() - Method in class org.orekit.orbits.FieldKeplerianOrbit
-
Get the eccentric longitude argument.
- getLE() - Method in class org.orekit.orbits.FieldOrbit
-
Get the eccentric longitude argument.
- getLE() - Method in class org.orekit.orbits.KeplerianOrbit
-
Get the eccentric longitude argument.
- getLE() - Method in class org.orekit.orbits.Orbit
-
Get the eccentric longitude argument.
- getLE() - Method in class org.orekit.propagation.FieldSpacecraftState
-
Get the eccentric latitude argument (as per equinoctial parameters).
- getLe() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldAuxiliaryElements
-
Get the eccentric longitude.
- getLE() - Method in class org.orekit.propagation.SpacecraftState
-
Get the eccentric latitude argument (as per equinoctial parameters).
- getLeap() - Method in class org.orekit.files.ilrs.CPF.CPFCoordinate
-
Get the leap second flag (= 0 or the value of the new leap second).
- getLeap(AbsoluteDate) - Method in class org.orekit.time.GLONASSScale
-
Get the value of the previous leap.
- getLeap(FieldAbsoluteDate<T>) - Method in class org.orekit.time.GLONASSScale
-
Get the value of the previous leap.
- getLeap(AbsoluteDate) - Method in interface org.orekit.time.TimeScale
-
Get the value of the previous leap.
- getLeap(FieldAbsoluteDate<T>) - Method in interface org.orekit.time.TimeScale
-
Get the value of the previous leap.
- getLeap(AbsoluteDate) - Method in class org.orekit.time.UTCScale
-
Get the value of the previous leap.
- getLeap(FieldAbsoluteDate<T>) - Method in class org.orekit.time.UTCScale
-
Get the value of the previous leap.
- getLeap() - Method in class org.orekit.time.UTCTAIOffset
-
Get the value of the leap at offset validity start (in seconds).
- getLeapSeconds() - Method in class org.orekit.gnss.RinexObservationHeader
-
Get the Number of leap seconds since 6-Jan-1980.
- getLeapSecondsDayNum() - Method in class org.orekit.gnss.RinexObservationHeader
-
Get the respective leap second day number.
- getLeapSecondsFuture() - Method in class org.orekit.gnss.RinexObservationHeader
-
Get the future or past leap seconds.
- getLeapSecondsWeekNum() - Method in class org.orekit.gnss.RinexObservationHeader
-
Get the respective leap second week number.
- getLEDot() - Method in class org.orekit.data.BodiesElements
-
Get the mean Earth longitude time derivative.
- getLEDot() - Method in class org.orekit.data.FieldBodiesElements
-
Get the mean Earth longitude time derivative.
- getLEDot() - Method in class org.orekit.orbits.CartesianOrbit
-
Get the eccentric longitude argument derivative.
- getLEDot() - Method in class org.orekit.orbits.CircularOrbit
-
Get the eccentric longitude argument derivative.
- getLEDot() - Method in class org.orekit.orbits.EquinoctialOrbit
-
Get the eccentric longitude argument derivative.
- getLEDot() - Method in class org.orekit.orbits.FieldCartesianOrbit
-
Get the eccentric longitude argument derivative.
- getLEDot() - Method in class org.orekit.orbits.FieldCircularOrbit
-
Get the eccentric longitude argument derivative.
- getLEDot() - Method in class org.orekit.orbits.FieldEquinoctialOrbit
-
Get the eccentric longitude argument derivative.
- getLEDot() - Method in class org.orekit.orbits.FieldKeplerianOrbit
-
Get the eccentric longitude argument derivative.
- getLEDot() - Method in class org.orekit.orbits.FieldOrbit
-
Get the eccentric longitude argument derivative.
- getLEDot() - Method in class org.orekit.orbits.KeplerianOrbit
-
Get the eccentric longitude argument derivative.
- getLEDot() - Method in class org.orekit.orbits.Orbit
-
Get the eccentric longitude argument derivative.
- getLength() - Method in class org.orekit.utils.units.Unit
-
Get the length exponent.
- getLf() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
-
Get the eccentric longitude.
- getLightingRatio(Vector3D, Frame, AbsoluteDate) - Method in class org.orekit.forces.radiation.SolarRadiationPressure
-
Get the lighting ratio ([0-1]).
- getLightingRatio(FieldVector3D<T>, Frame, FieldAbsoluteDate<T>) - Method in class org.orekit.forces.radiation.SolarRadiationPressure
-
Get the lighting ratio ([0-1]).
- getLine() - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherDataLoader.LineReader
-
Get the last line read from the stream.
- getLine1() - Method in class org.orekit.propagation.analytical.tle.FieldTLE
-
Get the first line.
- getLine1() - Method in class org.orekit.propagation.analytical.tle.TLE
-
Get the first line.
- getLine2() - Method in class org.orekit.propagation.analytical.tle.FieldTLE
-
Get the second line.
- getLine2() - Method in class org.orekit.propagation.analytical.tle.TLE
-
Get the second line.
- getLineNumber() - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken
-
Get the number of the line in the CCSDS data message.
- getLineNumber() - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherDataLoader.LineReader
-
Get the line number of the last line read from the file.
- getListAppliedDCBS() - Method in class org.orekit.gnss.clock.RinexClock
-
Getter for the applied differential code bias corrections.
- getListAppliedDCBS() - Method in class org.orekit.gnss.RinexObservationHeader
-
Get the list of applied differential code bias corrections.
- getListAppliedPCVS() - Method in class org.orekit.gnss.clock.RinexClock
-
Getter for the applied phase center variations.
- getListAppliedPCVS() - Method in class org.orekit.gnss.RinexObservationHeader
-
Get the list of antenna center variation corrections.
- getLJu() - Method in class org.orekit.data.BodiesElements
-
Get the mean Jupiter longitude.
- getLJu() - Method in class org.orekit.data.FieldBodiesElements
-
Get the mean Jupiter longitude.
- getLJuDot() - Method in class org.orekit.data.BodiesElements
-
Get the mean Jupiter longitude time derivative.
- getLJuDot() - Method in class org.orekit.data.FieldBodiesElements
-
Get the mean Jupiter longitude time derivative.
- getLLimits(SpacecraftState, AuxiliaryElements) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution
-
Compute the limits in L, the true longitude, for integration.
- getLLimits(FieldSpacecraftState<T>, FieldAuxiliaryElements<T>) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution
-
Compute the limits in L, the true longitude, for integration.
- getLLimits(SpacecraftState, AuxiliaryElements) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTAtmosphericDrag
-
Compute the limits in L, the true longitude, for integration.
- getLLimits(FieldSpacecraftState<T>, FieldAuxiliaryElements<T>) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTAtmosphericDrag
-
Compute the limits in L, the true longitude, for integration.
- getLLimits(SpacecraftState, AuxiliaryElements) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTSolarRadiationPressure
-
Compute the limits in L, the true longitude, for integration.
- getLLimits(FieldSpacecraftState<T>, FieldAuxiliaryElements<T>) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTSolarRadiationPressure
-
Compute the limits in L, the true longitude, for integration.
- getLM() - Method in class org.orekit.orbits.CartesianOrbit
-
Get the mean longitude argument.
- getLM() - Method in class org.orekit.orbits.CircularOrbit
-
Get the mean longitude argument.
- getLM() - Method in class org.orekit.orbits.EquinoctialOrbit
-
Get the mean longitude argument.
- getLM() - Method in class org.orekit.orbits.FieldCartesianOrbit
-
Get the mean longitude argument.
- getLM() - Method in class org.orekit.orbits.FieldCircularOrbit
-
Get the mean longitude argument.
- getLM() - Method in class org.orekit.orbits.FieldEquinoctialOrbit
-
Get the mean longitude argument.
- getLM() - Method in class org.orekit.orbits.FieldKeplerianOrbit
-
Get the mean longitude argument.
- getLM() - Method in class org.orekit.orbits.FieldOrbit
-
Get the mean longitude argument.
- getLM() - Method in class org.orekit.orbits.KeplerianOrbit
-
Get the mean longitude argument.
- getLM() - Method in class org.orekit.orbits.Orbit
-
Get the mean longitude argument.
- getLM() - Method in class org.orekit.propagation.FieldSpacecraftState
-
Get the mean longitude argument (as per equinoctial parameters).
- getLM() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
-
Get the mean longitude.
- getLM() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldAuxiliaryElements
-
Get the mean longitude.
- getLM() - Method in class org.orekit.propagation.SpacecraftState
-
Get the mean longitude argument (as per equinoctial parameters).
- getLMa() - Method in class org.orekit.data.BodiesElements
-
Get the mean Mars longitude.
- getLMa() - Method in class org.orekit.data.FieldBodiesElements
-
Get the mean Mars longitude.
- getLMaDot() - Method in class org.orekit.data.BodiesElements
-
Get the mean Mars longitude time derivative.
- getLMaDot() - Method in class org.orekit.data.FieldBodiesElements
-
Get the mean Mars longitude time derivative.
- getLMDot() - Method in class org.orekit.orbits.CartesianOrbit
-
Get the mean longitude argument derivative.
- getLMDot() - Method in class org.orekit.orbits.CircularOrbit
-
Get the mean longitude argument derivative.
- getLMDot() - Method in class org.orekit.orbits.EquinoctialOrbit
-
Get the mean longitude argument derivative.
- getLMDot() - Method in class org.orekit.orbits.FieldCartesianOrbit
-
Get the mean longitude argument derivative.
- getLMDot() - Method in class org.orekit.orbits.FieldCircularOrbit
-
Get the mean longitude argument derivative.
- getLMDot() - Method in class org.orekit.orbits.FieldEquinoctialOrbit
-
Get the mean longitude argument derivative.
- getLMDot() - Method in class org.orekit.orbits.FieldKeplerianOrbit
-
Get the mean longitude argument derivative.
- getLMDot() - Method in class org.orekit.orbits.FieldOrbit
-
Get the mean longitude argument derivative.
- getLMDot() - Method in class org.orekit.orbits.KeplerianOrbit
-
Get the mean longitude argument derivative.
- getLMDot() - Method in class org.orekit.orbits.Orbit
-
Get the mean longitude argument derivative.
- getLMe() - Method in class org.orekit.data.BodiesElements
-
Get the mean Mercury longitude.
- getLMe() - Method in class org.orekit.data.FieldBodiesElements
-
Get the mean Mercury longitude.
- getLMeDot() - Method in class org.orekit.data.BodiesElements
-
Get the mean Mercury longitude time derivative.
- getLMeDot() - Method in class org.orekit.data.FieldBodiesElements
-
Get the mean Mercury longitude time derivative.
- getLNe() - Method in class org.orekit.data.BodiesElements
-
Get the mean Neptune longitude.
- getLNe() - Method in class org.orekit.data.FieldBodiesElements
-
Get the mean Neptune longitude.
- getLNeDot() - Method in class org.orekit.data.BodiesElements
-
Get the mean Neptune longitude time derivative.
- getLNeDot() - Method in class org.orekit.data.FieldBodiesElements
-
Get the mean Neptune longitude time derivative.
- getLNFifthString() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data
-
Get the GLONASS ln Word extracted from fifth string of the subframe.
- getLns(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldLnsCoefficients
-
Get the value of Lns(γ).
- getLns(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.LnsCoefficients
-
Get the value of Lns(γ).
- getLNThirdString() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data
-
Get the GLONASS ln Word extracted from third string of the subframe.
- getLoadedAstronomicalUnit() - Method in class org.orekit.bodies.JPLEphemeridesLoader
-
Get astronomical unit.
- getLoadedConstant(String...) - Method in class org.orekit.bodies.JPLEphemeridesLoader
-
Get a constant defined in the ephemerides headers.
- getLoadedDataNames() - Method in class org.orekit.data.DataProvidersManager
-
Get an unmodifiable view of the set of data file names that have been loaded.
- getLoadedEarthMoonMassRatio() - Method in class org.orekit.bodies.JPLEphemeridesLoader
-
Get Earth/Moon mass ratio.
- getLoadedGravitationalCoefficient(JPLEphemeridesLoader.EphemerisType) - Method in class org.orekit.bodies.JPLEphemeridesLoader
-
Get the gravitational coefficient of a body.
- getLocalizedMessage() - Method in exception org.orekit.errors.OrekitException
- getLocalizedMessage() - Method in exception org.orekit.errors.OrekitIllegalArgumentException
- getLocalizedMessage() - Method in exception org.orekit.errors.OrekitIllegalStateException
- getLocalizedMessage() - Method in exception org.orekit.errors.OrekitInternalError
- getLocalizedMessage() - Method in exception org.orekit.errors.OrekitIOException
- getLocalizedMessage() - Method in exception org.orekit.errors.OrekitParseException
- getLocalizedString(Locale) - Method in enum org.orekit.errors.OrekitMessages
- getLocalTimingId() - Method in class org.orekit.files.ilrs.CRDConfiguration.TimingSystemConfiguration
-
Get the local timing system configuration ID.
- getLocation() - Method in class org.orekit.gnss.DOP
-
Gets the location with respect to the Earth where DOP was calculated.
- getLOD() - Method in class org.orekit.frames.EOPEntry
-
Get the LoD (Length of Day) value.
- getLOD(AbsoluteDate) - Method in class org.orekit.frames.EOPHistory
-
Get the LoD (Length of Day) value.
- getLOD(FieldAbsoluteDate<T>) - Method in class org.orekit.frames.EOPHistory
-
Get the LoD (Length of Day) value.
- getLofCartesianOrbitalParametersEvolution() - Method in class org.orekit.estimation.sequential.UnivariateProcessNoise
-
Getter for the lofCartesianOrbitalParametersEvolution.
- getLofType() - Method in class org.orekit.estimation.sequential.UnivariateProcessNoise
-
Getter for the lofType.
- getLofType() - Method in enum org.orekit.files.ccsds.definitions.OrbitRelativeFrame
-
Get the type of Local Orbital frame.
- getLoggedEvents() - Method in class org.orekit.propagation.events.EventsLogger
-
Get an immutable copy of the logged events.
- getLoggedEvents() - Method in class org.orekit.propagation.events.FieldEventsLogger
-
Get an immutable copy of the logged events.
- getLongitude() - Method in class org.orekit.bodies.FieldGeodeticPoint
-
Get the longitude.
- getLongitude() - Method in class org.orekit.bodies.GeodeticPoint
-
Get the longitude.
- getLongitude() - Method in class org.orekit.gnss.metric.ntrip.CasterRecord
-
Get the longitude.
- getLongitude() - Method in class org.orekit.gnss.metric.ntrip.DataStreamRecord
-
Get the longitude.
- getLongitude() - Method in class org.orekit.propagation.events.LongitudeCrossingDetector
-
Get the fixed longitude to be crossed (radians).
- getLossOfLockIndicator() - Method in class org.orekit.gnss.ObservationData
-
Get the Loss of Lock Indicator.
- getLoveNumbers() - Method in enum org.orekit.utils.IERSConventions
-
Get the Love numbers.
- getLowElevationThreshold() - Method in class org.orekit.models.earth.troposphere.SaastamoinenModel
-
Get the low elevation threshold value for path delay computation.
- getLowerCaseAbbreviation() - Method in enum org.orekit.time.Month
-
Get the lower case three letters abbreviation.
- getLowerCaseName() - Method in enum org.orekit.time.Month
-
Get the lower case full name.
- getLowReference() - Method in class org.orekit.estimation.measurements.gnss.AbstractLambdaMethod
-
Get a reference to the lower triangular matrix of the decomposition.
- getLPosition(LagrangianPoints) - Method in class org.orekit.bodies.CR3BPSystem
-
Get the position of the Lagrangian point in the CR3BP Rotating frame.
- getLPrime() - Method in class org.orekit.data.DelaunayArguments
-
Get the mean anomaly of the Sun.
- getLPrime() - Method in class org.orekit.data.FieldDelaunayArguments
-
Get the mean anomaly of the Sun.
- getLPrimeDot() - Method in class org.orekit.data.DelaunayArguments
-
Get the mean anomaly of the Sun time derivative.
- getLPrimeDot() - Method in class org.orekit.data.FieldDelaunayArguments
-
Get the mean anomaly of the Sun time derivative.
- getLSa() - Method in class org.orekit.data.BodiesElements
-
Get the mean Saturn longitude.
- getLSa() - Method in class org.orekit.data.FieldBodiesElements
-
Get the mean Saturn longitude.
- getLSaDot() - Method in class org.orekit.data.BodiesElements
-
Get the mean Saturn longitude time derivative.
- getLSaDot() - Method in class org.orekit.data.FieldBodiesElements
-
Get the mean Saturn longitude time derivative.
- getLst81Adj() - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherDataLoader.LineParameters
-
Gets the last 81-day arithmetic average of F10.7 (adjusted).
- getLst81Obs() - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherDataLoader.LineParameters
-
Gets the last 81-day arithmetic average of F10.7 (observed).
- getLUr() - Method in class org.orekit.data.BodiesElements
-
Get the mean Uranus longitude.
- getLUr() - Method in class org.orekit.data.FieldBodiesElements
-
Get the mean Uranus longitude.
- getLUrDot() - Method in class org.orekit.data.BodiesElements
-
Get the mean Uranus longitude time derivative.
- getLUrDot() - Method in class org.orekit.data.FieldBodiesElements
-
Get the mean Uranus longitude time derivative.
- getLv() - Method in class org.orekit.orbits.CartesianOrbit
-
Get the true longitude argument.
- getLv() - Method in class org.orekit.orbits.CircularOrbit
-
Get the true longitude argument.
- getLv() - Method in class org.orekit.orbits.EquinoctialOrbit
-
Get the true longitude argument.
- getLv() - Method in class org.orekit.orbits.FieldCartesianOrbit
-
Get the true longitude argument.
- getLv() - Method in class org.orekit.orbits.FieldCircularOrbit
-
Get the true longitude argument.
- getLv() - Method in class org.orekit.orbits.FieldEquinoctialOrbit
-
Get the true longitude argument.
- getLv() - Method in class org.orekit.orbits.FieldKeplerianOrbit
-
Get the true longitude argument.
- getLv() - Method in class org.orekit.orbits.FieldOrbit
-
Get the true longitude argument.
- getLv() - Method in class org.orekit.orbits.KeplerianOrbit
-
Get the true longitude argument.
- getLv() - Method in class org.orekit.orbits.Orbit
-
Get the true longitude argument.
- getLv() - Method in class org.orekit.propagation.FieldSpacecraftState
-
Get the true latitude argument (as per equinoctial parameters).
- getLv() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
-
Get the true longitude.
- getLv() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldAuxiliaryElements
-
Get the true longitude.
- getLv() - Method in class org.orekit.propagation.SpacecraftState
-
Get the true latitude argument (as per equinoctial parameters).
- getLvDot() - Method in class org.orekit.orbits.CartesianOrbit
-
Get the true longitude argument derivative.
- getLvDot() - Method in class org.orekit.orbits.CircularOrbit
-
Get the true longitude argument derivative.
- getLvDot() - Method in class org.orekit.orbits.EquinoctialOrbit
-
Get the true longitude argument derivative.
- getLvDot() - Method in class org.orekit.orbits.FieldCartesianOrbit
-
Get the true longitude argument derivative.
- getLvDot() - Method in class org.orekit.orbits.FieldCircularOrbit
-
Get the true longitude argument derivative.
- getLvDot() - Method in class org.orekit.orbits.FieldEquinoctialOrbit
-
Get the true longitude argument derivative.
- getLvDot() - Method in class org.orekit.orbits.FieldKeplerianOrbit
-
Get the true longitude argument derivative.
- getLvDot() - Method in class org.orekit.orbits.FieldOrbit
-
Get the true longitude argument derivative.
- getLvDot() - Method in class org.orekit.orbits.KeplerianOrbit
-
Get the true longitude argument derivative.
- getLvDot() - Method in class org.orekit.orbits.Orbit
-
Get the true longitude argument derivative.
- getLVe() - Method in class org.orekit.data.BodiesElements
-
Get the mean Venus longitude.
- getLVe() - Method in class org.orekit.data.FieldBodiesElements
-
Get the mean Venus longitude.
- getLVeDot() - Method in class org.orekit.data.BodiesElements
-
Get the mean Venus longitude time derivative.
- getLVeDot() - Method in class org.orekit.data.FieldBodiesElements
-
Get the mean Venus longitude time derivative.
- getLyapunovOrbitalPeriod(double) - Method in class org.orekit.orbits.RichardsonExpansion
-
Return the orbital period of the Halo Orbit.
- getM() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data
-
Get the GLONASS M Word.
- getM0() - Method in class org.orekit.propagation.analytical.gnss.data.CommonGnssData
-
Getter for the mean anomaly at reference time.
- getM0() - Method in interface org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElements
-
Gets the Mean Anomaly at Reference Time.
- getM2() - Method in class org.orekit.propagation.analytical.BrouwerLyddanePropagator
-
Get the value of the M2 drag parameter.
- getM2() - Method in class org.orekit.propagation.analytical.FieldBrouwerLyddanePropagator
-
Get the value of the M2 drag parameter.
- getM2aoA() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBodyContext
-
Get m2aoA = -2 * a / A.
- getM2aoA() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonalContext
-
Get m2aoA = -2 * a / A.
- getM2aoA() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTThirdBodyContext
-
Get m2aoA = -2 * a / A.
- getM2aoA() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTZonalContext
-
Get m2aoA = -2 * a / A.
- getMainStateEquations(ODEIntegrator) - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
-
Get the differential equations to integrate (for main state only).
- getMainStateEquations(FieldODEIntegrator<T>) - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator
-
Get the differential equations to integrate (for main state only).
- getMainStateEquations(FieldODEIntegrator<T>) - Method in class org.orekit.propagation.numerical.FieldNumericalPropagator
-
Get the differential equations to integrate (for main state only).
- getMainStateEquations(ODEIntegrator) - Method in class org.orekit.propagation.numerical.GLONASSNumericalPropagator
-
- getMainStateEquations(ODEIntegrator) - Method in class org.orekit.propagation.numerical.NumericalPropagator
-
Get the differential equations to integrate (for main state only).
- getMainStateEquations(ODEIntegrator) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator
-
Get the differential equations to integrate (for main state only).
- getMainStateEquations(FieldODEIntegrator<T>) - Method in class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator
-
Get the differential equations to integrate (for main state only).
- getManagedAdditionalStates() - Method in class org.orekit.propagation.AbstractPropagator
-
Get all the names of all managed states.
- getManagedAdditionalStates() - Method in class org.orekit.propagation.analytical.Ephemeris
-
Get all the names of all managed states.
- getManagedAdditionalStates() - Method in class org.orekit.propagation.FieldAbstractPropagator
-
Get all the names of all managed states.
- getManagedAdditionalStates() - Method in interface org.orekit.propagation.FieldPropagator
-
Get all the names of all managed states.
- getManagedAdditionalStates() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
-
Get all the names of all managed states.
- getManagedAdditionalStates() - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator
-
Get all the names of all managed states.
- getManagedAdditionalStates() - Method in interface org.orekit.propagation.Propagator
-
Get all the names of all managed states.
- getManBasis() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata
-
Get basis of this maneuver history data.
- getManBasisID() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata
-
Get identification number of the orbit determination or simulation upon which this maneuver is based.
- getManComposition() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata
-
Get maneuver elements of information.
- getManDeviceID() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata
-
Get identifier of the device used for this maneuver.
- getManeuver(int) - Method in class org.orekit.files.ccsds.ndm.adm.apm.ApmData
-
Get a maneuver.
- getManeuver(int) - Method in class org.orekit.files.ccsds.ndm.odm.opm.Opm
-
Get a maneuver.
- getManeuver(int) - Method in class org.orekit.files.ccsds.ndm.odm.opm.OpmData
-
Get a maneuver.
- getManeuverAttitudeProvider() - Method in class org.orekit.forces.maneuvers.propulsion.ThrustDirectionAndAttitudeProvider
-
Attitude provider to use.
- getManeuverBlocks() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmData
-
Get maneuvers logical blocks.
- getManeuvers() - Method in class org.orekit.files.ccsds.ndm.adm.apm.ApmData
-
Get a list of all maneuvers.
- getManeuvers() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistory
-
Get the maneuvers.
- getManeuvers() - Method in class org.orekit.files.ccsds.ndm.odm.opm.Opm
-
Get a list of all maneuvers.
- getManeuvers() - Method in class org.orekit.files.ccsds.ndm.odm.opm.OpmData
-
Get a list of all maneuvers.
- getManeuversFrequency() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
-
Get the average frequency of orbit or attitude maneuvers (in SI units, hence per second).
- getManeuversPerYear() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
-
Get the average number of orbit or attitude maneuvers per year.
- getManeuverTriggers() - Method in class org.orekit.forces.maneuvers.Maneuver
-
Get the maneuver triggers.
- getManFrameEpoch() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata
-
- getManID() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata
-
Get maneuver identification number.
- getManifolds(SpacecraftState, boolean) - Method in class org.orekit.orbits.LibrationOrbit
-
Return a manifold direction from one position on a libration Orbit.
- getManNextEpoch() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata
-
Get start time of next maneuver.
- getManNextID() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata
-
Get identification number of next maneuver.
- getManPredSource() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata
-
Get prediction source on which this maneuver is based.
- getManPrevEpoch() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata
-
Get completion time of previous maneuver.
- getManPrevID() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata
-
Get identification number of previous maneuver.
- getManPurpose() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata
-
Get the purposes of the maneuver.
- getManReferenceFrame() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata
-
Get reference frame of the maneuver.
- getManufacturer() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
-
Get manufacturer name.
- getManUnits() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata
-
Get maneuver elements of information units.
- getMapper() - Method in class org.orekit.propagation.analytical.tle.TLEPartialDerivativesEquations
-
Deprecated.
Get a mapper between two-dimensional Jacobians and one-dimensional additional state.
- getMapper() - Method in class org.orekit.propagation.numerical.AbsolutePartialDerivativesEquations
-
Deprecated.
Get a mapper between two-dimensional Jacobians and one-dimensional additional state.
- getMapper() - Method in class org.orekit.propagation.numerical.EpochDerivativesEquations
-
Get a mapper between two-dimensional Jacobians and one-dimensional additional state.
- getMapper() - Method in class org.orekit.propagation.numerical.PartialDerivativesEquations
-
Deprecated.
Get a mapper between two-dimensional Jacobians and one-dimensional additional state.
- getMapper() - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPartialDerivativesEquations
-
Deprecated.
Get a mapper between two-dimensional Jacobians and one-dimensional additional state.
- getMappers() - Method in class org.orekit.estimation.sequential.AbstractKalmanModel
-
- getMargin() - Method in class org.orekit.geometry.fov.AbstractFieldOfView
-
Get the angular margin to apply (radians).
- getMargin() - Method in interface org.orekit.geometry.fov.FieldOfView
-
Get the angular margin to apply (radians).
- getMargin() - Method in class org.orekit.propagation.events.GeographicZoneDetector
-
Get the angular margin to apply (radians).
- getMarkerName() - Method in class org.orekit.gnss.RinexObservationHeader
-
Get name of the antenna marker.
- getMarkerNumber() - Method in class org.orekit.gnss.RinexObservationHeader
-
Get number of the antenna marker.
- getMarkerType() - Method in class org.orekit.gnss.RinexObservationHeader
-
Get type of the antenna marker.
- getMars() - Method in interface org.orekit.bodies.CelestialBodies
-
Get the Mars singleton body.
- getMars() - Static method in class org.orekit.bodies.CelestialBodyFactory
-
Get the Mars singleton body.
- getMars() - Method in class org.orekit.bodies.LazyLoadedCelestialBodies
-
- getMass() - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmData
-
Get the mass.
- getMass() - Method in class org.orekit.files.ccsds.ndm.odm.opm.OpmData
-
Get the mass.
- getMass() - Method in class org.orekit.files.ccsds.ndm.odm.SpacecraftParameters
-
Get the spacecraft mass.
- getMass(AbsoluteDate) - Method in class org.orekit.propagation.analytical.AbstractAnalyticalPropagator
-
Get the mass.
- getMass(AbsoluteDate) - Method in class org.orekit.propagation.analytical.AdapterPropagator
-
Get the mass.
- getMass(AbsoluteDate) - Method in class org.orekit.propagation.analytical.AggregateBoundedPropagator
-
- getMass(AbsoluteDate) - Method in class org.orekit.propagation.analytical.BrouwerLyddanePropagator
-
Get the mass.
- getMass(AbsoluteDate) - Method in class org.orekit.propagation.analytical.EcksteinHechlerPropagator
-
Get the mass.
- getMass(AbsoluteDate) - Method in class org.orekit.propagation.analytical.Ephemeris
-
Get the mass.
- getMass(FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.analytical.FieldAbstractAnalyticalPropagator
-
Get the mass.
- getMass(FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.analytical.FieldBrouwerLyddanePropagator
-
Get the mass.
- getMass(FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.analytical.FieldEcksteinHechlerPropagator
-
Get the mass.
- getMass(FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.analytical.FieldKeplerianPropagator
-
Get the mass.
- getMass(AbsoluteDate) - Method in class org.orekit.propagation.analytical.gnss.GLONASSAnalyticalPropagator
-
Get the mass.
- getMass(AbsoluteDate) - Method in class org.orekit.propagation.analytical.gnss.GNSSPropagator
-
Get the mass.
- getMass(AbsoluteDate) - Method in class org.orekit.propagation.analytical.gnss.SBASPropagator
-
Get the mass.
- getMass(AbsoluteDate) - Method in class org.orekit.propagation.analytical.KeplerianPropagator
-
Get the mass.
- getMass(FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.analytical.tle.FieldTLEPropagator
-
Get the mass.
- getMass(AbsoluteDate) - Method in class org.orekit.propagation.analytical.tle.TLEPropagator
-
Get the mass.
- getMass() - Method in class org.orekit.propagation.conversion.DSSTPropagatorBuilder
-
Get the mass.
- getMass() - Method in class org.orekit.propagation.conversion.NumericalPropagatorBuilder
-
Get the mass.
- getMass() - Method in class org.orekit.propagation.FieldSpacecraftState
-
Gets the current mass.
- getMass(FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.integration.FieldIntegratedEphemeris
-
Get the mass.
- getMass(AbsoluteDate) - Method in class org.orekit.propagation.integration.IntegratedEphemeris
-
Get the mass.
- getMass() - Method in class org.orekit.propagation.SpacecraftState
-
Gets the current mass.
- getMass() - Method in class org.orekit.utils.units.Unit
-
Get the mass exponent.
- getMassDepletionDelay() - Method in class org.orekit.forces.maneuvers.jacobians.TriggerDate
-
Get the mass depletion effect processor.
- getMassDerivatives(SpacecraftState, double[]) - Method in interface org.orekit.forces.maneuvers.propulsion.PropulsionModel
-
Get the mass derivative (i.e.
- getMassDerivatives(FieldSpacecraftState<T>, T[]) - Method in interface org.orekit.forces.maneuvers.propulsion.PropulsionModel
-
Get the mass derivative (i.e.
- getMassDerivatives(SpacecraftState, double[]) - Method in interface org.orekit.forces.maneuvers.propulsion.ThrustPropulsionModel
-
Get the mass derivative (i.e.
- getMassDerivatives(FieldSpacecraftState<T>, T[]) - Method in interface org.orekit.forces.maneuvers.propulsion.ThrustPropulsionModel
-
Get the mass derivative (i.e.
- getMassRatio() - Method in class org.orekit.bodies.CR3BPSystem
-
Get the CR3BP mass ratio of the system mu2/(mu1+mu2).
- getMatrix() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Covariance
-
Get the covariance matrix.
- getMatrixLine(int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.PolynomialFunctionMatrix
-
Get a line of the matrix.
- getMaxAlt() - Method in class org.orekit.models.earth.atmosphere.HarrisPriester
-
Get the maximal altitude for the model.
- getMaxAR3Pow() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBodyContext
-
Get the value of max power for a/R3 in the serie expansion.
- getMaxAR3Pow() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTThirdBodyContext
-
Get the value of max power for a/R3 in the serie expansion.
- getMaxAreaForCollisionProbability() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
-
Get the maximum cross-sectional area for collision probability estimation purposes.
- getMaxAvailableDegree() - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
-
Get the maximal degree available in the last file parsed.
- getMaxAvailableOrder() - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
-
Get the maximal order available in the last file parsed.
- getMaxCheckInterval() - Method in class org.orekit.propagation.events.AbstractDetector
-
Get maximal time interval between switching function checks.
- getMaxCheckInterval() - Method in class org.orekit.propagation.events.AdapterDetector
-
Get maximal time interval between switching function checks.
- getMaxCheckInterval() - Method in interface org.orekit.propagation.events.EventDetector
-
Get maximal time interval between switching function checks.
- getMaxCheckInterval() - Method in class org.orekit.propagation.events.FieldAbstractDetector
-
Get maximal time interval between switching function checks.
- getMaxCheckInterval() - Method in interface org.orekit.propagation.events.FieldEventDetector
-
Get maximal time interval between switching function checks.
- getMaxChunksDuration() - Method in class org.orekit.bodies.JPLEphemeridesLoader
-
Get the maximal chunks duration.
- getMaxDate() - Method in class org.orekit.attitudes.AggregateBoundedAttitudeProvider
-
Get the last date of the range.
- getMaxDate() - Method in interface org.orekit.attitudes.BoundedAttitudeProvider
-
Get the last date of the range.
- getMaxDate() - Method in class org.orekit.attitudes.TabulatedLofOffset
-
Get the last date of the range.
- getMaxDate() - Method in class org.orekit.attitudes.TabulatedProvider
-
Get the last date of the range.
- getMaxDate() - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherData
-
Gets the available data range maximum date.
- getMaxDate() - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherDataLoader
-
Gets the available data range maximum date.
- getMaxDate() - Method in class org.orekit.models.earth.atmosphere.data.MarshallSolarActivityFutureEstimation
-
Gets the available data range maximum date.
- getMaxDate() - Method in interface org.orekit.models.earth.atmosphere.DTM2000InputParameters
-
Gets the available data range maximum date.
- getMaxDate() - Method in interface org.orekit.models.earth.atmosphere.JB2008InputParameters
-
Gets the available data range maximum date.
- getMaxDate() - Method in interface org.orekit.models.earth.atmosphere.NRLMSISE00InputParameters
-
Gets the available data range maximum date.
- getMaxDate() - Method in class org.orekit.propagation.analytical.AggregateBoundedPropagator
-
- getMaxDate() - Method in class org.orekit.propagation.analytical.Ephemeris
-
Get the last date of the range.
- getMaxDate() - Method in interface org.orekit.propagation.BoundedPropagator
-
Get the last date of the range.
- getMaxDate() - Method in interface org.orekit.propagation.FieldBoundedPropagator
-
Get the last date of the range.
- getMaxDate() - Method in class org.orekit.propagation.integration.FieldIntegratedEphemeris
-
Get the last date of the range.
- getMaxDate() - Method in class org.orekit.propagation.integration.IntegratedEphemeris
-
Get the last date of the range.
- getMaxDegree() - Method in class org.orekit.forces.gravity.potential.CachedNormalizedSphericalHarmonicsProvider
-
Get the maximal supported degree.
- getMaxDegree() - Method in class org.orekit.forces.gravity.potential.OceanTidesWave
-
Get the maximum supported degree.
- getMaxDegree() - Method in interface org.orekit.forces.gravity.potential.SphericalHarmonicsProvider
-
Get the maximal supported degree.
- getMaxDistance() - Method in class org.orekit.estimation.measurements.gnss.AbstractLambdaMethod
-
Get the maximum of distance among the solutions found.
- getMaxEccPow() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBodyContext
-
Get the value of max power for e in the serie expansion.
- getMaxEccPow() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTThirdBodyContext
-
Get the value of max power for e in the serie expansion.
- getMaxFreqF() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBodyContext
-
Get the value of max frequency of F.
- getMaxFreqF() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTThirdBodyContext
-
Get the value of max frequency of F.
- getMaximumObsGap() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
-
Get maximum time between observations in the OD of the object.
- getMaxIterationCount() - Method in class org.orekit.propagation.events.AbstractDetector
-
Get maximal number of iterations in the event time search.
- getMaxIterationCount() - Method in class org.orekit.propagation.events.AdapterDetector
-
Get maximal number of iterations in the event time search.
- getMaxIterationCount() - Method in interface org.orekit.propagation.events.EventDetector
-
Get maximal number of iterations in the event time search.
- getMaxIterationCount() - Method in class org.orekit.propagation.events.FieldAbstractDetector
-
Get maximal number of iterations in the event time search.
- getMaxIterationCount() - Method in interface org.orekit.propagation.events.FieldEventDetector
-
Get maximal number of iterations in the event time search.
- getMaxOrder() - Method in class org.orekit.forces.gravity.potential.CachedNormalizedSphericalHarmonicsProvider
-
Get the maximal supported order.
- getMaxOrder() - Method in class org.orekit.forces.gravity.potential.OceanTidesWave
-
Get the maximum supported order.
- getMaxOrder() - Method in interface org.orekit.forces.gravity.potential.SphericalHarmonicsProvider
-
Get the maximal supported order.
- getMaxOrder() - Method in enum org.orekit.utils.AngularDerivativesFilter
-
Get the maximum derivation order.
- getMaxOrder() - Method in enum org.orekit.utils.CartesianDerivativesFilter
-
Get the maximum derivation order.
- getMaxParseDegree() - Method in class org.orekit.forces.gravity.potential.OceanTidesReader
-
Get the degree limit for the next file parsing.
- getMaxParseDegree() - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
-
Get the degree limit for the next file parsing.
- getMaxParseOrder() - Method in class org.orekit.forces.gravity.potential.OceanTidesReader
-
Get the order limit for the next file parsing.
- getMaxParseOrder() - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
-
Get the order limit for the next file parsing.
- getMaxPredictedEigenMaj() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
-
Get maximum predicted major eigenvalue of 1σ positional error ellipsoid over entire time span of the OCM.
- getMaxRcs() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
-
Get the maximum radar cross-section.
- getMaxSigma() - Method in class org.orekit.estimation.measurements.modifiers.OutlierFilter
-
Get the value of the outlier detection limit.
- getMaxSlots() - Method in class org.orekit.utils.GenericTimeStampedCache
-
Get the maximum number of independent cached time slots.
- getMaxSolution() - Method in class org.orekit.estimation.measurements.gnss.AbstractLambdaMethod
-
Get the maximum number of solutions seeked.
- getMaxSpan() - Method in class org.orekit.utils.GenericTimeStampedCache
-
Get the maximum duration span in seconds of one slot.
- getMaxThrust() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
-
Get the maximum composite thrust the spacecraft can accomplish.
- getMaxTimeBeetween2Measurement() - Method in class org.orekit.estimation.measurements.gnss.AbstractCycleSlipDetector
-
Get the maximum time lapse between 2 measurements without considering a cycle-slip has occurring between both.
- getMaxValue() - Method in class org.orekit.utils.ParameterDriver
-
Get maximum parameter value.
- getMCo2AB() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBodyContext
-
Get mCo2AB = -C / 2AB.
- getMCo2AB() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonalContext
-
Get mCo2AB = -C / 2AB.
- getMCo2AB() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTThirdBodyContext
-
Get mCo2AB = -C / 2AB.
- getMCo2AB() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTZonalContext
-
Get mCo2AB = -C / 2AB.
- getMeanAnomaly() - Method in class org.orekit.orbits.FieldKeplerianOrbit
-
Get the mean anomaly.
- getMeanAnomaly() - Method in class org.orekit.orbits.KeplerianOrbit
-
Get the mean anomaly.
- getMeanAnomaly() - Method in class org.orekit.propagation.analytical.tle.FieldTLE
-
Get the mean anomaly.
- getMeanAnomaly() - Method in class org.orekit.propagation.analytical.tle.TLE
-
Get the mean anomaly.
- getMeanAnomalyDot() - Method in class org.orekit.orbits.FieldKeplerianOrbit
-
Get the mean anomaly derivative.
- getMeanAnomalyDot() - Method in class org.orekit.orbits.KeplerianOrbit
-
Get the mean anomaly derivative.
- getMeanElementRate(SpacecraftState, AuxiliaryElements, double[]) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution
-
Computes the mean equinoctial elements rates dai / dt.
- getMeanElementRate(FieldSpacecraftState<T>, FieldAuxiliaryElements<T>, T[]) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution
-
Computes the mean equinoctial elements rates dai / dt.
- getMeanElementRate(SpacecraftState, AbstractGaussianContribution.GaussQuadrature, double, double, AbstractGaussianContributionContext, double[]) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution
-
Computes the mean equinoctial elements rates dai / dt.
- getMeanElementRate(FieldSpacecraftState<T>, AbstractGaussianContribution.GaussQuadrature, T, T, FieldAbstractGaussianContributionContext<T>, T[]) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution
-
Computes the mean equinoctial elements rates dai / dt.
- getMeanElementRate(SpacecraftState, AuxiliaryElements, double[]) - Method in interface org.orekit.propagation.semianalytical.dsst.forces.DSSTForceModel
-
Computes the mean equinoctial elements rates dai / dt.
- getMeanElementRate(FieldSpacecraftState<T>, FieldAuxiliaryElements<T>, T[]) - Method in interface org.orekit.propagation.semianalytical.dsst.forces.DSSTForceModel
-
Computes the mean equinoctial elements rates dai / dt.
- getMeanElementRate(SpacecraftState, AuxiliaryElements, double[]) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTNewtonianAttraction
-
Computes the mean equinoctial elements rates dai / dt.
- getMeanElementRate(FieldSpacecraftState<T>, FieldAuxiliaryElements<T>, T[]) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTNewtonianAttraction
-
Computes the mean equinoctial elements rates dai / dt.
- getMeanElementRate(SpacecraftState, AuxiliaryElements, double[]) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseral
-
Computes the mean equinoctial elements rates dai / dt.
- getMeanElementRate(FieldSpacecraftState<T>, FieldAuxiliaryElements<T>, T[]) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseral
-
Computes the mean equinoctial elements rates dai / dt.
- getMeanElementRate(SpacecraftState, AuxiliaryElements, double[]) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBody
-
Computes the mean equinoctial elements rates dai / dt.
- getMeanElementRate(FieldSpacecraftState<T>, FieldAuxiliaryElements<T>, T[]) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBody
-
Computes the mean equinoctial elements rates dai / dt.
- getMeanElementRate(SpacecraftState, AuxiliaryElements, double[]) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonal
-
Computes the mean equinoctial elements rates dai / dt.
- getMeanElementRate(FieldSpacecraftState<T>, FieldAuxiliaryElements<T>, T[]) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonal
-
Computes the mean equinoctial elements rates dai / dt.
- getMeanElementTheory() - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmMetadata
-
Get the description of the Mean Element Theory.
- getMeanFlux(AbsoluteDate) - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherData
-
Get the value of the mean solar flux.
- getMeanFlux(AbsoluteDate) - Method in class org.orekit.models.earth.atmosphere.data.MarshallSolarActivityFutureEstimation
-
Get the value of the mean solar flux.
- getMeanFlux(AbsoluteDate) - Method in interface org.orekit.models.earth.atmosphere.DTM2000InputParameters
-
Get the value of the mean solar flux.
- getMeanMotion() - Method in class org.orekit.files.ccsds.ndm.odm.KeplerianElements
-
Get the orbit mean motion.
- getMeanMotion() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractAlmanac
-
Getter for the mean motion.
- getMeanMotion() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractNavigationMessage
-
Getter for the mean motion.
- getMeanMotion() - Method in interface org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElements
-
Gets the Mean Motion.
- getMeanMotion() - Method in class org.orekit.propagation.analytical.tle.FieldTLE
-
Get the mean motion.
- getMeanMotion() - Method in class org.orekit.propagation.analytical.tle.TLE
-
Get the mean motion.
- getMeanMotion() - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContributionContext
-
Get the Keplerian mean motion.
- getMeanMotion() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseralContext
-
Get the Keplerian mean motion.
- getMeanMotion() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBodyContext
-
Get the Keplerian mean motion.
- getMeanMotion() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonalContext
-
Get the Keplerian mean motion.
- getMeanMotion() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldAbstractGaussianContributionContext
-
Get the Keplerian mean motion.
- getMeanMotion() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTTesseralContext
-
Get the Keplerian mean motion.
- getMeanMotion() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTThirdBodyContext
-
Get the Keplerian mean motion.
- getMeanMotion() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTZonalContext
-
Get the Keplerian mean motion.
- getMeanMotion() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
-
Get the Keplerian mean motion.
- getMeanMotion() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldAuxiliaryElements
-
Get the Keplerian mean motion.
- getMeanMotionDot() - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmTle
-
Get the first time derivative of the mean motion.
- getMeanMotionDotDot() - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmTle
-
Get the second time derivative of the mean motion.
- getMeanMotionFirstDerivative() - Method in class org.orekit.propagation.analytical.tle.FieldTLE
-
Get the mean motion first derivative.
- getMeanMotionFirstDerivative() - Method in class org.orekit.propagation.analytical.tle.TLE
-
Get the mean motion first derivative.
- getMeanMotionSecondDerivative() - Method in class org.orekit.propagation.analytical.tle.FieldTLE
-
Get the mean motion second derivative.
- getMeanMotionSecondDerivative() - Method in class org.orekit.propagation.analytical.tle.TLE
-
Get the mean motion second derivative.
- getMeanObliquityFunction() - Method in enum org.orekit.utils.IERSConventions
-
Get the function computing mean obliquity of the ecliptic.
- getMeanObliquityFunction(TimeScales) - Method in enum org.orekit.utils.IERSConventions
-
Get the function computing mean obliquity of the ecliptic.
- getMeasurement() - Method in class org.orekit.files.ccsds.ndm.tdm.Observation
-
Getter for the measurement.
- getMeasurements() - Method in class org.orekit.estimation.measurements.MultiplexedMeasurement
-
Get the underlying measurements.
- getMeasurementsParametersDrivers(boolean) - Method in class org.orekit.estimation.leastsquares.BatchLSEstimator
-
Get the measurements parameters supported by this estimator (including measurements and modifiers).
- getMeasurementsParametersEvolution() - Method in class org.orekit.estimation.sequential.UnivariateProcessNoise
-
Getter for the measurementsParametersEvolution.
- getMeasurementType() - Method in class org.orekit.gnss.CombinedObservationData
-
Get the measurement type.
- getMeasurementType() - Method in enum org.orekit.gnss.ObservationType
-
Get the measurement type.
- getMedianDriver() - Method in class org.orekit.propagation.events.FieldParameterDrivenDateIntervalDetector
-
Get the driver for median date.
- getMedianDriver() - Method in class org.orekit.propagation.events.ParameterDrivenDateIntervalDetector
-
Get the driver for median date.
- getMelbourneWubbenaCombination(SatelliteSystem) - Static method in class org.orekit.estimation.measurements.gnss.MeasurementCombinationFactory
-
Get the Melbourne-Wübbena combination of measurements.
- getMercury() - Method in interface org.orekit.bodies.CelestialBodies
-
Get the Mercury singleton body.
- getMercury() - Static method in class org.orekit.bodies.CelestialBodyFactory
-
Get the Mercury singleton body.
- getMercury() - Method in class org.orekit.bodies.LazyLoadedCelestialBodies
-
- getMessage(Locale) - Method in interface org.orekit.errors.LocalizedException
-
Gets the message in a specified locale.
- getMessage(Locale) - Method in exception org.orekit.errors.OrekitException
-
Gets the message in a specified locale.
- getMessage() - Method in exception org.orekit.errors.OrekitException
- getMessage(Locale) - Method in exception org.orekit.errors.OrekitIllegalArgumentException
-
Gets the message in a specified locale.
- getMessage() - Method in exception org.orekit.errors.OrekitIllegalArgumentException
- getMessage(Locale) - Method in exception org.orekit.errors.OrekitIllegalStateException
-
Gets the message in a specified locale.
- getMessage() - Method in exception org.orekit.errors.OrekitIllegalStateException
- getMessage(Locale) - Method in exception org.orekit.errors.OrekitInternalError
-
Gets the message in a specified locale.
- getMessage() - Method in exception org.orekit.errors.OrekitInternalError
- getMessage(Locale) - Method in exception org.orekit.errors.OrekitIOException
-
Gets the message in a specified locale.
- getMessage() - Method in exception org.orekit.errors.OrekitIOException
- getMessage(Locale) - Method in exception org.orekit.errors.OrekitParseException
-
Gets the message in a specified locale.
- getMessage() - Method in exception org.orekit.errors.OrekitParseException
- getMessageId() - Method in class org.orekit.files.ccsds.section.Header
-
Get the ID that uniquely identifies a message from a given originator.
- getMessageType(String) - Method in class org.orekit.gnss.metric.parser.IgsSsrMessagesParser
-
Get the message type corresponding to the message number.
- getMessageType(String) - Static method in enum org.orekit.gnss.metric.parser.IgsSsrMessageType
-
Get the message type corresponding to a message number.
- getMessageType(String) - Method in class org.orekit.gnss.metric.parser.MessagesParser
-
Get the message type corresponding to the message number.
- getMessageType(String) - Method in class org.orekit.gnss.metric.parser.RtcmMessagesParser
-
Get the message type corresponding to the message number.
- getMessageType(String) - Static method in enum org.orekit.gnss.metric.parser.RtcmMessageType
-
Get the message type corresponding to a message number.
- getMetadata() - Method in class org.orekit.files.ccsds.ndm.adm.apm.Apm
-
Get the file metadata.
- getMetadata() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.CovarianceHistory
-
Get metadata.
- getMetadata() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistory
-
Get metadata.
- getMetadata() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Ocm
-
Get the metadata from the single
segment
.
- getMetadata() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistory
-
Get metadata.
- getMetadata() - Method in class org.orekit.files.ccsds.ndm.odm.omm.Omm
-
Get the file metadata.
- getMetadata() - Method in class org.orekit.files.ccsds.ndm.odm.opm.Opm
-
Get the file metadata.
- getMetadata() - Method in class org.orekit.files.ccsds.section.Segment
-
Get the segment metadata.
- getMeteo(AbsoluteDate) - Method in class org.orekit.files.ilrs.CRD.Meteo
-
Get the meteorological parameters at a given date.
- getMeteoData() - Method in class org.orekit.files.ilrs.CRD.CRDDataBlock
-
Get the meteorological data for the data block.
- getMeteorologicalId() - Method in class org.orekit.files.ilrs.CRDConfiguration.MeteorologicalConfiguration
-
Get the meteorological configuration ID.
- getMeteorologicalRecord() - Method in class org.orekit.files.ilrs.CRDConfiguration
-
Get the meteorological record.
- getMethod() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
-
Get orbit determination method.
- getMHzFrequency() - Method in enum org.orekit.gnss.Frequency
-
Get the value of the frequency in MHz.
- getMilliInWeek() - Method in class org.orekit.time.GNSSDate
-
Get the number of milliseconds since week start.
- getMinAlt() - Method in class org.orekit.models.earth.atmosphere.HarrisPriester
-
Get the minimal altitude for the model.
- getMinAreaForCollisionProbability() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
-
Get the minimum cross-sectional area for collision probability estimation purposes.
- getMinDate() - Method in class org.orekit.attitudes.AggregateBoundedAttitudeProvider
-
Get the first date of the range.
- getMinDate() - Method in interface org.orekit.attitudes.BoundedAttitudeProvider
-
Get the first date of the range.
- getMinDate() - Method in class org.orekit.attitudes.TabulatedLofOffset
-
Get the first date of the range.
- getMinDate() - Method in class org.orekit.attitudes.TabulatedProvider
-
Get the first date of the range.
- getMinDate() - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherData
-
Gets the available data range minimum date.
- getMinDate() - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherDataLoader
-
Gets the available data range minimum date.
- getMinDate() - Method in class org.orekit.models.earth.atmosphere.data.MarshallSolarActivityFutureEstimation
-
Gets the available data range minimum date.
- getMinDate() - Method in interface org.orekit.models.earth.atmosphere.DTM2000InputParameters
-
Gets the available data range minimum date.
- getMinDate() - Method in interface org.orekit.models.earth.atmosphere.JB2008InputParameters
-
Gets the available data range minimum date.
- getMinDate() - Method in interface org.orekit.models.earth.atmosphere.NRLMSISE00InputParameters
-
Gets the available data range minimum date.
- getMinDate() - Method in class org.orekit.propagation.analytical.AggregateBoundedPropagator
-
- getMinDate() - Method in class org.orekit.propagation.analytical.Ephemeris
-
Get the first date of the range.
- getMinDate() - Method in interface org.orekit.propagation.BoundedPropagator
-
Get the first date of the range.
- getMinDate() - Method in interface org.orekit.propagation.FieldBoundedPropagator
-
Get the first date of the range.
- getMinDate() - Method in class org.orekit.propagation.integration.FieldIntegratedEphemeris
-
Get the first date of the range.
- getMinDate() - Method in class org.orekit.propagation.integration.IntegratedEphemeris
-
Get the first date of the range.
- getMinElevation() - Method in class org.orekit.gnss.DOPComputer
-
Get the minimum elevation.
- getMinElevation() - Method in class org.orekit.propagation.events.ElevationDetector
-
Returns the currently configured minimum valid elevation value.
- getMinElevation() - Method in class org.orekit.propagation.events.FieldElevationDetector
-
Returns the currently configured minimum valid elevation value.
- getMinMeasurementNumber() - Method in class org.orekit.estimation.measurements.gnss.AbstractCycleSlipDetector
-
Get the minimum number of measurement needed before being able to figure out cycle-slip occurrence.
- getMinPredictedEigenMin() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
-
Get minimum predicted minor eigenvalue of 1σ positional error ellipsoid over entire time span of the OCM.
- getMinRcs() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
-
Get the minimum radar cross-section.
- getMinute() - Method in class org.orekit.time.TimeComponents
-
Get the minute number.
- getMinutesFromUTC() - Method in class org.orekit.time.TimeComponents
-
Get the offset between the specified date and UTC.
- getMinValue() - Method in class org.orekit.utils.ParameterDriver
-
Get minimum parameter value.
- getMisc() - Method in class org.orekit.gnss.metric.ntrip.Record
-
Get miscellaneous information.
- getMissionReferenceDate() - Method in class org.orekit.files.ccsds.ndm.AbstractBuilder
-
Get the mission reference date or Mission Elapsed Time or Mission Relative Time time systems.
- getMissionReferenceDate() - Method in class org.orekit.files.ccsds.ndm.adm.AdmParser
-
Get reference date for Mission Elapsed Time and Mission Relative Time time systems.
- getMissionReferenceDate() - Method in class org.orekit.files.ccsds.ndm.odm.OdmParser
-
Get reference date for Mission Elapsed Time and Mission Relative Time time systems.
- getMjd() - Method in class org.orekit.frames.EOPEntry
-
Get the entry date (modified julian day, 00h00 UTC scale).
- getMJD() - Method in class org.orekit.time.DateComponents
-
Get the modified julian day.
- getMJD() - Method in class org.orekit.time.UTCTAIOffset
-
Get the date of the start of the leap as Modified Julian Day.
- getMJDRef() - Method in class org.orekit.time.OffsetModel
-
Get the reference date of the linear model as a modified julian day.
- getMoa() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseralContext
-
Get μ / a .
- getMoa() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTTesseralContext
-
Get μ / a .
- getMOD(boolean) - Method in class org.orekit.frames.AbstractFrames
-
- getMOD(IERSConventions) - Method in class org.orekit.frames.AbstractFrames
-
- getMOD(boolean) - Method in interface org.orekit.frames.Frames
-
Get the MOD reference frame.
- getMOD(IERSConventions) - Method in interface org.orekit.frames.Frames
-
Get the MOD reference frame.
- getMOD(boolean) - Static method in class org.orekit.frames.FramesFactory
-
Get the MOD reference frame.
- getMOD(IERSConventions) - Static method in class org.orekit.frames.FramesFactory
-
Get the MOD reference frame.
- getMode() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
-
Getter for the mode.
- getModel() - Method in class org.orekit.propagation.conversion.AbstractPropagatorConverter
-
Get the Jacobian of the function computing position/velocity at sample points.
- getModel() - Method in class org.orekit.propagation.conversion.FiniteDifferencePropagatorConverter
-
Get the Jacobian of the function computing position/velocity at sample points.
- getModel() - Method in class org.orekit.propagation.conversion.JacobianPropagatorConverter
-
Get the Jacobian of the function computing position/velocity at sample points.
- getModelName() - Method in class org.orekit.models.earth.GeoMagneticField
-
Returns the model name.
- getModels() - Method in class org.orekit.models.earth.GeoMagneticModelLoader
-
- getModifiedJulianEpoch() - Method in class org.orekit.time.AbstractTimeScales
-
- getModifiedJulianEpoch(Field<T>) - Static method in class org.orekit.time.FieldAbsoluteDate
-
Reference epoch for modified julian dates: 1858-11-17T00:00:00 Terrestrial Time.
- getModifiedJulianEpoch() - Method in interface org.orekit.time.TimeScales
-
Reference epoch for modified julian dates: 1858-11-17T00:00:00 Terrestrial Time.
- getModifiedRodrigues(double) - Method in class org.orekit.utils.AngularCoordinates
-
Convert rotation, rate and acceleration to modified Rodrigues vector and derivatives.
- getModifiedRodrigues(double) - Method in class org.orekit.utils.FieldAngularCoordinates
-
Convert rotation, rate and acceleration to modified Rodrigues vector and derivatives.
- getModifiers() - Method in class org.orekit.estimation.measurements.AbstractMeasurement
-
Get the modifiers that apply to a measurement.
- getModifiers() - Method in class org.orekit.estimation.measurements.generation.AbstractMeasurementBuilder
-
Get the modifiers that apply to a measurement.
- getModifiers() - Method in interface org.orekit.estimation.measurements.generation.MeasurementBuilder
-
Get the modifiers that apply to a measurement.
- getModifiers() - Method in interface org.orekit.estimation.measurements.ObservedMeasurement
-
Get the modifiers that apply to a measurement.
- getMomentum() - Method in class org.orekit.utils.FieldPVCoordinates
-
Gets the momentum.
- getMomentum() - Method in class org.orekit.utils.PVCoordinates
-
Gets the momentum.
- getMonth() - Method in class org.orekit.time.DateComponents
-
Get the month.
- getMonth(int) - Static method in enum org.orekit.time.Month
-
Get the month corresponding to a number.
- getMonthEnum() - Method in class org.orekit.time.DateComponents
-
Get the month as an enumerate.
- getMoon() - Method in interface org.orekit.bodies.CelestialBodies
-
Get the Moon singleton body.
- getMoon() - Static method in class org.orekit.bodies.CelestialBodyFactory
-
Get the Moon singleton body.
- getMoon() - Method in class org.orekit.bodies.LazyLoadedCelestialBodies
-
- getMoonSemiMajorAxis() - Static method in class org.orekit.propagation.numerical.cr3bp.CR3BPConstants
-
Get the Moon semi-major axis.
- getMountPoint() - Method in class org.orekit.gnss.metric.ntrip.DataStreamRecord
-
Get the mount point.
- getMu() - Method in class org.orekit.files.ccsds.ndm.odm.KeplerianElements
-
Get the gravitational coefficient.
- getMu() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmSatelliteEphemeris
-
Get the standard gravitational parameter for the satellite.
- getMu() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistory
-
Get the standard gravitational parameter for the satellite.
- getMu() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemSatelliteEphemeris
-
Get the standard gravitational parameter for the satellite.
- getMu() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemSegment
-
Get the standard gravitational parameter for the satellite.
- getMu() - Method in class org.orekit.files.ccsds.ndm.ParserBuilder
-
Get the gravitational coefficient.
- getMu() - Method in interface org.orekit.files.general.EphemerisFile.EphemerisSegment
-
Get the standard gravitational parameter for the satellite.
- getMu() - Method in interface org.orekit.files.general.EphemerisFile.SatelliteEphemeris
-
Get the standard gravitational parameter for the satellite.
- getMu() - Method in class org.orekit.files.general.OrekitEphemerisFile.OrekitEphemerisSegment
-
Get the standard gravitational parameter for the satellite.
- getMu() - Method in class org.orekit.files.general.OrekitEphemerisFile.OrekitSatelliteEphemeris
-
Get the standard gravitational parameter for the satellite.
- getMu() - Method in class org.orekit.files.ilrs.CPF.CPFEphemeris
-
Get the standard gravitational parameter for the satellite.
- getMu() - Method in class org.orekit.files.sp3.SP3.SP3Ephemeris
-
- getMu() - Method in class org.orekit.forces.gravity.HolmesFeatherstoneAttractionModel
-
Get the central attraction coefficient μ.
- getMu() - Method in class org.orekit.forces.gravity.NewtonianAttraction
-
Get the central attraction coefficient μ.
- getMu(Field<T>) - Method in class org.orekit.forces.gravity.NewtonianAttraction
-
Get the central attraction coefficient μ.
- getMu() - Method in class org.orekit.forces.gravity.potential.CachedNormalizedSphericalHarmonicsProvider
-
Get the central body attraction coefficient.
- getMu() - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
-
Get the central body attraction coefficient.
- getMu() - Method in interface org.orekit.forces.gravity.potential.SphericalHarmonicsProvider
-
Get the central body attraction coefficient.
- getMu() - Method in class org.orekit.orbits.FieldOrbit
-
Get the central attraction coefficient used for position and velocity conversions (m³/s²).
- getMu() - Method in class org.orekit.orbits.Orbit
-
Get the central acceleration constant.
- getMu() - Method in class org.orekit.propagation.analytical.BrouwerLyddanePropagator
-
Get the central attraction coefficient μ.
- getMu() - Method in class org.orekit.propagation.analytical.EcksteinHechlerPropagator
-
Get the central attraction coefficient μ.
- getMu() - Method in class org.orekit.propagation.analytical.gnss.data.CommonGnssData
-
Getter for the Earth's universal gravitational parameter.
- getMu() - Method in interface org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElements
-
Gets the Earth's universal gravitational parameter.
- getMU() - Static method in class org.orekit.propagation.analytical.gnss.GLONASSAnalyticalPropagator
-
Get the Earth gravity coefficient used for GLONASS propagation.
- getMU() - Method in class org.orekit.propagation.analytical.gnss.GNSSPropagator
-
Gets the Earth gravity coefficient used for GNSS propagation.
- getMU() - Method in class org.orekit.propagation.analytical.gnss.SBASPropagator
-
Get the Earth gravity coefficient used for SBAS propagation.
- getMU() - Static method in class org.orekit.propagation.analytical.tle.FieldTLEPropagator
-
Get the Earth gravity coefficient used for TLE propagation.
- getMU() - Static method in class org.orekit.propagation.analytical.tle.TLEPropagator
-
Get the Earth gravity coefficient used for TLE propagation.
- getMu() - Method in class org.orekit.propagation.conversion.AbstractPropagatorBuilder
-
Get the central attraction coefficient (µ - m³/s²) value.
- getMu() - Method in class org.orekit.propagation.FieldSpacecraftState
-
Get the central attraction coefficient.
- getMu() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
-
Get the central attraction coefficient μ.
- getMu() - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator
-
Get the central attraction coefficient μ.
- getMu() - Method in class org.orekit.propagation.integration.FieldStateMapper
-
Get the central attraction coefficient μ.
- getMu() - Method in class org.orekit.propagation.integration.StateMapper
-
Get the central attraction coefficient μ.
- getMu() - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContributionContext
-
Get central attraction coefficient.
- getMu() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTNewtonianAttraction
-
Get the central attraction coefficient μ.
- getMu() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldAbstractGaussianContributionContext
-
Get central attraction coefficient.
- getMu() - Method in class org.orekit.propagation.SpacecraftState
-
Get the central attraction coefficient.
- getMultiplexer() - Method in class org.orekit.propagation.AbstractPropagator
-
Get the multiplexer holding all step handlers.
- getMultiplexer() - Method in class org.orekit.propagation.FieldAbstractPropagator
-
Get the multiplexer holding all step handlers.
- getMultiplexer() - Method in interface org.orekit.propagation.FieldPropagator
-
Get the multiplexer holding all step handlers.
- getMultiplexer() - Method in interface org.orekit.propagation.Propagator
-
Get the multiplexer holding all step handlers.
- getMuoa() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonalContext
-
Get μ / a .
- getMuoa() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTZonalContext
-
Get μ / a .
- getMuoR3() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBodyContext
-
Get muoR3 = mu3 / R3.
- getMuoR3() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTThirdBodyContext
-
Get muoR3 = mu3 / R3.
- getMuSet() - Method in class org.orekit.files.ccsds.ndm.odm.OdmParser
-
Get the gravitational coefficient set at construction.
- getN() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.CoefficientsFactory.NSKey
-
Get n.
- getN4() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data
-
Get the four-year interval number starting from 1996.
- getN4() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSAlmanac
-
- getN4() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSEphemeris
-
- getN4() - Method in interface org.orekit.propagation.analytical.gnss.data.GLONASSOrbitalElements
-
Get the number of the current four year interval.
- getNA() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data
-
Get the GLONASS NA Word.
- getNa() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSAlmanac
-
- getNa() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSEphemeris
-
- getNa() - Method in interface org.orekit.propagation.analytical.gnss.data.GLONASSOrbitalElements
-
Get the number of the current day in a four year interval.
- getNadir() - Method in class org.orekit.bodies.FieldGeodeticPoint
-
Get the direction below the point, expressed in parent shape frame.
- getNadir() - Method in class org.orekit.bodies.GeodeticPoint
-
Get the direction below the point, expressed in parent shape frame.
- getNadir() - Method in class org.orekit.frames.TopocentricFrame
-
Get the nadir direction of topocentric frame, expressed in parent shape frame.
- getName() - Method in interface org.orekit.bodies.CelestialBody
-
Get the name of the body.
- getName() - Method in class org.orekit.bodies.CR3BPSystem
-
Get the name of the CR3BP system.
- getName() - Method in class org.orekit.compiler.plugin.DefaultDataContextPlugin
-
- getName() - Method in class org.orekit.data.DataSource
-
Get the name of the data.
- getName() - Method in class org.orekit.estimation.measurements.gnss.AbstractDualFrequencyCombination
-
Get the name of the combination of measurements.
- getName() - Method in class org.orekit.estimation.measurements.gnss.AbstractSingleFrequencyCombination
-
Get the name of the combination of measurements.
- getName() - Method in enum org.orekit.estimation.measurements.gnss.CombinationType
-
Get the name of the combination of measurements.
- getName() - Method in interface org.orekit.estimation.measurements.gnss.MeasurementCombination
-
Get the name of the combination of measurements.
- getName() - Method in class org.orekit.estimation.measurements.gnss.MelbourneWubbenaCombination
-
Get the name of the combination of measurements.
- getName() - Method in class org.orekit.files.ccsds.definitions.BodyFacade
-
Get the CCSDS name for the body.
- getName() - Method in enum org.orekit.files.ccsds.definitions.CelestialBodyFrame
-
Get the name of celestial body frame.
- getName() - Method in class org.orekit.files.ccsds.definitions.FrameFacade
-
Get the CCSDS name for the frame.
- getName() - Method in class org.orekit.files.ccsds.definitions.OdMethodFacade
-
Get the name of the method.
- getName() - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken
-
Get the name of the block or entry.
- getName() - Method in class org.orekit.files.ilrs.ILRSHeader
-
Get the satellite target name.
- getName() - Method in enum org.orekit.files.sinex.Station.ReferenceSystem
-
Get the name used to define the reference system in SINEX file.
- getName() - Method in class org.orekit.forces.maneuvers.jacobians.Duration
-
Get the name of the additional state.
- getName() - Method in class org.orekit.forces.maneuvers.jacobians.MassDepletionDelay
-
Get the name of the additional derivatives (which will become state once integrated).
- getName() - Method in class org.orekit.forces.maneuvers.jacobians.MedianDate
-
Get the name of the additional state.
- getName() - Method in class org.orekit.forces.maneuvers.jacobians.TriggerDate
-
Get the name of the additional state.
- getName() - Method in class org.orekit.forces.maneuvers.Maneuver
-
Get the name of the maneuver.
- getName() - Method in class org.orekit.forces.maneuvers.propulsion.AbstractConstantThrustPropulsionModel
-
Get the maneuver name.
- getName() - Method in interface org.orekit.forces.maneuvers.propulsion.PropulsionModel
-
Get the maneuver name.
- getName() - Method in class org.orekit.forces.maneuvers.trigger.DateBasedManeuverTriggers
-
Get the maneuver name.
- getName() - Method in interface org.orekit.forces.maneuvers.trigger.ManeuverTriggers
-
Get the maneuver name.
- getName() - Method in class org.orekit.frames.Frame
-
Get the name.
- getName() - Method in enum org.orekit.frames.ITRFVersion
-
Get the name the frame version.
- getName() - Method in enum org.orekit.frames.Predefined
-
Get the name of the frame.
- getName() - Method in enum org.orekit.gnss.antenna.SatelliteType
-
Get the IGS name for the antenna code.
- getName() - Method in class org.orekit.gnss.clock.RinexClock.ClockDataLine
-
Getter for the receiver/satellite name.
- getName() - Method in enum org.orekit.gnss.Frequency
-
Get the RINEX name for the frequency.
- getName() - Method in interface org.orekit.propagation.AdditionalStateProvider
-
Get the name of the additional state.
- getName() - Method in class org.orekit.propagation.analytical.gnss.ClockCorrectionsProvider
-
Get the name of the additional state.
- getName() - Method in class org.orekit.propagation.analytical.tle.TLEPartialDerivativesEquations
-
Deprecated.
Get the name of the additional state.
- getName() - Method in interface org.orekit.propagation.FieldAdditionalStateProvider
-
Get the name of the additional state.
- getName() - Method in class org.orekit.propagation.integration.AbstractJacobiansMapper
-
Get the name of the partial Jacobians.
- getName() - Method in interface org.orekit.propagation.integration.AdditionalDerivativesProvider
-
Get the name of the additional derivatives (which will become state once integrated).
- getName() - Method in interface org.orekit.propagation.integration.AdditionalEquations
-
Deprecated.
Get the name of the additional state.
- getName() - Method in class org.orekit.propagation.integration.AdditionalEquationsAdapter
-
Deprecated.
Get the name of the additional derivatives (which will become state once integrated).
- getName() - Method in interface org.orekit.propagation.integration.FieldAdditionalDerivativesProvider
-
Get the name of the additional derivatives (which will become state once integrated).
- getName() - Method in interface org.orekit.propagation.integration.FieldAdditionalEquations
-
Deprecated.
Get the name of the additional state.
- getName() - Method in class org.orekit.propagation.integration.FieldAdditionalEquationsAdapter
-
Deprecated.
Get the name of the additional derivatives (which will become state once integrated).
- getName() - Method in class org.orekit.propagation.numerical.cr3bp.STMEquations
-
Get the name of the additional derivatives (which will become state once integrated).
- getName() - Method in class org.orekit.propagation.numerical.EpochDerivativesEquations
-
Get the name of the additional derivatives (which will become state once integrated).
- getName() - Method in class org.orekit.propagation.numerical.PartialDerivativesEquations
-
Deprecated.
Get the name of the additional derivatives (which will become state once integrated).
- getName() - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPartialDerivativesEquations
-
Deprecated.
Get the name of the additional derivatives (which will become state once integrated).
- getName() - Method in class org.orekit.time.BDTScale
-
Get the name time scale.
- getName() - Method in class org.orekit.time.GalileoScale
-
Get the name time scale.
- getName() - Method in class org.orekit.time.GLONASSScale
-
Get the name time scale.
- getName() - Method in class org.orekit.time.GMSTScale
-
Get the name time scale.
- getName() - Method in class org.orekit.time.GPSScale
-
Get the name time scale.
- getName() - Method in class org.orekit.time.IRNSSScale
-
Get the name time scale.
- getName() - Method in class org.orekit.time.QZSSScale
-
Get the name time scale.
- getName() - Method in class org.orekit.time.SatelliteClockScale
-
Get the name time scale.
- getName() - Method in class org.orekit.time.TAIScale
-
Get the name time scale.
- getName() - Method in class org.orekit.time.TCBScale
-
Get the name time scale.
- getName() - Method in class org.orekit.time.TCGScale
-
Get the name time scale.
- getName() - Method in class org.orekit.time.TDBScale
-
Get the name time scale.
- getName() - Method in interface org.orekit.time.TimeScale
-
Get the name time scale.
- getName() - Method in class org.orekit.time.TTScale
-
Get the name time scale.
- getName() - Method in class org.orekit.time.UT1Scale
-
Get the name time scale.
- getName() - Method in class org.orekit.time.UTCScale
-
Get the name time scale.
- getName() - Method in class org.orekit.utils.ParameterDriver
-
Get name.
- getName() - Method in class org.orekit.utils.units.Unit
-
Get the name of the unit.
- getNarrowLaneCombination(SatelliteSystem) - Static method in class org.orekit.estimation.measurements.gnss.MeasurementCombinationFactory
-
Get the Narrow-Lane combination of measurements.
- getNavigationSystem(String) - Static method in enum org.orekit.gnss.metric.ntrip.NavigationSystem
-
Get the navigation system corresponding to a keyword.
- getNavigationSystems() - Method in class org.orekit.gnss.metric.ntrip.DataStreamRecord
-
Get the navigation systems.
- getNbManeuvers() - Method in class org.orekit.files.ccsds.ndm.adm.apm.ApmData
-
Get the number of maneuvers present in the APM.
- getNbManeuvers() - Method in class org.orekit.files.ccsds.ndm.odm.opm.Opm
-
Get the number of maneuvers present in the OPM.
- getNbManeuvers() - Method in class org.orekit.files.ccsds.ndm.odm.opm.OpmData
-
Get the number of maneuvers present in the APM.
- getNBodyPerturbations() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
-
Get n-body perturbation bodies.
- getNbParams() - Method in class org.orekit.utils.ParameterDriversList
-
Get the number of parameters with different names.
- getNbSpecies() - Method in class org.orekit.models.earth.displacement.OceanLoadingCoefficients
-
Get the number of species.
- getNbTides(int) - Method in class org.orekit.models.earth.displacement.OceanLoadingCoefficients
-
Get the number of tides for one species.
- getNeighbors(AbsoluteDate) - Method in class org.orekit.frames.EOPHistory
-
Get the entries surrounding a central date.
- getNeighbors(AbsoluteDate) - Method in class org.orekit.utils.GenericTimeStampedCache
-
Get the entries surrounding a central date.
- getNeighbors(AbsoluteDate) - Method in class org.orekit.utils.ImmutableTimeStampedCache
-
Get the entries surrounding a central date.
- getNeighbors(AbsoluteDate) - Method in interface org.orekit.utils.TimeStampedCache
-
Get the entries surrounding a central date.
- getNeighborsSize() - Method in class org.orekit.utils.GenericTimeStampedCache
-
- getNeighborsSize() - Method in class org.orekit.utils.ImmutableTimeStampedCache
-
- getNeighborsSize() - Method in interface org.orekit.utils.TimeStampedCache
-
- getNeptune() - Method in interface org.orekit.bodies.CelestialBodies
-
Get the Neptune singleton body.
- getNeptune() - Static method in class org.orekit.bodies.CelestialBodyFactory
-
Get the Neptune singleton body.
- getNeptune() - Method in class org.orekit.bodies.LazyLoadedCelestialBodies
-
- getNeQuickAlpha() - Method in class org.orekit.gnss.navigation.RinexNavigation
-
Get the "alpha" ionospheric parameters.
- getNetwork() - Method in class org.orekit.gnss.metric.ntrip.DataStreamRecord
-
Get the network.
- getNetworkIdentifier() - Method in class org.orekit.gnss.metric.ntrip.NetworkRecord
-
Get the network identifier.
- getNetworkInfoAddress() - Method in class org.orekit.gnss.metric.ntrip.NetworkRecord
-
Get the web address for network information.
- getNetworks() - Method in class org.orekit.gnss.metric.ntrip.SourceTable
-
Get the networks records.
- getNewSlotQuantumGap() - Method in class org.orekit.utils.GenericTimeStampedCache
-
Get quantum gap above which a new slot is created instead of extending an existing one.
- getNewState() - Method in class org.orekit.propagation.events.EventState.EventOccurrence
-
Get the new state for a reset action.
- getNewState() - Method in class org.orekit.propagation.events.FieldEventState.EventOccurrence
-
Get the new state for a reset action.
- getNextMessageEpoch() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
-
Get the creation date of next message from a given originator.
- getNextMessageID() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
-
Get the unique ID identifying next message from a given originator.
- getNode(AbsoluteDate) - Method in interface org.orekit.bodies.IAUPole
-
Get the body Q Node direction in ICRF frame.
- getNode(FieldAbsoluteDate<T>) - Method in interface org.orekit.bodies.IAUPole
-
Get the body Q Node direction in ICRF frame.
- getNoise() - Method in class org.orekit.estimation.measurements.generation.AbstractMeasurementBuilder
-
Generate a noise vector.
- getNominalFireRate() - Method in class org.orekit.files.ilrs.CRDConfiguration.LaserConfiguration
-
Get the nominal fire rate.
- getNominalTidalDisplacement() - Method in enum org.orekit.utils.IERSConventions
-
Get the nominal values of the displacement numbers.
- getNonInterpolatingEOPHistory() - Method in class org.orekit.frames.EOPHistory
-
Get non-interpolating version of the instance.
- getNonInterpolatingProvider() - Method in interface org.orekit.frames.EOPBasedTransformProvider
-
Get a version of the provider that does not cache tidal corrections.
- getNonInterpolatingProvider() - Method in class org.orekit.frames.GTODProvider
-
Get a version of the provider that does not cache tidal corrections.
- getNonInterpolatingTransform(Frame, Frame, AbsoluteDate) - Static method in class org.orekit.frames.FramesFactory
-
Get the transform between two frames, suppressing all interpolation.
- getNonInterpolatingTransform(Frame, Frame, FieldAbsoluteDate<T>) - Static method in class org.orekit.frames.FramesFactory
-
Get the transform between two frames, suppressing all interpolation.
- getNonPolynomialSize() - Method in class org.orekit.data.PoissonSeries
-
Get the number of different terms in the non-polynomial part.
- getNonRotatinOriginNutationCorrection(AbsoluteDate) - Method in class org.orekit.frames.EOPHistory
-
Get the correction to the nutation parameters for Non-Rotating Origin paradigm.
- getNonRotatinOriginNutationCorrection(FieldAbsoluteDate<T>) - Method in class org.orekit.frames.EOPHistory
-
Get the correction to the nutation parameters for Non-Rotating Origin paradigm.
- getNoradID() - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmTle
-
Get the NORAD Catalog Number ("Satellite Number").
- getNoradId() - Method in class org.orekit.files.ilrs.ILRSHeader
-
Get the satellite NORAD ID (i.e.
- getNormal() - Method in class org.orekit.forces.BoxAndSolarArraySpacecraft.Facet
-
Get unit normal vector.
- getNormal(AbsoluteDate, Frame, Vector3D, Rotation) - Method in class org.orekit.forces.BoxAndSolarArraySpacecraft
-
Get solar array normal in spacecraft frame.
- getNormal(FieldAbsoluteDate<T>, Frame, FieldVector3D<T>, FieldRotation<T>) - Method in class org.orekit.forces.BoxAndSolarArraySpacecraft
-
Get solar array normal in spacecraft frame.
- getNormalGravity(double) - Method in class org.orekit.models.earth.ReferenceEllipsoid
-
Gets the normal gravity, that is gravity just due to the reference
ellipsoid's potential.
- getNormalizedCnm(int, int) - Method in interface org.orekit.forces.gravity.potential.NormalizedSphericalHarmonicsProvider.NormalizedSphericalHarmonics
-
Get a spherical harmonic cosine coefficient.
- getNormalizedProvider(int, int) - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory
-
Get the gravity field coefficients provider from the first supported file.
- getNormalizedProvider(double, double, TideSystem, double[][], double[][]) - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory
-
- getNormalizedProvider(UnnormalizedSphericalHarmonicsProvider) - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory
-
- getNormalizedProvider(int, int) - Method in interface org.orekit.forces.gravity.potential.GravityFields
-
Get a gravity field normalized coefficients provider.
- getNormalizedProvider(int, int) - Method in class org.orekit.forces.gravity.potential.LazyLoadedGravityFields
-
Get a gravity field normalized coefficients provider.
- getNormalizedSnm(int, int) - Method in interface org.orekit.forces.gravity.potential.NormalizedSphericalHarmonicsProvider.NormalizedSphericalHarmonics
-
Get a spherical harmonic sine coefficient.
- getNormalizedValue() - Method in class org.orekit.utils.ParameterDriver
-
Get normalized value.
- getNorth() - Method in class org.orekit.bodies.FieldGeodeticPoint
-
Get the direction to the north of point, expressed in parent shape frame.
- getNorth() - Method in class org.orekit.bodies.GeodeticPoint
-
Get the direction to the north of point, expressed in parent shape frame.
- getNorth() - Method in class org.orekit.frames.TopocentricFrame
-
Get the north direction of topocentric frame, expressed in parent shape frame.
- getNorthOffsetDriver() - Method in class org.orekit.estimation.measurements.GroundStation
-
Get a driver allowing to change station position along North axis.
- getNt() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data
-
Get the current date.
- getNtripFlags() - Method in class org.orekit.gnss.metric.ntrip.SourceTable
-
Get the flags set by server.
- getNumber() - Method in interface org.orekit.estimation.measurements.EstimationsProvider
-
Get the number of evaluations available.
- getNumber() - Method in enum org.orekit.time.Month
-
Get the month number.
- getNumberOfBiasesProcessed() - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm05Data
-
Get the number of biases processed for the current satellite.
- getNumberOfBiasesProcessed() - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm06Data
-
Get the number of biases processed for the current satellite.
- getNumberOfClockDataTypes() - Method in class org.orekit.gnss.clock.RinexClock
-
Get the number of different clock data types in the file.
- getNumberOfConstraints() - Method in class org.orekit.utils.AbstractMultipleShooting
-
Get the number of constraints.
- getNumberOfEpochs() - Method in class org.orekit.files.sp3.SP3
-
Returns the number of epochs contained in this orbit file.
- getNumberOfFreeEpoch() - Method in class org.orekit.utils.AbstractMultipleShooting
-
Get the number of free epoch.
- getNumberOfFreeVariables() - Method in class org.orekit.utils.AbstractMultipleShooting
-
Get the number of free variables.
- getNumberOfIonosphericLayers() - Method in class org.orekit.gnss.metric.messages.ssr.subtype.SsrIm201Header
-
Get the number of ionospheric layers.
- getNumberOfLeapSeconds() - Method in class org.orekit.gnss.clock.RinexClock
-
Getter for the number of leap seconds.
- getNumberOfLeapSeconds() - Method in class org.orekit.gnss.navigation.RinexNavigation
-
Getter for the current number of leap seconds.
- getNumberOfLeapSecondsGNSS() - Method in class org.orekit.gnss.clock.RinexClock
-
Getter for the number of leap second for GNSS time scales.
- getNumberOfReceivers() - Method in class org.orekit.gnss.clock.RinexClock
-
Get the number of receivers that are considered in the file.
- getNumberOfSatellites() - Method in class org.orekit.gnss.clock.RinexClock
-
Get the number of satellites that are considered in the file.
- getNumberOfSatellites() - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgmHeader
-
Get the number of satellites for the current IGM message.
- getNumberOfValues() - Method in class org.orekit.gnss.clock.RinexClock.ClockDataLine
-
Getter for the number of values to follow.
- getNutation() - Method in class org.orekit.files.ccsds.ndm.adm.apm.SpinStabilized
-
Get the nutation angle of spin axis (rad).
- getNutationArguments(TimeScales) - Method in enum org.orekit.utils.IERSConventions
-
Get the fundamental nutation arguments.
- getNutationArguments(TimeScale) - Method in enum org.orekit.utils.IERSConventions
-
Get the fundamental nutation arguments.
- getNutationArguments(TimeScale, TimeScales) - Method in enum org.orekit.utils.IERSConventions
-
Get the fundamental nutation arguments.
- getNutationCorrectionConverter() - Method in enum org.orekit.utils.IERSConventions
-
Create a function converting nutation corrections between
δX/δY and δΔψ/δΔε.
- getNutationCorrectionConverter(TimeScales) - Method in enum org.orekit.utils.IERSConventions
-
Create a function converting nutation corrections between
δX/δY and δΔψ/δΔε.
- getNutationFunction() - Method in enum org.orekit.utils.IERSConventions
-
Get the function computing the nutation angles.
- getNutationFunction(TimeScales) - Method in enum org.orekit.utils.IERSConventions
-
Get the function computing the nutation angles.
- getNutationPeriod() - Method in class org.orekit.files.ccsds.ndm.adm.apm.SpinStabilized
-
Get the body nutation period of the spin axis (s).
- getNutationPhase() - Method in class org.orekit.files.ccsds.ndm.adm.apm.SpinStabilized
-
Get the inertial nutation phase (rad).
- getNutationReferenceEpoch() - Method in enum org.orekit.utils.IERSConventions
-
Get the reference epoch for fundamental nutation arguments.
- getNutationReferenceEpoch(TimeScales) - Method in enum org.orekit.utils.IERSConventions
-
Get the reference epoch for fundamental nutation arguments.
- getObjectDesignator() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
-
Get the unique satellite identification designator for the object.
- getObjectID() - Method in class org.orekit.files.ccsds.ndm.adm.AdmMetadata
-
Get the spacecraft ID for which the attitude data are provided.
- getObjectID() - Method in class org.orekit.files.ccsds.ndm.odm.CommonMetadata
-
Get the spacecraft ID for which the orbit state is provided.
- getObjectiveFunction() - Method in class org.orekit.propagation.conversion.AbstractPropagatorConverter
-
Get the function computing position/velocity at sample points.
- getObjectiveFunction() - Method in class org.orekit.propagation.conversion.FiniteDifferencePropagatorConverter
-
Get the function computing position/velocity at sample points.
- getObjectiveFunction() - Method in class org.orekit.propagation.conversion.JacobianPropagatorConverter
-
Get the function computing position/velocity at sample points.
- getObjectName() - Method in class org.orekit.files.ccsds.ndm.adm.AdmMetadata
-
Get the spacecraft name for which the attitude data are provided.
- getObjectName() - Method in class org.orekit.files.ccsds.ndm.odm.OdmMetadata
-
Get the spacecraft name for which the orbit state is provided.
- getObjectType() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
-
Get the type of object.
- getOblateFlattening() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
-
Get central body oblate spheroid oblateness.
- getObsAvailable() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
-
Get number of observations available within the actual OD span.
- getObservationCode() - Method in class org.orekit.gnss.RinexObservationHeader
-
Get the observation code of the average phasecenter position w/r to antenna reference point.
- getObservationData() - Method in class org.orekit.gnss.CombinedObservationDataSet
-
Get list of observation data.
- getObservationData() - Method in class org.orekit.gnss.ObservationDataSet
-
Get list of observation data.
- getObservationDataSets() - Method in class org.orekit.gnss.RinexObservationLoader
-
Get parsed rinex observations data sets.
- getObservations() - Method in class org.orekit.files.ccsds.ndm.tdm.ObservationsBlock
-
Get the list of Observations data lines.
- getObservationType() - Method in class org.orekit.gnss.ObservationData
-
Get the observation type.
- getObservedMeasurement() - Method in class org.orekit.estimation.measurements.EstimatedMeasurement
-
Get the associated observed measurement.
- getObservedMeasurement() - Method in class org.orekit.estimation.sequential.MeasurementDecorator
-
Get the observed measurement.
- getObservedValue() - Method in class org.orekit.estimation.measurements.AbstractMeasurement
-
Get the observed value.
- getObservedValue() - Method in interface org.orekit.estimation.measurements.ComparableMeasurement
-
Get the observed value.
- getObservedValue() - Method in class org.orekit.estimation.measurements.EstimatedMeasurement
-
Get the observed value.
- getObserver() - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanModel
-
Get the observer for Kalman Filter estimations.
- getObserver() - Method in class org.orekit.propagation.events.AngularSeparationDetector
-
Get the observer for the spacecraft.
- getObserverName() - Method in class org.orekit.gnss.RinexObservationHeader
-
Get name of the observer.
- getObservers() - Method in class org.orekit.utils.ParameterDriver
-
Get the observers for this driver.
- getObsUsed() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
-
Get number of observations accepted within the actual OD span.
- getOcculted() - Method in class org.orekit.propagation.events.EclipseDetector
-
Getter for the occulted body.
- getOcculted() - Method in class org.orekit.propagation.events.FieldEclipseDetector
-
Get the occulted body.
- getOccultedRadius() - Method in class org.orekit.propagation.events.EclipseDetector
-
Getter for the occultedRadius.
- getOccultedRadius() - Method in class org.orekit.propagation.events.FieldEclipseDetector
-
Get the occulted body radius (m).
- getOcculting() - Method in class org.orekit.propagation.events.EclipseDetector
-
Getter for the occulting body.
- getOcculting() - Method in class org.orekit.propagation.events.FieldEclipseDetector
-
Get the occulting body.
- getOccultingRadius() - Method in class org.orekit.propagation.events.FieldEclipseDetector
-
Get the occulting body radius (m).
- getOceanLoadDeformationCoefficients() - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory
-
Get the configured ocean load deformation coefficients.
- getOceanLoadDeformationCoefficients() - Method in class org.orekit.forces.gravity.potential.LazyLoadedGravityFields
-
Get the configured ocean load deformation coefficients.
- getOceanPoleTide(EOPHistory) - Method in enum org.orekit.utils.IERSConventions
-
Get the function computing ocean pole tide (ΔC₂₁, ΔS₂₁).
- getOceanTidesModel() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
-
Get ocean tides model.
- getOceanTidesWaves(int, int) - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory
-
Get the ocean tides waves from the first supported file.
- getOceanTidesWaves(int, int) - Method in interface org.orekit.forces.gravity.potential.GravityFields
-
Get the ocean tides waves.
- getOceanTidesWaves(int, int) - Method in class org.orekit.forces.gravity.potential.LazyLoadedGravityFields
-
Get the ocean tides waves.
- getOcmDataElements() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
-
Get the list of elements of information data blocks included in this message.
- getOebAreaAlongIntermediate() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
-
Get the cross-sectional area of Optimally Enclosing Box along Y-OEB.
- getOebAreaAlongMax() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
-
Get the cross-sectional area of Optimally Enclosing Box along X-OEB.
- getOebAreaAlongMin() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
-
Get the cross-sectional area of Optimally Enclosing Box along Z-OEB.
- getOebIntermediate() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
-
Get the dimensions of Optimally Enclosing Box along Y-OEB (i.e intermediate).
- getOebMax() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
-
Get the dimensions of Optimally Enclosing Box along X-OEB (i.e max).
- getOebMin() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
-
Get the dimensions of Optimally Enclosing Box along Z-OEB (i.e min).
- getOebParentFrame() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
-
Get the Optimally Enclosing Box parent reference frame.
- getOebParentFrameEpoch() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
-
Get the Optimally Enclosing Box parent reference frame epoch.
- getOebQ() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
-
Get the quaternion defining Optimally Enclosing Box.
- getOffset(AbsoluteDate) - Method in class org.orekit.forces.gravity.potential.CachedNormalizedSphericalHarmonicsProvider
-
Deprecated.
- getOffset(AbsoluteDate) - Method in interface org.orekit.forces.gravity.potential.SphericalHarmonicsProvider
-
- getOffset() - Method in class org.orekit.time.OffsetModel
-
Offset at reference date in seconds (TAI minus UTC).
- getOffset(AbsoluteDate) - Method in class org.orekit.time.UTCTAIOffset
-
Get the TAI - UTC offset in seconds.
- getOffset(FieldAbsoluteDate<T>) - Method in class org.orekit.time.UTCTAIOffset
-
Get the TAI - UTC offset in seconds.
- getOffset(DateComponents, TimeComponents) - Method in class org.orekit.time.UTCTAIOffset
-
Get the TAI - UTC offset in seconds.
- getOffsetGeodeticPoint(AbsoluteDate) - Method in class org.orekit.estimation.measurements.GroundStation
-
Get the geodetic point at the center of the offset frame.
- getOffsetToInertial(Frame, AbsoluteDate) - Method in class org.orekit.estimation.measurements.GroundStation
-
Get the transform between offset frame and inertial frame.
- getOffsetToInertial(Frame, AbsoluteDate, int, Map<String, Integer>) - Method in class org.orekit.estimation.measurements.GroundStation
-
Get the transform between offset frame and inertial frame with derivatives.
- getOffsetToInertial(Frame, FieldAbsoluteDate<Gradient>, int, Map<String, Integer>) - Method in class org.orekit.estimation.measurements.GroundStation
-
Get the transform between offset frame and inertial frame with derivatives.
- getOmega() - Method in class org.orekit.data.DelaunayArguments
-
Get the mean longitude of the ascending node of the Moon.
- getOmega() - Method in class org.orekit.data.FieldDelaunayArguments
-
Get the mean longitude of the ascending node of the Moon.
- getOmega0() - Method in class org.orekit.propagation.analytical.gnss.data.CommonGnssData
-
Getter for the longitude of ascending node of orbit plane at weekly epoch.
- getOmega0() - Method in interface org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElements
-
Gets the Longitude of Ascending Node of Orbit Plane at Weekly Epoch.
- getOmegaDot() - Method in class org.orekit.data.DelaunayArguments
-
Get the mean longitude of the ascending node of the Moon time derivative.
- getOmegaDot() - Method in class org.orekit.data.FieldDelaunayArguments
-
Get the mean longitude of the ascending node of the Moon time derivative.
- getOmegaDot() - Method in class org.orekit.propagation.analytical.gnss.data.CommonGnssData
-
Getter for the rate of right ascension.
- getOmegaDot() - Method in interface org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElements
-
Gets the Rate of Right Ascension.
- getOOA() - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContributionContext
-
Get ooA = 1 / A.
- getOOA() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldAbstractGaussianContributionContext
-
Get ooA = 1 / A.
- getOOAB() - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContributionContext
-
Get ooAB = 1 / (A * B).
- getOoAB() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseralContext
-
Get ooAB = 1 / (A * B).
- getOoAB() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBodyContext
-
Get ooAB = 1 / (A * B).
- getOoAB() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonalContext
-
Get ooAB = 1 / (A * B).
- getOOAB() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldAbstractGaussianContributionContext
-
Get ooAB = 1 / (A * B).
- getOoAB() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTTesseralContext
-
Get ooAB = 1 / (A * B).
- getOoAB() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTThirdBodyContext
-
Get ooAB = 1 / (A * B).
- getOoAB() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTZonalContext
-
Get ooAB = 1 / (A * B).
- getOoBpo() - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContributionContext
-
Get ooBpo = 1 / (B + 1).
- getOoBpo() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldAbstractGaussianContributionContext
-
Get ooBpo = 1 / (B + 1).
- getOoMU() - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContributionContext
-
Get ooMu = 1 / mu.
- getOoMU() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldAbstractGaussianContributionContext
-
Get ooMu = 1 / mu.
- getOON2A2() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonalContext
-
Get 1 / (n² * a²).
- getOON2A2() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTZonalContext
-
Get 1 / (n² * a²).
- getOpener() - Method in class org.orekit.data.DataSource
-
Get the data stream opener.
- getOperator() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
-
Get the operator of the space object.
- getOperator() - Method in class org.orekit.gnss.metric.ntrip.CasterRecord
-
Get the institution/agency/company operating the caster.
- getOperator() - Method in class org.orekit.gnss.metric.ntrip.NetworkRecord
-
Get the institution/agency/company operating the caster.
- getOpsStatus() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
-
Get the operational status.
- getOptimum() - Method in class org.orekit.estimation.leastsquares.BatchLSEstimator
-
Get the optimum found.
- getOrbAveraging() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata
-
Get type of averaging (Osculating, mean Brouwer, other.
- getOrbit() - Method in class org.orekit.propagation.FieldSpacecraftState
-
Get the current orbit.
- getOrbit() - Method in class org.orekit.propagation.SpacecraftState
-
Get the current orbit.
- getOrbitalElements() - Method in class org.orekit.propagation.analytical.gnss.GNSSPropagator
-
Get the underlying GNSS orbital elements.
- getOrbitalParametersDrivers(boolean) - Method in class org.orekit.estimation.leastsquares.BatchLSEstimator
-
Get the orbital parameters supported by this estimator.
- getOrbitalParametersDrivers(boolean) - Method in class org.orekit.estimation.sequential.KalmanEstimator
-
Get the orbital parameters supported by this estimator.
- getOrbitalParametersDrivers(boolean) - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanEstimator
-
Get the orbital parameters supported by this estimator.
- getOrbitalParametersDrivers() - Method in class org.orekit.propagation.conversion.AbstractPropagatorBuilder
-
Get the drivers for the configurable orbital parameters.
- getOrbitalParametersDrivers() - Method in interface org.orekit.propagation.conversion.PropagatorBuilder
-
Get the drivers for the configurable orbital parameters.
- getOrbitalPeriod() - Method in class org.orekit.orbits.CR3BPDifferentialCorrection
-
Get the orbital period of the required orbit.
- getOrbitalPeriod() - Method in class org.orekit.orbits.LibrationOrbit
-
Return the orbital period of the libration orbit.
- getOrbitCategory() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
-
Get the orbit category.
- getOrbitCorrection() - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm01Data
-
Get the orbit correction data.
- getOrbitCorrection() - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm03Data
-
Get the orbit correction data.
- getOrbitDeterminationBlock() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmData
-
Get orbit determination logical block.
- getOrbitPeriod() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseralContext
-
Get the Keplerian period.
- getOrbitPeriod() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTTesseralContext
-
Get the Keplerian period.
- getOrbitType() - Method in class org.orekit.files.sp3.SP3
-
- getOrbitType() - Method in class org.orekit.propagation.conversion.AbstractPropagatorBuilder
-
- getOrbitType() - Method in interface org.orekit.propagation.conversion.PropagatorBuilder
-
- getOrbitType() - Method in class org.orekit.propagation.events.PositionAngleDetector
-
Get the orbit type defining the angle type.
- getOrbitType() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
-
Get propagation parameter type.
- getOrbitType() - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator
-
Get propagation parameter type.
- getOrbitType() - Method in class org.orekit.propagation.integration.FieldStateMapper
-
Get propagation parameter type.
- getOrbitType() - Method in class org.orekit.propagation.integration.StateMapper
-
Get propagation parameter type.
- getOrbitType() - Method in class org.orekit.propagation.numerical.FieldNumericalPropagator
-
Get propagation parameter type.
- getOrbitType() - Method in class org.orekit.propagation.numerical.NumericalPropagator
-
Get propagation parameter type.
- getOrbitType() - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator
-
Get propagation parameter type.
- getOrbitType() - Method in class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator
-
Get propagation parameter type.
- getOrbitTypeKey() - Method in class org.orekit.files.sp3.SP3
-
Returns the orbit type key for this SP3 file.
- getOrbRevNum() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata
-
Get the integer orbit revolution number.
- getOrbRevNumBasis() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata
-
Get the basis for orbit revolution number.
- getOrdinateGrid() - Method in class org.orekit.utils.InterpolationTableLoader
-
Returns a copy of the ordinate grid for the interpolation function.
- getOrientation() - Method in class org.orekit.attitudes.Attitude
-
Get the complete orientation including spin.
- getOrientation() - Method in class org.orekit.attitudes.FieldAttitude
-
Get the complete orientation including spin.
- getOrigin() - Method in enum org.orekit.frames.HelmertTransformation.Predefined
-
Get the origin ITRF.
- getOrigin() - Method in class org.orekit.frames.ITRFVersion.Converter
-
Get the origin ITRF.
- getOriginal() - Method in class org.orekit.propagation.events.NegateDetector
-
Get the delegate event detector.
- getOriginator() - Method in class org.orekit.files.ccsds.section.Header
-
Get the file originator.
- getOriginatorAddress() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
-
Get the address of Programmatic Point Of Contact at originator.
- getOriginatorPhone() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
-
Get the phone number of Programmatic Point Of Contact at originator.
- getOriginatorPOC() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
-
Get the programmatic Point Of Contact at originator.
- getOriginatorPosition() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
-
Get the position of Programmatic Point Of Contact at originator.
- getOriginIndicator() - Method in class org.orekit.files.ilrs.CRD.AnglesMeasurement
-
Get the angle origin indicator.
- getOtherOccultingBodies() - Method in class org.orekit.forces.radiation.AbstractRadiationForceModel
-
Getter for other occulting bodies to consider.
- getOTrajectoryBlocks() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmData
-
Get trajectory state histories logical blocks.
- getOutputName() - Method in class org.orekit.files.ccsds.utils.generation.AbstractGenerator
-
Get the name of the output (for error messages).
- getOutputName() - Method in interface org.orekit.files.ccsds.utils.generation.Generator
-
Get the name of the output (for error messages).
- getOutputPulseType() - Method in class org.orekit.files.ilrs.CRDConfiguration.DetectorConfiguration
-
Get the output pulse type.
- getOutputPulseWidth() - Method in class org.orekit.files.ilrs.CRDConfiguration.DetectorConfiguration
-
Get the output pulse width.
- getOwner() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
-
Get the owner of the space object.
- getP() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data
-
Get the GLONASS P Word.
- getP() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
-
Get the y component of inclination vector.
- getP() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldAuxiliaryElements
-
Get the y component of inclination vector.
- getP1() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data
-
Get the GLONASS P1 Word.
- getP2() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data
-
Get the GLONASS P2 Word.
- getP3() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data
-
Get the GLONASS P3 Word.
- getP4() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data
-
Get the GLONASS P4 Word.
- getPa() - Method in class org.orekit.data.BodiesElements
-
Get the general accumulated precession in longitude.
- getPa() - Method in class org.orekit.data.FieldBodiesElements
-
Get the general accumulated precession in longitude.
- getPa() - Method in class org.orekit.files.ccsds.ndm.odm.KeplerianElements
-
Get the orbit argument of pericenter.
- getPa() - Method in class org.orekit.propagation.analytical.gnss.data.CommonGnssData
-
Getter for the argument of perigee.
- getPa() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSAlmanac
-
- getPa() - Method in interface org.orekit.propagation.analytical.gnss.data.GLONASSOrbitalElements
-
Get the Argument of Perigee.
- getPa() - Method in interface org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElements
-
Gets the Argument of Perigee.
- getPaDot() - Method in class org.orekit.data.BodiesElements
-
Get the general accumulated precession in longitude time derivative.
- getPaDot() - Method in class org.orekit.data.FieldBodiesElements
-
Get the general accumulated precession in longitude time derivative.
- getParameterDerivatives(ParameterDriver) - Method in class org.orekit.estimation.measurements.EstimatedMeasurement
-
- getParameterDriver(String) - Method in class org.orekit.forces.AbstractForceModel
-
Get parameter value from its name.
- getParameterDriver(String) - Method in interface org.orekit.forces.ForceModel
-
Get parameter value from its name.
- getParameterDriver(String) - Method in class org.orekit.forces.inertia.InertialForces
-
Get parameter value from its name.
- getParameterDriver(String) - Method in class org.orekit.propagation.analytical.tle.TLE
-
Get parameter driver from its name.
- getParameters(FieldSpacecraftState<Gradient>, IonosphericModel) - Method in class org.orekit.estimation.measurements.modifiers.IonosphericGradientConverter
-
Get the ionospheric model parameters.
- getParameters(FieldSpacecraftState<Gradient>, DiscreteTroposphericModel) - Method in class org.orekit.estimation.measurements.modifiers.TroposphericGradientConverter
-
Get the tropospheric model parameters.
- getParameters() - Method in class org.orekit.files.ccsds.ndm.odm.UserDefined
-
Get all user defined parameters.
- getParameters() - Method in interface org.orekit.forces.ForceModel
-
Get force model parameters.
- getParameters(Field<T>) - Method in interface org.orekit.forces.ForceModel
-
Get force model parameters.
- getParameters() - Method in interface org.orekit.models.earth.ionosphere.IonosphericModel
-
Get ionospheric model parameters.
- getParameters(Field<T>) - Method in interface org.orekit.models.earth.ionosphere.IonosphericModel
-
Get ionospheric model parameters.
- getParameters() - Method in interface org.orekit.models.earth.troposphere.DiscreteTroposphericModel
-
Get tropospheric model parameters.
- getParameters(Field<T>) - Method in interface org.orekit.models.earth.troposphere.DiscreteTroposphericModel
-
Get tropospheric model parameters.
- getParameters(FieldSpacecraftState<Gradient>) - Method in class org.orekit.propagation.analytical.AbstractAnalyticalGradientConverter
-
Get the model parameters.
- getParameters(Field<T>) - Method in class org.orekit.propagation.analytical.FieldAbstractAnalyticalPropagator
-
Get model parameters.
- getParameters(Field<T>) - Method in class org.orekit.propagation.analytical.tle.FieldTLE
-
Get model parameters.
- getParameters() - Method in class org.orekit.propagation.integration.AbstractJacobiansMapper
-
Get the number of parameters.
- getParameters() - Method in interface org.orekit.propagation.semianalytical.dsst.forces.DSSTForceModel
-
Get force model parameters.
- getParameters(Field<T>) - Method in interface org.orekit.propagation.semianalytical.dsst.forces.DSSTForceModel
-
Get force model parameters.
- getParametersDrivers() - Method in class org.orekit.estimation.measurements.AbstractMeasurement
-
Get the drivers for this measurement parameters, including its modifiers parameters.
- getParametersDrivers() - Method in interface org.orekit.estimation.measurements.EstimationModifier
-
Get the drivers for this modifier parameters.
- getParametersDrivers() - Method in class org.orekit.estimation.measurements.gnss.WindUp
-
Get the drivers for this modifier parameters.
- getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.AngularIonosphericDelayModifier
-
Get the drivers for this modifier parameters.
- getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.AngularRadioRefractionModifier
-
Get the drivers for this modifier parameters.
- getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.AngularTroposphericDelayModifier
-
Get the drivers for this modifier parameters.
- getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.Bias
-
Get the drivers for this modifier parameters.
- getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.InterSatellitesPhaseAmbiguityModifier
-
Get the drivers for this modifier parameters.
- getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.OnBoardAntennaInterSatellitesPhaseModifier
-
Get the drivers for this modifier parameters.
- getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.OnBoardAntennaInterSatellitesRangeModifier
-
Get the drivers for this modifier parameters.
- getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.OnBoardAntennaOneWayGNSSPhaseModifier
-
Get the drivers for this modifier parameters.
- getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.OnBoardAntennaOneWayGNSSRangeModifier
-
Get the drivers for this modifier parameters.
- getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.OnBoardAntennaPhaseModifier
-
Get the drivers for this modifier parameters.
- getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.OnBoardAntennaRangeModifier
-
Get the drivers for this modifier parameters.
- getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.OnBoardAntennaTurnAroundRangeModifier
-
Get the drivers for this modifier parameters.
- getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.OneWayGNSSPhaseAmbiguityModifier
-
Get the drivers for this modifier parameters.
- getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.OutlierFilter
-
Get the drivers for this modifier parameters.
- getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.PhaseAmbiguityModifier
-
Get the drivers for this modifier parameters.
- getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.PhaseIonosphericDelayModifier
-
Get the drivers for this modifier parameters.
- getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.PhaseTroposphericDelayModifier
-
Get the drivers for this modifier parameters.
- getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.RangeIonosphericDelayModifier
-
Get the drivers for this modifier parameters.
- getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.RangeRateIonosphericDelayModifier
-
Get the drivers for this modifier parameters.
- getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.RangeRateTroposphericDelayModifier
-
Get the drivers for this modifier parameters.
- getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.RangeTroposphericDelayModifier
-
Get the drivers for this modifier parameters.
- getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.RelativisticClockInterSatellitesPhaseModifier
-
Get the drivers for this modifier parameters.
- getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.RelativisticClockInterSatellitesRangeModifier
-
Get the drivers for this modifier parameters.
- getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.RelativisticClockOneWayGNSSPhaseModifier
-
Get the drivers for this modifier parameters.
- getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.RelativisticClockOneWayGNSSRangeModifier
-
Get the drivers for this modifier parameters.
- getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.RelativisticClockPhaseModifier
-
Get the drivers for this modifier parameters.
- getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.RelativisticClockRangeModifier
-
Get the drivers for this modifier parameters.
- getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.RelativisticClockRangeRateModifier
-
Get the drivers for this modifier parameters.
- getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.ShapiroInterSatellitePhaseModifier
-
Get the drivers for this modifier parameters.
- getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.ShapiroInterSatelliteRangeModifier
-
Get the drivers for this modifier parameters.
- getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.ShapiroOneWayGNSSPhaseModifier
-
Get the drivers for this modifier parameters.
- getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.ShapiroOneWayGNSSRangeModifier
-
Get the drivers for this modifier parameters.
- getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.ShapiroPhaseModifier
-
Get the drivers for this modifier parameters.
- getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.ShapiroRangeModifier
-
Get the drivers for this modifier parameters.
- getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.TurnAroundRangeIonosphericDelayModifier
-
Get the drivers for this modifier parameters.
- getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.TurnAroundRangeTroposphericDelayModifier
-
Get the drivers for this modifier parameters.
- getParametersDrivers() - Method in interface org.orekit.estimation.measurements.ObservedMeasurement
-
Get the drivers for this measurement parameters, including its modifiers parameters.
- getParametersDrivers() - Method in class org.orekit.forces.drag.DragForce
-
Get the drivers for force model parameters.
- getParametersDrivers() - Method in class org.orekit.forces.drag.TimeSpanDragForce
-
Get the drivers for force model parameters.
- getParametersDrivers() - Method in interface org.orekit.forces.empirical.AccelerationModel
-
Get the drivers for acceleration model parameters.
- getParametersDrivers() - Method in class org.orekit.forces.empirical.HarmonicAccelerationModel
-
Get the drivers for acceleration model parameters.
- getParametersDrivers() - Method in class org.orekit.forces.empirical.ParametricAcceleration
-
Get the drivers for force model parameters.
- getParametersDrivers() - Method in class org.orekit.forces.empirical.PolynomialAccelerationModel
-
Get the drivers for acceleration model parameters.
- getParametersDrivers() - Method in class org.orekit.forces.empirical.TimeSpanParametricAcceleration
-
Get the drivers for force model parameters.
- getParametersDrivers() - Method in interface org.orekit.forces.ForceModel
-
Get the drivers for force model parameters.
- getParametersDrivers() - Method in class org.orekit.forces.gravity.DeSitterRelativity
-
Get the drivers for force model parameters.
- getParametersDrivers() - Method in class org.orekit.forces.gravity.HolmesFeatherstoneAttractionModel
-
Get the drivers for force model parameters.
- getParametersDrivers() - Method in class org.orekit.forces.gravity.LenseThirringRelativity
-
Get the drivers for force model parameters.
- getParametersDrivers() - Method in class org.orekit.forces.gravity.NewtonianAttraction
-
Get the drivers for force model parameters.
- getParametersDrivers() - Method in class org.orekit.forces.gravity.OceanTides
-
Get the drivers for force model parameters.
- getParametersDrivers() - Method in class org.orekit.forces.gravity.Relativity
-
Get the drivers for force model parameters.
- getParametersDrivers() - Method in class org.orekit.forces.gravity.SingleBodyAbsoluteAttraction
-
Get the drivers for force model parameters.
- getParametersDrivers() - Method in class org.orekit.forces.gravity.SingleBodyRelativeAttraction
-
Get the drivers for force model parameters.
- getParametersDrivers() - Method in class org.orekit.forces.gravity.SolidTides
-
Get the drivers for force model parameters.
- getParametersDrivers() - Method in class org.orekit.forces.gravity.ThirdBodyAttraction
-
Get the drivers for force model parameters.
- getParametersDrivers() - Method in class org.orekit.forces.inertia.InertialForces
-
Get the drivers for force model parameters.
- getParametersDrivers() - Method in class org.orekit.forces.maneuvers.Maneuver
-
- getParametersDrivers() - Method in class org.orekit.forces.maneuvers.propulsion.BasicConstantThrustPropulsionModel
-
Get the propulsion model parameter drivers.
- getParametersDrivers() - Method in interface org.orekit.forces.maneuvers.propulsion.PropulsionModel
-
Get the propulsion model parameter drivers.
- getParametersDrivers() - Method in class org.orekit.forces.maneuvers.propulsion.ScaledConstantThrustPropulsionModel
-
Get the propulsion model parameter drivers.
- getParametersDrivers() - Method in class org.orekit.forces.maneuvers.trigger.DateBasedManeuverTriggers
-
Get the maneuver triggers parameter drivers.
- getParametersDrivers() - Method in interface org.orekit.forces.maneuvers.trigger.ManeuverTriggers
-
Get the maneuver triggers parameter drivers.
- getParametersDrivers() - Method in class org.orekit.forces.radiation.ECOM2
-
Get the drivers for force model parameters.
- getParametersDrivers() - Method in class org.orekit.forces.radiation.KnockeRediffusedForceModel
-
Get the drivers for force model parameters.
- getParametersDrivers() - Method in class org.orekit.forces.radiation.SolarRadiationPressure
-
Get the drivers for force model parameters.
- getParametersDrivers() - Method in class org.orekit.models.earth.ionosphere.EstimatedIonosphericModel
-
- getParametersDrivers() - Method in class org.orekit.models.earth.ionosphere.GlobalIonosphereMapModel
-
- getParametersDrivers() - Method in interface org.orekit.models.earth.ionosphere.IonosphericModel
-
Get the drivers for ionospheric model parameters.
- getParametersDrivers() - Method in class org.orekit.models.earth.ionosphere.KlobucharIonoModel
-
- getParametersDrivers() - Method in class org.orekit.models.earth.ionosphere.NeQuickModel
-
- getParametersDrivers() - Method in class org.orekit.models.earth.ionosphere.SsrVtecIonosphericModel
-
Get the drivers for ionospheric model parameters.
- getParametersDrivers() - Method in interface org.orekit.models.earth.troposphere.DiscreteTroposphericModel
-
Get the drivers for tropospheric model parameters.
- getParametersDrivers() - Method in class org.orekit.models.earth.troposphere.EstimatedTroposphericModel
-
Get the drivers for tropospheric model parameters.
- getParametersDrivers() - Method in class org.orekit.models.earth.troposphere.FixedTroposphericDelay
-
Get the drivers for tropospheric model parameters.
- getParametersDrivers() - Method in class org.orekit.models.earth.troposphere.MariniMurrayModel
-
Get the drivers for tropospheric model parameters.
- getParametersDrivers() - Method in class org.orekit.models.earth.troposphere.MendesPavlisModel
-
Get the drivers for tropospheric model parameters.
- getParametersDrivers() - Method in class org.orekit.models.earth.troposphere.SaastamoinenModel
-
Get the drivers for tropospheric model parameters.
- getParametersDrivers() - Method in class org.orekit.models.earth.troposphere.TimeSpanEstimatedTroposphericModel
-
Get the drivers for tropospheric model parameters.
- getParametersDrivers() - Method in class org.orekit.models.earth.troposphere.ViennaOneModel
-
Get the drivers for tropospheric model parameters.
- getParametersDrivers() - Method in class org.orekit.models.earth.troposphere.ViennaThreeModel
-
Get the drivers for tropospheric model parameters.
- getParametersDrivers() - Method in class org.orekit.propagation.analytical.AbstractAnalyticalGradientConverter
-
Get the parameter drivers related to the analytical propagation model.
- getParametersDrivers() - Method in class org.orekit.propagation.analytical.BrouwerLyddanePropagator
-
Get the parameters driver for propagation model.
- getParametersDrivers() - Method in class org.orekit.propagation.analytical.FieldAbstractAnalyticalPropagator
-
Get the parameters driver for propagation model.
- getParametersDrivers() - Method in class org.orekit.propagation.analytical.FieldBrouwerLyddanePropagator
-
Get the parameters driver for propagation model.
- getParametersDrivers() - Method in class org.orekit.propagation.analytical.FieldEcksteinHechlerPropagator
-
Get the parameters driver for propagation model.
- getParametersDrivers() - Method in class org.orekit.propagation.analytical.FieldKeplerianPropagator
-
Get the parameters driver for propagation model.
- getParametersDrivers() - Method in class org.orekit.propagation.analytical.tle.FieldTLE
-
Get the drivers for TLE propagation SGP4 and SDP4.
- getParametersDrivers() - Method in class org.orekit.propagation.analytical.tle.FieldTLEPropagator
-
Get the parameters driver for propagation model.
- getParametersDrivers() - Method in class org.orekit.propagation.analytical.tle.TLE
-
Get the drivers for TLE propagation SGP4 and SDP4.
- getParametersDrivers() - Method in class org.orekit.propagation.integration.FieldIntegratedEphemeris
-
Get the parameters driver for propagation model.
- getParametersDrivers() - Method in class org.orekit.propagation.numerical.cr3bp.CR3BPForceModel
-
Get the drivers for force model parameters.
- getParametersDrivers() - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution
-
Get the drivers for force model parameters.
- getParametersDrivers() - Method in interface org.orekit.propagation.semianalytical.dsst.forces.DSSTForceModel
-
Get the drivers for force model parameters.
- getParametersDrivers() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTNewtonianAttraction
-
Get the drivers for force model parameters.
- getParametersDrivers() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseral
-
Get the drivers for force model parameters.
- getParametersDrivers() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBody
-
Get the drivers for force model parameters.
- getParametersDrivers() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonal
-
Get the drivers for force model parameters.
- getParametersDriversWithoutMu() - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution
-
Get the drivers for force model parameters except the one for the central
attraction coefficient.
- getParametersDriversWithoutMu() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTAtmosphericDrag
-
Get the drivers for force model parameters except the one for the central
attraction coefficient.
- getParametersDriversWithoutMu() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTSolarRadiationPressure
-
Get the drivers for force model parameters except the one for the central
attraction coefficient.
- getParametersJacobian(SpacecraftState) - Method in class org.orekit.propagation.AbstractMatricesHarvester
-
Get the Jacobian with respect to propagation parameters.
- getParametersJacobian(SpacecraftState) - Method in class org.orekit.propagation.analytical.AbstractAnalyticalMatricesHarvester
-
Get the Jacobian with respect to propagation parameters.
- getParametersJacobian(SpacecraftState, double[][]) - Method in class org.orekit.propagation.analytical.tle.TLEJacobiansMapper
-
Get the Jacobian with respect to parameters from a one-dimensional additional state array.
- getParametersJacobian(SpacecraftState) - Method in class org.orekit.propagation.integration.AbstractJacobiansMapper
-
Get the Jacobian with respect to propagation parameters.
- getParametersJacobian(SpacecraftState, double[][]) - Method in class org.orekit.propagation.integration.AbstractJacobiansMapper
-
Get the Jacobian with respect to parameters from a one-dimensional additional state array.
- getParametersJacobian(SpacecraftState) - Method in interface org.orekit.propagation.MatricesHarvester
-
Get the Jacobian with respect to propagation parameters.
- getParametersJacobian(SpacecraftState, double[][]) - Method in class org.orekit.propagation.numerical.JacobiansMapper
-
Get the Jacobian with respect to parameters from a one-dimensional additional state array.
- getParametersJacobian(SpacecraftState) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTHarvester
-
Get the Jacobian with respect to propagation parameters.
- getParametersJacobian(SpacecraftState, double[][]) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTJacobiansMapper
-
Get the Jacobian with respect to parameters from a one-dimensional additional state array.
- getParent() - Method in class org.orekit.frames.Frame
-
Get the parent frame.
- getParentShape() - Method in class org.orekit.frames.TopocentricFrame
-
Get the body shape on which the local point is defined.
- getParsedUnitsBehavior() - Method in class org.orekit.files.ccsds.ndm.ParserBuilder
-
Get the behavior to adopt for handling parsed units.
- getParsedUnitsBehavior() - Method in class org.orekit.files.ccsds.utils.ContextBinding
-
Get the behavior to adopt for handling parsed units.
- getParsedUnitsBehavior() - Method in class org.orekit.files.ccsds.utils.parsing.AbstractConstituentParser
-
Get the behavior to adopt for handling parsed units.
- getParser(List<Integer>) - Method in enum org.orekit.gnss.metric.ntrip.Type
-
Get the message parser associated to the SSR type.
- getParticipants() - Method in class org.orekit.estimation.measurements.EstimatedMeasurement
-
Get the coordinates of the measurements participants in signal travel order.
- getParticipants() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
-
Getter for the participants.
- getParts() - Method in interface org.orekit.errors.LocalizedException
-
Get the variable parts of the error message.
- getParts() - Method in exception org.orekit.errors.OrekitException
-
Get the variable parts of the error message.
- getParts() - Method in exception org.orekit.errors.OrekitIllegalArgumentException
-
Get the variable parts of the error message.
- getParts() - Method in exception org.orekit.errors.OrekitIllegalStateException
-
Get the variable parts of the error message.
- getParts() - Method in exception org.orekit.errors.OrekitInternalError
-
Get the variable parts of the error message.
- getParts() - Method in exception org.orekit.errors.OrekitIOException
-
Get the variable parts of the error message.
- getParts() - Method in exception org.orekit.errors.OrekitParseException
-
Get the variable parts of the error message.
- getPastInfinity() - Method in class org.orekit.time.AbstractTimeScales
-
- getPastInfinity(Field<T>) - Static method in class org.orekit.time.FieldAbsoluteDate
-
Dummy date at infinity in the past direction.
- getPastInfinity() - Method in interface org.orekit.time.TimeScales
-
Dummy date at infinity in the past direction.
- getPatchedSpacecraftState() - Method in class org.orekit.utils.AbstractMultipleShooting
-
Get the list of patched spacecraft states.
- getPatchPoint(int) - Method in class org.orekit.utils.AbstractMultipleShooting
-
Get a patch point.
- getPath() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
-
Getter for the path.
- getPath1() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
-
Getter for the path1.
- getPath2() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
-
Getter for the path2.
- getPattern() - Method in enum org.orekit.gnss.metric.parser.IgsSsrMessageType
-
Get the message number.
- getPattern() - Method in enum org.orekit.gnss.metric.parser.RtcmMessageType
-
Get the message number.
- getPdop() - Method in class org.orekit.gnss.DOP
-
Gets the position dilution of precision.
- getPendingEvent() - Method in class org.orekit.propagation.events.FieldEventState
-
Get PendingEvent.
- getPerigeeArgument() - Method in class org.orekit.orbits.FieldKeplerianOrbit
-
Get the perigee argument.
- getPerigeeArgument() - Method in class org.orekit.orbits.KeplerianOrbit
-
Get the perigee argument.
- getPerigeeArgument() - Method in class org.orekit.propagation.analytical.tle.FieldTLE
-
Get the argument of perigee.
- getPerigeeArgument() - Method in class org.orekit.propagation.analytical.tle.TLE
-
Get the argument of perigee.
- getPerigeeArgumentDot() - Method in class org.orekit.orbits.FieldKeplerianOrbit
-
Get the perigee argument derivative.
- getPerigeeArgumentDot() - Method in class org.orekit.orbits.KeplerianOrbit
-
Get the perigee argument derivative.
- getPermanentTide() - Method in enum org.orekit.utils.IERSConventions
-
Get the permanent tide to be removed from ΔC₂₀ when zero-tide potentials are used.
- getPerturbationsBlock() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmData
-
Get perturbations logical block.
- getPhase(BodiesElements) - Method in class org.orekit.models.earth.displacement.Tide
-
Get the phase of the tide.
- getPhaseBias() - Method in class org.orekit.gnss.metric.messages.ssr.igm.PhaseBias
-
Get the phase bias associated to the signal ID.
- getPhaseBias(int) - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm06Data
-
Get the phase bias for a given signal ID.
- getPhaseBiases() - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm06Data
-
Get the phase biases for the current satellite.
- getPhaseCenterVariation(Frequency, Vector3D) - Method in class org.orekit.gnss.antenna.Antenna
-
Get the value of the phase center variation in a signal direction.
- getPhaseCenterVariation(Vector3D) - Method in class org.orekit.gnss.antenna.FrequencyPattern
-
Get the value of the phase center variation in a signal direction.
- getPhaseMinusCodeCombination(SatelliteSystem) - Static method in class org.orekit.estimation.measurements.gnss.MeasurementCombinationFactory
-
Get the phase minus code combination of measurements.
- getPhaseShiftCorrections() - Method in class org.orekit.gnss.RinexObservationHeader
-
Get the list of phase shift correction used to generate phases consistent w/r to cycle shifts.
- getPhysicalCovariances(double) - Method in class org.orekit.estimation.leastsquares.BatchLSEstimator
-
Get the covariances matrix in space flight dynamics physical units.
- getPhysicalEstimatedCovarianceMatrix() - Method in class org.orekit.estimation.sequential.AbstractKalmanModel
-
Get the "physical" estimated covariance matrix (i.e.
- getPhysicalEstimatedCovarianceMatrix() - Method in interface org.orekit.estimation.sequential.KalmanEstimation
-
Get the "physical" estimated covariance matrix (i.e.
- getPhysicalEstimatedCovarianceMatrix() - Method in class org.orekit.estimation.sequential.KalmanEstimator
-
Get the "physical" estimated covariance matrix (i.e.
- getPhysicalEstimatedCovarianceMatrix() - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanEstimator
-
Get the "physical" estimated covariance matrix (i.e.
- getPhysicalEstimatedCovarianceMatrix() - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanModel
-
Get the "physical" estimated covariance matrix (i.e.
- getPhysicalEstimatedState() - Method in class org.orekit.estimation.sequential.AbstractKalmanModel
-
Get the "physical" estimated state (i.e.
- getPhysicalEstimatedState() - Method in interface org.orekit.estimation.sequential.KalmanEstimation
-
Get the "physical" estimated state (i.e.
- getPhysicalEstimatedState() - Method in class org.orekit.estimation.sequential.KalmanEstimator
-
Get the "physical" estimated state (i.e.
- getPhysicalEstimatedState() - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanEstimator
-
Get the "physical" estimated state (i.e.
- getPhysicalEstimatedState() - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanModel
-
Get the "physical" estimated state (i.e.
- getPhysicalInnovationCovarianceMatrix() - Method in class org.orekit.estimation.sequential.AbstractKalmanModel
-
Get the physical innovation covariance matrix.
- getPhysicalInnovationCovarianceMatrix() - Method in interface org.orekit.estimation.sequential.KalmanEstimation
-
Get the physical innovation covariance matrix.
- getPhysicalInnovationCovarianceMatrix() - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanModel
-
Get the physical innovation covariance matrix.
- getPhysicalKalmanGain() - Method in class org.orekit.estimation.sequential.AbstractKalmanModel
-
Get the physical Kalman gain matrix.
- getPhysicalKalmanGain() - Method in interface org.orekit.estimation.sequential.KalmanEstimation
-
Get the physical Kalman gain matrix.
- getPhysicalKalmanGain() - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanModel
-
Get the physical Kalman gain matrix.
- getPhysicalMeasurementJacobian() - Method in class org.orekit.estimation.sequential.AbstractKalmanModel
-
Get the physical Jacobian of the measurement with respect to the state (H matrix).
- getPhysicalMeasurementJacobian() - Method in interface org.orekit.estimation.sequential.KalmanEstimation
-
Get the physical Jacobian of the measurement with respect to the state (H matrix).
- getPhysicalMeasurementJacobian() - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanModel
-
Get the physical Jacobian of the measurement with respect to the state (H matrix).
- getPhysicalStateTransitionMatrix() - Method in class org.orekit.estimation.sequential.AbstractKalmanModel
-
Get physical state transition matrix between previous state and estimated (but not yet corrected) state.
- getPhysicalStateTransitionMatrix() - Method in interface org.orekit.estimation.sequential.KalmanEstimation
-
Get physical state transition matrix between previous state and estimated (but not yet corrected) state.
- getPhysicalStateTransitionMatrix() - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanModel
-
Get physical state transition matrix between previous state and estimated (but not yet corrected) state.
- getPhysicBlock() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmData
-
Get physical properties logical block.
- getPlaneSection(Vector3D, Vector3D) - Method in class org.orekit.bodies.Ellipsoid
-
Compute the 2D ellipse at the intersection of the 3D ellipsoid and a plane.
- getPlus(int, int) - Method in class org.orekit.utils.LoveNumbers
-
Get the real part of a nominal Love numbers.
- getPluto() - Method in interface org.orekit.bodies.CelestialBodies
-
Get the Pluto singleton body.
- getPluto() - Static method in class org.orekit.bodies.CelestialBodyFactory
-
Get the Pluto singleton body.
- getPluto() - Method in class org.orekit.bodies.LazyLoadedCelestialBodies
-
- getPnm(int, int) - Method in class org.orekit.utils.FieldLegendrePolynomials
-
Return the coefficient Pnm.
- getPnm(int, int) - Method in class org.orekit.utils.LegendrePolynomials
-
Return the coefficient Pnm.
- getPoint() - Method in class org.orekit.frames.TopocentricFrame
-
Get the surface point defining the origin of the frame.
- getPoint(Field<T>) - Method in class org.orekit.frames.TopocentricFrame
-
Get the surface point defining the origin of the frame.
- getPolarDriftXDriver() - Method in class org.orekit.estimation.measurements.EstimatedEarthFrameProvider
-
Get a driver allowing to add a polar drift along X.
- getPolarDriftXDriver() - Method in class org.orekit.estimation.measurements.GroundStation
-
Get a driver allowing to add a polar drift along X.
- getPolarDriftYDriver() - Method in class org.orekit.estimation.measurements.EstimatedEarthFrameProvider
-
Get a driver allowing to add a polar drift along Y.
- getPolarDriftYDriver() - Method in class org.orekit.estimation.measurements.GroundStation
-
Get a driver allowing to add a polar drift along Y.
- getPolarOffsetXDriver() - Method in class org.orekit.estimation.measurements.EstimatedEarthFrameProvider
-
Get a driver allowing to add a polar offset along X.
- getPolarOffsetXDriver() - Method in class org.orekit.estimation.measurements.GroundStation
-
Get a driver allowing to add a polar offset along X.
- getPolarOffsetYDriver() - Method in class org.orekit.estimation.measurements.EstimatedEarthFrameProvider
-
Get a driver allowing to add a polar offset along Y.
- getPolarOffsetYDriver() - Method in class org.orekit.estimation.measurements.GroundStation
-
Get a driver allowing to add a polar offset along Y.
- getPolarRadius() - Method in class org.orekit.models.earth.ReferenceEllipsoid
-
Get the radius of this ellipsoid at the poles.
- getPole(AbsoluteDate) - Method in interface org.orekit.bodies.IAUPole
-
Get the body North pole direction in ICRF frame.
- getPole(FieldAbsoluteDate<T>) - Method in interface org.orekit.bodies.IAUPole
-
Get the body North pole direction in ICRF frame.
- getPoleCorrection(AbsoluteDate) - Method in class org.orekit.frames.EOPHistory
-
Get the pole IERS Reference Pole correction.
- getPoleCorrection(FieldAbsoluteDate<T>) - Method in class org.orekit.frames.EOPHistory
-
Get the pole IERS Reference Pole correction.
- getPolynomial() - Method in class org.orekit.data.PoissonSeries
-
Get the polynomial part of the series.
- getPort() - Method in class org.orekit.gnss.metric.ntrip.CasterRecord
-
Get the port number.
- getPort() - Method in class org.orekit.gnss.metric.ntrip.NtripClient
-
Get the port to use for connection.
- getPosition() - Method in class org.orekit.estimation.measurements.Position
-
Get the position.
- getPosition() - Method in class org.orekit.estimation.measurements.PV
-
Get the position.
- getPosition() - Method in class org.orekit.files.sinex.Station
-
Get the station position.
- getPosition() - Method in class org.orekit.utils.FieldPVCoordinates
-
Gets the position.
- getPosition() - Method in class org.orekit.utils.PVCoordinates
-
Gets the position.
- getPositionAngle() - Method in class org.orekit.estimation.sequential.UnivariateProcessNoise
-
Getter for the positionAngle.
- getPositionAngle() - Method in class org.orekit.propagation.conversion.AbstractPropagatorBuilder
-
- getPositionAngle() - Method in interface org.orekit.propagation.conversion.PropagatorBuilder
-
- getPositionAngle() - Method in class org.orekit.propagation.events.PositionAngleDetector
-
Get the type of position angle.
- getPositionAngleType() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
-
Get propagation parameter type.
- getPositionAngleType() - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator
-
Get propagation parameter type.
- getPositionAngleType() - Method in class org.orekit.propagation.integration.FieldStateMapper
-
Get propagation parameter type.
- getPositionAngleType() - Method in class org.orekit.propagation.integration.StateMapper
-
Get propagation parameter type.
- getPositionAngleType() - Method in class org.orekit.propagation.numerical.FieldNumericalPropagator
-
Get propagation parameter type.
- getPositionAngleType() - Method in class org.orekit.propagation.numerical.NumericalPropagator
-
Get propagation parameter type.
- getPositionAngleType() - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator
-
Get propagation parameter type.
- getPositionAngleType() - Method in class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator
-
Get propagation parameter type.
- getPositionScale() - Method in class org.orekit.propagation.conversion.AbstractPropagatorBuilder
-
Get the position scale.
- getPotential(SpacecraftState) - Method in class org.orekit.propagation.numerical.cr3bp.CR3BPForceModel
-
Calculate spacecraft potential.
- getPotential(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.numerical.cr3bp.CR3BPForceModel
-
Calculate spacecraft potential.
- getPrecessionFunction() - Method in enum org.orekit.utils.IERSConventions
-
Get the function computing the precession angles.
- getPrecessionFunction(TimeScales) - Method in enum org.orekit.utils.IERSConventions
-
Get the function computing the precession angles.
- getPredictedMeasurement() - Method in class org.orekit.estimation.sequential.AbstractKalmanModel
-
Get the predicted measurement.
- getPredictedMeasurement() - Method in interface org.orekit.estimation.sequential.KalmanEstimation
-
Get the predicted measurement.
- getPredictedMeasurement() - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanModel
-
Get the predicted measurement.
- getPredictedSpacecraftStates() - Method in class org.orekit.estimation.sequential.AbstractKalmanModel
-
Get the predicted spacecraft states.
- getPredictedSpacecraftStates() - Method in interface org.orekit.estimation.sequential.KalmanEstimation
-
Get the predicted spacecraft states.
- getPredictedSpacecraftStates() - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanModel
-
Get the predicted spacecraft states.
- getPredictionProvider() - Method in class org.orekit.files.ilrs.CRDHeader
-
Get the prediction provider.
- getPredictionType() - Method in class org.orekit.files.ilrs.CRDHeader
-
Get the prediction type (CPF or TLE).
- getPressSensorManufacturer() - Method in class org.orekit.files.ilrs.CRDConfiguration.MeteorologicalConfiguration
-
Get the pressure sensor manufacturer.
- getPressSensorModel() - Method in class org.orekit.files.ilrs.CRDConfiguration.MeteorologicalConfiguration
-
Get the pressure sensor model.
- getPressSensorSerialNumber() - Method in class org.orekit.files.ilrs.CRDConfiguration.MeteorologicalConfiguration
-
Get the pressure sensor serial number.
- getPressure() - Method in class org.orekit.files.ilrs.CRD.MeteorologicalMeasurement
-
Get the surface pressure.
- getPressure() - Method in class org.orekit.models.earth.EarthStandardAtmosphereRefraction
-
Get the local pressure at the evaluation location.
- getPressure() - Method in class org.orekit.models.earth.weather.GlobalPressureTemperature2Model
-
Returns the pressure at the station [hPa].
- getPressure() - Method in class org.orekit.models.earth.weather.GlobalPressureTemperatureModel
-
Get the atmospheric pressure of the station depending its position.
- getPrevId() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
-
Get identification of previous orbit determination.
- getPreviousMessageEpoch() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
-
Get the creation date of previous message from a given originator.
- getPreviousMessageID() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
-
Get the unique ID identifying previous message from a given originator.
- getPreviousState() - Method in interface org.orekit.propagation.sampling.FieldOrekitStepInterpolator
-
Get the state at previous grid point date.
- getPreviousState() - Method in interface org.orekit.propagation.sampling.OrekitStepInterpolator
-
Get the state at previous grid point date.
- getPrf() - Method in class org.orekit.files.ilrs.CPFHeader
-
Get the Pulse Repetition Frequency (PRF).
- getPrimary() - Method in class org.orekit.bodies.CR3BPSystem
-
Get the primary CelestialBody.
- getPrimaryObject() - Method in class org.orekit.propagation.events.AngularSeparationFromSatelliteDetector
-
Get the primaryObject, at the center of the proximity zone.
- getPrimaryStation() - Method in class org.orekit.estimation.measurements.TurnAroundRange
-
Get the primary ground station from which measurement is performed.
- getPrimaryWavelength() - Method in class org.orekit.files.ilrs.CRDConfiguration.LaserConfiguration
-
Get the primary wavelength.
- getPrimeMeridianAngle(AbsoluteDate) - Method in interface org.orekit.bodies.IAUPole
-
Get the prime meridian angle.
- getPrimeMeridianAngle(FieldAbsoluteDate<T>) - Method in interface org.orekit.bodies.IAUPole
-
Get the prime meridian angle.
- getPrimeMeridianDriftDriver() - Method in class org.orekit.estimation.measurements.EstimatedEarthFrameProvider
-
Get a driver allowing to add a prime meridian rotation rate.
- getPrimeMeridianDriftDriver() - Method in class org.orekit.estimation.measurements.GroundStation
-
Get a driver allowing to add a prime meridian rotation rate.
- getPrimeMeridianOffsetDriver() - Method in class org.orekit.estimation.measurements.EstimatedEarthFrameProvider
-
Get a driver allowing to add a prime meridian rotation.
- getPrimeMeridianOffsetDriver() - Method in class org.orekit.estimation.measurements.GroundStation
-
Get a driver allowing to add a prime meridian rotation.
- getPrmMessageLink() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
-
Get the Unique identifier of Pointing Request Message linked to this Orbit Data Message.
- getPRN() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractEphemerisMessage
-
Getter for the PRN number of the satellite.
- getPRN() - Method in class org.orekit.propagation.analytical.gnss.data.CommonGnssData
-
Getter for the PRN number of the satellite.
- getPRN() - Method in interface org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElements
-
Gets the PRN number of the GNSS satellite.
- getPRN() - Method in interface org.orekit.propagation.analytical.gnss.data.SBASOrbitalElements
-
Gets the PRN number of the SBAS satellite.
- getPrnNumber() - Method in class org.orekit.gnss.antenna.SatelliteAntenna
-
Get PRN number.
- getPrnNumber() - Method in class org.orekit.gnss.CombinedObservationDataSet
-
Get PRN number.
- getPrnNumber() - Method in class org.orekit.gnss.ObservationDataSet
-
Get PRN number.
- getPRNNumbers() - Method in class org.orekit.gnss.SEMParser
-
Gets the PRN numbers of all the
GPS almanacs
read from the file.
- getPRNNumbers() - Method in class org.orekit.gnss.YUMAParser
-
Gets the PRN numbers of all the
GPS almanacs
read from the file.
- getProcessingSoftwares() - Method in class org.orekit.files.ilrs.CRDConfiguration.SoftwareConfiguration
-
Get the processing softwares.
- getProcessingSoftwareVersions() - Method in class org.orekit.files.ilrs.CRDConfiguration.SoftwareConfiguration
-
Get the processing software versions.
- getProcessNoiseMatrix(SpacecraftState, SpacecraftState) - Method in class org.orekit.estimation.sequential.ConstantProcessNoise
-
Get the process noise matrix between previous and current states.
- getProcessNoiseMatrix(SpacecraftState, SpacecraftState) - Method in interface org.orekit.estimation.sequential.CovarianceMatrixProvider
-
Get the process noise matrix between previous and current states.
- getProcessNoiseMatrix(SpacecraftState, SpacecraftState) - Method in class org.orekit.estimation.sequential.UnivariateProcessNoise
-
Get the process noise matrix between previous and current states.
- getProductionEpoch() - Method in class org.orekit.files.ilrs.ILRSHeader
-
Get the date component of the ephemeris production.
- getProductionHour() - Method in class org.orekit.files.ilrs.ILRSHeader
-
Get the hour of ephemeris production (UTC).
- getProgDCBS() - Method in class org.orekit.gnss.AppliedDCBS
-
Get the program name used to apply DCBs.
- getProgPCVS() - Method in class org.orekit.gnss.AppliedPCVS
-
Get the program name used to apply PCVs.
- getProgramName() - Method in class org.orekit.gnss.clock.RinexClock
-
Getter for the program name.
- getProgramName() - Method in class org.orekit.gnss.navigation.RinexNavigation
-
Getter for the program name.
- getPropagationParametersDrivers(boolean) - Method in class org.orekit.estimation.sequential.KalmanEstimator
-
Get the propagator parameters supported by this estimator.
- getPropagationParametersDrivers(boolean) - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanEstimator
-
Get the propagator parameters supported by this estimator.
- getPropagationParametersDrivers() - Method in class org.orekit.propagation.conversion.AbstractPropagatorBuilder
-
Get the drivers for the configurable propagation parameters.
- getPropagationParametersDrivers() - Method in interface org.orekit.propagation.conversion.PropagatorBuilder
-
Get the drivers for the configurable propagation parameters.
- getPropagationParametersEvolution() - Method in class org.orekit.estimation.sequential.UnivariateProcessNoise
-
Getter for the propagationParametersEvolution.
- getPropagationType() - Method in class org.orekit.propagation.conversion.DSSTPropagatorBuilder
-
Get the type of the orbit used for the propagation (mean or osculating).
- getPropagationType() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
-
Get the propagation type.
- getPropagator(ObservableSatellite) - Method in class org.orekit.estimation.measurements.generation.Generator
-
Get a registered propagator.
- getPropagator() - Method in interface org.orekit.files.general.EphemerisFile.EphemerisSegment
-
View this ephemeris segment as a propagator.
- getPropagator() - Method in interface org.orekit.files.general.EphemerisFile.SatelliteEphemeris
-
View this ephemeris as a propagator, combining data from all
segments
.
- getPropagator() - Method in class org.orekit.files.ilrs.CPF.CPFEphemeris
-
View this ephemeris as a propagator, combining data from all
segments
.
- getPropagator() - Method in class org.orekit.files.sp3.SP3.SP3Ephemeris
-
- getPropagator(FieldSpacecraftState<Gradient>, Gradient[]) - Method in class org.orekit.propagation.analytical.AbstractAnalyticalGradientConverter
-
Get the converted analytical orbit propagator.
- getPropagator() - Method in class org.orekit.propagation.analytical.AdapterPropagator
-
Get the reference propagator.
- getPropagatorIndex() - Method in class org.orekit.estimation.measurements.ObservableSatellite
-
Get the index of the propagator related to this satellite.
- getPropagatorList() - Method in class org.orekit.utils.AbstractMultipleShooting
-
Get the list of propagators.
- getPropagatorParametersDrivers(boolean) - Method in class org.orekit.estimation.leastsquares.BatchLSEstimator
-
Get the propagator parameters supported by this estimator.
- getPropagators() - Method in class org.orekit.propagation.PropagatorsParallelizer
-
Get an unmodifiable list of the underlying mono-satellite propagators.
- getPropulsionModel() - Method in class org.orekit.forces.maneuvers.Maneuver
-
Get the propulsion model.
- getProvider(boolean, int, int) - Method in class org.orekit.forces.gravity.potential.EGMFormatReader
-
Get a provider for read spherical harmonics coefficients.
- getProvider(boolean, int, int) - Method in class org.orekit.forces.gravity.potential.GRGSFormatReader
-
Get a provider for read spherical harmonics coefficients.
- getProvider(boolean, int, int) - Method in class org.orekit.forces.gravity.potential.ICGEMFormatReader
-
Get a provider for read spherical harmonics coefficients.
- getProvider(boolean, int, int) - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
-
Get a provider for read spherical harmonics coefficients.
- getProvider(boolean, int, int) - Method in class org.orekit.forces.gravity.potential.SHMFormatReader
-
Get a provider for read spherical harmonics coefficients.
- getProvider() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonal
-
Get the spherical harmonics provider.
- getProviders() - Method in class org.orekit.data.DataProvidersManager
-
Get an unmodifiable view of the list of supported providers.
- getProximityAngle() - Method in class org.orekit.propagation.events.AngularSeparationDetector
-
Get the proximity angle (rad).
- getProximityAngle() - Method in class org.orekit.propagation.events.AngularSeparationFromSatelliteDetector
-
Get the proximity angle (rad).
- getProxy() - Method in class org.orekit.gnss.metric.ntrip.NtripClient
-
Get proxy.
- getPulseEnergy() - Method in class org.orekit.files.ilrs.CRDConfiguration.LaserConfiguration
-
Get the pulse energy.
- getPulseInOutgoingSemiTrain() - Method in class org.orekit.files.ilrs.CRDConfiguration.LaserConfiguration
-
Get the number of pulses in outgoing semi-train.
- getPulseWidth() - Method in class org.orekit.files.ilrs.CRDConfiguration.LaserConfiguration
-
Get the pulse width (FWHM in ps).
- getPVCoordinates() - Method in class org.orekit.files.ccsds.ndm.odm.opm.Opm
-
Get the position/velocity coordinates contained in the OPM.
- getPVCoordinates(AbsoluteDate, Frame) - Method in class org.orekit.frames.TopocentricFrame
-
Get the
PVCoordinates
of the topocentric frame origin in the selected frame.
- getPVCoordinates(Frame) - Method in class org.orekit.orbits.FieldOrbit
-
- getPVCoordinates(FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.orbits.FieldOrbit
-
- getPVCoordinates() - Method in class org.orekit.orbits.FieldOrbit
-
- getPVCoordinates(Frame) - Method in class org.orekit.orbits.Orbit
-
- getPVCoordinates(AbsoluteDate, Frame) - Method in class org.orekit.orbits.Orbit
-
- getPVCoordinates() - Method in class org.orekit.orbits.Orbit
-
- getPVCoordinates(AbsoluteDate, Frame) - Method in class org.orekit.propagation.AbstractPropagator
-
- getPVCoordinates(AbsoluteDate, Frame) - Method in class org.orekit.propagation.analytical.AggregateBoundedPropagator
-
- getPVCoordinates(AbsoluteDate, Frame) - Method in class org.orekit.propagation.analytical.Ephemeris
-
- getPVCoordinates(FieldAbsoluteDate<T>, T[]) - Method in class org.orekit.propagation.analytical.tle.FieldTLEPropagator
-
Get the extrapolated position and velocity from an initial TLE.
- getPVCoordinates(AbsoluteDate) - Method in class org.orekit.propagation.analytical.tle.TLEPropagator
-
Get the extrapolated position and velocity from an initial TLE.
- getPVCoordinates(FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.propagation.FieldAbstractPropagator
-
- getPVCoordinates() - Method in class org.orekit.propagation.FieldSpacecraftState
-
- getPVCoordinates(Frame) - Method in class org.orekit.propagation.FieldSpacecraftState
-
- getPVCoordinates(FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.propagation.integration.FieldIntegratedEphemeris
-
- getPVCoordinates(AbsoluteDate, Frame) - Method in class org.orekit.propagation.integration.IntegratedEphemeris
-
- getPVCoordinates(FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.propagation.numerical.FieldNumericalPropagator
-
- getPVCoordinates(AbsoluteDate, Frame) - Method in class org.orekit.propagation.numerical.NumericalPropagator
-
- getPVCoordinates() - Method in class org.orekit.propagation.SpacecraftState
-
- getPVCoordinates(Frame) - Method in class org.orekit.propagation.SpacecraftState
-
- getPVCoordinates() - Method in class org.orekit.utils.AbsolutePVCoordinates
-
Get the TimeStampedPVCoordinates.
- getPVCoordinates(Frame) - Method in class org.orekit.utils.AbsolutePVCoordinates
-
Get the TimeStampedPVCoordinates in a specified frame.
- getPVCoordinates(AbsoluteDate, Frame) - Method in class org.orekit.utils.AbsolutePVCoordinates
-
- getPVCoordinates(FieldAbsoluteDate<T>, Frame) - Method in interface org.orekit.utils.ExtendedPVCoordinatesProvider
-
- getPVCoordinates() - Method in class org.orekit.utils.FieldAbsolutePVCoordinates
-
Get the TimeStampedFieldPVCoordinates.
- getPVCoordinates(Frame) - Method in class org.orekit.utils.FieldAbsolutePVCoordinates
-
Get the TimeStampedFieldPVCoordinates in a specified frame.
- getPVCoordinates(FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.utils.FieldAbsolutePVCoordinates
-
- getPVCoordinates(FieldAbsoluteDate<T>, Frame) - Method in interface org.orekit.utils.FieldPVCoordinatesProvider
-
- getPVCoordinates(AbsoluteDate, Frame) - Method in interface org.orekit.utils.PVCoordinatesProvider
-
- getPVCoordinatesProvider() - Method in class org.orekit.propagation.events.AlignmentDetector
-
Get the body to align.
- getPvProvider() - Method in class org.orekit.propagation.analytical.AbstractAnalyticalPropagator
-
Get PV coordinates provider.
- getPvProvider() - Method in class org.orekit.propagation.analytical.FieldAbstractAnalyticalPropagator
-
Get PV coordinates provider.
- getPVTarget() - Method in class org.orekit.propagation.events.FieldOfViewDetector
-
Get the position/velocity provider of the target .
- getPZ9011(IERSConventions, boolean) - Method in class org.orekit.frames.AbstractFrames
-
- getPZ9011(IERSConventions, boolean) - Method in interface org.orekit.frames.Frames
-
Get the PZ-90.11 (Parametry Zemly – 1990.11) reference frame.
- getPZ9011(IERSConventions, boolean) - Static method in class org.orekit.frames.FramesFactory
-
Get the PZ-90.11 (Parametry Zemly – 1990.11) reference frame.
- getQ() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
-
Get the x component of inclination vector.
- getQ() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldAuxiliaryElements
-
Get the x component of inclination vector.
- getQns() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBodyContext
-
Get the value of Qns coefficients.
- getQns() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTThirdBodyContext
-
Get the value of Qns coefficients.
- getQualityIndicator() - Method in class org.orekit.files.ilrs.CRDHeader
-
Get the data quality indicator.
- getQuantumEfficiency() - Method in class org.orekit.files.ilrs.CRDConfiguration.DetectorConfiguration
-
Get the quantum efficiency at applicable wavelength.
- getQuaternion() - Method in class org.orekit.files.ccsds.ndm.adm.apm.ApmQuaternion
-
Get the quaternion.
- getQuaternionBlock() - Method in class org.orekit.files.ccsds.ndm.adm.apm.ApmData
-
Get the quaternion logical block.
- getQuaternionDot() - Method in class org.orekit.files.ccsds.ndm.adm.apm.ApmQuaternion
-
Get the quaternion derivative.
- getQZSS() - Method in class org.orekit.time.LazyLoadedTimeScales
-
- getQZSS() - Method in interface org.orekit.time.TimeScales
-
Get the Quasi-Zenith Satellite System time scale.
- getQZSS() - Static method in class org.orekit.time.TimeScalesFactory
-
Get the Quasi-Zenith Satellite System time scale.
- getQzssCodeOnL2() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1044Data
-
Get the QZSS code on L2 Channel.
- getQzssEpoch() - Method in class org.orekit.time.AbstractTimeScales
-
- getQzssEpoch() - Method in interface org.orekit.time.TimeScales
-
Reference epoch for QZSS weeks: 1980-01-06T00:00:00 QZSS time.
- getQzssFitInterval() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1044Data
-
Get the QZSS fit interval.
- getQzssNavigationMessage() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1044Data
-
Get the QZSS navigation message corresponding to the current RTCM data.
- getQzssNavigationMessage(TimeScales) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1044Data
-
Get the QZSS navigation message corresponding to the current RTCM data.
- getQZSSNavigationMessages() - Method in class org.orekit.gnss.navigation.RinexNavigation
-
Get all the QZSS navigation messages contained in the file.
- getQZSSNavigationMessages(String) - Method in class org.orekit.gnss.navigation.RinexNavigation
-
Get the QZSS navigation messages for the given satellite Id.
- getQzssToc() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1044Data
-
Get the QZSS time of clock.
- getRaan() - Method in class org.orekit.files.ccsds.ndm.odm.KeplerianElements
-
Get the orbit right ascension of ascending node.
- getRaan() - Method in class org.orekit.propagation.analytical.tle.FieldTLE
-
Get Right Ascension of the Ascending node.
- getRaan() - Method in class org.orekit.propagation.analytical.tle.TLE
-
Get Right Ascension of the Ascending node.
- getRadiationParametersDrivers() - Method in class org.orekit.forces.BoxAndSolarArraySpacecraft
-
Get the drivers for supported parameters.
- getRadiationParametersDrivers() - Method in class org.orekit.forces.radiation.IsotropicRadiationClassicalConvention
-
Get the drivers for supported parameters.
- getRadiationParametersDrivers() - Method in class org.orekit.forces.radiation.IsotropicRadiationCNES95Convention
-
Get the drivers for supported parameters.
- getRadiationParametersDrivers() - Method in class org.orekit.forces.radiation.IsotropicRadiationSingleCoefficient
-
Get the drivers for supported parameters.
- getRadiationParametersDrivers() - Method in interface org.orekit.forces.radiation.RadiationSensitive
-
Get the drivers for supported parameters.
- getRange(Vector3D, Frame, AbsoluteDate) - Method in class org.orekit.frames.TopocentricFrame
-
Get the range of a point with regards to the topocentric frame center point.
- getRange(FieldVector3D<T>, Frame, FieldAbsoluteDate<T>) - Method in class org.orekit.frames.TopocentricFrame
-
Get the range of a point with regards to the topocentric frame center point.
- getRange1() - Method in class org.orekit.estimation.iod.IodGooding
-
Get the range for observation (1).
- getRange2() - Method in class org.orekit.estimation.iod.IodGooding
-
Get the range for observation (2).
- getRange3() - Method in class org.orekit.estimation.iod.IodGooding
-
Get the range for observation (3).
- getRangeData() - Method in class org.orekit.files.ilrs.CRD.CRDDataBlock
-
Get the range data for the data block.
- getRangeMode() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
-
Getter for the rangeMode.
- getRangeModulus(RangeUnitsConverter) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
-
Getter for the range modulus in meters.
- getRangeRate(PVCoordinates, Frame, AbsoluteDate) - Method in class org.orekit.frames.TopocentricFrame
-
Get the range rate of a point with regards to the topocentric frame center point.
- getRangeRate(FieldPVCoordinates<T>, Frame, FieldAbsoluteDate<T>) - Method in class org.orekit.frames.TopocentricFrame
-
Get the range rate of a point with regards to the topocentric frame center point.
- getRangeType() - Method in class org.orekit.files.ilrs.CRDHeader
-
Get the range type.
- getRangeType(int) - Static method in enum org.orekit.files.ilrs.CRDHeader.RangeType
-
Get the range type for the given indicator.
- getRangeUnits() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
-
Getter for the rangeUnits.
- getRangeUnitsConverter() - Method in class org.orekit.files.ccsds.ndm.AbstractBuilder
-
- getRate() - Method in class org.orekit.gnss.metric.ntrip.StreamedMessage
-
Get refresh rate.
- getRate(BodiesElements) - Method in class org.orekit.models.earth.displacement.Tide
-
Get the angular rate of the tide.
- getRatio() - Method in enum org.orekit.gnss.Frequency
-
Get the ratio f/f0, where
f0
is the common frequency.
- getRatio() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseralContext
-
Get the ratio of satellite period to central body rotation period.
- getRatio() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTTesseralContext
-
Get the ratio of satellite period to central body rotation period.
- getRawCnm(int, int) - Method in interface org.orekit.forces.gravity.potential.RawSphericalHarmonicsProvider.RawSphericalHarmonics
-
Get a spherical harmonic cosine coefficient.
- getRawContent() - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken
-
Get the raw content of the entry.
- getRawCorrectionRange() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
-
Getter for the raw correction for range.
- getRawDrivers() - Method in class org.orekit.utils.ParameterDriversList.DelegatingDriver
-
Get the raw drivers to which this one delegates.
- getRawProvider() - Method in class org.orekit.frames.InterpolatingTransformProvider
-
Get the underlying provider for raw (non-interpolated) transforms.
- getRawProvider() - Method in class org.orekit.frames.ShiftingTransformProvider
-
Get the underlying provider for raw (non-interpolated) transforms.
- getRawPV(AbsoluteDate) - Method in interface org.orekit.bodies.JPLEphemeridesLoader.RawPVProvider
-
Get the position-velocity at date.
- getRawPV(FieldAbsoluteDate<T>) - Method in interface org.orekit.bodies.JPLEphemeridesLoader.RawPVProvider
-
Get the position-velocity at date.
- getRawRangeModulus() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
-
Getter for the raw range modulus.
- getRawSnm(int, int) - Method in interface org.orekit.forces.gravity.potential.RawSphericalHarmonicsProvider.RawSphericalHarmonics
-
Get a spherical harmonic sine coefficient.
- getRbar() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTAtmosphericDrag
-
Get the critical distance.
- getRcs() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
-
Get the typical (50th percentile) radar cross-section.
- getRcvrClkOffset() - Method in class org.orekit.gnss.CombinedObservationDataSet
-
Get receiver clock offset.
- getRcvrClkOffset() - Method in class org.orekit.gnss.ObservationDataSet
-
Get receiver clock offset.
- getRdmMessageLink() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
-
Get the Unique identifier of Reentry Data Message linked to this Orbit Data Message.
- getReal(int, int) - Method in class org.orekit.utils.LoveNumbers
-
Get the real part of a nominal Love numbers.
- getRealAPV(AbsolutePVCoordinates, AbsoluteDate, Frame) - Method in class org.orekit.bodies.CR3BPSystem
-
Get the AbsolutePVCoordinates from normalized units to standard units in an output frame.
- getReceiveBand() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
-
Getter for the receiveBand.
- getReceiveDelays() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
-
Getter for receiveDelays.
- getReceiverIdentifier() - Method in class org.orekit.gnss.clock.RinexClock.Receiver
-
Getter for the receiver identifier.
- getReceiverNumber() - Method in class org.orekit.gnss.RinexObservationHeader
-
Get the number of the receiver.
- getReceivers() - Method in class org.orekit.gnss.clock.RinexClock
-
Getter for the receivers.
- getReceiversAntennas() - Method in class org.orekit.gnss.antenna.AntexLoader
-
Get parsed receivers antennas.
- getReceiverType() - Method in class org.orekit.gnss.RinexObservationHeader
-
Get the type of the receiver.
- getReceiverVersion() - Method in class org.orekit.gnss.RinexObservationHeader
-
Get the version of the receiver.
- getRecommendedOdSpan() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
-
Get sime span of observation recommended for the OD of the object.
- getRecordType() - Method in class org.orekit.gnss.metric.ntrip.CasterRecord
-
Get the type of record.
- getRecordType() - Method in class org.orekit.gnss.metric.ntrip.DataStreamRecord
-
Get the type of record.
- getRecordType() - Method in class org.orekit.gnss.metric.ntrip.NetworkRecord
-
Get the type of record.
- getRecordType() - Method in class org.orekit.gnss.metric.ntrip.Record
-
Get the type of record.
- getReductionTheory() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
-
Get reduction theory used for precession and nutation modeling.
- getReferenceAttitude() - Method in class org.orekit.attitudes.FixedRate
-
Get the reference attitude.
- getReferenceClocks() - Method in class org.orekit.gnss.clock.RinexClock
-
Getter for the reference clocks.
- getReferenceDate() - Method in class org.orekit.files.ccsds.utils.ContextBinding
-
Get initial date.
- getReferenceDate() - Method in class org.orekit.forces.gravity.potential.CachedNormalizedSphericalHarmonicsProvider
-
Get the reference date for the harmonics.
- getReferenceDate() - Method in interface org.orekit.forces.gravity.potential.SphericalHarmonicsProvider
-
Get the reference date for the harmonics.
- getReferenceDate() - Method in class org.orekit.propagation.integration.FieldStateMapper
-
Get reference date.
- getReferenceDate() - Method in class org.orekit.propagation.integration.StateMapper
-
Get reference date.
- getReferenceDate() - Method in class org.orekit.utils.ParameterDriver
-
Get current reference date.
- getReferenceDate() - Method in class org.orekit.utils.SecularAndHarmonic
-
Get the reference date.
- getReferenceFrame() - Method in class org.orekit.attitudes.Attitude
-
Get the reference frame.
- getReferenceFrame() - Method in class org.orekit.attitudes.FieldAttitude
-
Get the reference frame.
- getReferenceFrame() - Method in class org.orekit.estimation.measurements.AngularRaDec
-
Get the reference frame in which the right ascension - declination angles are given.
- getReferenceFrame() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemSegment
-
Get the reference frame from which attitude is defined.
- getReferenceFrame() - Method in class org.orekit.files.ccsds.ndm.odm.CartesianCovariance
-
Get the reference frame.
- getReferenceFrame() - Method in class org.orekit.files.ccsds.ndm.odm.CommonMetadata
-
Get the value of
REF_FRAME
as an Orekit
Frame
.
- getReferenceFrame() - Method in class org.orekit.files.ccsds.ndm.odm.opm.Maneuver
-
Get Coordinate system for velocity increment vector.
- getReferenceFrame() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
-
Get the the value of
REFERENCE_FRAME
as an Orekit
Frame
.
- getReferenceFrame() - Method in interface org.orekit.files.general.AttitudeEphemerisFile.AttitudeEphemerisSegment
-
Get the reference frame from which attitude is defined.
- getReferenceFrame() - Method in class org.orekit.files.general.OrekitAttitudeEphemerisFile.OrekitAttitudeEphemerisSegment
-
Get the reference frame from which attitude is defined.
- getReferenceName() - Method in class org.orekit.gnss.clock.RinexClock.ReferenceClock
-
Getter for the name of the receiver/satellite embedding the reference clock.
- getReferenceRadius() - Method in class org.orekit.propagation.analytical.BrouwerLyddanePropagator
-
Get the reference radius of the central body attraction model.
- getReferenceRadius() - Method in class org.orekit.propagation.analytical.EcksteinHechlerPropagator
-
Get the reference radius of the central body attraction model.
- getReferenceTrajectories() - Method in class org.orekit.estimation.sequential.AbstractKalmanModel
-
Getter for the reference trajectories.
- getReferenceValue() - Method in class org.orekit.utils.ParameterDriver
-
Get reference parameter value.
- getRefFrame() - Method in class org.orekit.files.ccsds.definitions.ModifiedFrame
-
Get the CCSDS reference frame.
- getRefFrame() - Method in class org.orekit.files.ilrs.CPFHeader
-
Get the reference frame.
- getRefFrameId() - Method in class org.orekit.files.ilrs.CPFHeader
-
Get the reference frame identifier.
- getRefFrameString() - Method in class org.orekit.files.ccsds.ndm.adm.apm.Maneuver
-
Get Coordinate system for the torque vector, for absolute frames.
- getReflectivity() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
-
Get the typical (50th percentile) coefficient of reflectivity.
- getRefraction(double) - Method in interface org.orekit.models.AtmosphericRefractionModel
-
Compute the refraction angle from the true (geometrical) elevation.
- getRefraction(double) - Method in class org.orekit.models.earth.EarthITU453AtmosphereRefraction
-
- getRefraction(double) - Method in class org.orekit.models.earth.EarthStandardAtmosphereRefraction
-
- getRefractionModel() - Method in class org.orekit.propagation.events.ElevationDetector
-
Returns the currently configured refraction model.
- getRefractionModel() - Method in class org.orekit.propagation.events.FieldElevationDetector
-
Returns the currently configured refraction model.
- getRegistrationAddress() - Method in class org.orekit.gnss.metric.ntrip.NetworkRecord
-
Get the web or mail address for registration.
- getRemainingDv() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
-
Get the total ΔV remaining for spacecraft.
- getResults() - Method in class org.orekit.estimation.measurements.gnss.AbstractCycleSlipDetector
-
Get on all the results computed by the detector (e.g.: dates of cycle-slip).
- getRetrogradeFactor() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
-
Get the retrograde factor.
- getRetrogradeFactor() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldAuxiliaryElements
-
Get the retrograde factor.
- getRevAtEpoch() - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmTle
-
Get the revolution rumber.
- getReversedProvider(TransformProvider) - Static method in class org.orekit.frames.TransformProviderUtils
-
Reverse a transform provider.
- getRevolutionNumberAtEpoch() - Method in class org.orekit.propagation.analytical.tle.FieldTLE
-
Get the revolution number.
- getRevolutionNumberAtEpoch() - Method in class org.orekit.propagation.analytical.tle.TLE
-
Get the revolution number.
- getRightAscensionOfAscendingNode() - Method in class org.orekit.orbits.CircularOrbit
-
Get the right ascension of the ascending node.
- getRightAscensionOfAscendingNode() - Method in class org.orekit.orbits.FieldCircularOrbit
-
Get the right ascension of the ascending node.
- getRightAscensionOfAscendingNode() - Method in class org.orekit.orbits.FieldKeplerianOrbit
-
Get the right ascension of the ascending node.
- getRightAscensionOfAscendingNode() - Method in class org.orekit.orbits.KeplerianOrbit
-
Get the right ascension of the ascending node.
- getRightAscensionOfAscendingNodeDot() - Method in class org.orekit.orbits.CircularOrbit
-
Get the right ascension of the ascending node derivative.
- getRightAscensionOfAscendingNodeDot() - Method in class org.orekit.orbits.FieldCircularOrbit
-
Get the right ascension of the ascending node derivative.
- getRightAscensionOfAscendingNodeDot() - Method in class org.orekit.orbits.FieldKeplerianOrbit
-
Get the right ascension of the ascending node derivative.
- getRightAscensionOfAscendingNodeDot() - Method in class org.orekit.orbits.KeplerianOrbit
-
Get the right ascension of the ascending node derivative.
- getRinexVersion() - Method in class org.orekit.gnss.RinexObservationHeader
-
Get Rinex Version.
- getRMS() - Method in class org.orekit.propagation.conversion.AbstractPropagatorConverter
-
Get the Root Mean Square Deviation of the fitting.
- getRnml(double, int, int, int, int, int) - Static method in class org.orekit.propagation.semianalytical.dsst.utilities.UpperBounds
-
Get the upper bound value Rεn,m,l(γ).
- getRnml(T, int, int, int, int, int) - Static method in class org.orekit.propagation.semianalytical.dsst.utilities.UpperBounds
-
Get the upper bound value Rεn,m,l(γ).
- getRoa() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseralContext
-
Get roa = R / a.
- getRoa() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonalContext
-
Get roa = R / a.
- getRoa() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTTesseralContext
-
Get roa = R / a.
- getRoa() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTZonalContext
-
Get roa = R / a.
- getRolloverReference() - Static method in class org.orekit.time.GNSSDate
-
Get the reference date ensuring continuity across GNSS week rollover.
- getRoot() - Static method in class org.orekit.frames.Frame
-
Get the unique root frame.
- getRotatingFrame() - Method in class org.orekit.bodies.CR3BPSystem
-
Get the CR3BP Rotating Frame.
- getRotation() - Method in class org.orekit.attitudes.Attitude
-
Get the attitude rotation.
- getRotation() - Method in class org.orekit.attitudes.FieldAttitude
-
Get the attitude rotation.
- getRotation() - Method in class org.orekit.frames.FieldTransform
-
Get the underlying elementary rotation.
- getRotation() - Method in class org.orekit.frames.Transform
-
Get the underlying elementary rotation.
- getRotation() - Method in class org.orekit.utils.AngularCoordinates
-
Get the rotation.
- getRotation() - Method in class org.orekit.utils.FieldAngularCoordinates
-
Get the rotation.
- getRotationAcceleration() - Method in class org.orekit.attitudes.Attitude
-
Get the satellite rotation acceleration.
- getRotationAcceleration() - Method in class org.orekit.attitudes.FieldAttitude
-
Get the satellite rotation acceleration.
- getRotationAcceleration() - Method in class org.orekit.frames.FieldTransform
-
Get the second time derivative of the rotation.
- getRotationAcceleration() - Method in class org.orekit.frames.Transform
-
Get the second time derivative of the rotation.
- getRotationAcceleration() - Method in class org.orekit.utils.AngularCoordinates
-
Get the rotation acceleration.
- getRotationAcceleration() - Method in class org.orekit.utils.FieldAngularCoordinates
-
Get the rotation acceleration.
- getRotationalAngleType() - Method in class org.orekit.files.ilrs.CPFHeader
-
Get the rotation angle type.
- getRotationAngles() - Method in class org.orekit.files.ccsds.ndm.adm.apm.Euler
-
Get the coordinates of the Euler angles (rad).
- getRotationRate() - Method in class org.orekit.frames.FieldTransform
-
Get the first time derivative of the rotation.
- getRotationRate() - Method in class org.orekit.frames.Transform
-
Get the first time derivative of the rotation.
- getRotationRate() - Method in class org.orekit.utils.AngularCoordinates
-
Get the rotation rate.
- getRotationRate() - Method in class org.orekit.utils.FieldAngularCoordinates
-
Get the rotation rate.
- getRotationRates() - Method in class org.orekit.files.ccsds.ndm.adm.apm.Euler
-
Get the rates of the Euler angles (rad/s).
- getS() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.CoefficientsFactory.NSKey
-
Get s.
- getS10(AbsoluteDate) - Method in interface org.orekit.models.earth.atmosphere.JB2008InputParameters
-
Get the EUV index (26-34 nm) scaled to F10.
- getS10B(AbsoluteDate) - Method in interface org.orekit.models.earth.atmosphere.JB2008InputParameters
-
Get the EUV 81-day averaged centered index.
- getSample() - Method in class org.orekit.propagation.conversion.AbstractPropagatorConverter
-
Get the states sample.
- getSatConfiguration() - Method in class org.orekit.propagation.analytical.gnss.data.GPSAlmanac
-
Gets the satellite configuration.
- getSatelliteCode() - Method in class org.orekit.gnss.antenna.SatelliteAntenna
-
Get satellite code.
- getSatelliteCount() - Method in class org.orekit.files.sp3.SP3
-
Get the number of satellites contained in this orbit file.
- getSatelliteID() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.RtcmEphemerisData
-
Get the satellite ID.
- getSatelliteID() - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgmData
-
Get the satellite ID.
- getSatelliteId(SatelliteSystem, int) - Static method in enum org.orekit.gnss.metric.parser.IgsSsrMessageType
-
Transform the satellite ID parsed from the IGS SSR message to the real ID.
- getSatelliteName() - Method in class org.orekit.estimation.measurements.gnss.CycleSlipDetectorResults
-
Get the satellite name.
- getSatelliteNumber() - Method in class org.orekit.propagation.analytical.tle.FieldTLE
-
Get the satellite id.
- getSatelliteNumber() - Method in class org.orekit.propagation.analytical.tle.TLE
-
Get the satellite id.
- getSatelliteRevolution() - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator
-
Get the number of satellite revolutions to use for converting osculating to mean elements.
- getSatelliteRevolution() - Method in class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator
-
Get the number of satellite revolutions to use for converting osculating to mean elements.
- getSatellites() - Method in class org.orekit.estimation.measurements.AbstractMeasurement
-
Get the satellites related to this measurement.
- getSatellites() - Method in class org.orekit.estimation.measurements.generation.AbstractMeasurementBuilder
-
Get the satellites related to this measurement.
- getSatellites() - Method in interface org.orekit.estimation.measurements.ObservedMeasurement
-
Get the satellites related to this measurement.
- getSatellites() - Method in class org.orekit.files.ccsds.ndm.adm.aem.Aem
-
Get the loaded ephemeris for each satellite in the file.
- getSatellites() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Ocm
-
Get the loaded ephemeris for each satellite in the file.
- getSatellites() - Method in class org.orekit.files.ccsds.ndm.odm.oem.Oem
-
Get the loaded ephemeris for each satellite in the file.
- getSatellites() - Method in interface org.orekit.files.general.AttitudeEphemerisFile
-
Get the loaded ephemeris for each satellite in the file.
- getSatellites() - Method in interface org.orekit.files.general.EphemerisFile
-
Get the loaded ephemeris for each satellite in the file.
- getSatellites() - Method in class org.orekit.files.general.OrekitAttitudeEphemerisFile
-
Get the loaded ephemeris for each satellite in the file.
- getSatellites() - Method in class org.orekit.files.general.OrekitEphemerisFile
-
Get the loaded ephemeris for each satellite in the file.
- getSatellites() - Method in class org.orekit.files.ilrs.CPF
-
Get the loaded ephemeris for each satellite in the file.
- getSatellites() - Method in class org.orekit.files.sp3.SP3
-
- getSatellites() - Method in class org.orekit.gnss.clock.RinexClock
-
Getter for the satellites.
- getSatellitesAntennas() - Method in class org.orekit.gnss.antenna.AntexLoader
-
Get parsed satellites antennas.
- getSatelliteSystem() - Method in class org.orekit.gnss.antenna.SatelliteAntenna
-
Get satellite system.
- getSatelliteSystem() - Method in class org.orekit.gnss.AppliedDCBS
-
Get the satellite system.
- getSatelliteSystem() - Method in class org.orekit.gnss.AppliedPCVS
-
Get the satellite system.
- getSatelliteSystem() - Method in class org.orekit.gnss.clock.RinexClock
-
Getter for the satellite system.
- getSatelliteSystem() - Method in class org.orekit.gnss.CombinedObservationDataSet
-
Get Satellite System.
- getSatelliteSystem() - Method in enum org.orekit.gnss.Frequency
-
Get the satellite system for which this frequency is defined.
- getSatelliteSystem() - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgmMessage
-
Get the satellite system associated to the message.
- getSatelliteSystem() - Method in class org.orekit.gnss.navigation.RinexNavigation
-
Getter for the satellite system.
- getSatelliteSystem() - Method in class org.orekit.gnss.ObservationDataSet
-
Get Satellite System.
- getSatelliteSystem() - Method in class org.orekit.gnss.RinexObservationHeader
-
Get Satellite System.
- getSatelliteSystem() - Method in class org.orekit.gnss.RinexObservationLoader.Parser.PhaseShiftCorrection
-
Get the Satellite System.
- getSatelliteSystem() - Method in class org.orekit.gnss.RinexObservationLoader.Parser.ScaleFactorCorrection
-
Get the Satellite System.
- getSatelliteType() - Method in class org.orekit.gnss.antenna.SatelliteAntenna
-
Get satellite type.
- getSatsCorrected() - Method in class org.orekit.gnss.RinexObservationLoader.Parser.PhaseShiftCorrection
-
Get the list of satellites involved.
- getSaturn() - Method in interface org.orekit.bodies.CelestialBodies
-
Get the Saturn singleton body.
- getSaturn() - Static method in class org.orekit.bodies.CelestialBodyFactory
-
Get the Saturn singleton body.
- getSaturn() - Method in class org.orekit.bodies.LazyLoadedCelestialBodies
-
- getSBASNavigationMessages() - Method in class org.orekit.gnss.navigation.RinexNavigation
-
Get all the SBAS navigation messages contained in the file.
- getSBASNavigationMessages(String) - Method in class org.orekit.gnss.navigation.RinexNavigation
-
Get the SBAS navigation messages for the given satellite Id.
- getSBASOrbitalElements() - Method in class org.orekit.propagation.analytical.gnss.SBASPropagator
-
Get the underlying SBAS orbital elements.
- getScale() - Method in class org.orekit.utils.ParameterDriver
-
Get scale.
- getScale() - Method in class org.orekit.utils.units.PowerTerm
-
Get the scaling factor.
- getScale() - Method in class org.orekit.utils.units.Unit
-
Get the scaling factor to SI units.
- getScaleFactor() - Method in class org.orekit.estimation.measurements.modifiers.AbstractRelativisticClockModifier
-
Get the scale factor used to compute relativistic effect.
- getSclkOffsetAtEpoch() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
-
- getSclkSecPerSISec() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
-
Get the number of spacecraft clock seconds occurring during one SI second.
- getSecInDay() - Method in class org.orekit.time.GLONASSDate
-
Get the number of seconds since Na start.
- getSecond() - Method in class org.orekit.time.TimeComponents
-
Get the seconds number.
- getSecondary() - Method in class org.orekit.bodies.CR3BPSystem
-
Get the secondary CelestialBody.
- getSecondary() - Method in class org.orekit.propagation.events.InterSatDirectViewDetector
-
Get the provider for the secondary satellite.
- getSecondaryObject() - Method in class org.orekit.propagation.events.AngularSeparationFromSatelliteDetector
-
Get the secondaryObject.
- getSecondaryStation() - Method in class org.orekit.estimation.measurements.TurnAroundRange
-
Get the secondary ground station reflecting the signal.
- getSecondsInLocalDay() - Method in class org.orekit.time.TimeComponents
-
Get the second number within the local day,
without applying the
offset from UTC
.
- getSecondsInUTCDay() - Method in class org.orekit.time.TimeComponents
-
- getSecondsOfWeek() - Method in class org.orekit.files.sp3.SP3
-
Returns the seconds of the GPS week as contained in the SP3 file.
- getSegments() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemSatelliteEphemeris
-
Get the segments of the attitude ephemeris.
- getSegments() - Method in class org.orekit.files.ccsds.ndm.NdmConstituent
-
Get the segments.
- getSegments() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmSatelliteEphemeris
-
Get the segments of the ephemeris.
- getSegments() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemSatelliteEphemeris
-
Get the segments of the ephemeris.
- getSegments() - Method in interface org.orekit.files.general.AttitudeEphemerisFile.SatelliteAttitudeEphemeris
-
Get the segments of the attitude ephemeris.
- getSegments() - Method in interface org.orekit.files.general.EphemerisFile.SatelliteEphemeris
-
Get the segments of the ephemeris.
- getSegments() - Method in class org.orekit.files.general.OrekitAttitudeEphemerisFile.OrekitSatelliteAttitudeEphemeris
-
Get the segments of the attitude ephemeris.
- getSegments() - Method in class org.orekit.files.general.OrekitEphemerisFile.OrekitSatelliteEphemeris
-
Get the segments of the ephemeris.
- getSegments() - Method in class org.orekit.files.ilrs.CPF.CPFEphemeris
-
Returns a list containing only this
.
- getSegments() - Method in class org.orekit.files.sp3.SP3.SP3Ephemeris
-
Returns a list containing only this
.
- getSelectedCoefficients() - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator
-
Get the selected short periodic coefficients that must be stored as additional states.
- getSelectedCoefficients() - Method in class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator
-
Get the selected short periodic coefficients that must be stored as additional states.
- getSelectedMu() - Method in class org.orekit.files.ccsds.ndm.odm.OdmParser
-
Select the gravitational coefficient to use.
- getSelectedNormalizedParameters() - Method in class org.orekit.propagation.conversion.AbstractPropagatorBuilder
-
Get the current value of selected normalized parameters.
- getSelectedNormalizedParameters() - Method in interface org.orekit.propagation.conversion.PropagatorBuilder
-
Get the current value of selected normalized parameters.
- getSelectedOrbitalParametersDriversForBuilder(int) - Method in class org.orekit.estimation.leastsquares.AbstractBatchLSModel
-
Get the selected orbital drivers for a propagatorBuilder.
- getSelectedParameters() - Method in class org.orekit.propagation.numerical.EpochDerivativesEquations
-
Get the selected parameters, in Jacobian matrix column order.
- getSelectedParameters() - Method in class org.orekit.propagation.numerical.PartialDerivativesEquations
-
Deprecated.
Get the selected parameters, in Jacobian matrix column order.
- getSelectedPropagationDriversForBuilder(int) - Method in class org.orekit.estimation.leastsquares.AbstractBatchLSModel
-
Get the selected propagation drivers for a propagatorBuilder.
- getSelector() - Method in class org.orekit.estimation.measurements.generation.AbstractScheduler
-
Get the dates selector.
- getSensors() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
-
Get description of sensors used.
- getSensorsN() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
-
Get number of sensors used.
- getSequenceNumber() - Method in class org.orekit.files.ilrs.ILRSHeader
-
Get the ephemeris sequence number.
- getSerialNumber() - Method in class org.orekit.gnss.antenna.ReceiverAntenna
-
Get the serial number.
- getShadowBodies() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
-
Get celestial bodies casting shadows.
- getShadowModel() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
-
Get shadow model used for solar radiation pressure.
- getShortPeriodTerms() - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator
-
Get the short periodic terms.
- getShortPeriodTermsValue(SpacecraftState) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator
-
Get the short period terms value.
- getSic() - Method in class org.orekit.files.ilrs.ILRSHeader
-
Get the SIC ID.
- getSigma() - Method in class org.orekit.estimation.measurements.modifiers.DynamicOutlierFilter
-
Get the current value of sigma.
- getSignalCode() - Method in enum org.orekit.gnss.ObservationType
-
Get the signal code.
- getSignalID() - Method in class org.orekit.gnss.metric.messages.ssr.igm.CodeBias
-
Get the GNSS signal and tracking mode identifier.
- getSignalID() - Method in class org.orekit.gnss.metric.messages.ssr.igm.PhaseBias
-
Get the GNSS signal and tracking mode identifier.
- getSignalStrength() - Method in class org.orekit.gnss.ObservationData
-
Get the signal strength.
- getSignalStrengthUnit() - Method in class org.orekit.gnss.RinexObservationHeader
-
Get the unit of the carrier to noise ratio observables.
- getSignalWideLaneIntegerIndicator() - Method in class org.orekit.gnss.metric.messages.ssr.igm.PhaseBias
-
Get the signal Wide-Lane integer indicator.
- getSij(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution.FieldFourierCjSjCoefficients
-
Get the coefficient Sij.
- getSij(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution.FourierCjSjCoefficients
-
Get the coefficient Sij.
- getSinexCode() - Method in class org.orekit.gnss.antenna.Antenna
-
Get the sinex code of the antenna.
- getSingularPoints() - Method in class org.orekit.models.earth.tessellation.AlongTrackAiming
-
Get points at which aiming direction cannot be computed.
- getSingularPoints() - Method in class org.orekit.models.earth.tessellation.ConstantAzimuthAiming
-
Get points at which aiming direction cannot be computed.
- getSingularPoints() - Method in class org.orekit.models.earth.tessellation.DivertedSingularityAiming
-
Get points at which aiming direction cannot be computed.
- getSingularPoints() - Method in interface org.orekit.models.earth.tessellation.TileAiming
-
Get points at which aiming direction cannot be computed.
- getSisa() - Method in class org.orekit.propagation.analytical.gnss.data.GalileoNavigationMessage
-
Getter for the signal in space accuracy (m).
- getSiteCode() - Method in class org.orekit.files.sinex.Station
-
Get the site code (station identifier).
- getSiteLocation() - Method in class org.orekit.models.earth.displacement.OceanLoadingCoefficients
-
Get the site location.
- getSiteName() - Method in class org.orekit.models.earth.displacement.OceanLoadingCoefficients
-
Get the site name.
- getSites() - Method in class org.orekit.models.earth.displacement.OceanLoadingCoefficientsBLQFactory
-
Get the list of sites for which we have found coefficients, in lexicographic order ignoring case.
- getSize() - Method in class org.orekit.estimation.measurements.gnss.AbstractLambdaMethod
-
Get the size of the problem.
- getSize() - Method in class org.orekit.utils.LoveNumbers
-
Get the size of the arrays.
- getSj(int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.CjSjCoefficient
-
Get the Sj coefficient.
- getSj(int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldCjSjCoefficient
-
Get the Sj coefficient.
- getSlope() - Method in class org.orekit.time.OffsetModel
-
Offset slope in seconds per UTC day (TAI minus UTC / dUTC).
- getSlots() - Method in class org.orekit.utils.GenericTimeStampedCache
-
Get the number of slots in use.
- getSlotsEvictions() - Method in class org.orekit.utils.GenericTimeStampedCache
-
Get the number of slots evictions.
- getSma() - Method in class org.orekit.propagation.analytical.gnss.data.CommonGnssData
-
Getter for the semi-major axis.
- getSma() - Method in interface org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElements
-
Gets the Semi-Major Axis.
- getSma() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
-
Get the semi-major axis.
- getSma() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldAuxiliaryElements
-
Get the semi-major axis.
- getSnm() - Method in class org.orekit.gnss.metric.messages.ssr.subtype.SsrIm201Data
-
Get the sine parameters of spherical harmonics expansion of degree N and order M.
- getSnr() - Method in class org.orekit.files.ilrs.CRD.RangeMeasurement
-
Get the signal to noise ratio.
- getSoftwareId() - Method in class org.orekit.files.ilrs.CRDConfiguration.SoftwareConfiguration
-
Get the software configuration ID.
- getSoftwareRecord() - Method in class org.orekit.files.ilrs.CRDConfiguration
-
Get the software configuration record.
- getSolarRadArea() - Method in class org.orekit.files.ccsds.ndm.odm.SpacecraftParameters
-
Get the solar radiation pressure area.
- getSolarRadCoeff() - Method in class org.orekit.files.ccsds.ndm.odm.SpacecraftParameters
-
Get the solar radiation pressure coefficient.
- getSolarSystemBarycenter() - Method in interface org.orekit.bodies.CelestialBodies
-
Get the solar system barycenter aggregated body.
- getSolarSystemBarycenter() - Static method in class org.orekit.bodies.CelestialBodyFactory
-
Get the solar system barycenter aggregated body.
- getSolarSystemBarycenter() - Method in class org.orekit.bodies.LazyLoadedCelestialBodies
-
- getSolidPoleTide(EOPHistory) - Method in enum org.orekit.utils.IERSConventions
-
Get the function computing solid pole tide (ΔC₂₁, ΔS₂₁).
- getSolidTidesModel() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
-
Get solid tides model.
- getSolution() - Method in class org.orekit.estimation.measurements.gnss.IntegerLeastSquareSolution
-
Get the solution array.
- getSolutionsSize() - Method in class org.orekit.estimation.measurements.gnss.AbstractLambdaMethod
-
Get the number of solutions found.
- getSolveN() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
-
Get number of solved-for states.
- getSolveStates() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
-
Get description of state elements solved-for.
- getSource() - Method in class org.orekit.files.ilrs.CPFHeader
-
Get the ephemeris source.
- getSource() - Method in class org.orekit.propagation.analytical.gnss.data.GPSAlmanac
-
Gets the source of this GPS almanac.
- getSource() - Method in class org.orekit.propagation.analytical.gnss.data.QZSSAlmanac
-
Gets the source of this QZSS almanac.
- getSourceDCBS() - Method in class org.orekit.gnss.AppliedDCBS
-
Get the source of corrections.
- getSourceIdentifier() - Method in class org.orekit.gnss.metric.ntrip.CasterRecord
-
Get the source identifier.
- getSourceIdentifier() - Method in class org.orekit.gnss.metric.ntrip.DataStreamRecord
-
Get the source identifier.
- getSourcePCVS() - Method in class org.orekit.gnss.AppliedPCVS
-
Get the source of corrections.
- getSourceString() - Method in enum org.orekit.errors.OrekitMessages
- getSourceTable() - Method in class org.orekit.gnss.metric.ntrip.NtripClient
-
Get a sourcetable.
- getSouth() - Method in class org.orekit.bodies.FieldGeodeticPoint
-
Get the direction to the south of point, expressed in parent shape frame.
- getSouth() - Method in class org.orekit.bodies.GeodeticPoint
-
Get the direction to the south of point, expressed in parent shape frame.
- getSouth() - Method in class org.orekit.frames.TopocentricFrame
-
Get the south direction of topocentric frame, expressed in parent shape frame.
- getSouthAmplitude(int, int) - Method in class org.orekit.models.earth.displacement.OceanLoadingCoefficients
-
Get the amplitude along South axis.
- getSouthPhase(int, int) - Method in class org.orekit.models.earth.displacement.OceanLoadingCoefficients
-
Get the phase along South axis.
- getSpacecraft() - Method in class org.orekit.forces.drag.DragForce
-
Get spacecraft that are sensitive to atmospheric drag forces.
- getSpacecraft() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTAtmosphericDrag
-
Get spacecraft shape.
- getSpacecraft() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTSolarRadiationPressure
-
Get spacecraft shape.
- getSpacecraftBodyFrame() - Method in class org.orekit.files.ccsds.ndm.adm.AttitudeEndoints
-
Get the spacecraft body frame.
- getSpacecraftClockAndDriftApplied() - Method in class org.orekit.files.ilrs.CRDConfiguration.TransponderConfiguration
-
Get the spacecraft clock offset and drift applied indicator.
- getSpacecraftEpochTimeScale() - Method in class org.orekit.files.ilrs.CRDHeader
-
Get the spacecraft epoch time scale.
- getSpacecraftParametersBlock() - Method in class org.orekit.files.ccsds.ndm.adm.apm.ApmData
-
Get the spacecraft parameters logical block.
- getSpacecraftParametersBlock() - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmData
-
Get the spacecraft parameters logical block.
- getSpacecraftParametersBlock() - Method in class org.orekit.files.ccsds.ndm.odm.opm.OpmData
-
Get the spacecraft parameters logical block.
- getSpaceWeatherEpoch() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
-
Get epoch of the Space Weather data.
- getSpaceWeatherSource() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
-
Get Space Weather data source.
- getSpan(AbsoluteDate) - Method in class org.orekit.utils.TimeSpanMap
-
Get the time span containing a specified date.
- getSpanAfter() - Method in class org.orekit.utils.TimeSpanMap.Transition
-
- getSpanBefore() - Method in class org.orekit.utils.TimeSpanMap.Transition
-
- getSpansNumber() - Method in class org.orekit.utils.TimeSpanMap
-
Get the number of spans.
- getSpatialFilter() - Method in class org.orekit.files.ilrs.CRDConfiguration.DetectorConfiguration
-
Get the spatial filter.
- getSpecialXmlElementsBuilders() - Method in class org.orekit.files.ccsds.ndm.adm.AdmParser
-
Get the non-default token builders for special XML elements.
- getSpecialXmlElementsBuilders() - Method in class org.orekit.files.ccsds.ndm.NdmParser
-
Get the non-default token builders for special XML elements.
- getSpecialXmlElementsBuilders() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmParser
-
Get the non-default token builders for special XML elements.
- getSpecialXmlElementsBuilders() - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmParser
-
Get the non-default token builders for special XML elements.
- getSpecialXmlElementsBuilders() - Method in class org.orekit.files.ccsds.ndm.odm.opm.OpmParser
-
Get the non-default token builders for special XML elements.
- getSpecialXmlElementsBuilders() - Method in interface org.orekit.files.ccsds.utils.lexical.MessageParser
-
Get the non-default token builders for special XML elements.
- getSpecialXmlElementsBuilders() - Method in class org.orekit.files.ccsds.utils.parsing.AbstractMessageParser
-
Get the non-default token builders for special XML elements.
- getSpecifier() - Method in interface org.orekit.errors.LocalizedException
-
Get the localizable specifier of the error message.
- getSpecifier() - Method in exception org.orekit.errors.OrekitException
-
Get the localizable specifier of the error message.
- getSpecifier() - Method in exception org.orekit.errors.OrekitIllegalArgumentException
-
Get the localizable specifier of the error message.
- getSpecifier() - Method in exception org.orekit.errors.OrekitIllegalStateException
-
Get the localizable specifier of the error message.
- getSpecifier() - Method in exception org.orekit.errors.OrekitInternalError
-
Get the localizable specifier of the error message.
- getSpecifier() - Method in exception org.orekit.errors.OrekitIOException
-
Get the localizable specifier of the error message.
- getSpecifier() - Method in exception org.orekit.errors.OrekitParseException
-
Get the localizable specifier of the error message.
- getSpectralFilter() - Method in class org.orekit.files.ilrs.CRDConfiguration.DetectorConfiguration
-
Get the spectral filter.
- getSphericalHarmonicsDegree() - Method in class org.orekit.gnss.metric.messages.ssr.subtype.SsrIm201Data
-
Get the degree of spherical harmonic expansion.
- getSphericalHarmonicsOrder() - Method in class org.orekit.gnss.metric.messages.ssr.subtype.SsrIm201Data
-
Get the order of spherical harmonic expansion.
- getSpin() - Method in class org.orekit.attitudes.Attitude
-
Get the satellite spin.
- getSpin() - Method in class org.orekit.attitudes.FieldAttitude
-
Get the satellite spin.
- getSpin() - Method in class org.orekit.models.earth.ReferenceEllipsoid
-
Gets the rotation of the ellipsoid about its axis.
- getSpinAlpha() - Method in class org.orekit.files.ccsds.ndm.adm.apm.SpinStabilized
-
Get the right ascension of spin axis vector (rad).
- getSpinAngle() - Method in class org.orekit.files.ccsds.ndm.adm.apm.SpinStabilized
-
Get the phase of the satellite about the spin axis (rad).
- getSpinAngleVel() - Method in class org.orekit.files.ccsds.ndm.adm.apm.SpinStabilized
-
Get the angular velocity of satellite around spin axis (rad/s).
- getSpinDelta() - Method in class org.orekit.files.ccsds.ndm.adm.apm.SpinStabilized
-
Get the declination of the spin axis vector (rad).
- getSpinStabilizedBlock() - Method in class org.orekit.files.ccsds.ndm.adm.apm.ApmData
-
Get the spin-stabilized logical block.
- getSquaredDistance() - Method in class org.orekit.estimation.measurements.gnss.IntegerLeastSquareSolution
-
Get the squared distance to the corresponding float solution.
- getSrpCoefficient() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
-
Get the nominal SRP coefficient.
- getSrpConstantArea() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
-
Get the attitude-independent SRP area, not already into attitude-dependent area along OEB.
- getSrpModel() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
-
Get Solar Radiation Pressure model.
- getSrpUncertainty() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
-
Get the SRP coefficient 1σ uncertainty.
- getSsrEpoch1s() - Method in class org.orekit.gnss.metric.messages.ssr.SsrHeader
-
Get the SSR Epoch Time 1s.
- getSsrIgm01Data() - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm01
-
Get the SSR IGM01 data parsed in the SSR message.
- getSsrIgm02Data() - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm02
-
Get the SSR IGM02 data parsed in the SSR message.
- getSsrIgm03Data() - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm03
-
Get the SSR IGM03 data parsed in the SSR message.
- getSsrIgm04Data() - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm04
-
Get the SSR IGM04 data parsed in the SSR message.
- getSsrIgm05Data() - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm05
-
Get the SSR IGM05 data parsed in the SSR message.
- getSsrIgm06Data() - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm06
-
Get the SSR IGM06 data parsed in the SSR message.
- getSsrIgm07Data() - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm07
-
Get the SSR IGM07 data parsed in the SSR message.
- getSsrMultipleMessageIndicator() - Method in class org.orekit.gnss.metric.messages.ssr.SsrHeader
-
Get the SSR Multiple Message Indicator.
- getSsrProviderId() - Method in class org.orekit.gnss.metric.messages.ssr.SsrHeader
-
Get the SSR Provider ID.
- getSsrSolutionId() - Method in class org.orekit.gnss.metric.messages.ssr.SsrHeader
-
Get the SSR Solution ID.
- getSsrUpdateInterval() - Method in class org.orekit.gnss.metric.messages.ssr.SsrHeader
-
Get the SSR Update Interval.
- getSsrUra() - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm07Data
-
Get the SSR User Range Accuracy (URA).
- getStandardModel(double) - Static method in class org.orekit.models.earth.troposphere.MariniMurrayModel
-
Create a new Marini-Murray model using a standard atmosphere model.
- getStandardModel(double) - Static method in class org.orekit.models.earth.troposphere.MendesPavlisModel
-
Create a new Mendes-Pavlis model using a standard atmosphere model.
- getStandardModel() - Static method in class org.orekit.models.earth.troposphere.SaastamoinenModel
-
Create a new Saastamoinen model using a standard atmosphere model.
- getStart() - Method in class org.orekit.estimation.measurements.generation.AbstractMeasurementBuilder
-
Get the start of the measurements time span.
- getStart() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemMetadata
-
Get the start date of this ephemeris segment.
- getStart() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemSatelliteEphemeris
-
Get the start date of the ephemeris.
- getStart() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemSegment
-
Get the start date of this ephemeris segment.
- getStart() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmSatelliteEphemeris
-
Get the start date of the ephemeris.
- getStart() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistory
-
Get the start date of this ephemeris segment.
- getStart() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemSatelliteEphemeris
-
Get the start date of the ephemeris.
- getStart() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemSegment
-
Get the start date of this ephemeris segment.
- getStart() - Method in interface org.orekit.files.general.AttitudeEphemerisFile.AttitudeEphemerisSegment
-
Get the start date of this ephemeris segment.
- getStart() - Method in interface org.orekit.files.general.AttitudeEphemerisFile.SatelliteAttitudeEphemeris
-
Get the start date of the ephemeris.
- getStart() - Method in interface org.orekit.files.general.EphemerisFile.EphemerisSegment
-
Get the start date of this ephemeris segment.
- getStart() - Method in interface org.orekit.files.general.EphemerisFile.SatelliteEphemeris
-
Get the start date of the ephemeris.
- getStart() - Method in class org.orekit.files.general.OrekitAttitudeEphemerisFile.OrekitAttitudeEphemerisSegment
-
Get the start date of this ephemeris segment.
- getStart() - Method in class org.orekit.files.general.OrekitAttitudeEphemerisFile.OrekitSatelliteAttitudeEphemeris
-
Get the start date of the ephemeris.
- getStart() - Method in class org.orekit.files.general.OrekitEphemerisFile.OrekitEphemerisSegment
-
Get the start date of this ephemeris segment.
- getStart() - Method in class org.orekit.files.general.OrekitEphemerisFile.OrekitSatelliteEphemeris
-
Get the start date of the ephemeris.
- getStart() - Method in class org.orekit.files.ilrs.CPF.CPFEphemeris
-
Get the start date of the ephemeris.
- getStart() - Method in class org.orekit.files.sp3.SP3.SP3Ephemeris
-
- getStart() - Method in class org.orekit.time.OffsetModel
-
Get the date of the offset start.
- getStart() - Method in class org.orekit.utils.TimeSpanMap.Span
-
Get the start of this time span.
- getStartDate() - Method in class org.orekit.forces.maneuvers.ConstantThrustManeuver
-
Get the start date.
- getStartDate() - Method in class org.orekit.forces.maneuvers.trigger.DateBasedManeuverTriggers
-
Get the start date.
- getStartDate() - Method in class org.orekit.frames.EOPHistory
-
Get the date of the first available Earth Orientation Parameters.
- getStartDate() - Method in class org.orekit.gnss.clock.RinexClock.ReferenceClock
-
Getter for the validity period start date.
- getStartDate() - Method in class org.orekit.propagation.AbstractPropagator
-
Get the start date.
- getStartDate() - Method in class org.orekit.propagation.FieldAbstractPropagator
-
Get the start date.
- getStartDetector() - Method in class org.orekit.forces.maneuvers.trigger.StartStopEventsTrigger
-
Getter for the firing start detector.
- getStartDriver() - Method in class org.orekit.propagation.events.FieldParameterDrivenDateIntervalDetector
-
Get the driver for start date.
- getStartDriver() - Method in class org.orekit.propagation.events.ParameterDrivenDateIntervalDetector
-
Get the driver for start date.
- getStartEpoch() - Method in class org.orekit.files.ilrs.ILRSHeader
-
Get the starting epoch (UTC).
- getStartFiringDetector() - Method in class org.orekit.forces.maneuvers.trigger.EventBasedManeuverTriggers
-
Getter for the start firing detector.
- getStartTime() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemMetadata
-
Get start of total time span covered by attitude data.
- getStartTime() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
-
Get the time of the earliest data contained in the OCM.
- getStartTime() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemMetadata
-
Get start of total time span covered by ephemerides data and
covariance data.
- getStartTime() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
-
Getter for the startTime.
- getStartTransition() - Method in class org.orekit.utils.TimeSpanMap.Span
-
Get the transition at start of this time span.
- getState(IonosphericModel) - Method in class org.orekit.estimation.measurements.modifiers.IonosphericGradientConverter
-
Get the state with the number of parameters consistent with ionospheric model.
- getState(DiscreteTroposphericModel) - Method in class org.orekit.estimation.measurements.modifiers.TroposphericGradientConverter
-
Get the state with the number of parameters consistent with tropospheric model.
- getState() - Method in class org.orekit.propagation.analytical.AbstractAnalyticalGradientConverter
-
Get the state with the number of parameters consistent with the propagation model.
- getState() - Method in class org.orekit.propagation.events.EventsLogger.LoggedEvent
-
Get the triggering state.
- getState() - Method in class org.orekit.propagation.events.FieldEventsLogger.FieldLoggedEvent
-
Get the triggering state.
- getState() - Method in class org.orekit.propagation.events.handlers.FieldRecordAndContinue.Event
-
Get the spacecraft's state at the event.
- getState() - Method in class org.orekit.propagation.events.handlers.RecordAndContinue.Event
-
Get the spacecraft's state at the event.
- getStateDerivatives(int) - Method in class org.orekit.estimation.measurements.EstimatedMeasurement
-
- getStateJacobian(SpacecraftState, double[][]) - Method in class org.orekit.propagation.analytical.tle.TLEJacobiansMapper
-
Get the Jacobian with respect to state from a one-dimensional additional state array.
- getStateJacobian(SpacecraftState, double[][]) - Method in class org.orekit.propagation.integration.AbstractJacobiansMapper
-
Get the Jacobian with respect to state from a one-dimensional additional state array.
- getStateJacobian(SpacecraftState, double[][]) - Method in class org.orekit.propagation.numerical.JacobiansMapper
-
Get the Jacobian with respect to state from a one-dimensional additional state array.
- getStateJacobian(SpacecraftState, double[][]) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTJacobiansMapper
-
Get the Jacobian with respect to state from a one-dimensional additional state array.
- getStates() - Method in class org.orekit.estimation.measurements.EstimatedMeasurement
-
Get the states of the spacecrafts.
- getStateSize() - Method in class org.orekit.estimation.measurements.EstimatedMeasurement
-
Get state size.
- getStateTransitionMatrix(SpacecraftState) - Method in class org.orekit.propagation.AbstractMatricesHarvester
-
Extract state transition matrix from state.
- getStateTransitionMatrix(SpacecraftState) - Method in class org.orekit.propagation.analytical.AbstractAnalyticalMatricesHarvester
-
Extract state transition matrix from state.
- getStateTransitionMatrix(SpacecraftState) - Method in class org.orekit.propagation.integration.AbstractJacobiansMapper
-
Extract state transition matrix from state.
- getStateTransitionMatrix(SpacecraftState) - Method in interface org.orekit.propagation.MatricesHarvester
-
Extract state transition matrix from state.
- getStateTransitionMatrix(SpacecraftState) - Method in class org.orekit.propagation.numerical.cr3bp.STMEquations
-
Method returning the State Transition Matrix.
- getStateTransitionMatrix(SpacecraftState) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTHarvester
-
Extract state transition matrix from state.
- getStateType() - Method in class org.orekit.propagation.conversion.DSSTPropagatorBuilder
-
Get the type of the elements used to define the orbital state (mean or osculating).
- getStateVectorBlock() - Method in class org.orekit.files.ccsds.ndm.odm.opm.OpmData
-
Get the state vector logical block.
- getStation() - Method in class org.orekit.estimation.measurements.AngularAzEl
-
Get the ground station from which measurement is performed.
- getStation() - Method in class org.orekit.estimation.measurements.AngularRaDec
-
Get the ground station from which measurement is performed.
- getStation() - Method in class org.orekit.estimation.measurements.gnss.Phase
-
Get the ground station from which measurement is performed.
- getStation() - Method in class org.orekit.estimation.measurements.Range
-
Get the ground station from which measurement is performed.
- getStation() - Method in class org.orekit.estimation.measurements.RangeRate
-
Get the ground station from which measurement is performed.
- getStation(String) - Method in class org.orekit.files.sinex.SinexLoader
-
Get the station corresponding to the given site code.
- getStationClockAndDriftApplied() - Method in class org.orekit.files.ilrs.CRDConfiguration.TransponderConfiguration
-
Get the station clock offset and drift applied indicator.
- getStationIdentifier() - Method in class org.orekit.gnss.clock.RinexClock
-
Getter for the station identifier.
- getStationName() - Method in class org.orekit.files.ilrs.CRDHeader
-
Get the station name from official list.
- getStationName() - Method in class org.orekit.gnss.clock.RinexClock
-
Getter for the station name.
- getStationNetword() - Method in class org.orekit.files.ilrs.CRDHeader
-
Get the station network.
- getStationOscDrift() - Method in class org.orekit.files.ilrs.CRDConfiguration.TransponderConfiguration
-
Get the estimated station oscillator drift in parts in 10¹⁵.
- getStations() - Method in class org.orekit.files.sinex.SinexLoader
-
Get the parsed station data.
- getStationUTCOffset() - Method in class org.orekit.files.ilrs.CRDConfiguration.TransponderConfiguration
-
Get the estimated station UTC offset.
- getStatus() - Method in class org.orekit.estimation.measurements.EstimatedMeasurement
-
Get the status.
- getStep() - Method in class org.orekit.files.ilrs.CPFHeader
-
Get the time between table entries.
- getStep() - Method in class org.orekit.frames.InterpolatingTransformProvider
-
Get the grid points time step.
- getStep() - Method in class org.orekit.frames.ShiftingTransformProvider
-
Get the grid points time step.
- getStmName() - Method in class org.orekit.propagation.AbstractMatricesHarvester
-
Get the State Transition Matrix state name.
- getStop() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemMetadata
-
Get the end date of this ephemeris segment.
- getStop() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemSatelliteEphemeris
-
Get the end date of the ephemeris.
- getStop() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemSegment
-
Get the end date of this ephemeris segment.
- getStop() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmSatelliteEphemeris
-
Get the end date of the ephemeris.
- getStop() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistory
-
Get the end date of this ephemeris segment.
- getStop() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemSatelliteEphemeris
-
Get the end date of the ephemeris.
- getStop() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemSegment
-
Get the end date of this ephemeris segment.
- getStop() - Method in interface org.orekit.files.general.AttitudeEphemerisFile.AttitudeEphemerisSegment
-
Get the end date of this ephemeris segment.
- getStop() - Method in interface org.orekit.files.general.AttitudeEphemerisFile.SatelliteAttitudeEphemeris
-
Get the end date of the ephemeris.
- getStop() - Method in interface org.orekit.files.general.EphemerisFile.EphemerisSegment
-
Get the end date of this ephemeris segment.
- getStop() - Method in interface org.orekit.files.general.EphemerisFile.SatelliteEphemeris
-
Get the end date of the ephemeris.
- getStop() - Method in class org.orekit.files.general.OrekitAttitudeEphemerisFile.OrekitAttitudeEphemerisSegment
-
Get the end date of this ephemeris segment.
- getStop() - Method in class org.orekit.files.general.OrekitAttitudeEphemerisFile.OrekitSatelliteAttitudeEphemeris
-
Get the end date of the ephemeris.
- getStop() - Method in class org.orekit.files.general.OrekitEphemerisFile.OrekitEphemerisSegment
-
Get the end date of this ephemeris segment.
- getStop() - Method in class org.orekit.files.general.OrekitEphemerisFile.OrekitSatelliteEphemeris
-
Get the end date of the ephemeris.
- getStop() - Method in class org.orekit.files.ilrs.CPF.CPFEphemeris
-
Get the end date of the ephemeris.
- getStop() - Method in class org.orekit.files.sp3.SP3.SP3Ephemeris
-
- getStopDate() - Method in class org.orekit.propagation.events.EventState.EventOccurrence
-
Get the new time for a stop action.
- getStopDate() - Method in class org.orekit.propagation.events.FieldEventState.EventOccurrence
-
Get the new time for a stop action.
- getStopDetector() - Method in class org.orekit.forces.maneuvers.trigger.StartStopEventsTrigger
-
Getter for the firing stop detector.
- getStopDriver() - Method in class org.orekit.propagation.events.FieldParameterDrivenDateIntervalDetector
-
Get the driver for stop date.
- getStopDriver() - Method in class org.orekit.propagation.events.ParameterDrivenDateIntervalDetector
-
Get the driver for stop date.
- getStopFiringDetector() - Method in class org.orekit.forces.maneuvers.trigger.EventBasedManeuverTriggers
-
Getter for the stop firing detector.
- getStopTime() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemMetadata
-
Get end of total time span covered by attitude data.
- getStopTime() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
-
Get the time of the latest data contained in the OCM.
- getStopTime() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemMetadata
-
Get end of total time span covered by ephemerides data and covariance
data.
- getStopTime() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
-
Getter for the stopTime.
- getStream(T) - Method in class org.orekit.data.AbstractListCrawler
-
Get the stream to read from an input.
- getStream(File) - Method in class org.orekit.data.FilesListCrawler
-
Get the stream to read from an input.
- getStream(URL) - Method in class org.orekit.data.NetworkCrawler
-
Get the stream to read from an input.
- getStreamInfoAddress() - Method in class org.orekit.gnss.metric.ntrip.NetworkRecord
-
Get the web address for stream information.
- getStrengthLevel() - Method in class org.orekit.models.earth.atmosphere.data.MarshallSolarActivityFutureEstimation
-
Get the strength level for activity.
- getStuffReference() - Method in class org.orekit.estimation.measurements.gnss.AbstractCycleSlipDetector
-
Get the stuff (all the things needed for, the detector).
- getSubDailySequenceNumber() - Method in class org.orekit.files.ilrs.CPFHeader
-
Get the sub-daily ephemeris sequence number.
- getSun() - Method in interface org.orekit.bodies.CelestialBodies
-
Get the Sun singleton body.
- getSun() - Static method in class org.orekit.bodies.CelestialBodyFactory
-
Get the Sun singleton body.
- getSun() - Method in class org.orekit.bodies.LazyLoadedCelestialBodies
-
- getSun() - Method in class org.orekit.forces.gravity.DeSitterRelativity
-
Get the sun model used to compute De Sitter effect.
- getSunEarthCR3BP(AbsoluteDate, TimeScale) - Static method in class org.orekit.bodies.CR3BPFactory
-
Get the Sun-Earth CR3BP singleton bodies pair.
- getSunJupiterCR3BP(AbsoluteDate, TimeScale) - Static method in class org.orekit.bodies.CR3BPFactory
-
Get the Sun-Jupiter CR3BP singleton bodies pair.
- getSupportedNames() - Method in class org.orekit.data.AbstractSelfFeedingLoader
-
Get the supported names regular expression.
- getSupportedNames() - Method in class org.orekit.forces.gravity.potential.AstronomicalAmplitudeReader
-
Get the regular expression for supported files names.
- getSupportedNames() - Method in class org.orekit.forces.gravity.potential.OceanTidesReader
-
Get the regular expression for supported files names.
- getSupportedNames() - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
-
Get the regular expression for supported files names.
- getSupportedNames() - Method in class org.orekit.gnss.SEMParser
-
- getSupportedNames() - Method in class org.orekit.gnss.YUMAParser
-
- getSupportedNames() - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherData
-
- getSupportedNames() - Method in class org.orekit.models.earth.atmosphere.data.MarshallSolarActivityFutureEstimation
-
- getSupportedNames() - Method in class org.orekit.models.earth.ionosphere.KlobucharIonoCoefficientsLoader
-
- getSupportedNames() - Method in class org.orekit.models.earth.troposphere.ViennaModelCoefficientsLoader
-
- getSvAccuracy() - Method in class org.orekit.propagation.analytical.gnss.data.BeidouNavigationMessage
-
Getter for the user SV accuray (meters).
- getSvAccuracy() - Method in class org.orekit.propagation.analytical.gnss.data.GPSNavigationMessage
-
Getter for the user SV accuray (meters).
- getSvAccuracy() - Method in class org.orekit.propagation.analytical.gnss.data.QZSSNavigationMessage
-
Getter for the user SV accuray (meters).
- getSvHealth() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1042Data
-
Get the satellite health status.
- getSvHealth() - Method in class org.orekit.propagation.analytical.gnss.data.GalileoNavigationMessage
-
Getter for the SV health status.
- getSvHealth() - Method in class org.orekit.propagation.analytical.gnss.data.GPSNavigationMessage
-
Getter for the satellite health status.
- getSvHealth() - Method in class org.orekit.propagation.analytical.gnss.data.IRNSSNavigationMessage
-
Getter for the satellite health status.
- getSvHealth() - Method in class org.orekit.propagation.analytical.gnss.data.QZSSNavigationMessage
-
Getter for the satellite health status.
- getSVN() - Method in class org.orekit.propagation.analytical.gnss.data.GPSAlmanac
-
Gets the satellite "SVN" reference number.
- getSystem(CelestialBody, CelestialBody, double) - Static method in class org.orekit.bodies.CR3BPFactory
-
Get the corresponding CR3BP System.
- getSystemId() - Method in class org.orekit.files.ilrs.CRDConfiguration.SystemConfiguration
-
Get the system configuration ID.
- getSystemIdentifier() - Method in class org.orekit.files.ilrs.CRDHeader
-
Get the system identifier.
- getSystemNumber() - Method in class org.orekit.files.ilrs.CRDHeader
-
Get the system number.
- getSystemObservationTypes() - Method in class org.orekit.gnss.clock.RinexClock
-
Getter for the different observation type for each satellite system.
- getSystemOccupancy() - Method in class org.orekit.files.ilrs.CRDHeader
-
Get the system occupancy.
- getSystemRecord() - Method in class org.orekit.files.ilrs.CRDConfiguration
-
Get the system configuration record.
- getTabDensity() - Method in class org.orekit.models.earth.atmosphere.HarrisPriester
-
Get the current density table.
- getTable() - Method in class org.orekit.attitudes.TabulatedLofOffset
-
Get an unmodifiable view of the tabulated attitudes.
- getTAI() - Method in class org.orekit.time.LazyLoadedTimeScales
-
- getTAI() - Method in interface org.orekit.time.TimeScales
-
Get the International Atomic Time scale.
- getTAI() - Static method in class org.orekit.time.TimeScalesFactory
-
Get the International Atomic Time scale.
- getTaimutcT0() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
-
- getTargetClass() - Method in class org.orekit.files.ilrs.ILRSHeader
-
Get the target class.
- getTargetLocation() - Method in class org.orekit.files.ilrs.ILRSHeader
-
Get the target location.
- getTargetPV(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.BodyCenterPointing
-
Compute the target point position/velocity in specified frame.
- getTargetPV(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.BodyCenterPointing
-
Compute the target point position/velocity in specified frame.
- getTargetPV(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.GroundPointing
-
Compute the target point position/velocity in specified frame.
- getTargetPV(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.GroundPointing
-
Compute the target point position/velocity in specified frame.
- getTargetPV(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.LofOffsetPointing
-
Compute the target point position/velocity in specified frame.
- getTargetPV(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.LofOffsetPointing
-
Compute the target point position/velocity in specified frame.
- getTargetPV(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.NadirPointing
-
Compute the target point position/velocity in specified frame.
- getTargetPV(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.NadirPointing
-
Compute the target point position/velocity in specified frame.
- getTargetPV(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.TargetPointing
-
Compute the target point position/velocity in specified frame.
- getTargetPV(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.TargetPointing
-
Compute the target point position/velocity in specified frame.
- getTargetPV(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.YawCompensation
-
Compute the target point position/velocity in specified frame.
- getTargetPV(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.YawCompensation
-
Compute the target point position/velocity in specified frame.
- getTargetPV(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.YawSteering
-
Compute the target point position/velocity in specified frame.
- getTargetPV(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.YawSteering
-
Compute the target point position/velocity in specified frame.
- getTargetSize() - Method in class org.orekit.propagation.conversion.AbstractPropagatorConverter
-
Get the size of the target.
- getTauC() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data
-
Get the GLONASS time scale correction to UTC time.
- getTauGps() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data
-
Get the correction to GPS time relative to GLONASS time.
- getTauMultiplier() - Method in class org.orekit.models.earth.displacement.Tide
-
Get the multiplier for the τ Doodson argument.
- getTC() - Method in class org.orekit.data.DelaunayArguments
-
Get the offset in Julian centuries.
- getTC() - Method in class org.orekit.data.FieldDelaunayArguments
-
Get the offset in Julian centuries.
- getTCB() - Method in class org.orekit.time.LazyLoadedTimeScales
-
- getTCB() - Method in interface org.orekit.time.TimeScales
-
Get the Barycentric Coordinate Time scale.
- getTCB() - Static method in class org.orekit.time.TimeScalesFactory
-
Get the Barycentric Coordinate Time scale.
- getTCG() - Method in class org.orekit.time.LazyLoadedTimeScales
-
- getTCG() - Method in interface org.orekit.time.TimeScales
-
Get the Geocentric Coordinate Time scale.
- getTCG() - Static method in class org.orekit.time.TimeScalesFactory
-
Get the Geocentric Coordinate Time scale.
- getTDB() - Method in class org.orekit.time.LazyLoadedTimeScales
-
- getTDB() - Method in interface org.orekit.time.TimeScales
-
Get the Barycentric Dynamic Time scale.
- getTDB() - Static method in class org.orekit.time.TimeScalesFactory
-
Get the Barycentric Dynamic Time scale.
- getTdim() - Method in class org.orekit.bodies.CR3BPSystem
-
Get the CR3BP orbital period of m2 around m1.
- getTdmMessageLink() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
-
Get the Unique identifier of Tracking Data Message linked to this Orbit Data Message.
- getTdop() - Method in class org.orekit.gnss.DOP
-
Gets the time dilution of precision.
- getTEC(AbsoluteDate, GeodeticPoint) - Method in class org.orekit.models.earth.ionosphere.GlobalIonosphereMapModel
-
Computes the Total Electron Content (TEC) at a given date by performing a
temporal interpolation with the two closest date in the IONEX file.
- getTEC(FieldAbsoluteDate<T>, GeodeticPoint) - Method in class org.orekit.models.earth.ionosphere.GlobalIonosphereMapModel
-
Computes the Total Electron Content (TEC) at a given date by performing a
temporal interpolation with the two closest date in the IONEX file.
- getTechAddress() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
-
Get the address of Technical Point Of Contact at originator.
- getTechOrg() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
-
Get the creating agency or operator.
- getTechPhone() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
-
Get the phone number of Technical Point Of Contact at originator.
- getTechPOC() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
-
Get the Technical Point Of Contact at originator.
- getTechPosition() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
-
Get the position of Technical Point Of Contact at originator.
- getTEME() - Method in class org.orekit.frames.AbstractFrames
-
- getTEME() - Method in interface org.orekit.frames.Frames
-
Get the TEME reference frame.
- getTEME() - Static method in class org.orekit.frames.FramesFactory
-
Get the TEME reference frame.
- getTemperature() - Method in class org.orekit.files.ilrs.CRD.MeteorologicalMeasurement
-
Get the surface temperature.
- getTemperature() - Method in class org.orekit.models.earth.EarthStandardAtmosphereRefraction
-
Get the local temperature at the evaluation location.
- getTemperature() - Method in class org.orekit.models.earth.weather.GlobalPressureTemperature2Model
-
Returns the temperature at the station [K].
- getTemperature() - Method in class org.orekit.models.earth.weather.GlobalPressureTemperatureModel
-
Get the atmospheric temperature of the station depending its position.
- getTemplateTLE() - Method in class org.orekit.propagation.conversion.TLEPropagatorBuilder
-
Getter for the template TLE.
- getTempSensorManufacturer() - Method in class org.orekit.files.ilrs.CRDConfiguration.MeteorologicalConfiguration
-
Get the temperature sensor manufacturer.
- getTempSensorModel() - Method in class org.orekit.files.ilrs.CRDConfiguration.MeteorologicalConfiguration
-
Get the temperature sensor model.
- getTempSensorSerialNumber() - Method in class org.orekit.files.ilrs.CRDConfiguration.MeteorologicalConfiguration
-
Get the temperature sensor serial number.
- getTFirstObs() - Method in class org.orekit.gnss.RinexObservationHeader
-
Get the time of First observation record.
- getTGD() - Method in interface org.orekit.propagation.analytical.gnss.data.GNSSClockElements
-
Gets the estimated group delay differential TGD for L1-L2 correction.
- getTGD() - Method in class org.orekit.propagation.analytical.gnss.data.GPSAlmanac
-
Gets for the Group Delay Differential (s).
- getTGD() - Method in class org.orekit.propagation.analytical.gnss.data.GPSNavigationMessage
-
Getter for the Group Delay Differential (s).
- getTGD() - Method in class org.orekit.propagation.analytical.gnss.data.IRNSSNavigationMessage
-
Getter for the estimated group delay differential TGD for L5-S correction.
- getTGD() - Method in class org.orekit.propagation.analytical.gnss.data.QZSSNavigationMessage
-
Getter for the Group Delay Differential (s).
- getTGD1() - Method in class org.orekit.propagation.analytical.gnss.data.BeidouNavigationMessage
-
Getter for the estimated group delay differential TGD1 for B1I signal.
- getTGD2() - Method in class org.orekit.propagation.analytical.gnss.data.BeidouNavigationMessage
-
Getter for the estimated group delay differential TGD for B2I signal.
- getTheoreticalStandardDeviation() - Method in class org.orekit.estimation.measurements.AbstractMeasurement
-
Get the theoretical standard deviation.
- getTheoreticalStandardDeviation() - Method in class org.orekit.estimation.measurements.generation.AbstractMeasurementBuilder
-
Get the theoretical standard deviation.
- getTheoreticalStandardDeviation() - Method in interface org.orekit.estimation.measurements.ObservedMeasurement
-
Get the theoretical standard deviation.
- getTheta() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseralContext
-
Get Central body rotation angle θ.
- getTheta() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTTesseralContext
-
Get Central body rotation angle θ.
- getTheta0() - Method in class org.orekit.models.earth.EarthITU453AtmosphereRefraction
-
Get the station elevation angle under free-space propagation .
- getThetaMin() - Method in class org.orekit.models.earth.EarthITU453AtmosphereRefraction
-
Get the station minimal elevation angle.
- getThreeHourlyAp() - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherDataLoader.LineParameters
-
Gets the array of the eight three-hourly Ap indices for the current entry.
- getThreeHourlyAp(int) - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherDataLoader.LineParameters
-
Gets the three-hourly Ap index at index i from the threeHourlyAp array.
- getThreeHourlyKP(AbsoluteDate) - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherData
-
Get the value of the 3 hours geomagnetic index.
- getThreeHourlyKp() - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherDataLoader.LineParameters
-
Gets the array of the eight three-hourly Kp indices for the current entry.
- getThreeHourlyKp(int) - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherDataLoader.LineParameters
-
Gets the three-hourly Kp index at index i from the threeHourlyKp array.
- getThreeHourlyKP(AbsoluteDate) - Method in class org.orekit.models.earth.atmosphere.data.MarshallSolarActivityFutureEstimation
-
Get the value of the 3 hours geomagnetic index.
- getThreeHourlyKP(AbsoluteDate) - Method in interface org.orekit.models.earth.atmosphere.DTM2000InputParameters
-
Get the value of the 3 hours geomagnetic index.
- getThreshold() - Method in class org.orekit.propagation.events.AbstractDetector
-
Get the convergence threshold in the event time search.
- getThreshold() - Method in class org.orekit.propagation.events.AdapterDetector
-
Get the convergence threshold in the event time search.
- getThreshold() - Method in interface org.orekit.propagation.events.EventDetector
-
Get the convergence threshold in the event time search.
- getThreshold() - Method in class org.orekit.propagation.events.FieldAbstractDetector
-
Get the convergence threshold in the event time search.
- getThreshold() - Method in interface org.orekit.propagation.events.FieldEventDetector
-
Get the convergence threshold in the event time search.
- getThrust() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Maneuver
-
Get thrust.
- getThrust() - Method in class org.orekit.forces.maneuvers.ConfigurableLowThrustManeuver
-
Get the thrust.
- getThrust() - Method in class org.orekit.forces.maneuvers.ConstantThrustManeuver
-
Get the thrust.
- getThrust() - Method in class org.orekit.forces.maneuvers.propulsion.AbstractConstantThrustPropulsionModel
-
Get the thrust value (N).
- getThrust(SpacecraftState) - Method in interface org.orekit.forces.maneuvers.propulsion.ThrustPropulsionModel
-
Get the thrust norm (N).
- getThrustDirectionProvider() - Method in class org.orekit.forces.maneuvers.ConfigurableLowThrustManeuver
-
Getter on Thrust direction and spaceraft attitude provided by an external
object.
- getThrustDirectionSigma() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Maneuver
-
Get one σ angular off-nominal thrust direction.
- getThrustEfficiency() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Maneuver
-
Get thrust efficiency η.
- getThrusterAxisInSatelliteFrame() - Method in class org.orekit.forces.maneuvers.propulsion.ThrustDirectionAndAttitudeProvider
-
Thruster axis in satellite frame.
- getThrustInterpolation() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Maneuver
-
Get interpolation mode between current and next thrust line.
- getThrustIsp() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Maneuver
-
Get thrust specific impulse.
- getThrustMagnitudeSigma() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Maneuver
-
Get one σ percent error on thrust magnitude.
- getThrustVector() - Method in class org.orekit.forces.maneuvers.ConstantThrustManeuver
-
Get the thrust vector (N) in S/C frame.
- getThrustVector(SpacecraftState) - Method in class org.orekit.forces.maneuvers.propulsion.AbstractConstantThrustPropulsionModel
-
Get the thrust vector in spacecraft frame (N).
- getThrustVector(SpacecraftState, double[]) - Method in class org.orekit.forces.maneuvers.propulsion.AbstractConstantThrustPropulsionModel
-
Get the thrust vector in spacecraft frame (N).
- getThrustVector(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.maneuvers.propulsion.AbstractConstantThrustPropulsionModel
-
Get the thrust vector in spacecraft frame (N).
- getThrustVector() - Method in class org.orekit.forces.maneuvers.propulsion.AbstractConstantThrustPropulsionModel
-
Get the thrust vector in spacecraft frame (N).
- getThrustVector(double[]) - Method in class org.orekit.forces.maneuvers.propulsion.AbstractConstantThrustPropulsionModel
-
Get the thrust vector in spacecraft frame (N).
- getThrustVector(T[]) - Method in class org.orekit.forces.maneuvers.propulsion.AbstractConstantThrustPropulsionModel
-
Get the thrust vector in spacecraft frame (N).
- getThrustVector() - Method in class org.orekit.forces.maneuvers.propulsion.BasicConstantThrustPropulsionModel
-
Get the thrust vector in spacecraft frame (N).
- getThrustVector(double[]) - Method in class org.orekit.forces.maneuvers.propulsion.BasicConstantThrustPropulsionModel
-
Get the thrust vector in spacecraft frame (N).
- getThrustVector(T[]) - Method in class org.orekit.forces.maneuvers.propulsion.BasicConstantThrustPropulsionModel
-
Get the thrust vector in spacecraft frame (N).
- getThrustVector() - Method in class org.orekit.forces.maneuvers.propulsion.ScaledConstantThrustPropulsionModel
-
Get the thrust vector in spacecraft frame (N).
- getThrustVector(double[]) - Method in class org.orekit.forces.maneuvers.propulsion.ScaledConstantThrustPropulsionModel
-
Get the thrust vector in spacecraft frame (N).
- getThrustVector(T[]) - Method in class org.orekit.forces.maneuvers.propulsion.ScaledConstantThrustPropulsionModel
-
Get the thrust vector in spacecraft frame (N).
- getThrustVector(SpacecraftState) - Method in interface org.orekit.forces.maneuvers.propulsion.ThrustPropulsionModel
-
Get the thrust vector in spacecraft frame (N).
- getThrustVector(SpacecraftState, double[]) - Method in interface org.orekit.forces.maneuvers.propulsion.ThrustPropulsionModel
-
Get the thrust vector in spacecraft frame (N).
- getThrustVector(FieldSpacecraftState<T>, T[]) - Method in interface org.orekit.forces.maneuvers.propulsion.ThrustPropulsionModel
-
Get the thrust vector in spacecraft frame (N).
- getTidalDisplacementFrequencyCorrectionDiurnal() - Method in enum org.orekit.utils.IERSConventions
-
Get the correction function for tidal displacement for diurnal tides.
- getTidalDisplacementFrequencyCorrectionDiurnal(String, int, int, int, int, int) - Static method in enum org.orekit.utils.IERSConventions
-
Get the correction function for tidal displacement for diurnal tides.
- getTidalDisplacementFrequencyCorrectionZonal() - Method in enum org.orekit.utils.IERSConventions
-
Get the correction function for tidal displacement for zonal tides.
- getTidalDisplacementFrequencyCorrectionZonal(String, int, int, int, int, int) - Static method in enum org.orekit.utils.IERSConventions
-
Get the correction function for tidal displacement for zonal tides.
- getTide(int, int) - Method in class org.orekit.models.earth.displacement.OceanLoadingCoefficients
-
Get the tide.
- getTideFrequencyDependenceFunction(TimeScale) - Method in enum org.orekit.utils.IERSConventions
-
Get the function computing frequency dependent terms (ΔC₂₀, ΔC₂₁, ΔS₂₁, ΔC₂₂, ΔS₂₂).
- getTideFrequencyDependenceFunction(TimeScale, TimeScales) - Method in enum org.orekit.utils.IERSConventions
-
Get the function computing frequency dependent terms (ΔC₂₀, ΔC₂₁, ΔS₂₁, ΔC₂₂,
ΔS₂₂).
- getTideSystem() - Method in class org.orekit.forces.gravity.HolmesFeatherstoneAttractionModel
-
- getTideSystem() - Method in class org.orekit.forces.gravity.potential.CachedNormalizedSphericalHarmonicsProvider
-
- getTideSystem() - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
-
- getTideSystem() - Method in interface org.orekit.forces.gravity.potential.TideSystemProvider
-
- getTime() - Method in class org.orekit.estimation.sequential.MeasurementDecorator
- getTime() - Method in class org.orekit.propagation.analytical.gnss.data.CommonGnssData
-
Getter for the reference time of the GNSS orbit as a duration from week start.
- getTime() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSAlmanac
-
- getTime() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSEphemeris
-
- getTime() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSNavigationMessage
-
Get the Reference Time.
- getTime() - Method in interface org.orekit.propagation.analytical.gnss.data.GLONASSOrbitalElements
-
Get the Reference Time.
- getTime() - Method in interface org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElements
-
Gets the Reference Time of the GNSS orbit as a duration from week start.
- getTime() - Method in class org.orekit.propagation.analytical.gnss.data.SBASNavigationMessage
-
Gets the Reference Time of the SBAS orbit in GPS seconds of the week.
- getTime() - Method in interface org.orekit.propagation.analytical.gnss.data.SBASOrbitalElements
-
Gets the Reference Time of the SBAS orbit in GPS seconds of the week.
- getTime() - Method in class org.orekit.time.DateTimeComponents
-
Get the time component.
- getTime() - Method in class org.orekit.utils.units.Unit
-
Get the time exponent.
- getTimeConverter() - Method in class org.orekit.files.ccsds.utils.generation.AbstractMessageWriter
-
Get the current time converter.
- getTimeOfFlight() - Method in class org.orekit.files.ilrs.CRD.RangeMeasurement
-
Get the time-of-flight.
- getTimeOffset() - Method in class org.orekit.estimation.measurements.EstimatedMeasurement
-
Get the time offset from first state date to measurement date.
- getTimer() - Method in class org.orekit.files.ilrs.CRDConfiguration.TimingSystemConfiguration
-
Get the timer name.
- getTimerSerialNumber() - Method in class org.orekit.files.ilrs.CRDConfiguration.TimingSystemConfiguration
-
Get the timer serial number.
- getTimeScale() - Method in class org.orekit.files.ccsds.definitions.TimeConverter
-
Get the base time scale.
- getTimeScale() - Method in class org.orekit.files.ilrs.CPF
-
Get the time scale used in CPF file.
- getTimeScale() - Method in class org.orekit.files.ilrs.CRDParser
-
Get the time scale used to read the file.
- getTimeScale() - Method in class org.orekit.gnss.clock.RinexClock
-
Getter for the data time scale.
- getTimeScale(TimeScales) - Method in enum org.orekit.gnss.TimeSystem
-
Get the time scale corresponding to time system.
- getTimeScales() - Method in class org.orekit.data.CompositeDataContext
-
- getTimeScales() - Method in interface org.orekit.data.DataContext
-
Get a factory for constructing
TimeScale
s based on the auxiliary data in
this context.
- getTimeScales() - Method in class org.orekit.data.ExceptionalDataContext
-
- getTimeScales() - Method in class org.orekit.data.LazyLoadedDataContext
-
- getTimeScales() - Method in class org.orekit.frames.AbstractFrames
-
Get the time scales.
- getTimeScales() - Method in class org.orekit.frames.EOPHistory
-
Get the time scales used in computing EOP corrections.
- getTimeScales() - Static method in class org.orekit.time.TimeScalesFactory
-
Get the instance of
TimeScales
that is called by all of the static methods
in this class.
- getTimeSinceFirstObservation() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
-
Get time elapsed between first accepted observation on epoch.
- getTimeSinceLastObservation() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
-
Get time elapsed between last accepted observation on epoch.
- getTimeSource() - Method in class org.orekit.files.ilrs.CRDConfiguration.TimingSystemConfiguration
-
Get the time source.
- getTimeSpan() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
-
Get the span of time in seconds that the OCM covers.
- getTimeSystem() - Method in class org.orekit.files.ccsds.section.Metadata
-
Get the Time System that: for OPM, is used for metadata, state vector,
maneuver and covariance data, for OMM, is used for metadata, orbit state
and covariance data, for OEM, is used for metadata, ephemeris and
covariance data.
- getTimeSystem() - Method in class org.orekit.files.ccsds.utils.ContextBinding
-
Get the time system.
- getTimeSystem() - Method in class org.orekit.files.sp3.SP3
-
Returns the
TimeSystem
used to time-stamp position entries.
- getTimeSystem() - Method in class org.orekit.gnss.clock.RinexClock
-
Getter for the file time system.
- getTimeSystemCorrectionA0() - Method in class org.orekit.gnss.navigation.RinexNavigation.TimeSystemCorrection
-
Getter for the A0 coefficient of the time system correction.
- getTimeSystemCorrectionA1() - Method in class org.orekit.gnss.navigation.RinexNavigation.TimeSystemCorrection
-
Getter for the A1 coefficient of the time system correction.
- getTimeSystemCorrections() - Method in class org.orekit.gnss.navigation.RinexNavigation
-
Getter for the time system corrections contained in the file header.
- getTimeSystemCorrectionSecOfWeek() - Method in class org.orekit.gnss.navigation.RinexNavigation.TimeSystemCorrection
-
Getter for the reference time of the time system correction polynomial.
- getTimeSystemCorrectionType() - Method in class org.orekit.gnss.navigation.RinexNavigation.TimeSystemCorrection
-
Getter for the time system correction type.
- getTimeSystemCorrectionWeekNumber() - Method in class org.orekit.gnss.navigation.RinexNavigation.TimeSystemCorrection
-
Getter for the reference week number of the time system correction polynomial.
- getTimetagRef() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
-
Getter for the timetagRef.
- getTimingRecord() - Method in class org.orekit.files.ilrs.CRDConfiguration
-
Get the timing system configuration record.
- getTIRF(IERSConventions) - Method in class org.orekit.frames.AbstractFrames
-
- getTIRF(IERSConventions, boolean) - Method in class org.orekit.frames.AbstractFrames
-
- getTIRF(IERSConventions) - Method in interface org.orekit.frames.Frames
-
Get the TIRF reference frame, ignoring tidal effects.
- getTIRF(IERSConventions, boolean) - Method in interface org.orekit.frames.Frames
-
Get the TIRF reference frame.
- getTIRF(IERSConventions) - Static method in class org.orekit.frames.FramesFactory
-
Get the TIRF reference frame, ignoring tidal effects.
- getTIRF(IERSConventions, boolean) - Static method in class org.orekit.frames.FramesFactory
-
Get the TIRF reference frame.
- getTk() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data
-
Get the time referenced to the beginning of the frame within the current day.
- getTLastObs() - Method in class org.orekit.gnss.RinexObservationHeader
-
Get the time of last observation record.
- getTLE() - Method in class org.orekit.propagation.analytical.tle.FieldTLEPropagator
-
Get the underlying TLE.
- getTLE() - Method in class org.orekit.propagation.analytical.tle.TLEPropagator
-
Get the underlying TLE.
- getTLEBlock() - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmData
-
Get the TLE logical block.
- getTN() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSNavigationMessage
-
Get the correction to the satellite time relative to GLONASS system time.
- getTN() - Method in interface org.orekit.propagation.analytical.gnss.data.GLONASSOrbitalElements
-
Get the correction to the satellite time relative to GLONASS system time.
- getTo() - Method in class org.orekit.utils.units.UnitsConverter
-
Get the destination unit.
- getToc() - Method in interface org.orekit.propagation.analytical.gnss.data.GNSSClockElements
-
Gets the clock correction reference time toc.
- getToc() - Method in interface org.orekit.propagation.analytical.gnss.data.SBASOrbitalElements
-
Gets the clock correction reference time toc.
- getTOD(boolean) - Method in class org.orekit.frames.AbstractFrames
-
- getTOD(IERSConventions, boolean) - Method in class org.orekit.frames.AbstractFrames
-
- getTOD(boolean) - Method in interface org.orekit.frames.Frames
-
Get the TOD reference frame.
- getTOD(IERSConventions, boolean) - Method in interface org.orekit.frames.Frames
-
Get the TOD reference frame.
- getTOD(boolean) - Static method in class org.orekit.frames.FramesFactory
-
Get the TOD reference frame.
- getTOD(IERSConventions, boolean) - Static method in class org.orekit.frames.FramesFactory
-
Get the TOD reference frame.
- getTon2a() - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContributionContext
-
Get ton2a = 2 / (n² * a).
- getTon2a() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldAbstractGaussianContributionContext
-
Get ton2a = 2 / (n² * a).
- getTool() - Method in class org.orekit.files.ccsds.definitions.OdMethodFacade
-
Get the tool used for OD.
- getTopocentricFrame() - Method in class org.orekit.propagation.events.ElevationDetector
-
Returns the currently configured topocentric frame definitions.
- getTopocentricFrame() - Method in class org.orekit.propagation.events.ElevationExtremumDetector
-
Returns the topocentric frame centered on ground point.
- getTopocentricFrame() - Method in class org.orekit.propagation.events.FieldElevationDetector
-
Returns the currently configured topocentric frame definitions.
- getTorque() - Method in class org.orekit.files.ccsds.ndm.adm.apm.Maneuver
-
Get the torque vector (N.m).
- getTotalEclipse() - Method in class org.orekit.propagation.events.EclipseDetector
-
Get the total eclipse detection flag.
- getTotalEclipse() - Method in class org.orekit.propagation.events.FieldEclipseDetector
-
Get the total eclipse detection flag.
- getTotalIntensity() - Method in class org.orekit.models.earth.GeoMagneticElements
-
Returns the total intensity of the magnetic field (= norm of the field vector).
- getTotalLightingRatio(Vector3D, Frame, AbsoluteDate) - Method in class org.orekit.forces.radiation.SolarRadiationPressure
-
Get the total lighting ratio ([0-1]).
- getTotalLightingRatio(FieldVector3D<T>, Frame, FieldAbsoluteDate<T>) - Method in class org.orekit.forces.radiation.SolarRadiationPressure
-
Get the total lighting ratio ([0-1]).
- getTotalNumberOfDataLines() - Method in class org.orekit.gnss.clock.RinexClock
-
Get the total number of complete data lines in the file.
- getTrackId() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
-
Getter for the tracking data identifier.
- getTrackingSoftwares() - Method in class org.orekit.files.ilrs.CRDConfiguration.SoftwareConfiguration
-
Get the tracking softwares.
- getTrackingSoftwareVersions() - Method in class org.orekit.files.ilrs.CRDConfiguration.SoftwareConfiguration
-
Get the tracking software versions.
- getTracksAvailable() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
-
Get number of sensors tracks available for the OD within the actual OD span.
- getTracksUsed() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
-
Get number of sensors tracks accepted for the OD within the actual OD span.
- getTrajBasis() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata
-
Get basis of this trajectory state time history data.
- getTrajBasisID() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata
-
Get identification number of the orbit determination or simulation upon which this trajectory is based.
- getTrajectoryStates() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistory
-
Get the trajectory states.
- getTrajFrameEpoch() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata
-
- getTrajID() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata
-
Get trajectory identification number.
- getTrajNextID() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata
-
Get identification number of next trajectory.
- getTrajPrevID() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata
-
Get identification number of previous trajectory.
- getTrajReferenceFrame() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata
-
Get reference frame of the trajectory.
- getTrajType() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata
-
Get trajectory element set type.
- getTrajUnits() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata
-
Get trajectory element set units.
- getTransform(AbsoluteDate) - Method in class org.orekit.estimation.measurements.EstimatedEarthFrameProvider
-
Get the
Transform
corresponding to specified date.
- getTransform(FieldAbsoluteDate<T>) - Method in class org.orekit.estimation.measurements.EstimatedEarthFrameProvider
-
- getTransform(FieldAbsoluteDate<Gradient>, int, Map<String, Integer>) - Method in class org.orekit.estimation.measurements.EstimatedEarthFrameProvider
-
Get the transform with derivatives.
- getTransform(AbsoluteDate) - Method in class org.orekit.frames.EclipticProvider
-
- getTransform(FieldAbsoluteDate<T>) - Method in class org.orekit.frames.EclipticProvider
-
- getTransform(AbsoluteDate) - Method in class org.orekit.frames.FixedTransformProvider
-
Get the
Transform
corresponding to specified date.
- getTransform(FieldAbsoluteDate<T>) - Method in class org.orekit.frames.FixedTransformProvider
-
- getTransform(AbsoluteDate) - Method in class org.orekit.frames.GTODProvider
-
Get the
Transform
corresponding to specified date.
- getTransform(FieldAbsoluteDate<T>) - Method in class org.orekit.frames.GTODProvider
-
- getTransform(AbsoluteDate) - Method in class org.orekit.frames.HelmertTransformation
-
Get the
Transform
corresponding to specified date.
- getTransform(FieldAbsoluteDate<T>) - Method in class org.orekit.frames.HelmertTransformation
-
- getTransform(AbsoluteDate) - Method in class org.orekit.frames.InterpolatingTransformProvider
-
Get the
Transform
corresponding to specified date.
- getTransform(FieldAbsoluteDate<T>) - Method in class org.orekit.frames.InterpolatingTransformProvider
-
- getTransform(AbsoluteDate) - Method in class org.orekit.frames.ITRFVersion.Converter
-
Get the
Transform
corresponding to specified date.
- getTransform(FieldAbsoluteDate<T>) - Method in class org.orekit.frames.ITRFVersion.Converter
-
- getTransform(AbsoluteDate) - Method in class org.orekit.frames.L1TransformProvider
-
Get the
Transform
corresponding to specified date.
- getTransform(FieldAbsoluteDate<T>) - Method in class org.orekit.frames.L1TransformProvider
-
- getTransform(AbsoluteDate) - Method in class org.orekit.frames.ShiftingTransformProvider
-
Get the
Transform
corresponding to specified date.
- getTransform(FieldAbsoluteDate<T>) - Method in class org.orekit.frames.ShiftingTransformProvider
-
- getTransform(AbsoluteDate) - Method in interface org.orekit.frames.TransformProvider
-
Get the
Transform
corresponding to specified date.
- getTransform(FieldAbsoluteDate<T>) - Method in interface org.orekit.frames.TransformProvider
-
- getTransformation() - Method in enum org.orekit.frames.HelmertTransformation.Predefined
-
- getTransformation(TimeScale) - Method in enum org.orekit.frames.HelmertTransformation.Predefined
-
- getTransformProvider() - Method in class org.orekit.frames.Frame
-
Get the provider for transform from parent frame to instance.
- getTransformTo(Frame, AbsoluteDate) - Method in class org.orekit.frames.Frame
-
Get the transform from the instance to another frame.
- getTransformTo(Frame, FieldAbsoluteDate<T>) - Method in class org.orekit.frames.Frame
-
Get the transform from the instance to another frame.
- getTransitions() - Method in class org.orekit.forces.drag.TimeSpanDragForce
-
- getTransitions() - Method in class org.orekit.forces.empirical.TimeSpanParametricAcceleration
-
- getTransitions() - Method in class org.orekit.models.earth.troposphere.TimeSpanEstimatedTroposphericModel
-
- getTransitions() - Method in class org.orekit.utils.FieldTimeSpanMap
-
Get an unmodifiable view of the sorted transitions.
- getTransitions() - Method in class org.orekit.utils.TimeSpanMap
-
- getTranslation() - Method in class org.orekit.frames.FieldTransform
-
Get the underlying elementary translation.
- getTranslation() - Method in class org.orekit.frames.Transform
-
Get the underlying elementary translation.
- getTransmissionOfSpectralFilter() - Method in class org.orekit.files.ilrs.CRDConfiguration.DetectorConfiguration
-
Get the percentage of transmission of spectral filter.
- getTransmitBand() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
-
Getter for the transmitBand.
- getTransmitDelays() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
-
Getter for the transmitDelays.
- getTranspClkRef() - Method in class org.orekit.files.ilrs.CPFHeader
-
Get the transponder Clock Reference Time.
- getTranspClkRefTime() - Method in class org.orekit.files.ilrs.CRDConfiguration.TransponderConfiguration
-
Get the transponder clock reference time.
- getTransponderId() - Method in class org.orekit.files.ilrs.CRDConfiguration.TransponderConfiguration
-
Get the transponder configuration ID.
- getTransponderRecord() - Method in class org.orekit.files.ilrs.CRDConfiguration
-
Get the transponder configuration record.
- getTranspOscDrift() - Method in class org.orekit.files.ilrs.CPFHeader
-
Get the transponder Oscillator Drift in parts in 10^15.
- getTranspOscDrift() - Method in class org.orekit.files.ilrs.CRDConfiguration.TransponderConfiguration
-
Get the estimated transponder oscillator drift in parts in 10¹⁵.
- getTranspTransmitDelay() - Method in class org.orekit.files.ilrs.CPFHeader
-
Get the transponder transmit delay.
- getTranspUtcOffset() - Method in class org.orekit.files.ilrs.CPFHeader
-
Get the transponder UTC offset.
- getTranspUTCOffset() - Method in class org.orekit.files.ilrs.CRDConfiguration.TransponderConfiguration
-
Get the estimated transponder UTC offset.
- getTrigger() - Method in class org.orekit.forces.maneuvers.ImpulseManeuver
-
Get the triggering event.
- getTriggeredEnd() - Method in class org.orekit.forces.maneuvers.trigger.EventBasedManeuverTriggers
-
Getter for the triggered date of engine stop.
- getTriggeredIncreasing() - Method in enum org.orekit.propagation.events.FilterType
-
Get the increasing status of triggered events.
- getTriggeredStart() - Method in class org.orekit.forces.maneuvers.trigger.EventBasedManeuverTriggers
-
Getter triggered date of engine start.
- getTroposphericModel(AbsoluteDate) - Method in class org.orekit.models.earth.troposphere.TimeSpanEstimatedTroposphericModel
-
- getTrueAnomaly() - Method in class org.orekit.orbits.FieldKeplerianOrbit
-
Get the true anomaly.
- getTrueAnomaly() - Method in class org.orekit.orbits.KeplerianOrbit
-
Get the true anomaly.
- getTrueAnomalyDot() - Method in class org.orekit.orbits.FieldKeplerianOrbit
-
Get the true anomaly derivative.
- getTrueAnomalyDot() - Method in class org.orekit.orbits.KeplerianOrbit
-
Get the true anomaly derivative.
- getTT() - Method in class org.orekit.time.LazyLoadedTimeScales
-
- getTT() - Method in interface org.orekit.time.TimeScales
-
Get the Terrestrial Time scale.
- getTT() - Static method in class org.orekit.time.TimeScalesFactory
-
Get the Terrestrial Time scale.
- getTurnaroundDenominator() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
-
Getter for the turnaroundDenominator.
- getTurnaroundNumerator() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
-
Getter for the turnaroundNumerator.
- getTypAreaForCollisionProbability() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
-
Get the typical (50th percentile) cross-sectional area for collision probability estimation purposes.
- getType() - Method in class org.orekit.files.ccsds.definitions.OdMethodFacade
-
Get the method type.
- getType() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Covariance
-
Get the type of the elements.
- getType() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryState
-
Get the type of the elements.
- getType() - Method in class org.orekit.files.ccsds.ndm.tdm.Observation
-
Get the type of observation.
- getType() - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken
-
Get the type of the token.
- getType() - Method in class org.orekit.files.sp3.SP3
-
- getType() - Method in class org.orekit.gnss.antenna.Antenna
-
Get the type of the antenna.
- getType() - Method in class org.orekit.orbits.CartesianOrbit
-
Get the orbit type.
- getType() - Method in class org.orekit.orbits.CircularOrbit
-
Get the orbit type.
- getType() - Method in class org.orekit.orbits.EquinoctialOrbit
-
Get the orbit type.
- getType() - Method in class org.orekit.orbits.FieldCartesianOrbit
-
Get the orbit type.
- getType() - Method in class org.orekit.orbits.FieldCircularOrbit
-
Get the orbit type.
- getType() - Method in class org.orekit.orbits.FieldEquinoctialOrbit
-
Get the orbit type.
- getType() - Method in class org.orekit.orbits.FieldKeplerianOrbit
-
Get the orbit type.
- getType() - Method in class org.orekit.orbits.FieldOrbit
-
Get the orbit type.
- getType() - Method in class org.orekit.orbits.KeplerianOrbit
-
Get the orbit type.
- getType() - Method in class org.orekit.orbits.Orbit
-
Get the orbit type.
- getTypeCode() - Method in class org.orekit.gnss.metric.messages.ParsedMessage
-
Get the code for the message type.
- getTypeObs() - Method in class org.orekit.gnss.RinexObservationLoader.Parser.PhaseShiftCorrection
-
Get the Carrier Phase Observation Code.
- getTypesObsScaled() - Method in class org.orekit.gnss.RinexObservationLoader.Parser.ScaleFactorCorrection
-
Get the list of Observation Types scaled.
- getU() - Method in class org.orekit.bodies.Ellipse
-
Get the unit vector along the major axis.
- getU1(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution.FieldUijVijCoefficients
-
Get the coefficient U₁j for Fourier index i.
- getU1(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution.UijVijCoefficients
-
Get the coefficient U₁j for Fourier index i.
- getU2(int) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution.FieldUijVijCoefficients
-
Get the coefficient U₂j for Fourier index = 1 (i == 0).
- getU2(int) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution.UijVijCoefficients
-
Get the coefficient U₂j for Fourier index = 1 (i == 0).
- getUnderlyingAttitudeProvider() - Method in interface org.orekit.attitudes.AttitudeProviderModifier
-
Get the underlying attitude provider.
- getUnderlyingAttitudeProvider() - Method in class org.orekit.attitudes.SpinStabilized
-
Get the underlying attitude provider.
- getUnderlyingAttitudeProvider() - Method in class org.orekit.attitudes.YawCompensation
-
Get the underlying (ground pointing) attitude provider.
- getUnderlyingAttitudeProvider() - Method in class org.orekit.attitudes.YawSteering
-
Get the underlying (ground pointing) attitude provider.
- getUndulation(double, double, AbsoluteDate) - Method in class org.orekit.models.earth.Geoid
-
Gets the Undulation of the Geoid, N at the given position.
- getUnit() - Method in enum org.orekit.files.ccsds.ndm.odm.ocm.ManeuverFieldType
-
Get the field unit.
- getUnits() - Method in enum org.orekit.files.ccsds.definitions.ElementsType
-
Get the elements units.
- getUnits() - Method in class org.orekit.files.ccsds.utils.lexical.ParseToken
-
Get the units.
- getUnits(String) - Method in class org.orekit.utils.units.UnitsCache
-
Get units from a string specification.
- getUnnormalizationFactors(int, int) - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory
-
Get a un-normalization factors array.
- getUnnormalizedCnm(int, int) - Method in interface org.orekit.forces.gravity.potential.UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics
-
Get a spherical harmonic cosine coefficient.
- getUnnormalizedProvider(int, int) - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory
-
Get the gravity field coefficients provider from the first supported file.
- getUnnormalizedProvider(double, double, TideSystem, double[][], double[][]) - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory
-
- getUnnormalizedProvider(NormalizedSphericalHarmonicsProvider) - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory
-
- getUnnormalizedProvider(int, int) - Method in interface org.orekit.forces.gravity.potential.GravityFields
-
Get a gravity field unnormalized coefficients provider.
- getUnnormalizedProvider(int, int) - Method in class org.orekit.forces.gravity.potential.LazyLoadedGravityFields
-
Get a gravity field unnormalized coefficients provider.
- getUnnormalizedSnm(int, int) - Method in interface org.orekit.forces.gravity.potential.UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics
-
Get a spherical harmonic sine coefficient.
- getUpperCaseAbbreviation() - Method in enum org.orekit.time.Month
-
Get the upper case three letters abbreviation.
- getUpperCaseName() - Method in enum org.orekit.time.Month
-
Get the upper case full name.
- getURA() - Method in class org.orekit.propagation.analytical.gnss.data.GPSAlmanac
-
Gets the average URA number.
- getURA() - Method in class org.orekit.propagation.analytical.gnss.data.IRNSSNavigationMessage
-
Getter for the user range accuray (meters).
- getURA() - Method in class org.orekit.propagation.analytical.gnss.data.SBASNavigationMessage
-
Getter for the user range accuray (meters).
- getUranus() - Method in interface org.orekit.bodies.CelestialBodies
-
Get the Uranus singleton body.
- getUranus() - Static method in class org.orekit.bodies.CelestialBodyFactory
-
Get the Uranus singleton body.
- getUranus() - Method in class org.orekit.bodies.LazyLoadedCelestialBodies
-
- getUseableStartTime() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemMetadata
-
Get start of useable time span covered by attitude data.
- getUseableStartTime() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata
-
Get start of useable time span covered by ephemerides data, it may be
necessary to allow for proper interpolation.
- getUseableStartTime() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemMetadata
-
Get start of useable time span covered by ephemerides data, it may be
necessary to allow for proper interpolation.
- getUseableStopTime() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemMetadata
-
Get end of useable time span covered by ephemerides data.
- getUseableStopTime() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata
-
Get end of useable time span covered by ephemerides data, it may be
necessary to allow for proper interpolation.
- getUseableStopTime() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemMetadata
-
Get end of useable time span covered by ephemerides data, it may be
necessary to allow for proper interpolation.
- getUsedObservationData() - Method in class org.orekit.gnss.CombinedObservationData
-
Get the list of observation data used to perform the combination of measurements.
- getUserDefinedBlock() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmData
-
Get user defined parameters logical block.
- getUserDefinedBlock() - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmData
-
Get the user defined parameters logical block.
- getUserDefinedBlock() - Method in class org.orekit.files.ccsds.ndm.odm.opm.OpmData
-
Get the user defined parameters logical block.
- getUT1(EOPHistory) - Method in class org.orekit.time.AbstractTimeScales
-
Get the Universal Time 1 scale.
- getUT1(IERSConventions, boolean) - Method in class org.orekit.time.AbstractTimeScales
-
- getUT1(IERSConventions, boolean) - Method in class org.orekit.time.LazyLoadedTimeScales
-
- getUT1(EOPHistory) - Method in class org.orekit.time.LazyLoadedTimeScales
-
Get the Universal Time 1 scale.
- getUT1(IERSConventions, boolean) - Method in interface org.orekit.time.TimeScales
-
Get the Universal Time 1 scale.
- getUT1(IERSConventions, boolean) - Static method in class org.orekit.time.TimeScalesFactory
-
Get the Universal Time 1 scale.
- getUT1(EOPHistory) - Static method in class org.orekit.time.TimeScalesFactory
-
Get the Universal Time 1 scale.
- getUT1MinusUTC() - Method in class org.orekit.frames.EOPEntry
-
Get the UT1-UTC value.
- getUT1MinusUTC(AbsoluteDate) - Method in class org.orekit.frames.EOPHistory
-
Get the UT1-UTC value.
- getUT1MinusUTC(FieldAbsoluteDate<T>) - Method in class org.orekit.frames.EOPHistory
-
Get the UT1-UTC value.
- getUt1mutcT0() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
-
- getUtc() - Method in class org.orekit.frames.AbstractEopLoader
-
Get the UTC time scale.
- getUtc() - Method in class org.orekit.propagation.analytical.tle.TLE
-
Get the UTC time scale used to create this TLE.
- getUTC() - Method in class org.orekit.time.LazyLoadedTimeScales
-
- getUTC() - Method in interface org.orekit.time.TimeScales
-
Get the Universal Time Coordinate scale.
- getUTC() - Static method in class org.orekit.time.TimeScalesFactory
-
Get the Universal Time Coordinate scale.
- getUTCScale() - Method in class org.orekit.time.UT1Scale
-
Get the associated UTC scale.
- getUTCTAIOffsets() - Method in class org.orekit.time.UTCScale
-
Returns the UTC-TAI offsets underlying this UTC scale.
- getV() - Method in class org.orekit.bodies.Ellipse
-
Get the unit vector along the minor axis.
- getV1(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution.FieldUijVijCoefficients
-
Get the coefficient V₁j for Fourier index i.
- getV1(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution.UijVijCoefficients
-
Get the coefficient V₁j for Fourier index i.
- getV2(int) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution.FieldUijVijCoefficients
-
Get the coefficient V₂j for Fourier index = 1 (i == 0).
- getV2(int) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution.UijVijCoefficients
-
Get the coefficient V₂j for Fourier index = 1 (i == 0).
- getValidFrom() - Method in class org.orekit.files.sinex.Station
-
Get start of validity.
- getValidFrom() - Method in class org.orekit.gnss.antenna.SatelliteAntenna
-
Get start of validity.
- getValidityStart() - Method in class org.orekit.time.UTCTAIOffset
-
Get the start time of validity for this offset.
- getValidUntil() - Method in class org.orekit.files.sinex.Station
-
Get end of validity.
- getValidUntil() - Method in class org.orekit.gnss.antenna.SatelliteAntenna
-
Get end of validity.
- getValue() - Method in class org.orekit.estimation.sequential.MeasurementDecorator
- getValue() - Method in class org.orekit.gnss.CombinedObservationData
-
Get the combined observed value.
- getValue() - Method in class org.orekit.gnss.ObservationData
-
Get the observed value.
- getValue(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGammaMnsFunction
-
Get Γ function value.
- getValue(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GammaMnsFunction
-
Get Γ function value.
- getValue(int, T) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.FieldHansenTesseralLinear
-
Compute the value of the Hansen coefficient Kj-n-1, s.
- getValue(int, T) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.FieldHansenThirdBodyLinear
-
Compute the value of the Hansen coefficient K₀n, s.
- getValue(int, T) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.FieldHansenZonalLinear
-
Get the K₀-n-1,s coefficient value.
- getValue(int, double) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenTesseralLinear
-
Compute the value of the Hansen coefficient Kj-n-1, s.
- getValue(int, double) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenThirdBodyLinear
-
Compute the value of the Hansen coefficient K₀n, s.
- getValue(int, double) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenZonalLinear
-
Get the K₀-n-1,s coefficient value.
- getValue(int, int, int, Gradient) - Static method in class org.orekit.propagation.semianalytical.dsst.utilities.JacobiPolynomials
-
Returns the value and derivatives of the Jacobi polynomial Plv,w evaluated at γ.
- getValue(int, int, int, FieldGradient<T>) - Static method in class org.orekit.propagation.semianalytical.dsst.utilities.JacobiPolynomials
-
Returns the value and derivatives of the Jacobi polynomial Plv,w evaluated at γ.
- getValue(int, int, int, int) - Static method in class org.orekit.propagation.semianalytical.dsst.utilities.NewcombOperators
-
Get the Newcomb operator evaluated at n, s, ρ, σ.
- getValue() - Method in class org.orekit.utils.DoubleArrayDictionary.Entry
-
Get the value.
- getValue() - Method in class org.orekit.utils.FieldArrayDictionary.Entry
-
Get the value.
- getValue() - Method in class org.orekit.utils.ParameterDriver
-
Get current parameter value.
- getValue(int, Map<String, Integer>) - Method in class org.orekit.utils.ParameterDriver
-
Get the value as a gradient.
- getValuesSamples() - Method in class org.orekit.utils.InterpolationTableLoader
-
Returns a copy of the values samples for the interpolation function.
- getVdim() - Method in class org.orekit.bodies.CR3BPSystem
-
Get the CR3BP orbital velocity of m2.
- getVdop() - Method in class org.orekit.gnss.DOP
-
Gets the vertical dilution of precision.
- getVectorF() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
-
Get equinoctial frame vector f.
- getVectorF() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldAuxiliaryElements
-
Get equinoctial frame vector f.
- getVectorG() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
-
Get equinoctial frame vector g.
- getVectorG() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldAuxiliaryElements
-
Get equinoctial frame vector g.
- getVectorW() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
-
Get equinoctial frame vector w.
- getVectorW() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldAuxiliaryElements
-
Get equinoctial frame vector w.
- getVeis1950() - Method in class org.orekit.frames.AbstractFrames
-
- getVeis1950() - Method in interface org.orekit.frames.Frames
-
Get the VEIS 1950 reference frame.
- getVeis1950() - Static method in class org.orekit.frames.FramesFactory
-
Get the VEIS 1950 reference frame.
- getVelocity() - Method in class org.orekit.estimation.measurements.PV
-
Get the velocity.
- getVelocity() - Method in class org.orekit.files.sinex.Station
-
Get the station velocity.
- getVelocity() - Method in class org.orekit.frames.FieldTransform
-
Get the first time derivative of the translation.
- getVelocity() - Method in class org.orekit.frames.Transform
-
Get the first time derivative of the translation.
- getVelocity(AbsoluteDate, Vector3D, Frame) - Method in interface org.orekit.models.earth.atmosphere.Atmosphere
-
Get the inertial velocity of atmosphere molecules.
- getVelocity(FieldAbsoluteDate<T>, FieldVector3D<T>, Frame) - Method in interface org.orekit.models.earth.atmosphere.Atmosphere
-
Get the inertial velocity of atmosphere molecules.
- getVelocity() - Method in class org.orekit.utils.FieldPVCoordinates
-
Gets the velocity.
- getVelocity() - Method in class org.orekit.utils.PVCoordinates
-
Gets the velocity.
- getVenus() - Method in interface org.orekit.bodies.CelestialBodies
-
Get the Venus singleton body.
- getVenus() - Static method in class org.orekit.bodies.CelestialBodyFactory
-
Get the Venus singleton body.
- getVenus() - Method in class org.orekit.bodies.LazyLoadedCelestialBodies
-
- getVersion() - Method in class org.orekit.files.ilrs.ILRSHeader
-
Get the format version.
- getVersion() - Method in class org.orekit.frames.ITRFVersionLoader.ITRFVersionConfiguration
-
Get ITRF version.
- getVertices() - Method in class org.orekit.models.earth.tessellation.Tile
-
Get the four vertices.
- getVmAbsolute() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
-
Get the typical (50th percentile) visual magnitude.
- getVmApparent() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
-
Get the typical (50th percentile) apparent visual magnitude.
- getVmApparentMax() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
-
Get the maximum apparent visual magnitude.
- getVmApparentMin() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
-
Get the minimum apparent visual magnitude.
- getVmns(int, int, int) - Static method in class org.orekit.propagation.semianalytical.dsst.utilities.CoefficientsFactory
-
Get the Vn,sm coefficient from Vn,s.
- getVtecQualityIndicator() - Method in class org.orekit.gnss.metric.messages.ssr.subtype.SsrIm201Header
-
Get the VTEC quality indicator.
- getWarmup() - Method in class org.orekit.estimation.measurements.modifiers.OutlierFilter
-
Get the value of warmup iterations.
- getWaterVaporPressure() - Method in class org.orekit.models.earth.weather.GlobalPressureTemperature2Model
-
Returns the water vapor pressure at the station [hPa].
- getWavelength() - Method in class org.orekit.estimation.measurements.gnss.InterSatellitesPhase
-
Get the wavelength.
- getWavelength() - Method in class org.orekit.estimation.measurements.gnss.OneWayGNSSPhase
-
Get the wavelength.
- getWavelength() - Method in class org.orekit.estimation.measurements.gnss.Phase
-
Get the wavelength.
- getWavelength() - Method in class org.orekit.files.ilrs.CRDConfiguration.SystemConfiguration
-
Get the transmit wavelength.
- getWavelength() - Method in enum org.orekit.gnss.Frequency
-
Get the wavelength in meters.
- getWaves() - Method in class org.orekit.forces.gravity.potential.OceanTidesReader
-
Get the loaded waves.
- getWeek() - Method in class org.orekit.propagation.analytical.gnss.data.CommonGnssData
-
Getter for the reference week of the GNSS orbit.
- getWeek() - Method in interface org.orekit.propagation.analytical.gnss.data.GNSSOrbitalElements
-
Gets the Reference Week of the GNSS orbit.
- getWeek() - Method in class org.orekit.propagation.analytical.gnss.data.SBASNavigationMessage
-
Gets the Reference Week of the SBAS orbit.
- getWeek() - Method in interface org.orekit.propagation.analytical.gnss.data.SBASOrbitalElements
-
Gets the Reference Week of the SBAS orbit.
- getWeekNumber() - Method in class org.orekit.time.GNSSDate
-
Get the week number since the GNSS reference epoch.
- getWeightedRms() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
-
Get weighted RMS residual ratio.
- getWest() - Method in class org.orekit.bodies.FieldGeodeticPoint
-
Get the direction to the west of point, expressed in parent shape frame.
- getWest() - Method in class org.orekit.bodies.GeodeticPoint
-
Get the direction to the west of point, expressed in parent shape frame.
- getWest() - Method in class org.orekit.frames.TopocentricFrame
-
Get the west direction of topocentric frame, expressed in parent shape frame.
- getWestAmplitude(int, int) - Method in class org.orekit.models.earth.displacement.OceanLoadingCoefficients
-
Get the amplitude along west axis.
- getWestPhase(int, int) - Method in class org.orekit.models.earth.displacement.OceanLoadingCoefficients
-
Get the phase along West axis.
- getWetMass() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
-
Get the total mass at T₀.
- getWgs84(Frame) - Static method in class org.orekit.models.earth.ReferenceEllipsoid
-
Get the WGS84 ellipsoid, attached to the given body frame.
- getWideLaneCombination(SatelliteSystem) - Static method in class org.orekit.estimation.measurements.gnss.MeasurementCombinationFactory
-
Get the Wide-Lane combination of measurements.
- getWindUp(SatelliteSystem, int, String) - Method in class org.orekit.estimation.measurements.gnss.WindUpFactory
-
Get a modifier for a satellite/receiver pair.
- getWMM(double) - Static method in class org.orekit.models.earth.GeoMagneticFieldFactory
-
Get the WMM model for the given year.
- getWMM(double) - Method in interface org.orekit.models.earth.GeoMagneticFields
-
Get the WMM model for the given year.
- getWMM(double) - Method in class org.orekit.models.earth.LazyLoadedGeoMagneticFields
-
- getX() - Method in class org.orekit.frames.EOPEntry
-
Get the X component of the pole motion.
- getX() - Method in class org.orekit.geometry.fov.SmoothFieldOfView
-
Get the X axis defining FoV boundary.
- getX() - Method in class org.orekit.gnss.clock.RinexClock.Receiver
-
Getter for the X coordinate in meters in considered Earth centered frame.
- getX() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractEphemerisMessage
-
Getter for the satellite X position.
- getX() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSEphemeris
-
- getX() - Method in interface org.orekit.propagation.analytical.gnss.data.GLONASSOrbitalElements
-
Get the ECEF-X component of satellite coordinates in PZ-90 datum.
- getX() - Method in interface org.orekit.propagation.analytical.gnss.data.SBASOrbitalElements
-
Get the ECEF-X component of satellite coordinates.
- getX() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBodyContext
-
Get Χ = 1 / sqrt(1 - e²) = 1 / B.
- getX() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonalContext
-
Get Χ = 1 / sqrt(1 - e²) = 1 / B.
- getX() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTThirdBodyContext
-
Get Χ = 1 / sqrt(1 - e²) = 1 / B.
- getX() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTZonalContext
-
Get Χ = 1 / sqrt(1 - e²) = 1 / B.
- getX2ON2A2XP1() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonalContext
-
Get (χ²) / (n² * a² * (χ + 1 ) ).
- getX2ON2A2XP1() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTZonalContext
-
Get (χ²) / (n² * a² * (χ + 1 ) ).
- getX3ON2A() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonalContext
-
Get χ³ / (n² * a).
- getX3ON2A() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTZonalContext
-
Get χ³ / (n² * a).
- getXDot() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractEphemerisMessage
-
Getter for the satellite X velocity.
- getXDot() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSEphemeris
-
- getXDot() - Method in interface org.orekit.propagation.analytical.gnss.data.GLONASSOrbitalElements
-
Get the ECEF-X component of satellite velocity vector in PZ-90 datum.
- getXDot() - Method in interface org.orekit.propagation.analytical.gnss.data.SBASOrbitalElements
-
Get the ECEF-X component of satellite velocity vector.
- getXDotDot() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractEphemerisMessage
-
Getter for the satellite X acceleration.
- getXDotDot() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSEphemeris
-
- getXDotDot() - Method in interface org.orekit.propagation.analytical.gnss.data.GLONASSOrbitalElements
-
Get the GLONASS ECEF-X component of satellite acceleration vector in PZ-90 datum.
- getXDotDot() - Method in interface org.orekit.propagation.analytical.gnss.data.SBASOrbitalElements
-
Get the ECEF-X component of satellite acceleration vector.
- getXM10(AbsoluteDate) - Method in interface org.orekit.models.earth.atmosphere.JB2008InputParameters
-
Get the MG2 index scaled to F10.
- getXM10B(AbsoluteDate) - Method in interface org.orekit.models.earth.atmosphere.JB2008InputParameters
-
Get the MG2 81-day average centered index.
- getXON2A2() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonalContext
-
Get χ / (n² * a²).
- getXON2A2() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTZonalContext
-
Get χ / (n² * a²).
- getXp() - Method in class org.orekit.frames.FieldPoleCorrection
-
Get the xp parameter.
- getXp() - Method in class org.orekit.frames.PoleCorrection
-
Get the xp parameter.
- getXX() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonalContext
-
Get Χ².
- getXX() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTZonalContext
-
Get Χ².
- getXXX() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonalContext
-
Get Χ³.
- getXXX() - Method in class org.orekit.propagation.semianalytical.dsst.forces.FieldDSSTZonalContext
-
Get Χ³.
- getXYSpXY2Function() - Method in enum org.orekit.utils.IERSConventions
-
Get the function computing the Celestial Intermediate Pole and Celestial Intermediate Origin components.
- getXYSpXY2Function(TimeScales) - Method in enum org.orekit.utils.IERSConventions
-
Get the function computing the Celestial Intermediate Pole and Celestial
Intermediate Origin components.
- getY() - Method in class org.orekit.frames.EOPEntry
-
Get the Y component of the pole motion.
- getY() - Method in class org.orekit.geometry.fov.SmoothFieldOfView
-
Get the Y axis defining FoV boundary.
- getY() - Method in class org.orekit.gnss.clock.RinexClock.Receiver
-
Getter for the Y coordinate in meters in considered Earth centered frame.
- getY() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractEphemerisMessage
-
Getter for the satellite Y position.
- getY() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSEphemeris
-
- getY() - Method in interface org.orekit.propagation.analytical.gnss.data.GLONASSOrbitalElements
-
Get the ECEF-Y component of satellite coordinates in PZ-90 datum.
- getY() - Method in interface org.orekit.propagation.analytical.gnss.data.SBASOrbitalElements
-
Get the ECEF-Y component of satellite coordinates.
- getY10(AbsoluteDate) - Method in interface org.orekit.models.earth.atmosphere.JB2008InputParameters
-
Get the Solar X-Ray & Lya index scaled to F10.
- getY10B(AbsoluteDate) - Method in interface org.orekit.models.earth.atmosphere.JB2008InputParameters
-
Get the Solar X-Ray & Lya 81-day ave.
- getYawAngle(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.YawCompensation
-
Compute the yaw compensation angle at date.
- getYawAngle(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.YawCompensation
-
Compute the yaw compensation angle at date.
- getYawAngle() - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm06Data
-
Get the yaw angle used for computation of phase wind-up correction.
- getYawRate() - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm06Data
-
Get the yaw rate.
- getYDot() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractEphemerisMessage
-
Getter for the satellite Y velocity.
- getYDot() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSEphemeris
-
- getYDot() - Method in interface org.orekit.propagation.analytical.gnss.data.GLONASSOrbitalElements
-
Get the ECEF-Y component of satellite velocity vector in PZ-90 datum.
- getYDot() - Method in interface org.orekit.propagation.analytical.gnss.data.SBASOrbitalElements
-
Get the ECEF-Y component of satellite velocity vector.
- getYDotDot() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractEphemerisMessage
-
Getter for the satellite Y acceleration.
- getYDotDot() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSEphemeris
-
- getYDotDot() - Method in interface org.orekit.propagation.analytical.gnss.data.GLONASSOrbitalElements
-
Get the GLONASS ECEF-Y component of satellite acceleration vector in PZ-90 datum.
- getYDotDot() - Method in interface org.orekit.propagation.analytical.gnss.data.SBASOrbitalElements
-
Get the ECEF-Y component of satellite acceleration vector.
- getYear() - Method in enum org.orekit.frames.ITRFVersion
-
Get the reference year of the frame version.
- getYear() - Method in class org.orekit.time.DateComponents
-
Get the year number.
- getYearOfCentury() - Method in class org.orekit.files.ilrs.CRDHeader
-
Get the year of century from CPF or TLE.
- getYp() - Method in class org.orekit.frames.FieldPoleCorrection
-
Get the yp parameter.
- getYp() - Method in class org.orekit.frames.PoleCorrection
-
Get the yp parameter.
- getZ() - Method in class org.orekit.geometry.fov.SmoothFieldOfView
-
Get the Z axis defining FoV boundary.
- getZ() - Method in class org.orekit.gnss.clock.RinexClock.Receiver
-
Getter for the Z coordinate in meters in considered Earth centered frame.
- getZ() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractEphemerisMessage
-
Getter for the satellite Z position.
- getZ() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSEphemeris
-
- getZ() - Method in interface org.orekit.propagation.analytical.gnss.data.GLONASSOrbitalElements
-
Get the ECEF-Z component of satellite coordinates in PZ-90 datum.
- getZ() - Method in interface org.orekit.propagation.analytical.gnss.data.SBASOrbitalElements
-
Get the ECEF-Z component of satellite coordinates.
- getZDot() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractEphemerisMessage
-
Getter for the satellite Z velocity.
- getZDot() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSEphemeris
-
- getZDot() - Method in interface org.orekit.propagation.analytical.gnss.data.GLONASSOrbitalElements
-
Get the ECEF-Z component of satellite velocity vector in PZ-90 datum.
- getZDot() - Method in interface org.orekit.propagation.analytical.gnss.data.SBASOrbitalElements
-
Get the ECEF-Z component of satellite velocity vector.
- getZDotDot() - Method in class org.orekit.propagation.analytical.gnss.data.AbstractEphemerisMessage
-
Getter for the satellite Z acceleration.
- getZDotDot() - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSEphemeris
-
- getZDotDot() - Method in interface org.orekit.propagation.analytical.gnss.data.GLONASSOrbitalElements
-
Get the GLONASS ECEF-Z component of satellite acceleration vector in PZ-90 datum.
- getZDotDot() - Method in interface org.orekit.propagation.analytical.gnss.data.SBASOrbitalElements
-
Get the ECEF-Z component of satellite acceleration vector.
- getZenith() - Method in class org.orekit.bodies.FieldGeodeticPoint
-
Get the direction above the point, expressed in parent shape frame.
- getZenith() - Method in class org.orekit.bodies.GeodeticPoint
-
Get the direction above the point, expressed in parent shape frame.
- getZenith() - Method in class org.orekit.frames.TopocentricFrame
-
Get the zenith direction of topocentric frame, expressed in parent shape frame.
- getZenithAmplitude(int, int) - Method in class org.orekit.models.earth.displacement.OceanLoadingCoefficients
-
Get the amplitude along zenith axis.
- getZenithDelay() - Method in class org.orekit.models.earth.troposphere.ViennaModelCoefficientsLoader
-
Returns the zenith delay array.
- getZenithOffsetDriver() - Method in class org.orekit.estimation.measurements.GroundStation
-
Get a driver allowing to change station position along Zenith axis.
- getZenithPhase(int, int) - Method in class org.orekit.models.earth.displacement.OceanLoadingCoefficients
-
Get the phase along zenith axis.
- getZero(Field<T>) - Static method in class org.orekit.utils.FieldPVCoordinates
-
Get fixed position/velocity at origin (both p, v and a are zero vectors).
- getZInverseTransformationReference() - Method in class org.orekit.estimation.measurements.gnss.AbstractLambdaMethod
-
Get a reference to the Z inverse transformation matrix.
- getZipJarCrawler(T) - Method in class org.orekit.data.AbstractListCrawler
-
Get a zip/jar crawler for an input.
- getZipJarCrawler(File) - Method in class org.orekit.data.FilesListCrawler
-
Get a zip/jar crawler for an input.
- getZipJarCrawler(URL) - Method in class org.orekit.data.NetworkCrawler
-
Get a zip/jar crawler for an input.
- getZone() - Method in class org.orekit.geometry.fov.PolygonalFieldOfView
-
Get the interior zone.
- getZone() - Method in class org.orekit.propagation.events.FootprintOverlapDetector
-
Get the geographic zone triggering the events.
- getZone() - Method in class org.orekit.propagation.events.GeographicZoneDetector
-
Get the geographic zone.
- GHIJjsPolynomials - Class in org.orekit.propagation.semianalytical.dsst.utilities
-
Compute the Gjs, Hjs, Ijs and Jjs
polynomials in the equinoctial elements h, k and the direction cosines α and β
and their partial derivatives with respect to k, h, α and β.
- GHIJjsPolynomials(double, double, double, double) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
-
Create a set of Gjs, Hjs, Ijs and Jjs polynomials.
- GHmsjPolynomials - Class in org.orekit.propagation.semianalytical.dsst.utilities
-
Compute the Gmsj and the Hmsj
polynomials in the equinoctial elements h, k and the direction cosines α and β
and their partial derivatives with respect to k, h, α and β.
- GHmsjPolynomials(double, double, double, double, int) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.GHmsjPolynomials
-
Create a set of Gmsj and Hmsj polynomials.
- GillIntegratorBuilder - Class in org.orekit.propagation.conversion
-
Builder for GillIntegrator.
- GillIntegratorBuilder(double) - Constructor for class org.orekit.propagation.conversion.GillIntegratorBuilder
-
Build a new instance.
- GlobalIonosphereMapModel - Class in org.orekit.models.earth.ionosphere
-
Global Ionosphere Map (GIM) model.
- GlobalIonosphereMapModel(String) - Constructor for class org.orekit.models.earth.ionosphere.GlobalIonosphereMapModel
-
Constructor with supported names given by user.
- GlobalIonosphereMapModel(String, DataProvidersManager, TimeScale) - Constructor for class org.orekit.models.earth.ionosphere.GlobalIonosphereMapModel
-
Constructor that uses user defined supported names and data context.
- GlobalMappingFunctionModel - Class in org.orekit.models.earth.troposphere
-
The Global Mapping Function model for radio techniques.
- GlobalMappingFunctionModel() - Constructor for class org.orekit.models.earth.troposphere.GlobalMappingFunctionModel
-
Build a new instance.
- GlobalMappingFunctionModel(TimeScale) - Constructor for class org.orekit.models.earth.troposphere.GlobalMappingFunctionModel
-
Build a new instance.
- GlobalPressureTemperature2Model - Class in org.orekit.models.earth.weather
-
The Global Pressure and Temperature 2 (GPT2) model.
- GlobalPressureTemperature2Model(String, double, double, Geoid) - Constructor for class org.orekit.models.earth.weather.GlobalPressureTemperature2Model
-
Constructor with supported names given by user.
- GlobalPressureTemperature2Model(String, double, double, Geoid, DataProvidersManager, TimeScale) - Constructor for class org.orekit.models.earth.weather.GlobalPressureTemperature2Model
-
Constructor with supported names and source of GPT2 auxiliary data given by user.
- GlobalPressureTemperature2Model(double, double, Geoid) - Constructor for class org.orekit.models.earth.weather.GlobalPressureTemperature2Model
-
Constructor with default supported names.
- GlobalPressureTemperatureModel - Class in org.orekit.models.earth.weather
-
The Global Pressure and Temperature model.
- GlobalPressureTemperatureModel(double, double, Frame) - Constructor for class org.orekit.models.earth.weather.GlobalPressureTemperatureModel
-
Build a new instance.
- GlobalPressureTemperatureModel(double, double, Frame, DataContext) - Constructor for class org.orekit.models.earth.weather.GlobalPressureTemperatureModel
-
Build a new instance.
- Glonass - Class in org.orekit.gnss.attitude
-
Attitude providers for Glonass navigation satellites.
- Glonass(double, AbsoluteDate, AbsoluteDate, ExtendedPVCoordinatesProvider, Frame) - Constructor for class org.orekit.gnss.attitude.Glonass
-
Simple constructor.
- GLONASS_EPOCH - Static variable in class org.orekit.time.AbsoluteDate
-
Reference epoch for GLONASS four-year interval number: 1996-01-01T00:00:00 GLONASS time.
- GLONASS_EPOCH - Static variable in class org.orekit.time.DateComponents
-
Reference epoch for GLONASS four-year interval number: 1996-01-01.
- GLONASS_MU - Static variable in interface org.orekit.propagation.analytical.gnss.data.GNSSConstants
-
Value of the Earth's universal gravitational parameter for GLONASS user in m³/s².
- GLONASS_PI - Static variable in interface org.orekit.propagation.analytical.gnss.data.GNSSConstants
-
Value of Pi for conversion from semicircles to radian.
- GLONASSAlmanac - Class in org.orekit.propagation.analytical.gnss.data
-
This class holds a GLONASS almanac as read from .agl files.
- GLONASSAlmanac(int, int, int, int, int, double, double, double, double, double, double, double, double, double, double) - Constructor for class org.orekit.propagation.analytical.gnss.data.GLONASSAlmanac
-
Constructor.
- GLONASSAlmanac(int, int, int, int, int, double, double, double, double, double, double, double, double, double, double, TimeScale) - Constructor for class org.orekit.propagation.analytical.gnss.data.GLONASSAlmanac
-
Constructor.
- GLONASSAnalyticalPropagator - Class in org.orekit.propagation.analytical.gnss
-
- GLONASSAnalyticalPropagatorBuilder - Class in org.orekit.propagation.analytical.gnss
-
This nested class aims at building a GLONASSAnalyticalPropagator.
- GLONASSAnalyticalPropagatorBuilder(GLONASSOrbitalElements) - Constructor for class org.orekit.propagation.analytical.gnss.GLONASSAnalyticalPropagatorBuilder
-
Initializes the builder.
- GLONASSAnalyticalPropagatorBuilder(GLONASSOrbitalElements, DataContext) - Constructor for class org.orekit.propagation.analytical.gnss.GLONASSAnalyticalPropagatorBuilder
-
Initializes the builder.
- GLONASSDate - Class in org.orekit.time
-
Container for date in GLONASS form.
- GLONASSDate(int, int, double) - Constructor for class org.orekit.time.GLONASSDate
-
Build an instance corresponding to a GLONASS date.
- GLONASSDate(int, int, double, TimeScale) - Constructor for class org.orekit.time.GLONASSDate
-
Build an instance corresponding to a GLONASS date.
- GLONASSDate(AbsoluteDate) - Constructor for class org.orekit.time.GLONASSDate
-
Build an instance from an absolute date.
- GLONASSDate(AbsoluteDate, TimeScale) - Constructor for class org.orekit.time.GLONASSDate
-
Build an instance from an absolute date.
- GLONASSEphemeris - Class in org.orekit.propagation.analytical.gnss.data
-
- GLONASSEphemeris(int, int, double, double, double, double, double, double, double, double, double, double) - Constructor for class org.orekit.propagation.analytical.gnss.data.GLONASSEphemeris
-
Build a new instance.
- GLONASSEphemeris(int, int, double, double, double, double, double, double, double, double, double, double, AbsoluteDate) - Constructor for class org.orekit.propagation.analytical.gnss.data.GLONASSEphemeris
-
Build a new instance.
- GLONASSNavigationMessage - Class in org.orekit.propagation.analytical.gnss.data
-
Container for data contained in a Glonass navigation message.
- GLONASSNavigationMessage() - Constructor for class org.orekit.propagation.analytical.gnss.data.GLONASSNavigationMessage
-
Constructor.
- GLONASSNumericalPropagator - Class in org.orekit.propagation.numerical
-
This class propagates GLONASS orbits using numerical integration.
- GLONASSNumericalPropagator(ClassicalRungeKuttaIntegrator, GLONASSOrbitalElements, Frame, AttitudeProvider, double, DataContext, boolean) - Constructor for class org.orekit.propagation.numerical.GLONASSNumericalPropagator
-
Private constructor.
- GLONASSNumericalPropagatorBuilder - Class in org.orekit.propagation.numerical
-
This nested class aims at building a GLONASSNumericalPropagator.
- GLONASSNumericalPropagatorBuilder(ClassicalRungeKuttaIntegrator, GLONASSOrbitalElements, boolean) - Constructor for class org.orekit.propagation.numerical.GLONASSNumericalPropagatorBuilder
-
Initializes the builder.
- GLONASSNumericalPropagatorBuilder(ClassicalRungeKuttaIntegrator, GLONASSOrbitalElements, boolean, DataContext) - Constructor for class org.orekit.propagation.numerical.GLONASSNumericalPropagatorBuilder
-
Initializes the builder.
- GLONASSOrbitalElements - Interface in org.orekit.propagation.analytical.gnss.data
-
- GLONASSScale - Class in org.orekit.time
-
GLONASS time scale.
- GlonassUserRangeAccuracy - Class in org.orekit.gnss.metric.messages.rtcm.ephemeris.utils
-
Enumerate for GLONASS User Range Accuracy.
- GlonassUserRangeAccuracy(int) - Constructor for class org.orekit.gnss.metric.messages.rtcm.ephemeris.utils.GlonassUserRangeAccuracy
-
Simple constructor.
- GMSTScale - Class in org.orekit.time
-
Greenwich Mean Sidereal Time.
- GNSS_PI - Static variable in interface org.orekit.propagation.analytical.gnss.data.GNSSConstants
-
Value of Pi for conversion from semicircles to radians in GNSS.
- GNSS_WEEK_IN_SECONDS - Static variable in interface org.orekit.propagation.analytical.gnss.data.GNSSConstants
-
Duration of the GNSS week in seconds.
- GNSSAttitudeProvider - Interface in org.orekit.gnss.attitude
-
Attitude providers for navigation satellites.
- GNSSClockElements - Interface in org.orekit.propagation.analytical.gnss.data
-
- GNSSConstants - Interface in org.orekit.propagation.analytical.gnss.data
-
Set of useful physical constants used in Global Navigation Satellite Systems (GNSS).
- GnssData - Class in org.orekit.gnss.metric.ntrip
-
GNSS data retrieved from Ntrip caster.
- GnssData(byte[], int) - Constructor for class org.orekit.gnss.metric.ntrip.GnssData
-
Build a GNSS data bloc.
- GNSSDate - Class in org.orekit.time
-
Container for date in GNSS form.
- GNSSDate(int, double, SatelliteSystem) - Constructor for class org.orekit.time.GNSSDate
-
Build an instance corresponding to a GNSS date.
- GNSSDate(int, double, SatelliteSystem, TimeScales) - Constructor for class org.orekit.time.GNSSDate
-
Build an instance corresponding to a GNSS date.
- GNSSDate(AbsoluteDate, SatelliteSystem) - Constructor for class org.orekit.time.GNSSDate
-
Build an instance from an absolute date.
- GNSSDate(AbsoluteDate, SatelliteSystem, TimeScales) - Constructor for class org.orekit.time.GNSSDate
-
Build an instance from an absolute date.
- GNSSOrbitalElements - Interface in org.orekit.propagation.analytical.gnss.data
-
This interface provides the minimal set of orbital elements needed by the
GNSSPropagator
.
- GNSSPropagator - Class in org.orekit.propagation.analytical.gnss
-
- GNSSPropagatorBuilder - Class in org.orekit.propagation.analytical.gnss
-
This nested class aims at building a GNSSPropagator.
- GNSSPropagatorBuilder(GNSSOrbitalElements) - Constructor for class org.orekit.propagation.analytical.gnss.GNSSPropagatorBuilder
-
Initializes the builder.
- GNSSPropagatorBuilder(GNSSOrbitalElements, Frames) - Constructor for class org.orekit.propagation.analytical.gnss.GNSSPropagatorBuilder
-
Initializes the builder.
- GPS_AV - Static variable in interface org.orekit.propagation.analytical.gnss.data.GNSSConstants
-
Value of the earth's rotation rate in rad/s for GPS user.
- GPS_EPOCH - Static variable in class org.orekit.time.AbsoluteDate
-
Reference epoch for GPS weeks: 1980-01-06T00:00:00 GPS time.
- GPS_EPOCH - Static variable in class org.orekit.time.DateComponents
-
Reference epoch for GPS weeks: 1980-01-06.
- GPS_MU - Static variable in interface org.orekit.propagation.analytical.gnss.data.GNSSConstants
-
WGS 84 value of the Earth's universal gravitational parameter for GPS user in m³/s².
- GPS_WEEK_NB - Static variable in interface org.orekit.propagation.analytical.gnss.data.GNSSConstants
-
Number of weeks in the GPS cycle.
- GPSAlmanac - Class in org.orekit.propagation.analytical.gnss.data
-
This class holds a GPS almanac as read from SEM or YUMA files.
- GPSAlmanac() - Constructor for class org.orekit.propagation.analytical.gnss.data.GPSAlmanac
-
Constructor.
- GPSBlockIIA - Class in org.orekit.gnss.attitude
-
Attitude providers for GPS block IIA navigation satellites.
- GPSBlockIIA(double, double, AbsoluteDate, AbsoluteDate, ExtendedPVCoordinatesProvider, Frame) - Constructor for class org.orekit.gnss.attitude.GPSBlockIIA
-
Simple constructor.
- GPSBlockIIF - Class in org.orekit.gnss.attitude
-
Attitude providers for GPS block IIF navigation satellites.
- GPSBlockIIF(double, double, AbsoluteDate, AbsoluteDate, ExtendedPVCoordinatesProvider, Frame) - Constructor for class org.orekit.gnss.attitude.GPSBlockIIF
-
Simple constructor.
- GPSBlockIIR - Class in org.orekit.gnss.attitude
-
Attitude providers for GPS block IIR navigation satellites.
- GPSBlockIIR(double, AbsoluteDate, AbsoluteDate, ExtendedPVCoordinatesProvider, Frame) - Constructor for class org.orekit.gnss.attitude.GPSBlockIIR
-
Simple constructor.
- GPSNavigationMessage - Class in org.orekit.propagation.analytical.gnss.data
-
Container for data contained in a GPS navigation message.
- GPSNavigationMessage() - Constructor for class org.orekit.propagation.analytical.gnss.data.GPSNavigationMessage
-
Constructor.
- GPSScale - Class in org.orekit.time
-
GPS time scale.
- gradient(AbsoluteDate, Vector3D, double) - Method in class org.orekit.forces.gravity.HolmesFeatherstoneAttractionModel
-
Compute the gradient of the non-central part of the gravity field.
- gradient(FieldAbsoluteDate<T>, FieldVector3D<T>, T) - Method in class org.orekit.forces.gravity.HolmesFeatherstoneAttractionModel
-
Compute the gradient of the non-central part of the gravity field.
- GraggBulirschStoerIntegratorBuilder - Class in org.orekit.propagation.conversion
-
Builder for GraggBulirschStoerIntegrator.
- GraggBulirschStoerIntegratorBuilder(double, double, double) - Constructor for class org.orekit.propagation.conversion.GraggBulirschStoerIntegratorBuilder
-
Build a new instance.
- GRAM - Static variable in class org.orekit.utils.units.Unit
-
Gram unit.
- GRAPHICCombination - Class in org.orekit.estimation.measurements.gnss
-
GRoup And Phase Ionospheric Calibration (GRAPHIC) combination.
- GravityFieldFactory - Class in org.orekit.forces.gravity.potential
-
Factory used to read gravity field files in several supported formats.
- GravityFields - Interface in org.orekit.forces.gravity.potential
-
Defines methods for obtaining gravity fields.
- GRGS_FILENAME - Static variable in class org.orekit.forces.gravity.potential.GravityFieldFactory
-
Default regular expression for GRGS files.
- GRGSFormatReader - Class in org.orekit.forces.gravity.potential
-
Reader for the GRGS gravity field format.
- GRGSFormatReader(String, boolean) - Constructor for class org.orekit.forces.gravity.potential.GRGSFormatReader
-
Simple constructor.
- GRGSFormatReader(String, boolean, TimeScale) - Constructor for class org.orekit.forces.gravity.potential.GRGSFormatReader
-
Simple constructor.
- GRIM5C1_EARTH_ANGULAR_VELOCITY - Static variable in interface org.orekit.utils.Constants
-
Earth angular velocity from GRIM5C1 model: 7.292115e-5 rad/s.
- GRIM5C1_EARTH_C20 - Static variable in interface org.orekit.utils.Constants
-
Earth un-normalized second zonal coefficient from GRIM5C1 model: -1.082626110612609e-3.
- GRIM5C1_EARTH_C30 - Static variable in interface org.orekit.utils.Constants
-
Earth un-normalized third zonal coefficient from GRIM5C1 model: 2.536150841690056e-6.
- GRIM5C1_EARTH_C40 - Static variable in interface org.orekit.utils.Constants
-
Earth un-normalized fourth zonal coefficient from GRIM5C1 model: 1.61936352497151e-6.
- GRIM5C1_EARTH_C50 - Static variable in interface org.orekit.utils.Constants
-
Earth un-normalized fifth zonal coefficient from GRIM5C1 model: 2.231013736607540e-7.
- GRIM5C1_EARTH_C60 - Static variable in interface org.orekit.utils.Constants
-
Earth un-normalized sixth zonal coefficient from GRIM5C1 model: -5.402895357302363e-7.
- GRIM5C1_EARTH_EQUATORIAL_RADIUS - Static variable in interface org.orekit.utils.Constants
-
Earth equatorial radius from GRIM5C1 model: 6378136.46 m.
- GRIM5C1_EARTH_FLATTENING - Static variable in interface org.orekit.utils.Constants
-
Earth flattening from GRIM5C1 model: 1.0 / 298.25765.
- GRIM5C1_EARTH_MU - Static variable in interface org.orekit.utils.Constants
-
Earth gravitational constant from GRIM5C1 model: 3.986004415e14 m³/s².
- GroundAtNightDetector - Class in org.orekit.propagation.events
-
Detector for ground location being at night.
- GroundAtNightDetector(TopocentricFrame, PVCoordinatesProvider, double, AtmosphericRefractionModel) - Constructor for class org.orekit.propagation.events.GroundAtNightDetector
-
Simple constructor.
- GroundFieldOfViewDetector - Class in org.orekit.propagation.events
-
Finder for satellite entry/exit events with respect to a sensor
Field Of View
attached to an arbitrary frame.
- GroundFieldOfViewDetector(Frame, FieldOfView) - Constructor for class org.orekit.propagation.events.GroundFieldOfViewDetector
-
Build a new instance.
- GroundPointing - Class in org.orekit.attitudes
-
Base class for ground pointing attitude providers.
- GroundPointing(Frame, Frame) - Constructor for class org.orekit.attitudes.GroundPointing
-
Default constructor.
- GroundStation - Class in org.orekit.estimation.measurements
-
Class modeling a ground station that can perform some measurements.
- GroundStation(TopocentricFrame) - Constructor for class org.orekit.estimation.measurements.GroundStation
-
- GroundStation(TopocentricFrame, EOPHistory, StationDisplacement...) - Constructor for class org.orekit.estimation.measurements.GroundStation
-
Simple constructor.
- GRS80_EARTH_ANGULAR_VELOCITY - Static variable in interface org.orekit.utils.Constants
-
Earth angular velocity from GRS80 model: 7.292115e-5 rad/s.
- GRS80_EARTH_C20 - Static variable in interface org.orekit.utils.Constants
-
Earth un-normalized second zonal coefficient from GRS80 model: -1.08263e-3.
- GRS80_EARTH_EQUATORIAL_RADIUS - Static variable in interface org.orekit.utils.Constants
-
Earth equatorial radius from GRS80 model: 6378137.0 m.
- GRS80_EARTH_FLATTENING - Static variable in interface org.orekit.utils.Constants
-
Earth flattening from GRS80 model: 1.0 / 298.257222101.
- GRS80_EARTH_MU - Static variable in interface org.orekit.utils.Constants
-
Earth gravitational constant from GRS80 model: 3.986005e14 m³/s².
- GTODProvider - Class in org.orekit.frames
-
Greenwich True Of Date Frame, also known as True of Date Rotating frame (TDR)
or Greenwich Rotating Coordinate frame (GCR).
- GTODProvider(IERSConventions, EOPHistory, TimeScales) - Constructor for class org.orekit.frames.GTODProvider
-
Simple constructor.
- guessCenter(Frame) - Static method in enum org.orekit.files.ccsds.definitions.CenterName
-
Guess the name of the center of the reference frame.
- guessFrame(Frame) - Static method in enum org.orekit.files.ccsds.definitions.CelestialBodyFrame
-
Guesses names from ODM Table 5-3 and Annex A.
- GzipFilter - Class in org.orekit.data
-
Filter for gzip compressed data.
- GzipFilter() - Constructor for class org.orekit.data.GzipFilter
-
- S - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants
-
- S2 - Static variable in class org.orekit.models.earth.displacement.Tide
-
S₂ tide.
- s4 - Variable in class org.orekit.propagation.analytical.tle.FieldTLEPropagator
-
s* new value for the contant s.
- s4 - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator
-
s* new value for the contant s.
- S_2FASX4 - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants
-
- S_3FASX6 - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants
-
- S_FASX2 - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants
-
- S_G22 - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants
-
- S_G32 - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants
-
- S_G44 - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants
-
- S_G52 - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants
-
- S_G54 - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants
-
- SaastamoinenModel - Class in org.orekit.models.earth.troposphere
-
The modified Saastamoinen model.
- SaastamoinenModel(double, double, double) - Constructor for class org.orekit.models.earth.troposphere.SaastamoinenModel
-
Create a new Saastamoinen model for the troposphere using the given environmental
conditions and table from the reference book.
- SaastamoinenModel(double, double, double, String) - Constructor for class org.orekit.models.earth.troposphere.SaastamoinenModel
-
Create a new Saastamoinen model for the troposphere using the given
environmental conditions.
- SaastamoinenModel(double, double, double, String, DataProvidersManager) - Constructor for class org.orekit.models.earth.troposphere.SaastamoinenModel
-
Create a new Saastamoinen model for the troposphere using the given
environmental conditions.
- sameDimension(Unit) - Method in class org.orekit.utils.units.Unit
-
Check if a unit has the same dimension as another unit.
- sameDimensionSI() - Method in class org.orekit.utils.units.Unit
-
Create the SI unit with same dimension.
- sample(SphericalPolygonsSet, double, double) - Method in class org.orekit.models.earth.tessellation.EllipsoidTessellator
-
- SatelliteAntenna - Class in org.orekit.gnss.antenna
-
GNSS satellite antenna model.
- SatelliteAntenna(String, String, Map<Frequency, FrequencyPattern>, SatelliteSystem, int, SatelliteType, int, String, AbsoluteDate, AbsoluteDate) - Constructor for class org.orekit.gnss.antenna.SatelliteAntenna
-
Simple constructor.
- SatelliteClockScale - Class in org.orekit.time
-
Scale for on-board clock.
- SatelliteClockScale(String, AbsoluteDate, TimeScale, double, double) - Constructor for class org.orekit.time.SatelliteClockScale
-
Create a linear model for satellite clock.
- SatelliteSystem - Enum in org.orekit.gnss
-
Enumerate for satellite system.
- SatelliteType - Enum in org.orekit.gnss.antenna
-
Enumerate for satellite types.
- SATURN - Static variable in class org.orekit.bodies.CelestialBodyFactory
-
Predefined name for Saturn.
- SBAS_MU - Static variable in interface org.orekit.propagation.analytical.gnss.data.GNSSConstants
-
WGS 84 value of the Earth's universal gravitational parameter for SBAS user in m³/s².
- SBASNavigationMessage - Class in org.orekit.propagation.analytical.gnss.data
-
Container for data contained in a SBAS navigation message.
- SBASNavigationMessage() - Constructor for class org.orekit.propagation.analytical.gnss.data.SBASNavigationMessage
-
Constructor.
- SBASOrbitalElements - Interface in org.orekit.propagation.analytical.gnss.data
-
This interface provides the minimal set of orbital elements needed by the
SBASPropagator
.
- SBASPropagator - Class in org.orekit.propagation.analytical.gnss
-
- SBASPropagatorBuilder - Class in org.orekit.propagation.analytical.gnss
-
This nested class aims at building a SBASPropagator.
- SBASPropagatorBuilder(SBASOrbitalElements, Frames) - Constructor for class org.orekit.propagation.analytical.gnss.SBASPropagatorBuilder
-
Initializes the builder.
- scale(double, Orbit) - Method in enum org.orekit.orbits.OrbitType
-
Compute scaling factor for parameters drivers.
- scale(String, double) - Method in class org.orekit.utils.units.Unit
-
Scale a unit.
- scaleChanged(double, ParameterDriver) - Method in interface org.orekit.utils.ParameterObserver
-
Notify that a parameter scale has been changed.
- ScaledConstantThrustPropulsionModel - Class in org.orekit.forces.maneuvers.propulsion
-
Thrust propulsion model with parameters (for estimation) represented by scale factors
on the X, Y and Z axis of the spacecraft frame.
- ScaledConstantThrustPropulsionModel(double, double, Vector3D, String) - Constructor for class org.orekit.forces.maneuvers.propulsion.ScaledConstantThrustPropulsionModel
-
Constructor with min/max deviation for the scale factors.
- scaledIncrement(double, DoubleArrayDictionary.Entry) - Method in class org.orekit.utils.DoubleArrayDictionary.Entry
-
Increment the value with another scaled entry.
- scaledIncrement(T, FieldArrayDictionary<T>.Entry) - Method in class org.orekit.utils.FieldArrayDictionary.Entry
-
Increment the value with another scaled entry.
- scaledIncrement(double, FieldArrayDictionary<T>.Entry) - Method in class org.orekit.utils.FieldArrayDictionary.Entry
-
Increment the value with another scaled entry.
- Scheduler<T extends ObservedMeasurement<T>> - Interface in org.orekit.estimation.measurements.generation
-
- SDP4 - Static variable in class org.orekit.propagation.analytical.tle.FieldTLE
-
Identifier for SDP4 type of ephemeris.
- SDP4 - Static variable in class org.orekit.propagation.analytical.tle.TLE
-
Identifier for SDP4 type of ephemeris.
- SDP8 - Static variable in class org.orekit.propagation.analytical.tle.FieldTLE
-
Identifier for SDP8 type of ephemeris.
- SDP8 - Static variable in class org.orekit.propagation.analytical.tle.TLE
-
Identifier for SDP8 type of ephemeris.
- SEC_TO_MILLI - Static variable in class org.orekit.gnss.metric.messages.rtcm.ephemeris.RtcmEphemerisData
-
Seconds to milliseconds converter.
- SECOND - Static variable in class org.orekit.utils.units.Unit
-
Second unit.
- Section - Interface in org.orekit.files.ccsds.section
-
Top level interface for all CCSDS message sections.
- SecularAndHarmonic - Class in org.orekit.utils
-
Class for fitting evolution of osculating orbital parameters.
- SecularAndHarmonic(int, double...) - Constructor for class org.orekit.utils.SecularAndHarmonic
-
Simple constructor.
- Segment<M extends Metadata,D extends Data> - Class in org.orekit.files.ccsds.section
-
- Segment(M, D) - Constructor for class org.orekit.files.ccsds.section.Segment
-
Constructor.
- SegmentWriter() - Constructor for class org.orekit.files.ccsds.ndm.adm.aem.StreamingAemWriter.SegmentWriter
-
- SegmentWriter() - Constructor for class org.orekit.files.ccsds.ndm.odm.oem.StreamingOemWriter.SegmentWriter
-
- select(Unit, Unit) - Method in enum org.orekit.files.ccsds.ndm.ParsedUnitsBehavior
-
Select the unit to use for interpreting parsed value.
- select(DataSource) - Static method in class org.orekit.files.ccsds.utils.lexical.LexicalAnalyzerSelector
-
- selectDates(AbsoluteDate, AbsoluteDate) - Method in class org.orekit.time.BurstSelector
-
Select dates within an interval.
- selectDates(AbsoluteDate, AbsoluteDate) - Method in interface org.orekit.time.DatesSelector
-
Select dates within an interval.
- selectDates(AbsoluteDate, AbsoluteDate) - Method in class org.orekit.time.FixedStepSelector
-
Select dates within an interval.
- selectExtrapolator(FieldTLE<T>, T[]) - Static method in class org.orekit.propagation.analytical.tle.FieldTLEPropagator
-
Selects the extrapolator to use with the selected TLE.
- selectExtrapolator(FieldTLE<T>, Frames, T[]) - Static method in class org.orekit.propagation.analytical.tle.FieldTLEPropagator
-
Selects the extrapolator to use with the selected TLE.
- selectExtrapolator(FieldTLE<T>, AttitudeProvider, T, T[]) - Static method in class org.orekit.propagation.analytical.tle.FieldTLEPropagator
-
Selects the extrapolator to use with the selected TLE.
- selectExtrapolator(FieldTLE<T>, AttitudeProvider, T, Frame, T[]) - Static method in class org.orekit.propagation.analytical.tle.FieldTLEPropagator
-
Selects the extrapolator to use with the selected TLE.
- selectExtrapolator(TLE) - Static method in class org.orekit.propagation.analytical.tle.TLEPropagator
-
Selects the extrapolator to use with the selected TLE.
- selectExtrapolator(TLE, Frames) - Static method in class org.orekit.propagation.analytical.tle.TLEPropagator
-
Selects the extrapolator to use with the selected TLE.
- selectExtrapolator(TLE, AttitudeProvider, double) - Static method in class org.orekit.propagation.analytical.tle.TLEPropagator
-
Selects the extrapolator to use with the selected TLE.
- selectExtrapolator(TLE, AttitudeProvider, double, Frame) - Static method in class org.orekit.propagation.analytical.tle.TLEPropagator
-
Selects the extrapolator to use with the selected TLE.
- selectionChanged(boolean, ParameterDriver) - Method in interface org.orekit.utils.ParameterObserver
-
Notify that a parameter selection status has been changed.
- selectTransformer(Transformer, double, boolean) - Method in enum org.orekit.propagation.events.FilterType
-
Get next function transformer in the specified direction.
- SEMI_CIRCLE - Static variable in class org.orekit.gnss.metric.parser.Units
-
Semi-circles units.
- SemiAnalyticalKalmanEstimator - Class in org.orekit.estimation.sequential
-
Implementation of an Extended Semi-analytical Kalman Filter (ESKF) to perform orbit determination.
- SemiAnalyticalKalmanEstimator(MatrixDecomposer, DSSTPropagatorBuilder, CovarianceMatrixProvider, ParameterDriversList, CovarianceMatrixProvider) - Constructor for class org.orekit.estimation.sequential.SemiAnalyticalKalmanEstimator
-
Kalman filter estimator constructor (package private).
- SemiAnalyticalKalmanEstimatorBuilder - Class in org.orekit.estimation.sequential
-
Builder for a Semi-analytical Kalman Filter.
- SemiAnalyticalKalmanEstimatorBuilder() - Constructor for class org.orekit.estimation.sequential.SemiAnalyticalKalmanEstimatorBuilder
-
Default constructor.
- SemiAnalyticalKalmanModel - Class in org.orekit.estimation.sequential
-
- SemiAnalyticalKalmanModel(DSSTPropagatorBuilder, CovarianceMatrixProvider, ParameterDriversList, CovarianceMatrixProvider) - Constructor for class org.orekit.estimation.sequential.SemiAnalyticalKalmanModel
-
Kalman process model constructor (package private).
- SEMParser - Class in org.orekit.gnss
-
This class reads SEM almanac files and provides
GPS almanacs
.
- SEMParser(String) - Constructor for class org.orekit.gnss.SEMParser
-
Simple constructor.
- SEMParser(String, DataProvidersManager, TimeScales) - Constructor for class org.orekit.gnss.SEMParser
-
Create a SEM loader/parser with the given source of SEM auxiliary data files.
- SequentialBatchLSEstimator - Class in org.orekit.estimation.leastsquares
-
Sequential least squares estimator for orbit determination.
- SequentialBatchLSEstimator(SequentialGaussNewtonOptimizer, OrbitDeterminationPropagatorBuilder...) - Constructor for class org.orekit.estimation.leastsquares.SequentialBatchLSEstimator
-
Simple constructor.
- setA(double) - Method in class org.orekit.files.ccsds.ndm.odm.KeplerianElements
-
Set the orbit semi-major axis.
- setA(int, double) - Method in class org.orekit.files.ccsds.ndm.odm.StateVector
-
Set acceleration component.
- setA2b(boolean) - Method in class org.orekit.files.ccsds.ndm.adm.AttitudeEndoints
-
Set rotation direction.
- setAcceleration(int, double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Maneuver
-
Set acceleration component.
- setAccelerationDirectionSigma(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Maneuver
-
Set one σ angular off-nominal acceleration direction.
- setAccelerationInterpolation(OnOff) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Maneuver
-
Set interpolation mode between current and next acceleration line.
- setAccelerationMagnitudeSigma(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Maneuver
-
Set one σ percent error on acceleration magnitude.
- setAccuracy(int, double) - Method in class org.orekit.files.sp3.SP3
-
Set the formal accuracy for a satellite.
- setAccuracy(double) - Method in class org.orekit.files.sp3.SP3.SP3Ephemeris
-
Set the accuracy for this satellite.
- setAccuracyProvider(AccuracyProvider) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.RtcmEphemerisData
-
Set the accuracy provider of the ephemeris message.
- setActualOdSpan(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
-
Set actual time span used for the OD of the object.
- setAdmMessageLink(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
-
Set the Unique identifier of Attitude Data Message linked to this Orbit Data Message.
- setAe(double) - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
-
Set the central body reference radius.
- setAf0(double) - Method in class org.orekit.propagation.analytical.gnss.data.CommonGnssData
-
Setter for the SV Clock Bias Correction Coefficient (s).
- setAf1(double) - Method in class org.orekit.propagation.analytical.gnss.data.CommonGnssData
-
Setter for the SV Clock Drift Correction Coefficient (s/s).
- setAf2(double) - Method in class org.orekit.propagation.analytical.gnss.data.AbstractNavigationMessage
-
Setter for the Drift Rate Correction Coefficient (s/s²).
- setAgency(String) - Method in class org.orekit.files.sp3.SP3
-
Set the agency string for this SP3 file.
- setAgencyName(String) - Method in class org.orekit.gnss.clock.RinexClock
-
Setter for the agency name.
- setAgencyName(String) - Method in class org.orekit.gnss.navigation.RinexNavigation
-
Setter for the agency name.
- setAGf0(double) - Method in class org.orekit.propagation.analytical.gnss.data.SBASNavigationMessage
-
Setter for the SV clock bias.
- setAGf1(double) - Method in class org.orekit.propagation.analytical.gnss.data.SBASNavigationMessage
-
Setter for the SV relative frequency.
- setAlbedoGridSize(int) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
-
Set albedo grid size.
- setAlbedoModel(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
-
Set albedo model.
- setAlternateNames(List<String>) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
-
Set the alternate names for this space object.
- setAmplifierBandwidth(double) - Method in class org.orekit.files.ilrs.CRDConfiguration.DetectorConfiguration
-
Set the amplifier bandwidth.
- setAmplifierGain(double) - Method in class org.orekit.files.ilrs.CRDConfiguration.DetectorConfiguration
-
Set the amplifier gain.
- setAmplifierInUse(String) - Method in class org.orekit.files.ilrs.CRDConfiguration.DetectorConfiguration
-
Set the amplifier in use.
- setAnalysisCenterID(String) - Method in class org.orekit.gnss.clock.RinexClock
-
Setter for the analysis center ID.
- setAnalysisCenterName(String) - Method in class org.orekit.gnss.clock.RinexClock
-
Setter for the analysis center name.
- setAngleType(AngleType) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
-
Setter for the angleType.
- setAngularThreshold(double) - Method in class org.orekit.bodies.OneAxisEllipsoid
-
Set the angular convergence threshold.
- setAnomaly(double) - Method in class org.orekit.files.ccsds.ndm.odm.KeplerianElements
-
Set the orbit anomaly.
- setAnomalyType(PositionAngle) - Method in class org.orekit.files.ccsds.ndm.odm.KeplerianElements
-
Set the type of anomaly.
- setAODC(double) - Method in class org.orekit.propagation.analytical.gnss.data.BeidouNavigationMessage
-
Setter for the age of data clock.
- setAODE(double) - Method in class org.orekit.propagation.analytical.gnss.data.BeidouNavigationMessage
-
Setter for the age of data ephemeric.
- setApplicableWavelength(double) - Method in class org.orekit.files.ilrs.CRDConfiguration.DetectorConfiguration
-
Set the applicable wavelength.
- setAppliedVoltage(double) - Method in class org.orekit.files.ilrs.CRDConfiguration.DetectorConfiguration
-
Set the applied voltage.
- setAreAdditionalDataAvailable(boolean) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data
-
Set the flag indicating if additional parameters are in the message.
- setAtmosphericModel(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
-
Set name of atmospheric model.
- setAttitudeActuatorType(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
-
Set the type of actuator for attitude control.
- setAttitudeControlAccuracy(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
-
Set the accuracy of attitude control.
- setAttitudeControlMode(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
-
Set the attitude control mode.
- setAttitudeKnowledgeAccuracy(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
-
Set the accuracy of attitude knowledge.
- setAttitudePointingAccuracy(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
-
Set the overall accuracy of spacecraft to maintain attitude.
- setAttitudeProvider(AttitudeProvider) - Method in class org.orekit.propagation.AbstractPropagator
-
Set attitude provider.
- setAttitudeProvider(AttitudeProvider) - Method in class org.orekit.propagation.conversion.AbstractPropagatorBuilder
-
Set the attitude provider.
- setAttitudeProvider(AttitudeProvider) - Method in class org.orekit.propagation.FieldAbstractPropagator
-
Set attitude provider.
- setAttitudeProvider(AttitudeProvider) - Method in interface org.orekit.propagation.FieldPropagator
-
Set attitude provider.
- setAttitudeProvider(AttitudeProvider) - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
-
Set attitude provider.
- setAttitudeProvider(AttitudeProvider) - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator
-
Set attitude provider.
- setAttitudeProvider(AttitudeProvider) - Method in class org.orekit.propagation.integration.IntegratedEphemeris
-
Set attitude provider.
- setAttitudeProvider(AttitudeProvider) - Method in class org.orekit.propagation.integration.StateMapper
-
Set the attitude provider.
- setAttitudeProvider(AttitudeProvider) - Method in interface org.orekit.propagation.Propagator
-
Set attitude provider.
- setAttitudeProvider(AttitudeProvider) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator
-
Set attitude provider.
- setAttitudeProvider(AttitudeProvider) - Method in class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator
-
Set attitude provider.
- setAttitudeType(AttitudeType) - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemMetadata
-
Set the format of the data lines in the message.
- setBeamDivergence(double) - Method in class org.orekit.files.ilrs.CRDConfiguration.LaserConfiguration
-
Set the beam divergence.
- setBeidouNavigationMessage(BeidouNavigationMessage) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1042Data
-
Set the Beidou navigation message.
- setBeidouToc(double) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1042Data
-
Set the Beidou time of clock.
- setBGDE1E5a(double) - Method in class org.orekit.propagation.analytical.gnss.data.GalileoNavigationMessage
-
Setter for the E1/E5a broadcast group delay (s).
- setBGDE5bE1(double) - Method in class org.orekit.propagation.analytical.gnss.data.GalileoNavigationMessage
-
Setter for the E5b/E1 broadcast group delay (s).
- setBN(int) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data
-
Set the GLONASS Bn Word.
- setBolDv(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
-
Set the total ΔV capability at beginning of life.
- setBStar(double) - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmTle
-
Set the SGP/SGP4 drag-like coefficient.
- setBusModel(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
-
Set the bus model name.
- setCacheSlotsNumber(int) - Static method in class org.orekit.utils.OrekitConfiguration
-
Set the number of slots to use in caches.
- setCatalogName(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
-
Set the specification of satellite catalog source.
- setCdmMessageLink(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
-
Set the Unique identifier of Conjunction Data Message linked to this Orbit Data Message.
- setCelestialSource(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
-
Set the source and version of celestial body (e.g.
- setCenter(BodyFacade) - Method in class org.orekit.files.ccsds.ndm.adm.AdmMetadata
-
Set the body at origin of reference frame.
- setCenter(BodyFacade) - Method in class org.orekit.files.ccsds.ndm.odm.CommonMetadata
-
Set the origin of reference frame.
- setCenter(BodyFacade) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata
-
Set the origin of reference frame.
- setCenterOfMassOffset(double) - Method in class org.orekit.files.ilrs.CPFHeader
-
Set the approximate center of mass to reflector offset.
- setCentralBodyRotation(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
-
Set central body angular rotation rate.
- setCic(double) - Method in class org.orekit.propagation.analytical.gnss.data.AbstractNavigationMessage
-
Setter for te Cic parameter.
- setCis(double) - Method in class org.orekit.propagation.analytical.gnss.data.AbstractNavigationMessage
-
Setter for the Cis parameter.
- setClassification(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
-
Set the message classification.
- setClassificationType(char) - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmTle
-
Set the classification type.
- setClockCorrection(ClockCorrection) - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm02Data
-
Set the clock correction data.
- setClockCorrection(ClockCorrection) - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm03Data
-
Set the clock correction data.
- setClosedOrbitConstraint(boolean) - Method in class org.orekit.utils.AbstractMultipleShooting
-
Set the constraint of a closed orbit or not.
- setCnm(double[][]) - Method in class org.orekit.gnss.metric.messages.ssr.subtype.SsrIm201Data
-
Set the cosine parameters of spherical harmonics expansion of degree N and order M.
- setComparator(Comparator<IntegerLeastSquareSolution>) - Method in class org.orekit.estimation.measurements.gnss.AbstractLambdaMethod
-
Set a custom comparator for integer least square solutions comparison.
- setConfidence(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
-
Set confidence metric.
- setConfigurationRecords(CRDConfiguration) - Method in class org.orekit.files.ilrs.CRD.CRDDataBlock
-
Set the configuration records for the current data block.
- setConsiderN(int) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
-
Set number of consider parameters.
- setConsiderParameters(List<String>) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
-
Set description of consider parameters.
- setConstellation(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
-
Set the name of the constellation this space object belongs to.
- setContext(ContextBinding) - Method in class org.orekit.files.ccsds.utils.generation.AbstractMessageWriter
-
Reset context binding.
- setConvergenceChecker(ConvergenceChecker<LeastSquaresProblem.Evaluation>) - Method in class org.orekit.estimation.leastsquares.BatchLSEstimator
-
Set a custom convergence checker.
- setConvergenceRMS(double) - Method in class org.orekit.utils.SecularAndHarmonic
-
Set RMS for convergence.
- setCoordinateSystem(String) - Method in class org.orekit.files.sp3.SP3
-
Set the coordinate system used for the orbit entries.
- setCorrectionAberrationDiurnal(double) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
-
Setter for the diurnal aberration correction.
- setCorrectionAberrationYearly(double) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
-
Setter for the yearly aberration correction.
- setCorrectionAngle1(double) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
-
Setter for the correctionAngle1.
- setCorrectionAngle2(double) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
-
Setter for the correctionAngle2.
- setCorrectionDoppler(double) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
-
Setter for the correctionDoppler.
- setCorrectionMagnitude(double) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
-
Setter for the magnitude correction.
- setCorrectionRcs(double) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
-
Setter for the radar cross section correction.
- setCorrectionReceive(double) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
-
Setter for the correctionReceive.
- setCorrectionsApplied(CorrectionApplied) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
-
Setter for the correctionApplied.
- setCorrectionTransmit(double) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
-
Setter for the correctionTransmit.
- setCountry(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
-
Set the name of the country where the space object owner is based.
- setCovarianceMatrixEntry(int, int, double) - Method in class org.orekit.files.ccsds.ndm.odm.CartesianCovariance
-
Set an entry in the Position/Velocity covariance matrix.
- setCovBasis(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.CovarianceHistoryMetadata
-
Set basis of this covariance time history data.
- setCovBasisID(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.CovarianceHistoryMetadata
-
Set identification number of the orbit determination or simulation upon which this covariance is based.
- setCovConfidence(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.CovarianceHistoryMetadata
-
Set the measure of confidence in covariance error matching reality.
- setCovFrameEpoch(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.CovarianceHistoryMetadata
-
- setCovID(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.CovarianceHistoryMetadata
-
Set covariance identification number.
- setCovNextID(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.CovarianceHistoryMetadata
-
Set identification number of next covariance.
- setCovOrdering(Ordering) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.CovarianceHistoryMetadata
-
Set covariance ordering.
- setCovPrevID(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.CovarianceHistoryMetadata
-
Set identification number of previous covariance.
- setCovReferenceFrame(FrameFacade) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.CovarianceHistoryMetadata
-
Set reference frame of the covariance.
- setCovScaleMax(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.CovarianceHistoryMetadata
-
Set the maximum scale factor to apply to achieve realism.
- setCovScaleMin(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.CovarianceHistoryMetadata
-
Set the minimum scale factor to apply to achieve realism.
- setCovType(ElementsType) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.CovarianceHistoryMetadata
-
Set covariance element set type.
- setCovUnits(List<Unit>) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.CovarianceHistoryMetadata
-
Set covariance element set units.
- setCrc(double) - Method in class org.orekit.propagation.analytical.gnss.data.AbstractNavigationMessage
-
Setter for the Crc parameter.
- setCreationDate(AbsoluteDate) - Method in class org.orekit.files.ccsds.section.Header
-
Set the file creation date and time in UTC.
- setCreationDate(AbsoluteDate) - Method in class org.orekit.gnss.clock.RinexClock
-
Setter for the creation date.
- setCreationDate(AbsoluteDate) - Method in class org.orekit.gnss.navigation.RinexNavigation
-
Setter for the creation date.
- setCreationDateString(String) - Method in class org.orekit.gnss.clock.RinexClock
-
Setter for the creation date as a string.
- setCreationDateString(String) - Method in class org.orekit.gnss.navigation.RinexNavigation
-
Setter for the creation date as a string.
- setCreationTimeString(String) - Method in class org.orekit.gnss.clock.RinexClock
-
Setter for the creation time as a string.
- setCreationTimeString(String) - Method in class org.orekit.gnss.navigation.RinexNavigation
-
Setter for the creation time as a string.
- setCreationTimeZoneString(String) - Method in class org.orekit.gnss.clock.RinexClock
-
Setter for the creation time zone.
- setCreationTimeZoneString(String) - Method in class org.orekit.gnss.navigation.RinexNavigation
-
Setter for the creation time zone.
- setCrs(double) - Method in class org.orekit.propagation.analytical.gnss.data.AbstractNavigationMessage
-
Setter for the Crs parameter.
- setCrsIndicator(int) - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm01Header
-
Set the Global/Regional CRS Indicator.
- setCrsIndicator(int) - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm03Header
-
Set the Global/Regional CRS Indicator.
- setCuc(double) - Method in class org.orekit.propagation.analytical.gnss.data.AbstractNavigationMessage
-
Setter for the Cuc parameter.
- setCus(double) - Method in class org.orekit.propagation.analytical.gnss.data.AbstractNavigationMessage
-
Setter for the Cus parameter.
- setDarkCount(double) - Method in class org.orekit.files.ilrs.CRDConfiguration.DetectorConfiguration
-
Set the dark count.
- setDataQuality(DataQuality) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
-
Setter for the dataQuality.
- setDataReleaseFlag(int) - Method in class org.orekit.files.ilrs.CRDHeader
-
Set the flag indicating the data release.
- setDataType(int) - Method in class org.orekit.files.ilrs.CRDHeader
-
Set the data type.
- setDataTypes(List<String>) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
-
Set observation data types used.
- setDataTypes(List<ObservationType>) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
-
Setter for the data types in the data section.
- setDataUsed(String) - Method in class org.orekit.files.sp3.SP3
-
Set the data used indicator for this SP3 file.
- setDate(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Maneuver
-
Set date.
- setDate(AbsoluteDate) - Method in class org.orekit.propagation.analytical.gnss.data.AbstractEphemerisMessage
-
Setter for the reference date of the ephemeris.
- setDate(AbsoluteDate) - Method in class org.orekit.propagation.analytical.gnss.data.CommonGnssData
-
Setter for the reference epoch.
- setDateAndTime(String) - Method in class org.orekit.files.ilrs.CRDHeader
-
Set the string value of date and time.
- setDayFraction(double) - Method in class org.orekit.files.sp3.SP3
-
Set the day fraction for this SP3 file.
- setDcBodyFrame(SpacecraftBodyFrame) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata
-
- setDcBodyTrigger(Vector3D) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata
-
Set direction in
body frame
for triggering duty cycle.
- setDcExecStart(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata
-
Set the start time of initial duty cycle-based maneuver execution.
- setDcExecStop(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata
-
Set the end time of final duty cycle-based maneuver execution.
- setDcMaxCycles(int) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata
-
Set the maximum number of "ON" duty cycles.
- setDcMinCycles(int) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata
-
Set the minimum number of "ON" duty cycles.
- setDcPhaseStartAngle(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata
-
Set phase angle of pulse start.
- setDcPhaseStopAngle(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata
-
Set phase angle of pulse stop.
- setDcRefDir(Vector3D) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata
-
Set reference direction for triggering duty cycle.
- setDcRefTime(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata
-
Set duty cycle thrust reference time.
- setDcTimePulseDuration(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata
-
Set duty cycle pulse "ON" duration.
- setDcTimePulsePeriod(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata
-
Set duty cycle elapsed time between start of a pulse and start of next pulse.
- setDcType(DutyCycleType) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata
-
Set type of duty cycle.
- setDcWindowClose(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata
-
Set the end time of duty cycle-based maneuver window.
- setDcWindowOpen(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata
-
Set the start time of duty cycle-based maneuver window.
- setDefault(LazyLoadedDataContext) - Static method in interface org.orekit.data.DataContext
-
Set the default data context that is used to implement Orekit's static factories.
- setDeltaInc(double) - Method in class org.orekit.propagation.analytical.gnss.data.GalileoAlmanac
-
Sets the the correction of orbit reference inclination at reference time.
- setDeltaMass(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Maneuver
-
Set mass change.
- setDeltaMass(double) - Method in class org.orekit.files.ccsds.ndm.odm.opm.Maneuver
-
Set mass change during maneuver (value is < 0).
- setDeltaN(double) - Method in class org.orekit.propagation.analytical.gnss.data.AbstractNavigationMessage
-
Setter for the delta of satellite mean motion.
- setDeltaSqrtA(double) - Method in class org.orekit.propagation.analytical.gnss.data.GalileoAlmanac
-
Sets the difference between the square root of the semi-major axis
and the square root of the nominal semi-major axis.
- setDeltaTN(double) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data
-
Set the deltaTauN value.
- setDeployDirSigma(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Maneuver
-
Set one σ angular off-nominal deployment vector direction.
- setDeployDv(int, double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Maneuver
-
Set velocity increment component of deployed "child" object.
- setDeployDvCda(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Maneuver
-
Set typical (50th percentile) product of drag coefficient times cross-sectional area of deployed "child" object.
- setDeployDvRatio(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Maneuver
-
Set ratio of child-to-host ΔV vectors.
- setDeployDvSigma(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Maneuver
-
Set one σ percent error on deployment ΔV magnitude.
- setDeployId(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Maneuver
-
Set identifier of resulting "child" object deployed from this host.
- setDeployMass(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Maneuver
-
Set decrement in host mass as a result of deployment.
- setDetectorId(String) - Method in class org.orekit.files.ilrs.CRDConfiguration.DetectorConfiguration
-
Set the detector configuration ID.
- setDetectorRecord(CRDConfiguration.DetectorConfiguration) - Method in class org.orekit.files.ilrs.CRDConfiguration
-
Set the detector configuration record.
- setDetectorType(String) - Method in class org.orekit.files.ilrs.CRDConfiguration.DetectorConfiguration
-
Set the detector type.
- setDockedWith(List<String>) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
-
Set the other space objects this object is docked to.
- setDomes(String) - Method in class org.orekit.files.sinex.Station
-
Set the DOMES number.
- setDopplerCountBias(double) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
-
Set the Doppler count bias.
- setDopplerCountRollover(boolean) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
-
Set the indicator for Doppler count rollover.
- setDopplerCountScale(double) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
-
Set the Doppler count Scale.
- setDragArea(double) - Method in class org.orekit.files.ccsds.ndm.odm.SpacecraftParameters
-
Set the drag area.
- setDragCoeff(double) - Method in class org.orekit.files.ccsds.ndm.odm.SpacecraftParameters
-
Set the drag coefficient.
- setDragCoefficient(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
-
Set the the nominal drag coefficient.
- setDragConstantArea(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
-
Set the attitude-independent drag cross-sectional area, not already into attitude-dependent area along OEB.
- setDragUncertainty(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
-
Set the drag coefficient 1σ uncertainty.
- setDryMass(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
-
Set the mass without propellant.
- setDuration(double) - Method in class org.orekit.files.ccsds.ndm.adm.apm.Maneuver
-
Set duration (value is 0 for impulsive maneuver).
- setDuration(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Maneuver
-
Set duration.
- setDuration(double) - Method in class org.orekit.files.ccsds.ndm.odm.opm.Maneuver
-
Set duration (value is 0 for impulsive maneuver).
- setDv(int, double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Maneuver
-
Set velocity increment component.
- setDV(int, double) - Method in class org.orekit.files.ccsds.ndm.odm.opm.Maneuver
-
Set velocity increment component.
- setDvDirSigma(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Maneuver
-
Set one σ angular off-nominal ΔV direction.
- setDvMagSigma(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Maneuver
-
Set one σ percent error on ΔV magnitude.
- setE(double) - Method in class org.orekit.files.ccsds.ndm.odm.KeplerianElements
-
Set the orbit eccentricity.
- setE(double) - Method in class org.orekit.propagation.analytical.gnss.data.CommonGnssData
-
Setter the eccentricity.
- setEccentricities(Vector3D) - Method in class org.orekit.files.sinex.Station
-
Set the last known station antenna eccentricities.
- setEccRefSystem(Station.ReferenceSystem) - Method in class org.orekit.files.sinex.Station
-
Set the reference system used to define the eccentricity vector (local or cartesian).
- setElem(int, int, PolynomialFunction) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.PolynomialFunctionMatrix
-
Set an element of the matrix.
- setElementSetNo(int) - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmTle
-
Set the element set number for this satellite.
- setEn(int) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data
-
Get the GLONASS En Word.
- setEnabled(boolean) - Method in class org.orekit.estimation.measurements.AbstractMeasurement
-
Enable or disable a measurement.
- setEnabled(boolean) - Method in interface org.orekit.estimation.measurements.ObservedMeasurement
-
Enable or disable a measurement.
- setEndEpoch(AbsoluteDate) - Method in class org.orekit.files.ilrs.ILRSHeader
-
Set the ending epoch (UTC).
- setEndTagSeen(boolean) - Method in class org.orekit.files.ccsds.utils.parsing.AbstractMessageParser
-
Set the flag for XML end tag.
- setEOPContinuityThreshold(double) - Static method in class org.orekit.frames.FramesFactory
-
Set the threshold to check EOP continuity.
- setEOPContinuityThreshold(double) - Method in class org.orekit.frames.LazyLoadedEop
-
Set the threshold to check EOP continuity.
- setEOPContinuityThreshold(double) - Method in class org.orekit.frames.LazyLoadedFrames
-
Set the threshold to check EOP continuity.
- setEopSource(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
-
Set the source and version of Earth Orientation Parameters.
- setEphemerisNames(Map<Integer, String>) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
-
Setter for the external ephemeris names for participants.
- setEphemerisType(int) - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmTle
-
Set the ephemeris type.
- setEpoch(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.adm.apm.ApmQuaternion
-
Set the epoch of the data.
- setEpoch(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.odm.CartesianCovariance
-
Set matrix epoch.
- setEpoch(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.odm.KeplerianElements
-
Set epoch of state vector, Keplerian elements and covariance matrix data.
- setEpoch(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
-
Set time tag for orbit determination solved-for state.
- setEpoch(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.odm.StateVector
-
Set epoch of state vector, Keplerian elements and covariance matrix data.
- setEpoch(AbsoluteDate) - Method in class org.orekit.files.sinex.Station
-
Set the coordinates reference epoch.
- setEpoch(AbsoluteDate) - Method in class org.orekit.files.sp3.SP3
-
Set the epoch of the SP3 file.
- setEpochDelayCorrection(double) - Method in class org.orekit.files.ilrs.CRDConfiguration.TimingSystemConfiguration
-
Set the epoch delay correction.
- setEpochEigenMaj(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
-
Set positional error ellipsoid 1σ major eigenvalue at the epoch of OD.
- setEpochEigenMed(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
-
Set positional error ellipsoid 1σ intermediate eigenvalue at the epoch of OD.
- setEpochEigenMin(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
-
Set positional error ellipsoid 1σ minor eigenvalue at the epoch of OD.
- setEpochFreedom(int, boolean) - Method in class org.orekit.utils.AbstractMultipleShooting
-
Set the epoch a patch point to free or not.
- setEpochIdentifier(int) - Method in class org.orekit.files.ilrs.CRDHeader
-
Set the epoch identifier.
- setEpochIgnition(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.odm.opm.Maneuver
-
Set epoch ignition.
- setEpochInterval(double) - Method in class org.orekit.files.sp3.SP3
-
Set the epoch interval for this SP3 file.
- setEpochStart(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.adm.apm.Maneuver
-
Set epoch start.
- setEpochT0(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
-
Set the epoch to which all relative times are referenced in data blocks.
- setEpochToc(AbsoluteDate) - Method in class org.orekit.propagation.analytical.gnss.data.AbstractEphemerisMessage
-
Setter for the time of clock epoch.
- setEpochToc(AbsoluteDate) - Method in class org.orekit.propagation.analytical.gnss.data.AbstractNavigationMessage
-
Setter for the time of clock epoch.
- setEquatorialRadius(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
-
Set oblate spheroid equatorial radius of central body.
- setEstimatedValue(double...) - Method in class org.orekit.estimation.measurements.EstimatedMeasurement
-
Set the estimated value.
- setEulerRotSeq(RotationOrder) - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemMetadata
-
Set the rotation order for Euler angles.
- setEulerRotSeq(RotationOrder) - Method in class org.orekit.files.ccsds.ndm.adm.apm.Euler
-
Set the rotation order for Euler angles.
- setEvaluationsCounter(Incrementor) - Method in class org.orekit.estimation.leastsquares.AbstractBatchLSModel
-
Set the counter for evaluations.
- setExternalClockReference(String) - Method in class org.orekit.gnss.clock.RinexClock
-
Setter for the external clock reference.
- setExternalSignalProcessing(String) - Method in class org.orekit.files.ilrs.CRDConfiguration.DetectorConfiguration
-
Set the external signal processing.
- setFallback(ProcessingState) - Method in class org.orekit.files.ccsds.utils.parsing.AbstractMessageParser
-
Set fallback processing state.
- setFileType(String) - Method in class org.orekit.gnss.navigation.RinexNavigation
-
Setter for the file type.
- setFilter(CartesianDerivativesFilter) - Method in class org.orekit.files.ilrs.CPF
-
Set the derivatives filter.
- setFilter(CartesianDerivativesFilter) - Method in class org.orekit.files.sp3.SP3
-
Set the derivatives filter.
- setFiring(boolean, AbsoluteDate) - Method in class org.orekit.forces.maneuvers.trigger.EventBasedManeuverTriggers
-
Set the firing start or end date depending on the firing flag.
- setFix(int, int, double, double, double, double, double) - Method in class org.orekit.gnss.metric.ntrip.NtripClient
-
Set GPS fix data to send as NMEA sentence to Ntrip caster if required.
- setFixedF10P7(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
-
Set fixed (time invariant) value of the Solar Flux Unit daily proxy F10.7.
- setFixedF10P7Mean(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
-
Set fixed (time invariant) value of the Solar Flux Unit 81-day running center-average proxy F10.7.
- setFixedGeomagneticAp(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
-
Set fixed (time invariant) value of the planetary 3-hour-range geomagnetic index aₚ.
- setFixedGeomagneticDst(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
-
Set fixed (time invariant) value of the planetary 1-hour-range geomagnetic index Dst.
- setFixedGeomagneticKp(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
-
Set fixed (time invariant) value of the planetary 3-hour-range geomagnetic index Kₚ.
- setFixedM10P7(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
-
Set fixed (time invariant) value of the Solar Flux daily proxy M10.7.
- setFixedM10P7Mean(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
-
Set fixed (time invariant) value of the Solar Flux 81-day running center-average proxy M10.7.
- setFixedS10P7(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
-
Set fixed (time invariant) value of the Solar Flux daily proxy S10.7.
- setFixedS10P7Mean(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
-
Set fixed (time invariant) value of the Solar Flux 81-day running center-average proxy S10.7.
- setFixedY10P7(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
-
Set fixed (time invariant) value of the Solar Flux daily proxy Y10.7.
- setFixedY10P7Mean(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
-
Set fixed (time invariant) value of the Solar Flux 81-day running center-average proxy Y10.7.
- setFormat(String) - Method in class org.orekit.files.ilrs.ILRSHeader
-
Set the file format.
- setFormatVersion(double) - Method in class org.orekit.files.ccsds.section.Header
-
Set the CCSDS NDM (ADM, ODM or TDM) format version.
- setFormatVersion(double) - Method in class org.orekit.gnss.clock.RinexClock
-
Setter for the format version.
- setFormatVersion(double) - Method in class org.orekit.gnss.navigation.RinexNavigation
-
Setter for the format version.
- setFrameA(FrameFacade) - Method in class org.orekit.files.ccsds.ndm.adm.AttitudeEndoints
-
Set frame A.
- setFrameB(FrameFacade) - Method in class org.orekit.files.ccsds.ndm.adm.AttitudeEndoints
-
Set frame B.
- setFrameEpoch(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.odm.CommonMetadata
-
Set epoch of reference frame, if not intrinsic to the definition of the
reference frame.
- setFrameEpochString(String) - Method in class org.orekit.files.ccsds.ndm.odm.CommonMetadata
-
Set epoch of reference frame, if not intrinsic to the definition of the
reference frame.
- setFrameName(String) - Method in class org.orekit.gnss.clock.RinexClock
-
Setter for the frame name.
- setFreqOffset(double) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
-
Setter for the freqOffset.
- setFrequencyNumber(double) - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSNavigationMessage
-
Setter for the frequency number.
- setFrequencySource(String) - Method in class org.orekit.files.ilrs.CRDConfiguration.TimingSystemConfiguration
-
Set the frequency source.
- setFT(int) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data
-
Set the GLONASS FT Word.
- setGalileoDataValidityStatus(int) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1045Data
-
Set the Galileo data validity status.
- setGalileoNavigationMessage(GalileoNavigationMessage) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1045Data
-
Set the Galileo navigation message.
- setGalileoToc(double) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1045Data
-
Set the Galileo time of clock.
- setGammaN(double) - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSNavigationMessage
-
Setter for the SV relative frequency bias.
- setGdop(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
-
Set generalize Dilution Of Precision.
- setGlonassNavigationMessage(GLONASSNavigationMessage) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data
-
Set the Glonass navigation message.
- setGm(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
-
Set gravitational coefficient of attracting body.
- setGnssIod(int) - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm01Data
-
Set the GNSS IOD.
- setGnssIod(int) - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm03Data
-
Set the GNSS IOD.
- setGpsCodeOnL2(int) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1019Data
-
Set the GPS code on L2.
- setGpsFitInterval(int) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1019Data
-
Set the GPS fit interval.
- setGpsL2PDataFlag(boolean) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1019Data
-
Set the GPS L2 P-code data flag.
- setGpsNavigationMessage(GPSNavigationMessage) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1019Data
-
Set the GPS navigation message.
- setGpsToc(double) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1019Data
-
Set the GPS time of clock.
- setGpsWeek(int) - Method in class org.orekit.files.sp3.SP3
-
Set the GPS week of the SP3 file.
- setGravitationalAssist(BodyFacade) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata
-
Set the origin of gravitational assist.
- setGravityModel(String, int, int) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
-
Set gravity model.
- setHandlers(List<EventHandler<D>>) - Method in class org.orekit.propagation.events.handlers.EventMultipleHandler
-
Change handlers list with user input.
- setHarvesters(MatricesHarvester[]) - Method in class org.orekit.estimation.sequential.AbstractKalmanModel
-
Setter for the jacobian harvesters.
- setHeader(CRDHeader) - Method in class org.orekit.files.ilrs.CRD.CRDDataBlock
-
Set the header for the current data block.
- setHealth(double) - Method in class org.orekit.propagation.analytical.gnss.data.AbstractEphemerisMessage
-
Setter for the health status.
- setHealth(int) - Method in class org.orekit.propagation.analytical.gnss.data.BeidouAlmanac
-
Sets the health status.
- setHealth(int) - Method in class org.orekit.propagation.analytical.gnss.data.GPSAlmanac
-
Sets the health status.
- setHealth(int) - Method in class org.orekit.propagation.analytical.gnss.data.QZSSAlmanac
-
Sets the health status.
- setHealthAvailabilityIndicator(boolean) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data
-
Set the flag indicating if GLONASS almanac health is available.
- setHealthE1(int) - Method in class org.orekit.propagation.analytical.gnss.data.GalileoAlmanac
-
Sets the E1-B/C signal health status.
- setHealthE5a(int) - Method in class org.orekit.propagation.analytical.gnss.data.GalileoAlmanac
-
Sets the E5a signal health status.
- setHealthE5b(int) - Method in class org.orekit.propagation.analytical.gnss.data.GalileoAlmanac
-
Sets the E5b signal health status.
- setHeightIonosphericLayer(double) - Method in class org.orekit.gnss.metric.messages.ssr.subtype.SsrIm201Data
-
Set the height of the ionospheric layer.
- setHighRateClockCorrection(double) - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm04Data
-
Set the high rate clock correction to be added to the polynomial clock correction.
- setHumiSensorManufacturer(String) - Method in class org.orekit.files.ilrs.CRDConfiguration.MeteorologicalConfiguration
-
Set the humidity sensor manufacturer.
- setHumiSensorModel(String) - Method in class org.orekit.files.ilrs.CRDConfiguration.MeteorologicalConfiguration
-
Set the humidity sensor model.
- setHumiSensorSerialNumber(String) - Method in class org.orekit.files.ilrs.CRDConfiguration.MeteorologicalConfiguration
-
Set the humidity sensor serial number.
- setI(double) - Method in class org.orekit.files.ccsds.ndm.odm.KeplerianElements
-
Set the orbit inclination.
- setI0(double, double) - Method in class org.orekit.propagation.analytical.gnss.data.BeidouAlmanac
-
Sets the Inclination Angle at Reference Time (rad).
- setI0(double) - Method in class org.orekit.propagation.analytical.gnss.data.CommonGnssData
-
Setter for the Inclination Angle at Reference Time (rad).
- setI11(double) - Method in class org.orekit.files.ccsds.ndm.adm.apm.SpacecraftParameters
-
Set the moment of Inertia about the 1-axis (N.m²).
- setI12(double) - Method in class org.orekit.files.ccsds.ndm.adm.apm.SpacecraftParameters
-
Set the moment of Inertia about the 1 and 2 axes (N.m²).
- setI13(double) - Method in class org.orekit.files.ccsds.ndm.adm.apm.SpacecraftParameters
-
Set the moment of Inertia about the 1 and 3 axes (N.m²).
- setI22(double) - Method in class org.orekit.files.ccsds.ndm.adm.apm.SpacecraftParameters
-
Set the moment of Inertia about the 2-axis (N.m²).
- setI23(double) - Method in class org.orekit.files.ccsds.ndm.adm.apm.SpacecraftParameters
-
Set the moment of Inertia about the 2 and 3 axes (N.m²).
- setI33(double) - Method in class org.orekit.files.ccsds.ndm.adm.apm.SpacecraftParameters
-
Set the moment of Inertia about the 3-axis (N.m²).
- setId(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
-
Set identification number.
- setIDot(double) - Method in class org.orekit.propagation.analytical.gnss.data.AbstractNavigationMessage
-
Setter for the Rate of Inclination Angle (rad/s).
- setIgnoreCentralAttraction(boolean) - Method in class org.orekit.propagation.numerical.FieldNumericalPropagator
-
- setIgnoreCentralAttraction(boolean) - Method in class org.orekit.propagation.numerical.NumericalPropagator
-
- setIlrsSatelliteId(String) - Method in class org.orekit.files.ilrs.ILRSHeader
-
Set the IRLS satellite ID (based on COSPAR ID).
- setInertiaMatrixEntry(int, int, double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
-
Set an entry in the inertia matrix.
- setInertiaReferenceFrame(FrameFacade) - Method in class org.orekit.files.ccsds.ndm.adm.apm.SpacecraftParameters
-
Set the coordinate system for the inertia tensor.
- setInitialJacobians(SpacecraftState, double[][], double[][], double[]) - Method in class org.orekit.propagation.analytical.tle.TLEJacobiansMapper
-
Set the Jacobian with respect to state into a one-dimensional additional state array.
- setInitialJacobians(SpacecraftState) - Method in class org.orekit.propagation.analytical.tle.TLEPartialDerivativesEquations
-
Deprecated.
Set the initial value of the Jacobian with respect to state and parameter.
- setInitialJacobians(SpacecraftState, double[][], double[][]) - Method in class org.orekit.propagation.analytical.tle.TLEPartialDerivativesEquations
-
Deprecated.
Set the initial value of the Jacobian with respect to state and parameter.
- setInitialJacobians(SpacecraftState, double[][], double[][], double[]) - Method in class org.orekit.propagation.integration.AbstractJacobiansMapper
-
Set the Jacobian with respect to state into a one-dimensional additional state array.
- setInitialJacobians(SpacecraftState) - Method in class org.orekit.propagation.numerical.EpochDerivativesEquations
-
Set the initial value of the Jacobian with respect to state and parameter.
- setInitialJacobians(SpacecraftState, double[][], double[][]) - Method in class org.orekit.propagation.numerical.EpochDerivativesEquations
-
Set the initial value of the Jacobian with respect to state and parameter.
- setInitialJacobians(SpacecraftState, double[][], double[][], double[]) - Method in class org.orekit.propagation.numerical.JacobiansMapper
-
Set the Jacobian with respect to state into a one-dimensional additional state array.
- setInitialJacobians(SpacecraftState) - Method in class org.orekit.propagation.numerical.PartialDerivativesEquations
-
Deprecated.
Set the initial value of the Jacobian with respect to state and parameter.
- setInitialJacobians(SpacecraftState, double[][], double[][]) - Method in class org.orekit.propagation.numerical.PartialDerivativesEquations
-
Deprecated.
Set the initial value of the Jacobian with respect to state and parameter.
- setInitialJacobians(SpacecraftState, double[][], double[][], double[]) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTJacobiansMapper
-
Set the Jacobian with respect to state into a one-dimensional additional state array.
- setInitialJacobians(SpacecraftState) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPartialDerivativesEquations
-
Deprecated.
Set the initial value of the Jacobian with respect to state and parameter.
- setInitialJacobians(SpacecraftState, double[][], double[][]) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPartialDerivativesEquations
-
Deprecated.
Set the initial value of the Jacobian with respect to state and parameter.
- setInitialPhi(SpacecraftState) - Method in class org.orekit.propagation.numerical.cr3bp.STMEquations
-
Method adding the standard initial values of the additional state to the initial spacecraft state.
- setInitialState(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.numerical.FieldNumericalPropagator
-
Set the initial state.
- setInitialState(SpacecraftState) - Method in class org.orekit.propagation.numerical.NumericalPropagator
-
Set the initial state.
- setInitialState(SpacecraftState) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator
-
Set the initial state with osculating orbital elements.
- setInitialState(SpacecraftState, PropagationType) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator
-
Set the initial state.
- setInitialState(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator
-
Set the initial state with osculating orbital elements.
- setInitialState(FieldSpacecraftState<T>, PropagationType) - Method in class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator
-
Set the initial state.
- setInitialWetMass(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
-
Set the total mass at beginning of life.
- setInRotationAngles(boolean) - Method in class org.orekit.files.ccsds.ndm.adm.apm.Euler
-
Set flag for rotation angle parsing.
- setIntegrationInterval(double) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
-
Setter for the integrationInterval.
- setIntegrationRef(IntegrationReference) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
-
Setter for the integrationRef.
- setInternationalDesignator(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
-
Set the international designator for the object.
- setInterpMethodEOP(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
-
Set the interpolation method for Earth Orientation Parameters.
- setInterpMethodSW(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
-
Set the interpolation method for Space Weather data.
- setInterpolationDegree(int) - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemMetadata
-
Set the interpolation degree.
- setInterpolationDegree(int) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata
-
Set the interpolation degree.
- setInterpolationDegree(int) - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemMetadata
-
Set the interpolation degree.
- setInterpolationDegree(int) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
-
Set the interpolation degree.
- setInterpolationGridToFixedNumberOfPoints(int) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator
-
Set the interpolation grid generator.
- setInterpolationGridToFixedNumberOfPoints(int) - Method in class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator
-
Set the interpolation grid generator.
- setInterpolationGridToMaxTimeGap(double) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator
-
Set the interpolation grid generator.
- setInterpolationGridToMaxTimeGap(T) - Method in class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator
-
Set the interpolation grid generator.
- setInterpolationMethod(String) - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemMetadata
-
Set the interpolation method to be used.
- setInterpolationMethod(InterpolationMethod) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata
-
Set the interpolation method to be used.
- setInterpolationMethod(InterpolationMethod) - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemMetadata
-
Set the interpolation method to be used.
- setInterpolationMethod(String) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
-
Set the interpolation method to be used.
- setInterpolationSample(int) - Method in class org.orekit.files.ilrs.CPF
-
Set the interpolation sample.
- setIOD(int) - Method in class org.orekit.propagation.analytical.gnss.data.GalileoAlmanac
-
Sets the Issue of Data (IOD).
- setIODC(double) - Method in class org.orekit.propagation.analytical.gnss.data.GPSNavigationMessage
-
Setter for the Issue of Data Clock.
- setIODC(double) - Method in class org.orekit.propagation.analytical.gnss.data.QZSSNavigationMessage
-
Setter for the Issue of Data, Clock.
- setIODE(double) - Method in class org.orekit.propagation.analytical.gnss.data.GPSNavigationMessage
-
Setter for the Issue of Data Ephemeris.
- setIODE(double) - Method in class org.orekit.propagation.analytical.gnss.data.QZSSNavigationMessage
-
Setter for the Issue of Data, Ephemeris.
- setIODEC(double) - Method in class org.orekit.propagation.analytical.gnss.data.IRNSSNavigationMessage
-
Setter for the Issue of Data, Ephemeris and Clock.
- setIODN(double) - Method in class org.orekit.propagation.analytical.gnss.data.SBASNavigationMessage
-
Setter for the issue of data navigation.
- setIODNav(double) - Method in class org.orekit.propagation.analytical.gnss.data.GalileoNavigationMessage
-
Setter for the Issue of Data of the navigation batch.
- setIodSsr(int) - Method in class org.orekit.gnss.metric.messages.ssr.SsrHeader
-
Set the IOD SSR.
- setIonosphericCorrectionType(String) - Method in class org.orekit.gnss.navigation.RinexNavigation
-
Setter for the ionospheric correction type.
- setIsCenterOfMassCorrectionApplied(boolean) - Method in class org.orekit.files.ilrs.CPFHeader
-
Set the flag telling if the center of mass correction is applied.
- setIsCenterOfMassCorrectionApplied(boolean) - Method in class org.orekit.files.ilrs.CRDHeader
-
Set the center of mass correction applied indicator.
- setIsCompatibleWithTIVs(boolean) - Method in class org.orekit.files.ilrs.CPFHeader
-
Set the flag for compatibility with TIVs.
- setIsConsistencyMaintained(boolean) - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm06Header
-
Set the flag indicating if phase biases maintain consistency
between non-dispersive and all original dispersive phase signals.
- setIsFirst(boolean) - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemMetadata
-
Set the flag for the placement of the quaternion QC in the attitude data.
- setIsMelbourneWubbenaConsistencyMaintained(boolean) - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm06Header
-
Set the flag indicating if consistency between
code and phase biases is maintained for the MW combinations.
- setIsReceiveAmplitudeCorrectionApplied(boolean) - Method in class org.orekit.files.ilrs.CRDHeader
-
Set the receive amplitude correction applied indicator.
- setIsSpacecraftTimeSimplified(boolean) - Method in class org.orekit.files.ilrs.CRDConfiguration.TransponderConfiguration
-
Set the spacecraft time simplified flag.
- setIsStationSystemDelayApplied(boolean) - Method in class org.orekit.files.ilrs.CRDHeader
-
Set the station system delay applied indicator.
- setIsTransponderDelayApplied(boolean) - Method in class org.orekit.files.ilrs.CRDHeader
-
Set the spacecraft system delay applied (transponders) indicator.
- setIsTroposphericRefractionApplied(boolean) - Method in class org.orekit.files.ilrs.CRDHeader
-
Set the tropospheric refraction correction applied indicator.
- setIterationsCounter(Incrementor) - Method in class org.orekit.estimation.leastsquares.AbstractBatchLSModel
-
Set the counter for iterations.
- setJulianDay(int) - Method in class org.orekit.files.sp3.SP3
-
Set the julian day for this SP3 file.
- setKlobucharAlpha(double[]) - Method in class org.orekit.gnss.navigation.RinexNavigation
-
Set the "alpha" ionspheric parameters.
- setKlobucharBeta(double[]) - Method in class org.orekit.gnss.navigation.RinexNavigation
-
Set the "beta" ionospheric parameters.
- setLaserId(String) - Method in class org.orekit.files.ilrs.CRDConfiguration.LaserConfiguration
-
Set the laser configuration ID.
- setLaserRecord(CRDConfiguration.LaserConfiguration) - Method in class org.orekit.files.ilrs.CRDConfiguration
-
Set the laser configuration record.
- setLaserType(String) - Method in class org.orekit.files.ilrs.CRDConfiguration.LaserConfiguration
-
Set the laser type.
- setLNFifthString(int) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data
-
Set the GLONASS ln Word extracted from fifth string of the subframe.
- setLNThirdString(int) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data
-
Set the GLONASS ln Word extracted from third string of the subframe.
- setLocalTimingId(String) - Method in class org.orekit.files.ilrs.CRDConfiguration.TimingSystemConfiguration
-
Set the local timing system configuration ID.
- setLowElevationThreshold(double) - Method in class org.orekit.models.earth.troposphere.SaastamoinenModel
-
Set the low elevation threshold value for path delay computation.
- setM(int) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data
-
Set the GLONASS M Word.
- setM0(double) - Method in class org.orekit.propagation.analytical.gnss.data.CommonGnssData
-
Setter for the Mean Anomaly at Reference Time (rad).
- setMainFieldCoefficients(int, int, double, double) - Method in class org.orekit.models.earth.GeoMagneticField
-
Set the given main field coefficients.
- setManBasis(ManBasis) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata
-
Set basis of this maneuver history data.
- setManBasisID(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata
-
Set identification number of the orbit determination or simulation upon which this maneuver is based.
- setManComposition(List<ManeuverFieldType>) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata
-
Set maneuver element of information.
- setManDeviceID(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata
-
Set identifier of the device used for this maneuver.
- setManeuversFrequency(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
-
Set the average frequency of orbit or attitude maneuvers (in SI units, hence per second).
- setManFrameEpoch(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata
-
- setManID(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata
-
Set maneuver identification number.
- setManNextEpoch(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata
-
Set start time of next maneuver.
- setManNextID(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata
-
Set identification number of next maneuver.
- setManPredSource(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata
-
Set prediction source on which this maneuver is based.
- setManPrevEpoch(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata
-
Set completion time of previous maneuver.
- setManPrevID(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata
-
Set identification number of previous maneuver.
- setManPurpose(List<String>) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata
-
Set the purposes of the maneuver.
- setManReferenceFrame(FrameFacade) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata
-
Set reference frame of the maneuver.
- setManufacturer(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
-
Set manufacturer name.
- setManUnits(List<Unit>) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.ManeuverHistoryMetadata
-
Set maneuver element of information units.
- setMappers(AbstractJacobiansMapper[]) - Method in class org.orekit.estimation.sequential.AbstractKalmanModel
-
- setMass(double) - Method in class org.orekit.files.ccsds.ndm.odm.SpacecraftParameters
-
Set the spacecraft mass.
- setMass(double) - Method in class org.orekit.propagation.conversion.DSSTPropagatorBuilder
-
Set the initial mass.
- setMass(double) - Method in class org.orekit.propagation.conversion.NumericalPropagatorBuilder
-
Set the initial mass.
- setMatrix(PolynomialFunction[][]) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.PolynomialFunctionMatrix
-
Set values for all elements.
- setMatrixLine(int, PolynomialFunction[]) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.PolynomialFunctionMatrix
-
Set the value of a line of the matrix.
- setMaxAreaForCollisionProbability(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
-
Set the maximum cross-sectional area for collision probability estimation purposes.
- setMaxEvaluations(int) - Method in class org.orekit.estimation.leastsquares.BatchLSEstimator
-
Set the maximum number of model evaluations.
- setMaximumObsGap(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
-
Set maximum time between observations in the OD of the object.
- setMaxIter(int) - Method in class org.orekit.utils.SecularAndHarmonic
-
Set maximum number of iterations.
- setMaxIterations(int) - Method in class org.orekit.estimation.leastsquares.BatchLSEstimator
-
Set the maximum number of iterations.
- setMaxParseDegree(int) - Method in class org.orekit.forces.gravity.potential.OceanTidesReader
-
Set the degree limit for the next file parsing.
- setMaxParseDegree(int) - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
-
Set the degree limit for the next file parsing.
- setMaxParseOrder(int) - Method in class org.orekit.forces.gravity.potential.OceanTidesReader
-
Set the order limit for the next file parsing.
- setMaxParseOrder(int) - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
-
Set the order limit for the next file parsing.
- setMaxPredictedEigenMaj(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
-
Set maximum predicted major eigenvalue of 1σ positional error ellipsoid over entire time span of the OCM.
- setMaxRcs(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
-
Set the maximum radar cross-section.
- setMaxThrust(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
-
Set the maximum composite thrust the spacecraft can accomplish.
- setMaxValue(double) - Method in class org.orekit.utils.ParameterDriver
-
Set maximum parameter value.
- setMeanElementTheory(String) - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmMetadata
-
Set the description of the Mean Element Theory.
- setMeanMotion(double) - Method in class org.orekit.files.ccsds.ndm.odm.KeplerianElements
-
Set the orbit mean motion.
- setMeanMotionDot(double) - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmTle
-
Set the first time derivative of the mean motion.
- setMeanMotionDotDot(double) - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmTle
-
Set the second time derivative of the mean motion.
- setMessageId(String) - Method in class org.orekit.files.ccsds.section.Header
-
Set the ID that uniquely identifies a message from a given originator.
- setMeteorologicalId(String) - Method in class org.orekit.files.ilrs.CRDConfiguration.MeteorologicalConfiguration
-
Set the meteorological configuration ID.
- setMeteorologicalRecord(CRDConfiguration.MeteorologicalConfiguration) - Method in class org.orekit.files.ilrs.CRDConfiguration
-
Set the meteorological record.
- setMethod(OdMethodFacade) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
-
Set orbit determination method.
- setMinAreaForCollisionProbability(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
-
Set the minimum cross-sectional area for collision probability estimation purposes.
- setMinPredictedEigenMin(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
-
Set minimum predicted minor eigenvalue of 1σ positional error ellipsoid over entire time span of the OCM.
- setMinRcs(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
-
Set the minimum radar cross-section.
- setMinValue(double) - Method in class org.orekit.utils.ParameterDriver
-
Set minimum parameter value.
- setMode(TrackingMode) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
-
Setter for the mode.
- setMu(double) - Method in class org.orekit.files.ccsds.ndm.odm.KeplerianElements
-
Set the gravitational coefficient.
- setMu(double) - Method in class org.orekit.files.ilrs.CPF
-
Set the gravitational coefficient.
- setMu(double) - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
-
Set the central body attraction coefficient.
- setMu(double) - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
-
Set the central attraction coefficient μ.
- setMu(T) - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator
-
Set the central attraction coefficient μ.
- setMu(T) - Method in class org.orekit.propagation.numerical.FieldNumericalPropagator
-
Set the central attraction coefficient μ.
- setMu(double) - Method in class org.orekit.propagation.numerical.NumericalPropagator
-
Set the central attraction coefficient μ.
- setMu(double) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator
-
Set the central attraction coefficient μ.
- setMu(T) - Method in class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator
-
Set the central attraction coefficient μ.
- setMuCreated(double) - Method in class org.orekit.files.ccsds.ndm.odm.OdmParser
-
Set the gravitational coefficient created from the knowledge of the central body.
- setMuParsed(double) - Method in class org.orekit.files.ccsds.ndm.odm.OdmParser
-
Set the gravitational coefficient parsed in the ODM File.
- setN4(int) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data
-
Set the four-year interval number starting from 1996.
- setNA(int) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data
-
Set the GLONASS NA Word.
- setName(int, SatelliteSystem) - Method in class org.orekit.estimation.measurements.gnss.AbstractCycleSlipDetector
-
Create the name of a satellite from its PRN number and satellite System it belongs to.
- setName(String) - Method in class org.orekit.files.ilrs.ILRSHeader
-
Set the satellite target name.
- setName(String) - Method in class org.orekit.utils.ParameterDriver
-
Change the name of this parameter driver.
- setNBodyPerturbations(List<BodyFacade>) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
-
Set n-body perturbation bodies.
- setNeQuickAlpha(double[]) - Method in class org.orekit.gnss.navigation.RinexNavigation
-
Set the "alpha" ionospheric parameters.
- setNextMessageEpoch(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
-
Set the creation date of next message from a given originator.
- setNextMessageID(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
-
Set the unique ID identifying next message from a given originator.
- setNominalFireRate(double) - Method in class org.orekit.files.ilrs.CRDConfiguration.LaserConfiguration
-
Set the nominal fire rate.
- setNoradID(int) - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmTle
-
Set the NORAD Catalog Number ("Satellite Number").
- setNoradId(String) - Method in class org.orekit.files.ilrs.ILRSHeader
-
Set the satellite NORAD ID.
- setNormalizedValue(double) - Method in class org.orekit.utils.ParameterDriver
-
Set normalized value.
- setNt(int) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data
-
Set the current date.
- setNumberOfBiasesProcessed(int) - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm05Data
-
Set the number of biases processed for the current satellite.
- setNumberOfBiasesProcessed(int) - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm06Data
-
Set the number of biases processed for the current satellite.
- setNumberOfEpochs(int) - Method in class org.orekit.files.sp3.SP3
-
Set the number of epochs as contained in the SP3 file.
- setNumberOfIonosphericLayers(int) - Method in class org.orekit.gnss.metric.messages.ssr.subtype.SsrIm201Header
-
Set the number of ionospheric layers.
- setNumberOfLeapSeconds(int) - Method in class org.orekit.gnss.clock.RinexClock
-
Setter for the number of leap seconds.
- setNumberOfLeapSeconds(int) - Method in class org.orekit.gnss.navigation.RinexNavigation
-
Setter for the current number of leap seconds.
- setNumberOfLeapSecondsGNSS(int) - Method in class org.orekit.gnss.clock.RinexClock
-
Setter for the number of leap seconds for GNSS time scales.
- setNumberOfSatellites(int) - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgmHeader
-
Set the number of satellites for the current IGM message.
- setNutation(double) - Method in class org.orekit.files.ccsds.ndm.adm.apm.SpinStabilized
-
Set the nutation angle of spin axis (rad).
- setNutationPeriod(double) - Method in class org.orekit.files.ccsds.ndm.adm.apm.SpinStabilized
-
Set the body nutation period of the spin axis (s).
- setNutationPhase(double) - Method in class org.orekit.files.ccsds.ndm.adm.apm.SpinStabilized
-
Set the inertial nutation phase (rad).
- setObjectDesignator(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
-
Set the unique satellite identification designator for the object.
- setObjectID(String) - Method in class org.orekit.files.ccsds.ndm.adm.AdmMetadata
-
Set the spacecraft ID for which the attitude data are provided.
- setObjectID(String) - Method in class org.orekit.files.ccsds.ndm.odm.CommonMetadata
-
Set the spacecraft ID for which the orbit state is provided.
- setObjectName(String) - Method in class org.orekit.files.ccsds.ndm.adm.AdmMetadata
-
Set the spacecraft name for which the attitude data are provided.
- setObjectName(String) - Method in class org.orekit.files.ccsds.ndm.odm.OdmMetadata
-
Set the spacecraft name for which the orbit state is provided.
- setObjectType(ObjectType) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
-
Set the type of object.
- setOblateFlattening(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
-
Set central body oblate spheroid oblateness.
- setObsAvailable(int) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
-
Set number of observations available within the actual OD span.
- setObservations(List<Observation>) - Method in class org.orekit.files.ccsds.ndm.tdm.ObservationsBlock
-
Set the list of Observations Data Lines.
- setObserver(BatchLSObserver) - Method in class org.orekit.estimation.leastsquares.BatchLSEstimator
-
Set an observer for iterations.
- setObserver(KalmanObserver) - Method in class org.orekit.estimation.sequential.KalmanEstimator
-
Set the observer.
- setObserver(KalmanObserver) - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanEstimator
-
Set the observer.
- setObserver(KalmanObserver) - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanModel
-
Set the observer.
- setObsUsed(int) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
-
Set number of observations accepted within the actual OD span.
- setOceanTidesModel(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
-
Set ocean tides model.
- setOcmDataElements(List<String>) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
-
Set the list of elements of information data blocks included in this message.
- setOebAreaAlongIntermediate(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
-
Set the cross-sectional area of Optimally Enclosing Box along Y-OEB.
- setOebAreaAlongMax(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
-
Set the cross-sectional area of Optimally Enclosing Box along X-OEB.
- setOebAreaAlongMin(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
-
Set the cross-sectional area of Optimally Enclosing Box along Z-OEB.
- setOebIntermediate(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
-
Set the dimensions of Optimally Enclosing Box along Y-OEB (i.e intermediate).
- setOebMax(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
-
Set the dimensions of Optimally Enclosing Box along X-OEB (i.e max).
- setOebMin(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
-
Set the dimensions of Optimally Enclosing Box along Z-OEB (i.e min).
- setOebParentFrame(FrameFacade) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
-
Set the Optimally Enclosing Box parent reference frame.
- setOebParentFrameEpoch(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
-
Set the Optimally Enclosing Box parent reference frame epoch.
- setOebQ(int, double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
-
set the component of quaternion defining Optimally Enclosing Box.
- setOmega0(double) - Method in class org.orekit.propagation.analytical.gnss.data.CommonGnssData
-
Setter for the Longitude of Ascending Node of Orbit Plane at Weekly Epoch (rad).
- setOmegaDot(double) - Method in class org.orekit.propagation.analytical.gnss.data.CommonGnssData
-
Setter for the rate of Rate of Right Ascension (rad/s).
- setOperator(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
-
Set the operator of the space object.
- setOpsStatus(OpsStatus) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
-
Set the operational status.
- setOrbAveraging(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata
-
Set type of averaging (Osculating, mean Brouwer, other.
- setOrbitCategory(OrbitCategory) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
-
Set the orbit category.
- setOrbitCorrection(OrbitCorrection) - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm01Data
-
Set the orbit correction data.
- setOrbitCorrection(OrbitCorrection) - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm03Data
-
Set the orbit correction data.
- setOrbitType(OrbitType) - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
-
Set propagation orbit type.
- setOrbitType(OrbitType) - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator
-
Set propagation orbit type.
- setOrbitType(OrbitType) - Method in class org.orekit.propagation.numerical.FieldNumericalPropagator
-
Set propagation orbit type.
- setOrbitType(OrbitType) - Method in class org.orekit.propagation.numerical.NumericalPropagator
-
Set propagation orbit type.
- setOrbitTypeKey(String) - Method in class org.orekit.files.sp3.SP3
-
Set the orbit type key for this SP3 file.
- setOrbRevNum(int) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata
-
Set the integer orbit revolution number.
- setOrbRevNumBasis(int) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata
-
Set the basis for orbit revolution number.
- setOriginator(String) - Method in class org.orekit.files.ccsds.section.Header
-
Set the file originator.
- setOriginatorAddress(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
-
Set the address of Programmatic Point Of Contact at originator.
- setOriginatorPhone(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
-
GSet the phone number of Programmatic Point Of Contact at originator.
- setOriginatorPOC(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
-
Set the programmatic Point Of Contact at originator.
- setOriginatorPosition(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
-
Set the position of Programmatic Point Of Contact at originator.
- setOutputPulseType(String) - Method in class org.orekit.files.ilrs.CRDConfiguration.DetectorConfiguration
-
Set the output pulse type.
- setOutputPulseWidth(double) - Method in class org.orekit.files.ilrs.CRDConfiguration.DetectorConfiguration
-
Set the output pulse width.
- setOwner(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
-
Set the owner of the space object.
- setP(int, double) - Method in class org.orekit.files.ccsds.ndm.odm.StateVector
-
Set position component.
- setP(int) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data
-
Set the GLONASS P Word.
- setP1(int) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data
-
Set the GLONASS P1 Word.
- setP2(int) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data
-
Set the GLONASS P2 Word.
- setP3(int) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data
-
Set the the GLONASS P3 Word.
- setP4(int) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data
-
Set the GLONASS P4 Word.
- setPa(double) - Method in class org.orekit.files.ccsds.ndm.odm.KeplerianElements
-
Set the orbit argument of pericenter.
- setPa(double) - Method in class org.orekit.propagation.analytical.gnss.data.CommonGnssData
-
Setter fir the Argument of Perigee (rad).
- setParameterDerivatives(ParameterDriver, double...) - Method in class org.orekit.estimation.measurements.EstimatedMeasurement
-
- setParameters(double[]) - Method in class org.orekit.propagation.conversion.AbstractPropagatorBuilder
-
Set the selected parameters.
- setParametersConvergenceThreshold(double) - Method in class org.orekit.estimation.leastsquares.BatchLSEstimator
-
Set convergence threshold.
- setParticipants(Map<Integer, String>) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
-
Setter for the participants.
- setPatchPointComponentFreedom(int, int, boolean) - Method in class org.orekit.utils.AbstractMultipleShooting
-
Set a component of a patch point to free or not.
- setPath(int[]) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
-
Setter for the path.
- setPath1(int[]) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
-
Setter for the path1.
- setPath2(int[]) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
-
Setter for the path2.
- setPosition(Vector3D) - Method in class org.orekit.files.sinex.Station
-
Set the station position.
- setPositionAngleType(PositionAngle) - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
-
Set position angle type.
- setPositionAngleType(PositionAngle) - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator
-
Set position angle type.
- setPositionAngleType() - Method in class org.orekit.propagation.integration.FieldStateMapper
-
Set position angle type.
- setPositionAngleType(PositionAngle) - Method in class org.orekit.propagation.numerical.FieldNumericalPropagator
-
Set position angle type.
- setPositionAngleType(PositionAngle) - Method in class org.orekit.propagation.numerical.NumericalPropagator
-
Set position angle type.
- setPredictionProvider(String) - Method in class org.orekit.files.ilrs.CRDHeader
-
Set the prediction provider.
- setPredictionType(int) - Method in class org.orekit.files.ilrs.CRDHeader
-
Set the prediction type.
- setPressSensorManufacturer(String) - Method in class org.orekit.files.ilrs.CRDConfiguration.MeteorologicalConfiguration
-
Set the pressure sensor manufacturer.
- setPressSensorModel(String) - Method in class org.orekit.files.ilrs.CRDConfiguration.MeteorologicalConfiguration
-
Set the pressure sensor model.
- setPressSensorSerialNumber(String) - Method in class org.orekit.files.ilrs.CRDConfiguration.MeteorologicalConfiguration
-
Set the pressure sensor serial number.
- setPressure(double) - Method in class org.orekit.models.earth.EarthStandardAtmosphereRefraction
-
Set the local pressure at the evaluation location
- setPrevId(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
-
Set identification of previous orbit determination.
- setPreviousMessageEpoch(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
-
Set the creation date of previous message from a given originator.
- setPreviousMessageID(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
-
Set the unique ID identifying previous message from a given originator.
- setPrf(double) - Method in class org.orekit.files.ilrs.CPFHeader
-
Set the Pulse Repetition Frequency (PRF).
- setPrimaryWavelength(double) - Method in class org.orekit.files.ilrs.CRDConfiguration.LaserConfiguration
-
Set the primary wavelength.
- setPrmMessageLink(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
-
Set the Unique identifier of Pointing Request Message linked to this Orbit Data Message.
- setPRN(int) - Method in class org.orekit.propagation.analytical.gnss.data.AbstractEphemerisMessage
-
Setter for the PRN number of the satellite.
- setPRN(int) - Method in class org.orekit.propagation.analytical.gnss.data.CommonGnssData
-
Setter for the PRN number of the satellite.
- setProcessingSoftwares(String[]) - Method in class org.orekit.files.ilrs.CRDConfiguration.SoftwareConfiguration
-
Set the processing softwares.
- setProcessingSoftwareVersions(String[]) - Method in class org.orekit.files.ilrs.CRDConfiguration.SoftwareConfiguration
-
Set the processing software versions.
- setProductionEpoch(DateComponents) - Method in class org.orekit.files.ilrs.ILRSHeader
-
Set the date component of the ephemeris production.
- setProductionHour(int) - Method in class org.orekit.files.ilrs.ILRSHeader
-
Set the hour of ephemeris production.
- setProgramName(String) - Method in class org.orekit.gnss.clock.RinexClock
-
Setter for the program name.
- setProgramName(String) - Method in class org.orekit.gnss.navigation.RinexNavigation
-
Setter for the program name.
- setProxy(Proxy.Type, String, int) - Method in class org.orekit.gnss.metric.ntrip.NtripClient
-
Set proxy parameters.
- setPulseEnergy(double) - Method in class org.orekit.files.ilrs.CRDConfiguration.LaserConfiguration
-
Set the pulse energy.
- setPulseInOutgoingSemiTrain(int) - Method in class org.orekit.files.ilrs.CRDConfiguration.LaserConfiguration
-
Set the number of pulses in outgoing semi-train.
- setPulseWidth(double) - Method in class org.orekit.files.ilrs.CRDConfiguration.LaserConfiguration
-
Set the pulse width.
- setQ(int, double) - Method in class org.orekit.files.ccsds.ndm.adm.apm.ApmQuaternion
-
Set quaternion component.
- setQDot(int, double) - Method in class org.orekit.files.ccsds.ndm.adm.apm.ApmQuaternion
-
Set quaternion derivative component.
- setQualityIndicator(int) - Method in class org.orekit.files.ilrs.CRDHeader
-
Set the data quality indicator.
- setQuantumEfficiency(double) - Method in class org.orekit.files.ilrs.CRDConfiguration.DetectorConfiguration
-
Set the quantum efficiency at applicable wavelength.
- setQzssCodeOnL2(int) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1044Data
-
Set the QZSS code on L2.
- setQzssFitInterval(int) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1044Data
-
Set the QZSS fit interval.
- setQzssNavigationMessage(QZSSNavigationMessage) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1044Data
-
Set the QZSS navigation message.
- setQzssToc(double) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1044Data
-
Set the QZSS time of clock.
- setRaan(double) - Method in class org.orekit.files.ccsds.ndm.odm.KeplerianElements
-
Set the orbit right ascension of ascending node.
- setRangeMode(RangeMode) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
-
Setter for the rangeMode.
- setRangeType(int) - Method in class org.orekit.files.ilrs.CRDHeader
-
Set the range type indicator.
- setRangeUnits(RangeUnits) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
-
Setter for the rangeUnits.
- setRateFrameIsA(boolean) - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemMetadata
-
Set the frame in which rates are specified.
- setRateFrameIsA(boolean) - Method in class org.orekit.files.ccsds.ndm.adm.apm.Euler
-
Set the frame in which rates are specified.
- setRawCoefficients(boolean, double[][], double[][], String) - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
-
- setRawCoefficients(boolean, Flattener, double[], double[], String) - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
-
Set the tesseral-sectorial coefficients matrix.
- setRawCorrectionRange(double) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
-
Setter for the raw correction for range.
- setRawRangeModulus(double) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
-
Setter for the raw range modulus.
- setRcs(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
-
Set the typical (50th percentile) radar cross-section.
- setRdmMessageLink(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
-
Set the Unique identifier of Reentry Data Message linked to this Orbit Data Message.
- setReadComplete(boolean) - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
-
Set the indicator for completed read.
- setReceiveBand(String) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
-
Setter for the receiveBand.
- setReceiveDelays(Map<Integer, Double>) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
-
Setter for the receiveDelays.
- setRecommendedOdSpan(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
-
Set sime span of observation recommended for the OD of the object.
- setReconnectParameters(double, double, int) - Method in class org.orekit.gnss.metric.ntrip.NtripClient
-
Set Reconnect parameters.
- setReductionTheory(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
-
Set reduction theory used for precession and nutation modeling.
- setReferenceDate(AbsoluteDate) - Method in class org.orekit.utils.ParameterDriver
-
Set reference date.
- setReferenceFrame(FrameFacade) - Method in class org.orekit.files.ccsds.ndm.odm.CartesianCovariance
-
Set the reference frame in which data are given.
- setReferenceFrame(FrameFacade) - Method in class org.orekit.files.ccsds.ndm.odm.CommonMetadata
-
Set the reference frame in which data are given: used for state vector
and Keplerian elements data (and for the covariance reference frame if none is given).
- setReferenceFrame(FrameFacade) - Method in class org.orekit.files.ccsds.ndm.odm.opm.Maneuver
-
Set Coordinate system for velocity increment vector.
- setReferenceFrame(FrameFacade) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
-
Set the reference frame in which data are given: used for RADEC tracking data.
- setReferenceState(SpacecraftState) - Method in class org.orekit.propagation.AbstractMatricesHarvester
-
Set up reference state.
- setReferenceState(SpacecraftState) - Method in class org.orekit.propagation.analytical.AbstractAnalyticalMatricesHarvester
-
Set up reference state.
- setReferenceState(SpacecraftState) - Method in class org.orekit.propagation.integration.AbstractJacobiansMapper
-
Set up reference state.
- setReferenceState(SpacecraftState) - Method in interface org.orekit.propagation.MatricesHarvester
-
Set up reference state.
- setReferenceState(SpacecraftState) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTHarvester
-
Set up reference state.
- setReferenceState(SpacecraftState) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTJacobiansMapper
-
Set up reference state.
- setReferenceTrajectories(Propagator[]) - Method in class org.orekit.estimation.sequential.AbstractKalmanModel
-
Setter for the reference trajectories.
- setReferenceValue(double) - Method in class org.orekit.utils.ParameterDriver
-
Set reference parameter value.
- setRefFrame(Frame) - Method in class org.orekit.files.ilrs.CPFHeader
-
Set the reference frame.
- setRefFrameId(int) - Method in class org.orekit.files.ilrs.CPFHeader
-
Set the reference frame identifier.
- setRefFrameString(String) - Method in class org.orekit.files.ccsds.ndm.adm.apm.Maneuver
-
Set Coordinate system for the torque vector, for absolute frames.
- setReflectivity(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
-
Set the typical (50th percentile) coefficient of reflectivity.
- setRemainingDv(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
-
Set the total ΔV remaining for spacecraft.
- setResetAtEnd(boolean) - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
-
Allow/disallow resetting the initial state at end of propagation.
- setResetAtEnd(boolean) - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator
-
Allow/disallow resetting the initial state at end of propagation.
- setRevAtEpoch(int) - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmTle
-
Set the revolution rumber.
- setRolloverReference(DateComponents) - Static method in class org.orekit.time.GNSSDate
-
Set a reference date for ensuring continuity across GNSS week rollover.
- setRotationalAngleType(int) - Method in class org.orekit.files.ilrs.CPFHeader
-
Set the rotation angle type.
- setRotationAngle(char, double) - Method in class org.orekit.files.ccsds.ndm.adm.apm.Euler
-
Set the Euler angle about (rad).
- setRotationRate(char, double) - Method in class org.orekit.files.ccsds.ndm.adm.apm.Euler
-
Set the rate of Euler angle (rad/s).
- setSatConfiguration(int) - Method in class org.orekit.propagation.analytical.gnss.data.GPSAlmanac
-
Sets the satellite configuration.
- setSatelliteID(int) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.RtcmEphemerisData
-
Set the satellite ID.
- setSatelliteID(int) - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgmData
-
Set the satellite ID.
- setSatelliteRevolution(int) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator
-
Override the default value of the parameter.
- setSatelliteRevolution(int) - Method in class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator
-
Override the default value of the parameter.
- setSatelliteSystem(SatelliteSystem) - Method in class org.orekit.gnss.clock.RinexClock
-
Setter for the satellite system.
- setSatelliteSystem(SatelliteSystem) - Method in class org.orekit.gnss.navigation.RinexNavigation
-
Setter for the satellite system.
- setScale(double) - Method in class org.orekit.utils.ParameterDriver
-
Set scale.
- setSclkOffsetAtEpoch(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
-
- setSclkSecPerSISec(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
-
Set the number of spacecraft clock seconds occurring during one SI second.
- setSecondsOfWeek(double) - Method in class org.orekit.files.sp3.SP3
-
Set the seconds of the GPS week for this SP3 file.
- setSecularVariationCoefficients(int, int, double, double) - Method in class org.orekit.models.earth.GeoMagneticField
-
Set the given secular variation coefficients.
- setSelected(boolean) - Method in class org.orekit.utils.ParameterDriver
-
Configure a parameter selection status.
- setSelectedCoefficients(Set<String>) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator
-
Set the selected short periodic coefficients that must be stored as additional states.
- setSelectedCoefficients(Set<String>) - Method in class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator
-
Set the selected short periodic coefficients that must be stored as additional states.
- setSensors(List<String>) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
-
Set description of sensors used.
- setSensorsN(int) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
-
Set number of sensors used.
- setSequenceNumber(int) - Method in class org.orekit.files.ilrs.ILRSHeader
-
Set the ephemeris sequence number.
- setShadowBodies(List<BodyFacade>) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
-
Set celestial bodies casting shadows.
- setShadowModel(ShadowModel) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
-
Set shadow model used for solar radiation pressure.
- setShortPeriodJacobians(SpacecraftState) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTJacobiansMapper
-
- setShortPeriodTerms(List<ShortPeriodTerms>) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator
-
Override the default value short periodic terms.
- setSic(String) - Method in class org.orekit.files.ilrs.ILRSHeader
-
Set the SIC ID.
- setSigma(double[]) - Method in class org.orekit.estimation.measurements.modifiers.DynamicOutlierFilter
-
Set the current value of sigma.
- setSisa(double) - Method in class org.orekit.propagation.analytical.gnss.data.GalileoNavigationMessage
-
Setter for the signal in space accuracy.
- setSiteCode(String) - Method in class org.orekit.files.sinex.Station
-
Set the site code (station identifier).
- setSma(double) - Method in class org.orekit.propagation.analytical.gnss.data.CommonGnssData
-
Setter for the semi-major axis.
- setSnm(double[][]) - Method in class org.orekit.gnss.metric.messages.ssr.subtype.SsrIm201Data
-
Set the sine parameters of spherical harmonics expansion of degree N and order M.
- setSoftwareId(String) - Method in class org.orekit.files.ilrs.CRDConfiguration.SoftwareConfiguration
-
Set the software configuration ID.
- setSoftwareRecord(CRDConfiguration.SoftwareConfiguration) - Method in class org.orekit.files.ilrs.CRDConfiguration
-
Set the software configuration record.
- setSolarRadArea(double) - Method in class org.orekit.files.ccsds.ndm.odm.SpacecraftParameters
-
Set the solar radiation pressure area.
- setSolarRadCoeff(double) - Method in class org.orekit.files.ccsds.ndm.odm.SpacecraftParameters
-
Get the solar radiation pressure coefficient.
- setSolidTidesModel(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
-
Set solid tides model.
- setSolveN(int) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
-
Set number of solved-for states.
- setSolveStates(List<String>) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
-
Set description of state elements solved-for.
- setSource(String) - Method in class org.orekit.files.ilrs.CPFHeader
-
Set the ephemeris source.
- setSource(String) - Method in class org.orekit.propagation.analytical.gnss.data.GPSAlmanac
-
Sets the source of this GPS almanac.
- setSource(String) - Method in class org.orekit.propagation.analytical.gnss.data.QZSSAlmanac
-
Sets the source of this GPS almanac.
- setSpacecraftClockAndDriftApplied(int) - Method in class org.orekit.files.ilrs.CRDConfiguration.TransponderConfiguration
-
Set the spacecraft clock offset and drift applied indicator.
- setSpacecraftEpochTimeScale(int) - Method in class org.orekit.files.ilrs.CRDHeader
-
Set the spacecraft epoch time scale.
- setSpaceWeatherEpoch(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
-
Set epoch of the Space Weather data.
- setSpaceWeatherSource(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
-
Set Space Weather data source.
- setSpatialFilter(double) - Method in class org.orekit.files.ilrs.CRDConfiguration.DetectorConfiguration
-
Set the spatial filter.
- setSpectralFilter(double) - Method in class org.orekit.files.ilrs.CRDConfiguration.DetectorConfiguration
-
Set the spectral filter.
- setSphericalHarmonicsDegree(int) - Method in class org.orekit.gnss.metric.messages.ssr.subtype.SsrIm201Data
-
Set the degree of spherical harmonic expansion.
- setSphericalHarmonicsOrder(int) - Method in class org.orekit.gnss.metric.messages.ssr.subtype.SsrIm201Data
-
Set the order of spherical harmonic expansion.
- setSpinAlpha(double) - Method in class org.orekit.files.ccsds.ndm.adm.apm.SpinStabilized
-
Set the right ascension of spin axis vector (rad).
- setSpinAngle(double) - Method in class org.orekit.files.ccsds.ndm.adm.apm.SpinStabilized
-
Set the phase of the satellite about the spin axis (rad).
- setSpinAngleVel(double) - Method in class org.orekit.files.ccsds.ndm.adm.apm.SpinStabilized
-
Set the angular velocity of satellite around spin axis (rad/s).
- setSpinDelta(double) - Method in class org.orekit.files.ccsds.ndm.adm.apm.SpinStabilized
-
Set the declination of the spin axis vector (rad).
- setSqrtA(double) - Method in class org.orekit.propagation.analytical.gnss.data.AbstractNavigationMessage
-
Setter for the Square Root of Semi-Major Axis (m^1/2).
- setSqrtA(double) - Method in class org.orekit.propagation.analytical.gnss.data.BeidouAlmanac
-
Sets the Square Root of Semi-Major Axis (m^1/2).
- setSqrtA(double) - Method in class org.orekit.propagation.analytical.gnss.data.GPSAlmanac
-
Setter for the Square Root of Semi-Major Axis (m^1/2).
- setSqrtA(double) - Method in class org.orekit.propagation.analytical.gnss.data.IRNSSAlmanac
-
Setter for the Square Root of Semi-Major Axis (m^1/2).
- setSqrtA(double) - Method in class org.orekit.propagation.analytical.gnss.data.QZSSAlmanac
-
Setter for the Square Root of Semi-Major Axis (m^1/2).
- setSrpCoefficient(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
-
Set the nominal SRP coefficient.
- setSrpConstantArea(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
-
Set the attitude-independent SRP area, not already into attitude-dependent area along OEB.
- setSrpModel(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Perturbations
-
Set Solar Radiation Pressure model.
- setSrpUncertainty(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
-
Set the SRP coefficient 1σ uncertainty.
- setSsrEpoch1s(double) - Method in class org.orekit.gnss.metric.messages.ssr.SsrHeader
-
Set the SSR Epoch Time 1s.
- setSsrMultipleMessageIndicator(int) - Method in class org.orekit.gnss.metric.messages.ssr.SsrHeader
-
Set the SSR Multiple Message Indicator.
- setSsrProviderId(int) - Method in class org.orekit.gnss.metric.messages.ssr.SsrHeader
-
Set the SSR Provider ID.
- setSsrSolutionId(int) - Method in class org.orekit.gnss.metric.messages.ssr.SsrHeader
-
Set the SSR Solution ID.
- setSsrUpdateInterval(int) - Method in class org.orekit.gnss.metric.messages.ssr.SsrHeader
-
Set the SSR Update Interval.
- setSsrUra(double) - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm07Data
-
Set the SSR User Range Accuracy (URA).
- setStartDate(AbsoluteDate) - Method in class org.orekit.propagation.AbstractPropagator
-
Set a start date.
- setStartDate(FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.FieldAbstractPropagator
-
Set a start date.
- setStartEpoch(AbsoluteDate) - Method in class org.orekit.files.ilrs.ILRSHeader
-
Set the staring epoch (UTC).
- setStartTime(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemMetadata
-
Set start of total time span covered by attitude data.
- setStartTime(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
-
Set the time of the earliest data contained in the OCM.
- setStartTime(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemMetadata
-
Set start of total time span covered by ephemerides data and
covariance data.
- setStartTime(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
-
Setter for the startTime.
- setStateDerivatives(int, double[]...) - Method in class org.orekit.estimation.measurements.EstimatedMeasurement
-
- setStationClockAndDriftApplied(int) - Method in class org.orekit.files.ilrs.CRDConfiguration.TransponderConfiguration
-
Set the station clock offset and drift applied indicator.
- setStationIdentifier(String) - Method in class org.orekit.gnss.clock.RinexClock
-
Setter for the station identifier.
- setStationName(String) - Method in class org.orekit.files.ilrs.CRDHeader
-
Set the station name from official list.
- setStationName(String) - Method in class org.orekit.gnss.clock.RinexClock
-
Setter for the station name.
- setStationNetword(String) - Method in class org.orekit.files.ilrs.CRDHeader
-
Set the station network.
- setStationOscDrift(double) - Method in class org.orekit.files.ilrs.CRDConfiguration.TransponderConfiguration
-
Set the estimated station oscillator drift in parts in 10¹⁵.
- setStationUTCOffset(double) - Method in class org.orekit.files.ilrs.CRDConfiguration.TransponderConfiguration
-
Set the estimated station UTC offset.
- setStatus(EstimatedMeasurement.Status) - Method in class org.orekit.estimation.measurements.EstimatedMeasurement
-
Set the status.
- setStep(int) - Method in class org.orekit.files.ilrs.CPFHeader
-
Set the time between table entries.
- setStepHandler(T, FieldOrekitFixedStepHandler<T>) - Method in interface org.orekit.propagation.FieldPropagator
-
Set a single handler for fixed stepsizes.
- setStepHandler(FieldOrekitStepHandler<T>) - Method in interface org.orekit.propagation.FieldPropagator
-
Set a single handler for variable stepsizes.
- setStepHandler(double, OrekitFixedStepHandler) - Method in interface org.orekit.propagation.Propagator
-
Set a single handler for fixed stepsizes.
- setStepHandler(OrekitStepHandler) - Method in interface org.orekit.propagation.Propagator
-
Set a single handler for variable stepsizes.
- setStopTime(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemMetadata
-
Set end of total time span covered by attitude data.
- setStopTime(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
-
Set the time of the latest data contained in the OCM.
- setStopTime(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemMetadata
-
Set end of total time span covered by ephemerides data and covariance
data.
- setStopTime(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
-
Setter for the stopTime.
- setSubDailySequenceNumber(int) - Method in class org.orekit.files.ilrs.CPFHeader
-
Set the sub-daily ephemeris sequence number.
- setSupportedNames(String) - Method in class org.orekit.data.AbstractSelfFeedingLoader
-
Set the supported names regular expression.
- setSvAccuracy(double) - Method in class org.orekit.propagation.analytical.gnss.data.BeidouNavigationMessage
-
Setter for the user SV accuracy.
- setSvAccuracy(double) - Method in class org.orekit.propagation.analytical.gnss.data.GPSNavigationMessage
-
Setter for the user SV accuracy.
- setSvAccuracy(double) - Method in class org.orekit.propagation.analytical.gnss.data.QZSSNavigationMessage
-
Setter for the user SV accuracy.
- setSvHealth(double) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1042Data
-
Set the satellite health status.
- setSvHealth(double) - Method in class org.orekit.propagation.analytical.gnss.data.GalileoNavigationMessage
-
Setter for the SV health status.
- setSvHealth(double) - Method in class org.orekit.propagation.analytical.gnss.data.GPSNavigationMessage
-
Setter for the satellite health status.
- setSvHealth(double) - Method in class org.orekit.propagation.analytical.gnss.data.IRNSSNavigationMessage
-
Setter for the satellite health status.
- setSvHealth(double) - Method in class org.orekit.propagation.analytical.gnss.data.QZSSNavigationMessage
-
Setter for the satellite health status.
- setSVN(int) - Method in class org.orekit.propagation.analytical.gnss.data.GPSAlmanac
-
Sets the "SVN" reference number.
- setSystemId(String) - Method in class org.orekit.files.ilrs.CRDConfiguration.SystemConfiguration
-
Set the system configuration ID.
- setSystemIdentifier(int) - Method in class org.orekit.files.ilrs.CRDHeader
-
Set the system identifier.
- setSystemNumber(int) - Method in class org.orekit.files.ilrs.CRDHeader
-
Set the system number.
- setSystemOccupancy(int) - Method in class org.orekit.files.ilrs.CRDHeader
-
Set the system occupancy.
- setSystemRecord(CRDConfiguration.SystemConfiguration) - Method in class org.orekit.files.ilrs.CRDConfiguration
-
Set the system configuration record.
- setTaimutcT0(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
-
- setTargetClass(int) - Method in class org.orekit.files.ilrs.ILRSHeader
-
Set the target class.
- setTargetLocation(int) - Method in class org.orekit.files.ilrs.ILRSHeader
-
Set the target location.
- setTauC(double) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data
-
Set the GLONASS time scale correction to UTC time.
- setTauGps(double) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data
-
Set the correction to GPS time relative to GLONASS time.
- setTauN(double) - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSNavigationMessage
-
Setter for the SV clock bias.
- setTdmMessageLink(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
-
Set the Unique identifier of Tracking Data Message linked to this Orbit Data Message.
- setTechAddress(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
-
Set the address of Technical Point Of Contact at originator.
- setTechOrg(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
-
Set the creating agency or operator.
- setTechPhone(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
-
Set the phone number of Technical Point Of Contact at originator.
- setTechPOC(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
-
Set the Technical Point Of Contact at originator.
- setTechPosition(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
-
Set the position of Technical Point Of Contact at originator.
- setTemperature(double) - Method in class org.orekit.models.earth.EarthStandardAtmosphereRefraction
-
Set the local temperature at the evaluation location
- setTempSensorManufacturer(String) - Method in class org.orekit.files.ilrs.CRDConfiguration.MeteorologicalConfiguration
-
Set the temperature sensor manufacturer.
- setTempSensorModel(String) - Method in class org.orekit.files.ilrs.CRDConfiguration.MeteorologicalConfiguration
-
Set the temperature sensor model.
- setTempSensorSerialNumber(String) - Method in class org.orekit.files.ilrs.CRDConfiguration.MeteorologicalConfiguration
-
Set the temperature sensor serial number.
- setTGD(double) - Method in class org.orekit.propagation.analytical.gnss.data.GPSNavigationMessage
-
Setter for the Group Delay Differential (s).
- setTGD(double) - Method in class org.orekit.propagation.analytical.gnss.data.IRNSSNavigationMessage
-
Setter for the Group Delay Differential (s).
- setTGD(double) - Method in class org.orekit.propagation.analytical.gnss.data.QZSSNavigationMessage
-
Setter for the Group Delay Differential (s).
- setTGD1(double) - Method in class org.orekit.propagation.analytical.gnss.data.BeidouNavigationMessage
-
Setter for the B1/B3 Group Delay Differential (s).
- setTGD2(double) - Method in class org.orekit.propagation.analytical.gnss.data.BeidouNavigationMessage
-
Setter for the B2/B3 Group Delay Differential (s).
- setThrust(int, double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Maneuver
-
Set thrust component.
- setThrustDirectionSigma(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Maneuver
-
Set one σ angular off-nominal thrust direction.
- setThrustEfficiency(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Maneuver
-
Set thrust efficiency η.
- setThrustInterpolation(OnOff) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Maneuver
-
Set interpolation mode between current and next thrust line.
- setThrustIsp(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Maneuver
-
Set thrust specific impulse.
- setThrustMagnitudeSigma(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.Maneuver
-
Set one σ percent error on thrust magnitude.
- setTideSystem(TideSystem) - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
-
- setTime(double) - Method in class org.orekit.propagation.analytical.gnss.data.CommonGnssData
-
Setter for the reference time of the orbit as a duration from week start.
- setTime(double) - Method in class org.orekit.propagation.analytical.gnss.data.GLONASSNavigationMessage
-
Setter for the message frame time.
- setTime(double) - Method in class org.orekit.propagation.analytical.gnss.data.SBASNavigationMessage
-
Setter for the reference time of the SBAS orbit in GPS seconds of the week.
- setTimeout(int) - Method in class org.orekit.data.NetworkCrawler
-
Set the timeout for connection.
- setTimeout(int) - Method in class org.orekit.gnss.metric.ntrip.NtripClient
-
Set timeout for connections and reads.
- setTimer(String) - Method in class org.orekit.files.ilrs.CRDConfiguration.TimingSystemConfiguration
-
Set the timer name.
- setTimerSerialNumber(String) - Method in class org.orekit.files.ilrs.CRDConfiguration.TimingSystemConfiguration
-
Set the timer serial number.
- setTimeScale(TimeScale) - Method in class org.orekit.files.ilrs.CPF
-
Set the time scale.
- setTimeScale(TimeScale) - Method in class org.orekit.gnss.clock.RinexClock
-
Setter for the data time scale.
- setTimeSinceFirstObservation(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
-
Set time elapsed between first accepted observation on epoch.
- setTimeSinceLastObservation(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
-
Set time elapsed between last accepted observation on epoch.
- setTimeSource(String) - Method in class org.orekit.files.ilrs.CRDConfiguration.TimingSystemConfiguration
-
Set the time source.
- setTimeSpan(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
-
Set the span of time in seconds that the OCM covers.
- setTimeSystem(TimeSystem) - Method in class org.orekit.files.ccsds.section.Metadata
-
Set the Time System that: for OPM, is used for metadata, state vector,
maneuver and covariance data, for OMM, is used for metadata, orbit state
and covariance data, for OEM, is used for metadata, ephemeris and
covariance data.
- setTimeSystem(TimeSystem) - Method in class org.orekit.files.sp3.SP3
-
Set the time system used in this SP3 file.
- setTimeSystem(TimeSystem) - Method in class org.orekit.gnss.clock.RinexClock
-
Setter for the file time system.
- setTimetagRef(TimetagReference) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
-
Setter for the timetagRef.
- setTimingRecord(CRDConfiguration.TimingSystemConfiguration) - Method in class org.orekit.files.ilrs.CRDConfiguration
-
Set the timing system configuration record.
- setTk(double) - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data
-
Set the time referenced to the beginning of the frame within the current day.
- setTorque(int, double) - Method in class org.orekit.files.ccsds.ndm.adm.apm.Maneuver
-
Set the torque vector (N.m).
- setTrackId(String) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
-
Setter for the tracking data identifier.
- setTrackingSoftwares(String[]) - Method in class org.orekit.files.ilrs.CRDConfiguration.SoftwareConfiguration
-
Set the tracking softwares.
- setTrackingSoftwareVersions(String[]) - Method in class org.orekit.files.ilrs.CRDConfiguration.SoftwareConfiguration
-
Set the tracking software versions.
- setTracksAvailable(int) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
-
Set number of sensors tracks available for the OD within the actual OD span.
- setTracksUsed(int) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
-
Set number of sensors tracks accepted for the OD within the actual OD span.
- setTrajBasis(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata
-
Set basis of this trajectory state time history data.
- setTrajBasisID(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata
-
Set identification number of the orbit determination or simulation upon which this trajectory is based.
- setTrajFrameEpoch(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata
-
- setTrajID(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata
-
Set trajectory identification number.
- setTrajNextID(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata
-
Set identification number of next trajectory.
- setTrajPrevID(String) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata
-
Set identification number of previous trajectory.
- setTrajReferenceFrame(FrameFacade) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata
-
Set reference frame of the trajectory.
- setTrajType(ElementsType) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata
-
Set trajectory element set type.
- setTrajUnits(List<Unit>) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata
-
Set trajectory element set units.
- setTransmissionOfSpectralFilter(double) - Method in class org.orekit.files.ilrs.CRDConfiguration.DetectorConfiguration
-
Set the percentage of transmission of spectral filter.
- setTransmitBand(String) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
-
Setter for the transmitBand.
- setTransmitDelays(Map<Integer, Double>) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
-
Setter for the transmitDelays.
- setTranspClkRef(double) - Method in class org.orekit.files.ilrs.CPFHeader
-
Set the transponder Clock Reference Time.
- setTranspClkRefTime(double) - Method in class org.orekit.files.ilrs.CRDConfiguration.TransponderConfiguration
-
Set the transponder clock reference time.
- setTransponderId(String) - Method in class org.orekit.files.ilrs.CRDConfiguration.TransponderConfiguration
-
Set the transponder configuration ID.
- setTransponderRecord(CRDConfiguration.TransponderConfiguration) - Method in class org.orekit.files.ilrs.CRDConfiguration
-
Set the transponder configuration record.
- setTranspOscDrift(double) - Method in class org.orekit.files.ilrs.CPFHeader
-
Set the transponder Oscillator Drift in parts.
- setTranspOscDrift(double) - Method in class org.orekit.files.ilrs.CRDConfiguration.TransponderConfiguration
-
Set the estimated transponder oscillator drift in parts in 10¹⁵.
- setTranspTransmitDelay(double) - Method in class org.orekit.files.ilrs.CPFHeader
-
Set the transponder transmit delay.
- setTranspUtcOffset(double) - Method in class org.orekit.files.ilrs.CPFHeader
-
Set the transponder UTC offset.
- setTranspUTCOffset(double) - Method in class org.orekit.files.ilrs.CRDConfiguration.TransponderConfiguration
-
Set the estimated transponder UTC offset.
- setTurnaroundDenominator(int) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
-
Setter for the turnaroundDenominator.
- setTurnaroundNumerator(int) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
-
Setter for the turnaroundNumerator.
- setTypAreaForCollisionProbability(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
-
Get the typical (50th percentile) cross-sectional area for collision probability estimation purposes.
- setType(SP3.SP3FileType) - Method in class org.orekit.files.sp3.SP3
-
Set the file type for this SP3 file.
- setUpEventDetector(ODEIntegrator, EventDetector) - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
-
Wrap an Orekit event detector and register it to the integrator.
- setUpEventDetector(FieldODEIntegrator<T>, FieldEventDetector<T>) - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator
-
Wrap an Orekit event detector and register it to the integrator.
- setupMatricesComputation(String, RealMatrix, DoubleArrayDictionary) - Method in class org.orekit.propagation.AbstractPropagator
-
Set up computation of State Transition Matrix and Jacobians matrix with respect to parameters.
- setupMatricesComputation(String, RealMatrix, DoubleArrayDictionary) - Method in interface org.orekit.propagation.Propagator
-
Set up computation of State Transition Matrix and Jacobians matrix with respect to parameters.
- setUpStmAndJacobianGenerators() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
-
Set up State Transition Matrix and Jacobian matrix handling.
- setUpStmAndJacobianGenerators() - Method in class org.orekit.propagation.numerical.NumericalPropagator
-
Set up State Transition Matrix and Jacobian matrix handling.
- setUpStmAndJacobianGenerators() - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator
-
Set up State Transition Matrix and Jacobian matrix handling.
- setUpUserEventDetectors() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
-
Set up all user defined event detectors.
- setUpUserEventDetectors() - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator
-
Set up all user defined event detectors.
- setURA(int) - Method in class org.orekit.propagation.analytical.gnss.data.GPSAlmanac
-
Sets the average URA number.
- setURA(double) - Method in class org.orekit.propagation.analytical.gnss.data.IRNSSNavigationMessage
-
Setter for the user range accuracy.
- setURA(double) - Method in class org.orekit.propagation.analytical.gnss.data.SBASNavigationMessage
-
Setter for the user range accuracy.
- setUseableStartTime(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemMetadata
-
Set start of useable time span covered by attitude data.
- setUseableStartTime(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata
-
Set start of useable time span covered by ephemerides data, it may be
necessary to allow for proper interpolation.
- setUseableStartTime(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemMetadata
-
Set start of useable time span covered by ephemerides data, it may be
necessary to allow for proper interpolation.
- setUseableStopTime(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemMetadata
-
Set end of useable time span covered by ephemerides data.
- setUseableStopTime(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata
-
Set end of useable time span covered by ephemerides data, it may be
necessary to allow for proper interpolation.
- setUseableStopTime(AbsoluteDate) - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemMetadata
-
Set end of useable time span covered by ephemerides data, it may be
necessary to allow for proper interpolation.
- setUt1mutcT0(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
-
- setV(int, double) - Method in class org.orekit.files.ccsds.ndm.odm.StateVector
-
Set velocity component.
- setValidFrom(AbsoluteDate) - Method in class org.orekit.files.sinex.Station
-
Set the start of validity.
- setValidUntil(AbsoluteDate) - Method in class org.orekit.files.sinex.Station
-
Set the end of validity.
- setValue(double) - Method in class org.orekit.utils.ParameterDriver
-
Set parameter value.
- setVelocity(Vector3D) - Method in class org.orekit.files.sinex.Station
-
Set the station velocity.
- setVersion(int) - Method in class org.orekit.files.ilrs.ILRSHeader
-
Set the format version.
- setVmAbsolute(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
-
Set the typical (50th percentile) visual magnitude.
- setVmApparent(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
-
Set the typical (50th percentile) apparent visual magnitude.
- setVmApparentMax(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
-
Set the maximum apparent visual magnitude.
- setVmApparentMin(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
-
Set the minimum apparent visual magnitude.
- setVtecQualityIndicator(double) - Method in class org.orekit.gnss.metric.messages.ssr.subtype.SsrIm201Header
-
Set the VTEC quality indicator.
- setWavelength(double) - Method in class org.orekit.files.ilrs.CRDConfiguration.SystemConfiguration
-
Set the transmit wavelength.
- setWeek(int) - Method in class org.orekit.propagation.analytical.gnss.data.CommonGnssData
-
Setter for the reference week of the orbit.
- setWeightedRms(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OrbitDetermination
-
Set weighted RMS residual ratio.
- setWetMass(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.PhysicalProperties
-
Set the total mass at T₀.
- setX(double) - Method in class org.orekit.propagation.analytical.gnss.data.AbstractEphemerisMessage
-
Setter for the satellite X position.
- setXDot(double) - Method in class org.orekit.propagation.analytical.gnss.data.AbstractEphemerisMessage
-
Setter for the satellite X velocity.
- setXDotDot(double) - Method in class org.orekit.propagation.analytical.gnss.data.AbstractEphemerisMessage
-
Setter for the satellite X acceleration.
- setY(double) - Method in class org.orekit.propagation.analytical.gnss.data.AbstractEphemerisMessage
-
Setter for the satellite Y position.
- setYawAngle(double) - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm06Data
-
Set the yaw angle used for computation of phase wind-up correction.
- setYawRate(double) - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm06Data
-
Set the yaw rate.
- setYDot(double) - Method in class org.orekit.propagation.analytical.gnss.data.AbstractEphemerisMessage
-
Setter for the satellite Y velocity.
- setYDotDot(double) - Method in class org.orekit.propagation.analytical.gnss.data.AbstractEphemerisMessage
-
Setter for the satellite Y acceleration.
- setYearOfCentury(int) - Method in class org.orekit.files.ilrs.CRDHeader
-
Set the year of century from CPF or TLE.
- setZ(double) - Method in class org.orekit.propagation.analytical.gnss.data.AbstractEphemerisMessage
-
Setter for the satellite Z position.
- setZDot(double) - Method in class org.orekit.propagation.analytical.gnss.data.AbstractEphemerisMessage
-
Setter for the satellite Z velocity.
- setZDotDot(double) - Method in class org.orekit.propagation.analytical.gnss.data.AbstractEphemerisMessage
-
Setter for the satellite Z acceleration.
- SGP - Static variable in class org.orekit.propagation.analytical.tle.FieldTLE
-
Identifier for SGP type of ephemeris.
- SGP - Static variable in class org.orekit.propagation.analytical.tle.TLE
-
Identifier for SGP type of ephemeris.
- SGP4 - Static variable in class org.orekit.propagation.analytical.tle.FieldTLE
-
Identifier for SGP4 type of ephemeris.
- SGP4 - Class in org.orekit.propagation.analytical.tle
-
This class contains methods to compute propagated coordinates with the SGP4 model.
- SGP4(TLE, AttitudeProvider, double) - Constructor for class org.orekit.propagation.analytical.tle.SGP4
-
Constructor for a unique initial TLE.
- SGP4(TLE, AttitudeProvider, double, Frame) - Constructor for class org.orekit.propagation.analytical.tle.SGP4
-
Constructor for a unique initial TLE.
- SGP4 - Static variable in class org.orekit.propagation.analytical.tle.TLE
-
Identifier for SGP4 type of ephemeris.
- SGP8 - Static variable in class org.orekit.propagation.analytical.tle.FieldTLE
-
Identifier for SGP8 type of ephemeris.
- SGP8 - Static variable in class org.orekit.propagation.analytical.tle.TLE
-
Identifier for SGP8 type of ephemeris.
- SGP_SGP4_THEORY - Static variable in class org.orekit.files.ccsds.ndm.odm.omm.OmmMetadata
-
Constant for SGP/SGP4 mean elements theory.
- ShadowModel - Enum in org.orekit.files.ccsds.ndm.odm.ocm
-
Shadow model for solar radiation pressure.
- shapiroCorrection(TimeStampedPVCoordinates, TimeStampedPVCoordinates) - Method in class org.orekit.estimation.measurements.modifiers.AbstractShapiroBaseModifier
-
Compute Shapiro path dilation between two points in a gravity field.
- ShapiroInterSatellitePhaseModifier - Class in org.orekit.estimation.measurements.modifiers
-
Class modifying theoretical inter-satellites phase measurement with Shapiro time delay.
- ShapiroInterSatellitePhaseModifier(double) - Constructor for class org.orekit.estimation.measurements.modifiers.ShapiroInterSatellitePhaseModifier
-
Simple constructor.
- ShapiroInterSatelliteRangeModifier - Class in org.orekit.estimation.measurements.modifiers
-
Class modifying theoretical range measurement with Shapiro time delay.
- ShapiroInterSatelliteRangeModifier(double) - Constructor for class org.orekit.estimation.measurements.modifiers.ShapiroInterSatelliteRangeModifier
-
Simple constructor.
- ShapiroOneWayGNSSPhaseModifier - Class in org.orekit.estimation.measurements.modifiers
-
Class modifying theoretical one-way GNSS phase measurement with Shapiro time delay.
- ShapiroOneWayGNSSPhaseModifier(double) - Constructor for class org.orekit.estimation.measurements.modifiers.ShapiroOneWayGNSSPhaseModifier
-
Simple constructor.
- ShapiroOneWayGNSSRangeModifier - Class in org.orekit.estimation.measurements.modifiers
-
Class modifying theoretical range measurement with Shapiro time delay.
- ShapiroOneWayGNSSRangeModifier(double) - Constructor for class org.orekit.estimation.measurements.modifiers.ShapiroOneWayGNSSRangeModifier
-
Simple constructor.
- ShapiroPhaseModifier - Class in org.orekit.estimation.measurements.modifiers
-
Class modifying theoretical phase measurement with Shapiro time delay.
- ShapiroPhaseModifier(double) - Constructor for class org.orekit.estimation.measurements.modifiers.ShapiroPhaseModifier
-
Simple constructor.
- ShapiroRangeModifier - Class in org.orekit.estimation.measurements.modifiers
-
Class modifying theoretical range measurement with Shapiro time delay.
- ShapiroRangeModifier(double) - Constructor for class org.orekit.estimation.measurements.modifiers.ShapiroRangeModifier
-
Simple constructor.
- shiftedBy(double) - Method in class org.orekit.attitudes.Attitude
-
Get a time-shifted attitude.
- shiftedBy(double) - Method in class org.orekit.attitudes.FieldAttitude
-
Get a time-shifted attitude.
- shiftedBy(T) - Method in class org.orekit.attitudes.FieldAttitude
-
Get a time-shifted attitude.
- shiftedBy(double) - Method in class org.orekit.frames.FieldTransform
-
Get a time-shifted instance.
- shiftedBy(T) - Method in class org.orekit.frames.FieldTransform
-
Get a time-shifted instance.
- shiftedBy(double) - Method in class org.orekit.frames.Transform
-
Get a time-shifted instance.
- shiftedBy(double) - Method in class org.orekit.orbits.CartesianOrbit
-
Get a time-shifted orbit.
- shiftedBy(double) - Method in class org.orekit.orbits.CircularOrbit
-
Get a time-shifted orbit.
- shiftedBy(double) - Method in class org.orekit.orbits.EquinoctialOrbit
-
Get a time-shifted orbit.
- shiftedBy(double) - Method in class org.orekit.orbits.FieldCartesianOrbit
-
Get a time-shifted instance.
- shiftedBy(T) - Method in class org.orekit.orbits.FieldCartesianOrbit
-
Get a time-shifted orbit.
- shiftedBy(double) - Method in class org.orekit.orbits.FieldCircularOrbit
-
Get a time-shifted instance.
- shiftedBy(T) - Method in class org.orekit.orbits.FieldCircularOrbit
-
Get a time-shifted orbit.
- shiftedBy(double) - Method in class org.orekit.orbits.FieldEquinoctialOrbit
-
Get a time-shifted instance.
- shiftedBy(T) - Method in class org.orekit.orbits.FieldEquinoctialOrbit
-
Get a time-shifted orbit.
- shiftedBy(double) - Method in class org.orekit.orbits.FieldKeplerianOrbit
-
Get a time-shifted instance.
- shiftedBy(T) - Method in class org.orekit.orbits.FieldKeplerianOrbit
-
Get a time-shifted orbit.
- shiftedBy(T) - Method in class org.orekit.orbits.FieldOrbit
-
Get a time-shifted orbit.
- shiftedBy(double) - Method in class org.orekit.orbits.KeplerianOrbit
-
Get a time-shifted orbit.
- shiftedBy(double) - Method in class org.orekit.orbits.Orbit
-
Get a time-shifted orbit.
- shiftedBy(double) - Method in class org.orekit.propagation.FieldSpacecraftState
-
Get a time-shifted state.
- shiftedBy(T) - Method in class org.orekit.propagation.FieldSpacecraftState
-
Get a time-shifted state.
- shiftedBy(double) - Method in class org.orekit.propagation.SpacecraftState
-
Get a time-shifted state.
- shiftedBy(double) - Method in class org.orekit.time.AbsoluteDate
-
Get a time-shifted date.
- shiftedBy(T) - Method in class org.orekit.time.FieldAbsoluteDate
-
Get a time-shifted date.
- shiftedBy(double) - Method in class org.orekit.time.FieldAbsoluteDate
-
Get a time-shifted date.
- shiftedBy(double) - Method in interface org.orekit.time.FieldTimeShiftable
-
Get a time-shifted instance.
- shiftedBy(KK) - Method in interface org.orekit.time.FieldTimeShiftable
-
Get a time-shifted instance.
- shiftedBy(double) - Method in interface org.orekit.time.TimeShiftable
-
Get a time-shifted instance.
- shiftedBy(double) - Method in class org.orekit.utils.AbsolutePVCoordinates
-
Get a time-shifted state.
- shiftedBy(double) - Method in class org.orekit.utils.AngularCoordinates
-
Get a time-shifted state.
- shiftedBy(T) - Method in class org.orekit.utils.FieldAbsolutePVCoordinates
-
Get a time-shifted state.
- shiftedBy(double) - Method in class org.orekit.utils.FieldAbsolutePVCoordinates
-
Get a time-shifted state.
- shiftedBy(double) - Method in class org.orekit.utils.FieldAngularCoordinates
-
Get a time-shifted state.
- shiftedBy(T) - Method in class org.orekit.utils.FieldAngularCoordinates
-
Get a time-shifted state.
- shiftedBy(double) - Method in class org.orekit.utils.FieldPVCoordinates
-
Get a time-shifted state.
- shiftedBy(T) - Method in class org.orekit.utils.FieldPVCoordinates
-
Get a time-shifted state.
- shiftedBy(double) - Method in class org.orekit.utils.PVCoordinates
-
Get a time-shifted state.
- shiftedBy(double) - Method in class org.orekit.utils.TimeStampedAngularCoordinates
-
Get a time-shifted state.
- shiftedBy(double) - Method in class org.orekit.utils.TimeStampedFieldAngularCoordinates
-
Get a time-shifted state.
- shiftedBy(T) - Method in class org.orekit.utils.TimeStampedFieldAngularCoordinates
-
Get a time-shifted state.
- shiftedBy(double) - Method in class org.orekit.utils.TimeStampedFieldPVCoordinates
-
Get a time-shifted state.
- shiftedBy(T) - Method in class org.orekit.utils.TimeStampedFieldPVCoordinates
-
Get a time-shifted state.
- shiftedBy(double) - Method in class org.orekit.utils.TimeStampedPVCoordinates
-
Get a time-shifted state.
- ShiftingTransformProvider - Class in org.orekit.frames
-
Transform provider using thread-safe shifts on transforms sample.
- ShiftingTransformProvider(TransformProvider, CartesianDerivativesFilter, AngularDerivativesFilter, int, double, int, double, double) - Constructor for class org.orekit.frames.ShiftingTransformProvider
-
Simple constructor.
- SHM_FILENAME - Static variable in class org.orekit.forces.gravity.potential.GravityFieldFactory
-
Default regular expression for SHM files.
- SHMFormatReader - Class in org.orekit.forces.gravity.potential
-
Reader for the SHM gravity field format.
- SHMFormatReader(String, boolean) - Constructor for class org.orekit.forces.gravity.potential.SHMFormatReader
-
Simple constructor.
- SHMFormatReader(String, boolean, TimeScale) - Constructor for class org.orekit.forces.gravity.potential.SHMFormatReader
-
Simple constructor.
- SHORT_PERIOD_PREFIX - Static variable in class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseral
-
Name of the prefix for short period coefficients keys.
- SHORT_PERIOD_PREFIX - Static variable in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBody
-
Name of the prefix for short period coefficients keys.
- SHORT_PERIOD_PREFIX - Static variable in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonal
-
Name of the prefix for short period coefficients keys.
- ShortPeriodicsInterpolatedCoefficient - Class in org.orekit.propagation.semianalytical.dsst.utilities
-
Interpolated short periodics coefficients.
- ShortPeriodicsInterpolatedCoefficient(int) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.ShortPeriodicsInterpolatedCoefficient
-
Simple constructor.
- ShortPeriodTerms - Interface in org.orekit.propagation.semianalytical.dsst.forces
-
Additive short period terms contributing to the mean to osculating orbit mapping.
- sign(double) - Method in class org.orekit.estimation.measurements.gnss.ModifiedLambdaMethod
-
Return the symbol of parameter a.
- SignalCode - Enum in org.orekit.gnss
-
Enumerate for satellite signal code.
- SignalInSpaceAccuracy - Class in org.orekit.gnss.metric.messages.rtcm.ephemeris.utils
-
Signal-In-Space Accuracy (SISA).
- SignalInSpaceAccuracy(int) - Constructor for class org.orekit.gnss.metric.messages.rtcm.ephemeris.utils.SignalInSpaceAccuracy
-
Simple constructor.
- signalTimeOfFlight(TimeStampedPVCoordinates, Vector3D, AbsoluteDate) - Static method in class org.orekit.estimation.measurements.AbstractMeasurement
-
Compute propagation delay on a link leg (typically downlink or uplink).
- signalTimeOfFlight(TimeStampedFieldPVCoordinates<T>, FieldVector3D<T>, FieldAbsoluteDate<T>) - Static method in class org.orekit.estimation.measurements.AbstractMeasurement
-
Compute propagation delay on a link leg (typically downlink or uplink).
- signedAmplitude(SpacecraftState, double[]) - Method in interface org.orekit.forces.empirical.AccelerationModel
-
Compute the signed amplitude of the acceleration.
- signedAmplitude(FieldSpacecraftState<T>, T[]) - Method in interface org.orekit.forces.empirical.AccelerationModel
-
Compute the signed amplitude of the acceleration.
- signedAmplitude(SpacecraftState, double[]) - Method in class org.orekit.forces.empirical.HarmonicAccelerationModel
-
Compute the signed amplitude of the acceleration.
- signedAmplitude(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.empirical.HarmonicAccelerationModel
-
Compute the signed amplitude of the acceleration.
- signedAmplitude(SpacecraftState, double[]) - Method in class org.orekit.forces.empirical.PolynomialAccelerationModel
-
Compute the signed amplitude of the acceleration.
- signedAmplitude(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.empirical.PolynomialAccelerationModel
-
Compute the signed amplitude of the acceleration.
- SignSemantic - Enum in org.orekit.estimation.measurements.generation
-
Enumerate for the semantic of the g
function sign during measurements generation.
- SimpleExponentialAtmosphere - Class in org.orekit.models.earth.atmosphere
-
Simple exponential atmospheric model.
- SimpleExponentialAtmosphere(BodyShape, double, double, double) - Constructor for class org.orekit.models.earth.atmosphere.SimpleExponentialAtmosphere
-
Create an exponential atmosphere.
- SimpleRatioAmbiguityAcceptance - Class in org.orekit.estimation.measurements.gnss
-
Ambiguity acceptance test based on a ratio of the two best candidates.
- SimpleRatioAmbiguityAcceptance(double) - Constructor for class org.orekit.estimation.measurements.gnss.SimpleRatioAmbiguityAcceptance
-
Simple constructor.
- SimpleTimeStampedTableParser<T extends TimeStamped> - Class in org.orekit.data
-
- SimpleTimeStampedTableParser(int, SimpleTimeStampedTableParser.RowConverter<T>) - Constructor for class org.orekit.data.SimpleTimeStampedTableParser
-
Simple constructor.
- SimpleTimeStampedTableParser.RowConverter<S extends TimeStamped> - Interface in org.orekit.data
-
Interface for converting a table row into time-stamped data.
- SinexLoader - Class in org.orekit.files.sinex
-
Loader for Solution INdependent EXchange (SINEX) files.
- SinexLoader(String) - Constructor for class org.orekit.files.sinex.SinexLoader
-
Simple constructor.
- SinexLoader(String, DataProvidersManager, TimeScale) - Constructor for class org.orekit.files.sinex.SinexLoader
-
Construct a loader by specifying the source of SINEX auxiliary data files.
- SinexLoader(DataSource) - Constructor for class org.orekit.files.sinex.SinexLoader
-
Simple constructor.
- SinexLoader(DataSource, TimeScale) - Constructor for class org.orekit.files.sinex.SinexLoader
-
Loads SINEX from the given input stream using the specified auxiliary data.
- SingleBodyAbsoluteAttraction - Class in org.orekit.forces.gravity
-
Body attraction force model computed as absolute acceleration towards a body.
- SingleBodyAbsoluteAttraction(CelestialBody) - Constructor for class org.orekit.forces.gravity.SingleBodyAbsoluteAttraction
-
Simple constructor.
- SingleBodyRelativeAttraction - Class in org.orekit.forces.gravity
-
Body attraction force model computed as relative acceleration towards frame center.
- SingleBodyRelativeAttraction(CelestialBody) - Constructor for class org.orekit.forces.gravity.SingleBodyRelativeAttraction
-
Simple constructor.
- SingleLayerModelMappingFunction - Class in org.orekit.models.earth.ionosphere
-
Single Layer Model (SLM) ionospheric mapping function.
- SingleLayerModelMappingFunction() - Constructor for class org.orekit.models.earth.ionosphere.SingleLayerModelMappingFunction
-
Constructor with default value.
- SingleLayerModelMappingFunction(double) - Constructor for class org.orekit.models.earth.ionosphere.SingleLayerModelMappingFunction
-
Constructor.
- sini0 - Variable in class org.orekit.propagation.analytical.tle.FieldTLEPropagator
-
sinus original inclination.
- sini0 - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator
-
sinus original inclination.
- siToCcsdsName(String) - Method in class org.orekit.files.ccsds.utils.generation.AbstractGenerator
-
Convert a SI unit name to a CCSDS name.
- siToCcsdsName(String) - Method in interface org.orekit.files.ccsds.utils.generation.Generator
-
Convert a SI unit name to a CCSDS name.
- siToRaw(RangeUnitsConverter, TdmMetadata, AbsoluteDate, double) - Method in enum org.orekit.files.ccsds.ndm.tdm.ObservationType
-
Convert a measurement from SI units.
- size() - Method in class org.orekit.utils.DoubleArrayDictionary.Entry
-
Get the size of the value array.
- size() - Method in class org.orekit.utils.DoubleArrayDictionary
-
Get the number of dictionary entries.
- size() - Method in class org.orekit.utils.FieldArrayDictionary.Entry
-
Get the size of the value array.
- size() - Method in class org.orekit.utils.FieldArrayDictionary
-
Get the number of dictionary entries.
- SM_COEFFICIENTS - Static variable in class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseral
-
Identifier for sMm coefficients.
- SmallManeuverAnalyticalModel - Class in org.orekit.forces.maneuvers
-
Analytical model for small maneuvers.
- SmallManeuverAnalyticalModel(SpacecraftState, Vector3D, double) - Constructor for class org.orekit.forces.maneuvers.SmallManeuverAnalyticalModel
-
Build a maneuver defined in spacecraft frame.
- SmallManeuverAnalyticalModel(SpacecraftState, Frame, Vector3D, double) - Constructor for class org.orekit.forces.maneuvers.SmallManeuverAnalyticalModel
-
Build a maneuver defined in user-specified frame.
- SmoothFieldOfView - Class in org.orekit.geometry.fov
-
Class representing a spacecraft sensor Field Of View with shape defined by a smooth single loop.
- SmoothFieldOfView(Vector3D, Vector3D, double) - Constructor for class org.orekit.geometry.fov.SmoothFieldOfView
-
Build a new instance.
- SoftwareConfiguration() - Constructor for class org.orekit.files.ilrs.CRDConfiguration.SoftwareConfiguration
-
- SOLAR_FLUX_UNIT - Static variable in class org.orekit.utils.units.Unit
-
Solar Flux Unit.
- SOLAR_SYSTEM_BARYCENTER - Static variable in class org.orekit.bodies.CelestialBodyFactory
-
Predefined name for solar system barycenter.
- SolarRadiationPressure - Class in org.orekit.forces.radiation
-
Solar radiation pressure force model.
- SolarRadiationPressure(ExtendedPVCoordinatesProvider, double, RadiationSensitive) - Constructor for class org.orekit.forces.radiation.SolarRadiationPressure
-
Simple constructor with default reference values.
- SolarRadiationPressure(double, double, ExtendedPVCoordinatesProvider, double, RadiationSensitive) - Constructor for class org.orekit.forces.radiation.SolarRadiationPressure
-
Complete constructor.
- SolidTides - Class in org.orekit.forces.gravity
-
Solid tides force model.
- SolidTides(Frame, double, double, TideSystem, IERSConventions, UT1Scale, CelestialBody...) - Constructor for class org.orekit.forces.gravity.SolidTides
-
Simple constructor.
- SolidTides(Frame, double, double, TideSystem, boolean, double, int, IERSConventions, UT1Scale, CelestialBody...) - Constructor for class org.orekit.forces.gravity.SolidTides
-
Simple constructor.
- solveILS(int, double[], int[], RealMatrix) - Method in class org.orekit.estimation.measurements.gnss.AbstractLambdaMethod
-
Find the best solutions to an Integer Least Square problem.
- solveILS(int, double[], int[], RealMatrix) - Method in interface org.orekit.estimation.measurements.gnss.IntegerLeastSquareSolver
-
Find the best solutions to an Integer Least Square problem.
- sort() - Method in class org.orekit.utils.ParameterDriversList
-
Sort the parameters lexicographically.
- SourceTable - Class in org.orekit.gnss.metric.ntrip
-
Source table for ntrip streams retrieval.
- SOUTH_POLE - Static variable in class org.orekit.bodies.GeodeticPoint
-
South pole.
- SP3 - Class in org.orekit.files.sp3
-
Represents a parsed SP3 orbit file.
- SP3(double, int, Function<? super String, ? extends Frame>) - Constructor for class org.orekit.files.sp3.SP3
-
Create a new SP3 file object.
- SP3.SP3Coordinate - Class in org.orekit.files.sp3
-
A single record of position clock and possibly derivatives in an SP3 file.
- SP3.SP3Ephemeris - Class in org.orekit.files.sp3
-
An ephemeris for a single satellite in a SP3 file.
- SP3.SP3FileType - Enum in org.orekit.files.sp3
-
File type indicator.
- SP3.SP3OrbitType - Enum in org.orekit.files.sp3
-
Orbit type indicator.
- SP3_FRAME_CENTER_STRING - Static variable in class org.orekit.files.sp3.SP3
-
String representation of the center of ephemeris coordinate system.
- SP3Coordinate(AbsoluteDate, Vector3D, double) - Constructor for class org.orekit.files.sp3.SP3.SP3Coordinate
-
Create a coordinate with only position.
- SP3Coordinate(AbsoluteDate, Vector3D, Vector3D, double, double) - Constructor for class org.orekit.files.sp3.SP3.SP3Coordinate
-
Create a coordinate with position and velocity.
- SP3Ephemeris(String) - Constructor for class org.orekit.files.sp3.SP3.SP3Ephemeris
-
Create an ephemeris for a single satellite.
- SP3Parser - Class in org.orekit.files.sp3
-
A parser for the SP3 orbit file format.
- SP3Parser() - Constructor for class org.orekit.files.sp3.SP3Parser
-
Create an SP3 parser using default values.
- SP3Parser(double, int, Function<? super String, ? extends Frame>) - Constructor for class org.orekit.files.sp3.SP3Parser
-
Create an SP3 parser and specify the extra information needed to create a
Propagator
from the ephemeris data.
- SP3Parser(double, int, Function<? super String, ? extends Frame>, TimeScales) - Constructor for class org.orekit.files.sp3.SP3Parser
-
Create an SP3 parser and specify the extra information needed to create a
Propagator
from the ephemeris data.
- SpacecraftBodyFrame - Class in org.orekit.files.ccsds.definitions
-
Frames used in CCSDS Attitude Data Messages for the spacecraft body.
- SpacecraftBodyFrame(SpacecraftBodyFrame.BaseEquipment, String) - Constructor for class org.orekit.files.ccsds.definitions.SpacecraftBodyFrame
-
Simple constructor.
- SpacecraftBodyFrame.BaseEquipment - Enum in org.orekit.files.ccsds.definitions
-
Equipment on which the frame is located.
- SpacecraftParameters - Class in org.orekit.files.ccsds.ndm.adm.apm
-
Container for spacecraft parameters data.
- SpacecraftParameters() - Constructor for class org.orekit.files.ccsds.ndm.adm.apm.SpacecraftParameters
-
Simple constructor.
- SpacecraftParameters - Class in org.orekit.files.ccsds.ndm.odm
-
Container for spacecraft parameters.
- SpacecraftParameters() - Constructor for class org.orekit.files.ccsds.ndm.odm.SpacecraftParameters
-
Create an empty state data set.
- SpacecraftParametersKey - Enum in org.orekit.files.ccsds.ndm.adm.apm
-
- SpacecraftParametersKey - Enum in org.orekit.files.ccsds.ndm.odm
-
- SpacecraftParametersWriter - Class in org.orekit.files.ccsds.ndm.odm
-
Writer for spacecraft parameters data.
- SpacecraftParametersWriter(String, String, SpacecraftParameters) - Constructor for class org.orekit.files.ccsds.ndm.odm.SpacecraftParametersWriter
-
Create a writer.
- SpacecraftState - Class in org.orekit.propagation
-
This class is the representation of a complete state holding orbit, attitude
and mass information at a given date.
- SpacecraftState(Orbit) - Constructor for class org.orekit.propagation.SpacecraftState
-
Build a spacecraft state from orbit only.
- SpacecraftState(Orbit, Attitude) - Constructor for class org.orekit.propagation.SpacecraftState
-
Build a spacecraft state from orbit and attitude.
- SpacecraftState(Orbit, double) - Constructor for class org.orekit.propagation.SpacecraftState
-
Create a new instance from orbit and mass.
- SpacecraftState(Orbit, Attitude, double) - Constructor for class org.orekit.propagation.SpacecraftState
-
Build a spacecraft state from orbit, attitude and mass.
- SpacecraftState(Orbit, Map<String, double[]>) - Constructor for class org.orekit.propagation.SpacecraftState
-
- SpacecraftState(Orbit, DoubleArrayDictionary) - Constructor for class org.orekit.propagation.SpacecraftState
-
Build a spacecraft state from orbit and additional states.
- SpacecraftState(Orbit, Attitude, Map<String, double[]>) - Constructor for class org.orekit.propagation.SpacecraftState
-
- SpacecraftState(Orbit, Attitude, DoubleArrayDictionary) - Constructor for class org.orekit.propagation.SpacecraftState
-
Build a spacecraft state from orbit, attitude and additional states.
- SpacecraftState(Orbit, double, Map<String, double[]>) - Constructor for class org.orekit.propagation.SpacecraftState
-
- SpacecraftState(Orbit, double, DoubleArrayDictionary) - Constructor for class org.orekit.propagation.SpacecraftState
-
Create a new instance from orbit, mass and additional states.
- SpacecraftState(Orbit, Attitude, double, Map<String, double[]>) - Constructor for class org.orekit.propagation.SpacecraftState
-
- SpacecraftState(Orbit, Attitude, double, DoubleArrayDictionary) - Constructor for class org.orekit.propagation.SpacecraftState
-
Build a spacecraft state from orbit, attitude, mass and additional states.
- SpacecraftState(Orbit, Attitude, double, DoubleArrayDictionary, DoubleArrayDictionary) - Constructor for class org.orekit.propagation.SpacecraftState
-
Build a spacecraft state from orbit, attitude, mass, additional states and derivatives.
- SpacecraftState(AbsolutePVCoordinates) - Constructor for class org.orekit.propagation.SpacecraftState
-
Build a spacecraft state from position-velocity-acceleration only.
- SpacecraftState(AbsolutePVCoordinates, Attitude) - Constructor for class org.orekit.propagation.SpacecraftState
-
Build a spacecraft state from position-velocity-acceleration and attitude.
- SpacecraftState(AbsolutePVCoordinates, double) - Constructor for class org.orekit.propagation.SpacecraftState
-
Create a new instance from position-velocity-acceleration and mass.
- SpacecraftState(AbsolutePVCoordinates, Attitude, double) - Constructor for class org.orekit.propagation.SpacecraftState
-
Build a spacecraft state from position-velocity-acceleration, attitude and mass.
- SpacecraftState(AbsolutePVCoordinates, Map<String, double[]>) - Constructor for class org.orekit.propagation.SpacecraftState
-
- SpacecraftState(AbsolutePVCoordinates, DoubleArrayDictionary) - Constructor for class org.orekit.propagation.SpacecraftState
-
Build a spacecraft state from position-velocity-acceleration and additional states.
- SpacecraftState(AbsolutePVCoordinates, Attitude, Map<String, double[]>) - Constructor for class org.orekit.propagation.SpacecraftState
-
- SpacecraftState(AbsolutePVCoordinates, Attitude, DoubleArrayDictionary) - Constructor for class org.orekit.propagation.SpacecraftState
-
Build a spacecraft state from position-velocity-acceleration, attitude and additional states.
- SpacecraftState(AbsolutePVCoordinates, double, Map<String, double[]>) - Constructor for class org.orekit.propagation.SpacecraftState
-
- SpacecraftState(AbsolutePVCoordinates, double, DoubleArrayDictionary) - Constructor for class org.orekit.propagation.SpacecraftState
-
Create a new instance from position-velocity-acceleration, mass and additional states.
- SpacecraftState(AbsolutePVCoordinates, Attitude, double, Map<String, double[]>) - Constructor for class org.orekit.propagation.SpacecraftState
-
- SpacecraftState(AbsolutePVCoordinates, Attitude, double, DoubleArrayDictionary) - Constructor for class org.orekit.propagation.SpacecraftState
-
Build a spacecraft state from position-velocity-acceleration, attitude, mass and additional states.
- SpacecraftState(AbsolutePVCoordinates, Attitude, double, DoubleArrayDictionary, DoubleArrayDictionary) - Constructor for class org.orekit.propagation.SpacecraftState
-
Build a spacecraft state from position-velocity-acceleration, attitude, mass and additional states and derivatives.
- SPEED_OF_LIGHT - Static variable in interface org.orekit.utils.Constants
-
Speed of light: 299792458.0 m/s.
- SphericalHarmonicsProvider - Interface in org.orekit.forces.gravity.potential
-
Interface used to provide spherical harmonics coefficients.
- SpinStabilized - Class in org.orekit.attitudes
-
This class handles a spin stabilized attitude provider.
- SpinStabilized(AttitudeProvider, AbsoluteDate, Vector3D, double) - Constructor for class org.orekit.attitudes.SpinStabilized
-
Creates a new instance.
- SpinStabilized - Class in org.orekit.files.ccsds.ndm.adm.apm
-
Container for Attitude Parameter Message data lines.
- SpinStabilized() - Constructor for class org.orekit.files.ccsds.ndm.adm.apm.SpinStabilized
-
Simple constructor.
- SpinStabilizedKey - Enum in org.orekit.files.ccsds.ndm.adm.apm
-
- sqrt(String) - Method in class org.orekit.utils.units.Unit
-
Create root of unit.
- SSA - Static variable in class org.orekit.models.earth.displacement.Tide
-
Ssa tide.
- SsrData - Class in org.orekit.gnss.metric.messages.ssr
-
Container for common data in SSR message data.
- SsrData() - Constructor for class org.orekit.gnss.metric.messages.ssr.SsrData
-
- SsrHeader - Class in org.orekit.gnss.metric.messages.ssr
-
Container for common data in SSR messages header.
- SsrHeader() - Constructor for class org.orekit.gnss.metric.messages.ssr.SsrHeader
-
- SsrIgm01 - Class in org.orekit.gnss.metric.messages.ssr.igm
-
GNSS SSR Orbit Correction Message.
- SsrIgm01(int, SatelliteSystem, SsrIgm01Header, List<SsrIgm01Data>) - Constructor for class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm01
-
Constructor.
- SsrIgm01Data - Class in org.orekit.gnss.metric.messages.ssr.igm
-
Container for SSR IGM01 data.
- SsrIgm01Data() - Constructor for class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm01Data
-
Constructor.
- SsrIgm01Header - Class in org.orekit.gnss.metric.messages.ssr.igm
-
Container for SSR IGM01 header.
- SsrIgm01Header() - Constructor for class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm01Header
-
Constructor.
- SsrIgm02 - Class in org.orekit.gnss.metric.messages.ssr.igm
-
GNSS SSR Clock Correction Message.
- SsrIgm02(int, SatelliteSystem, SsrIgm02Header, List<SsrIgm02Data>) - Constructor for class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm02
-
Constructor.
- SsrIgm02Data - Class in org.orekit.gnss.metric.messages.ssr.igm
-
Container for SSR IGM02 data.
- SsrIgm02Data() - Constructor for class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm02Data
-
Constructor.
- SsrIgm02Header - Class in org.orekit.gnss.metric.messages.ssr.igm
-
Container for SSR IGM02 header.
- SsrIgm02Header() - Constructor for class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm02Header
-
Constructor.
- SsrIgm03 - Class in org.orekit.gnss.metric.messages.ssr.igm
-
GNSS SSR Combined Orbit and Clock Correction Message.
- SsrIgm03(int, SatelliteSystem, SsrIgm03Header, List<SsrIgm03Data>) - Constructor for class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm03
-
Constructor.
- SsrIgm03Data - Class in org.orekit.gnss.metric.messages.ssr.igm
-
Container for SSR IGM03 data.
- SsrIgm03Data() - Constructor for class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm03Data
-
Constructor.
- SsrIgm03Header - Class in org.orekit.gnss.metric.messages.ssr.igm
-
Container for SSR IGM03 header.
- SsrIgm03Header() - Constructor for class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm03Header
-
Constructor.
- SsrIgm04 - Class in org.orekit.gnss.metric.messages.ssr.igm
-
GNSS SSR High Rate Clock Correction Message.
- SsrIgm04(int, SatelliteSystem, SsrIgm04Header, List<SsrIgm04Data>) - Constructor for class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm04
-
Constructor.
- SsrIgm04Data - Class in org.orekit.gnss.metric.messages.ssr.igm
-
Container for SSR IGM04 data.
- SsrIgm04Data() - Constructor for class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm04Data
-
Constructor.
- SsrIgm04Header - Class in org.orekit.gnss.metric.messages.ssr.igm
-
Container for SSR IGM04 header.
- SsrIgm04Header() - Constructor for class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm04Header
-
Constructor.
- SsrIgm05 - Class in org.orekit.gnss.metric.messages.ssr.igm
-
GNSS SSR Code Bias Message.
- SsrIgm05(int, SatelliteSystem, SsrIgm05Header, List<SsrIgm05Data>) - Constructor for class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm05
-
Constructor.
- SsrIgm05Data - Class in org.orekit.gnss.metric.messages.ssr.igm
-
Container for SSR IGM05 data.
- SsrIgm05Data() - Constructor for class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm05Data
-
Constructor.
- SsrIgm05Header - Class in org.orekit.gnss.metric.messages.ssr.igm
-
Container for SSR IGM05 header.
- SsrIgm05Header() - Constructor for class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm05Header
-
Constructor.
- SsrIgm06 - Class in org.orekit.gnss.metric.messages.ssr.igm
-
GNSS SSR Phase Bias Message.
- SsrIgm06(int, SatelliteSystem, SsrIgm06Header, List<SsrIgm06Data>) - Constructor for class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm06
-
Constructor.
- SsrIgm06Data - Class in org.orekit.gnss.metric.messages.ssr.igm
-
Container for SSR IGM06 data.
- SsrIgm06Data() - Constructor for class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm06Data
-
Constructor.
- SsrIgm06Header - Class in org.orekit.gnss.metric.messages.ssr.igm
-
Container for SSR IGM06 header.
- SsrIgm06Header() - Constructor for class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm06Header
-
Constructor.
- SsrIgm07 - Class in org.orekit.gnss.metric.messages.ssr.igm
-
GNSS SSR SSR URA Message.
- SsrIgm07(int, SatelliteSystem, SsrIgm07Header, List<SsrIgm07Data>) - Constructor for class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm07
-
Constructor.
- SsrIgm07Data - Class in org.orekit.gnss.metric.messages.ssr.igm
-
Container for SSR IGM07 data.
- SsrIgm07Data() - Constructor for class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm07Data
-
Constructor.
- SsrIgm07Header - Class in org.orekit.gnss.metric.messages.ssr.igm
-
Container for SSR IGM07 header.
- SsrIgm07Header() - Constructor for class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm07Header
-
Constructor.
- SsrIgmData - Class in org.orekit.gnss.metric.messages.ssr.igm
-
Container for common data in IGS Generic SSR Message type.
- SsrIgmData() - Constructor for class org.orekit.gnss.metric.messages.ssr.igm.SsrIgmData
-
Constructor.
- SsrIgmHeader - Class in org.orekit.gnss.metric.messages.ssr.igm
-
Container for common data in IGS Generic SSR Message type header.
- SsrIgmHeader() - Constructor for class org.orekit.gnss.metric.messages.ssr.igm.SsrIgmHeader
-
Constructor.
- SsrIgmMessage<H extends SsrIgmHeader,D extends SsrIgmData> - Class in org.orekit.gnss.metric.messages.ssr.igm
-
The IGS Generic SSR Message types provide elements
to calculate GNSS satellite corrections.
- SsrIgmMessage(int, SatelliteSystem, H, List<D>) - Constructor for class org.orekit.gnss.metric.messages.ssr.igm.SsrIgmMessage
-
Constructor.
- SsrIm201 - Class in org.orekit.gnss.metric.messages.ssr.subtype
-
SSR Ionosphere VTEC Spherical Harmonics Message.
- SsrIm201(int, SsrIm201Header, List<SsrIm201Data>) - Constructor for class org.orekit.gnss.metric.messages.ssr.subtype.SsrIm201
-
Constructor.
- SsrIm201Data - Class in org.orekit.gnss.metric.messages.ssr.subtype
-
Container for SSR IM201 data.
- SsrIm201Data() - Constructor for class org.orekit.gnss.metric.messages.ssr.subtype.SsrIm201Data
-
Constructor.
- SsrIm201Header - Class in org.orekit.gnss.metric.messages.ssr.subtype
-
Container for SSR IM201 header.
- SsrIm201Header() - Constructor for class org.orekit.gnss.metric.messages.ssr.subtype.SsrIm201Header
-
Constructor.
- SsrMessage<H extends SsrHeader,D extends SsrData> - Class in org.orekit.gnss.metric.messages.ssr
-
Base class for SSR messages.
- SsrMessage(int, H, List<D>) - Constructor for class org.orekit.gnss.metric.messages.ssr.SsrMessage
-
Constructor.
- SsrVtecIonosphericModel - Class in org.orekit.models.earth.ionosphere
-
Ionospheric model based on SSR IM201 message.
- SsrVtecIonosphericModel(SsrIm201) - Constructor for class org.orekit.models.earth.ionosphere.SsrVtecIonosphericModel
-
Constructor.
- STANDARD_ATM_PRESSURE - Static variable in class org.orekit.models.earth.EarthStandardAtmosphereRefraction
-
NIST standard atmospheric pressure (Pa).
- STANDARD_ATM_TEMPERATURE - Static variable in class org.orekit.models.earth.EarthStandardAtmosphereRefraction
-
NIST standard atmospheric temperature (K).
- STANDARDIZED_LOCALE - Static variable in class org.orekit.utils.AccurateFormatter
-
Standardized locale to use, to ensure files can be exchanged without
internationalization issues.
- start() - Method in class org.orekit.gnss.metric.parser.AbstractEncodedMessages
-
Start message extraction.
- start() - Method in class org.orekit.gnss.metric.parser.ByteArrayEncodedMessages
-
Start message extraction.
- start() - Method in interface org.orekit.gnss.metric.parser.EncodedMessage
-
Start message extraction.
- START_SUFFIX - Static variable in class org.orekit.propagation.events.FieldParameterDrivenDateIntervalDetector
-
Default suffix for start driver.
- START_SUFFIX - Static variable in class org.orekit.propagation.events.ParameterDrivenDateIntervalDetector
-
Default suffix for start driver.
- started(TaskEvent) - Method in class org.orekit.compiler.plugin.DefaultDataContextPlugin
-
- startMessage(String, String, double) - Method in interface org.orekit.files.ccsds.utils.generation.Generator
-
Start CCSDS message.
- startMessage(String, String, double) - Method in class org.orekit.files.ccsds.utils.generation.KvnGenerator
-
Start CCSDS message.
- startMessage(String, String, double) - Method in class org.orekit.files.ccsds.utils.generation.XmlGenerator
-
Start CCSDS message.
- startParse(String) - Method in class org.orekit.forces.gravity.potential.OceanTidesReader
-
Start parsing.
- StartStopEventsTrigger<A extends AbstractDetector<A>,O extends AbstractDetector<O>> - Class in org.orekit.forces.maneuvers.trigger
-
Maneuver triggers based on a pair of event detectors that defines firing start and stop.
- StartStopEventsTrigger(A, O) - Constructor for class org.orekit.forces.maneuvers.trigger.StartStopEventsTrigger
-
Simple constructor.
- startStreaming(String, Type, boolean, boolean) - Method in class org.orekit.gnss.metric.ntrip.NtripClient
-
Connect to a mount point and start streaming data from it.
- STATE_DIMENSION - Static variable in class org.orekit.propagation.AbstractMatricesHarvester
-
State dimension, fixed to 6.
- STATE_DIMENSION - Static variable in class org.orekit.propagation.analytical.tle.TLEJacobiansMapper
-
State dimension, fixed to 6.
- STATE_DIMENSION - Static variable in class org.orekit.propagation.integration.AbstractJacobiansMapper
-
State dimension, fixed to 6.
- STATE_DIMENSION - Static variable in class org.orekit.propagation.numerical.AbsoluteJacobiansMapper
-
State dimension, fixed to 6.
- STATE_DIMENSION - Static variable in class org.orekit.propagation.numerical.JacobiansMapper
-
State dimension, fixed to 6.
- STATE_DIMENSION - Static variable in class org.orekit.propagation.semianalytical.dsst.DSSTJacobiansMapper
-
State dimension, fixed to 6.
- stateChanged(SpacecraftState) - Method in class org.orekit.propagation.AbstractPropagator
-
Notify about a state change.
- stateChanged(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.FieldAbstractPropagator
-
Notify about a state change.
- StateFunction - Interface in org.orekit.utils
-
- StateJacobian - Interface in org.orekit.utils
-
Interface representing the Jacobian of a vector function depending on
SpacecraftState
.
- StateMapper - Class in org.orekit.propagation.integration
-
- StateMapper(AbsoluteDate, double, OrbitType, PositionAngle, AttitudeProvider, Frame) - Constructor for class org.orekit.propagation.integration.StateMapper
-
Simple constructor.
- stateToTLE(FieldSpacecraftState<T>, FieldTLE<T>) - Static method in class org.orekit.propagation.analytical.tle.FieldTLE
-
Convert Spacecraft State into TLE.
- stateToTLE(FieldSpacecraftState<T>, FieldTLE<T>, TimeScale, Frame) - Static method in class org.orekit.propagation.analytical.tle.FieldTLE
-
Convert Spacecraft State into TLE.
- stateToTLE(FieldSpacecraftState<T>, FieldTLE<T>, TimeScale, Frame, double, int) - Static method in class org.orekit.propagation.analytical.tle.FieldTLE
-
Convert Spacecraft State into TLE.
- stateToTLE(SpacecraftState, TLE) - Static method in class org.orekit.propagation.analytical.tle.TLE
-
Convert Spacecraft State into TLE.
- stateToTLE(SpacecraftState, TLE, TimeScale, Frame) - Static method in class org.orekit.propagation.analytical.tle.TLE
-
Convert Spacecraft State into TLE.
- stateToTLE(SpacecraftState, TLE, TimeScale, Frame, double, int) - Static method in class org.orekit.propagation.analytical.tle.TLE
-
Convert Spacecraft State into TLE.
- StateVector - Class in org.orekit.files.ccsds.ndm.odm
-
Container for state vector data.
- StateVector() - Constructor for class org.orekit.files.ccsds.ndm.odm.StateVector
-
Create an empty data set.
- StateVectorKey - Enum in org.orekit.files.ccsds.ndm.odm
-
- StateVectorWriter - Class in org.orekit.files.ccsds.ndm.odm
-
Writer for state vector data.
- StateVectorWriter(String, String, StateVector, TimeConverter) - Constructor for class org.orekit.files.ccsds.ndm.odm.StateVectorWriter
-
Create a writer.
- Station - Class in org.orekit.files.sinex
-
Station model.
- Station() - Constructor for class org.orekit.files.sinex.Station
-
Constructor.
- Station.ReferenceSystem - Enum in org.orekit.files.sinex
-
Eccentricity reference system.
- StationDisplacement - Interface in org.orekit.models.earth.displacement
-
Interface for computing reference points displacement.
- stec(AbsoluteDate, GeodeticPoint, GeodeticPoint) - Method in class org.orekit.models.earth.ionosphere.NeQuickModel
-
This method allows the computation of the Stant Total Electron Content (STEC).
- stec(FieldAbsoluteDate<T>, FieldGeodeticPoint<T>, FieldGeodeticPoint<T>) - Method in class org.orekit.models.earth.ionosphere.NeQuickModel
-
This method allows the computation of the Stant Total Electron Content (STEC).
- StepHandlerMultiplexer - Class in org.orekit.propagation.sampling
-
- StepHandlerMultiplexer() - Constructor for class org.orekit.propagation.sampling.StepHandlerMultiplexer
-
Simple constructor.
- stillAcceptsData() - Method in interface org.orekit.data.DataLoader
-
Check if the loader still accepts new data.
- stillAcceptsData() - Method in class org.orekit.forces.gravity.potential.AstronomicalAmplitudeReader
-
Check if the loader still accepts new data.
- stillAcceptsData() - Method in class org.orekit.forces.gravity.potential.OceanTidesReader
-
Check if the loader still accepts new data.
- stillAcceptsData() - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
-
Check if the loader still accepts new data.
- stillAcceptsData() - Method in class org.orekit.gnss.RinexObservationLoader.Parser
-
Check if the loader still accepts new data.
- stillAcceptsData() - Method in class org.orekit.gnss.SEMParser
-
- stillAcceptsData() - Method in class org.orekit.gnss.YUMAParser
-
- stillAcceptsData() - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherDataLoader
-
Check if the loader still accepts new data.
- stillAcceptsData() - Method in class org.orekit.models.earth.atmosphere.data.MarshallSolarActivityFutureEstimation
-
Check if the loader still accepts new data.
- stillAcceptsData() - Method in class org.orekit.models.earth.GeoMagneticModelLoader
-
Check if the loader still accepts new data.
- stillAcceptsData() - Method in class org.orekit.models.earth.ionosphere.KlobucharIonoCoefficientsLoader
-
Check if the loader still accepts new data.
- stillAcceptsData() - Method in class org.orekit.models.earth.troposphere.ViennaModelCoefficientsLoader
-
- stillAcceptsData() - Method in class org.orekit.utils.InterpolationTableLoader
-
Check if the loader still accepts new data.
- STMEquations - Class in org.orekit.propagation.numerical.cr3bp
-
Class calculating the state transition matrix coefficient for CR3BP Computation.
- STMEquations(CR3BPSystem) - Constructor for class org.orekit.propagation.numerical.cr3bp.STMEquations
-
Simple constructor.
- STOP_SUFFIX - Static variable in class org.orekit.propagation.events.FieldParameterDrivenDateIntervalDetector
-
Default suffix for stop driver.
- STOP_SUFFIX - Static variable in class org.orekit.propagation.events.ParameterDrivenDateIntervalDetector
-
Default suffix for stop driver.
- stopMonitoring() - Method in class org.orekit.gnss.metric.ntrip.StreamMonitor
-
Stop monitoring.
- StopOnDecreasing<T extends EventDetector> - Class in org.orekit.propagation.events.handlers
-
Handle a detection event and choose what to do next.
- StopOnDecreasing() - Constructor for class org.orekit.propagation.events.handlers.StopOnDecreasing
-
- StopOnEvent<T extends EventDetector> - Class in org.orekit.propagation.events.handlers
-
Event handler which will always return
stop
as a state.
- StopOnEvent() - Constructor for class org.orekit.propagation.events.handlers.StopOnEvent
-
- StopOnIncreasing<T extends EventDetector> - Class in org.orekit.propagation.events.handlers
-
Handle a detection event and choose what to do next.
- StopOnIncreasing() - Constructor for class org.orekit.propagation.events.handlers.StopOnIncreasing
-
- stopStreaming(int) - Method in class org.orekit.gnss.metric.ntrip.NtripClient
-
Stop streaming data from all connected mount points.
- StreamedMessage - Class in org.orekit.gnss.metric.ntrip
-
Container for streamed messages meta-data.
- StreamingAemWriter - Class in org.orekit.files.ccsds.ndm.adm.aem
-
A writer for AEM files.
- StreamingAemWriter(Generator, AemWriter, Header, AemMetadata) - Constructor for class org.orekit.files.ccsds.ndm.adm.aem.StreamingAemWriter
-
Simple constructor.
- StreamingAemWriter.SegmentWriter - Class in org.orekit.files.ccsds.ndm.adm.aem
-
A writer for a segment of an AEM.
- StreamingCpfWriter - Class in org.orekit.files.ilrs
-
A writer for CPF files.
- StreamingCpfWriter(Appendable, TimeScale, CPFHeader) - Constructor for class org.orekit.files.ilrs.StreamingCpfWriter
-
Create a CPF writer than streams data to the given output stream.
- StreamingCpfWriter.HeaderLineWriter - Enum in org.orekit.files.ilrs
-
Writer for specific header lines.
- StreamingCpfWriter.Segment - Class in org.orekit.files.ilrs
-
A writer for a segment of a CPF.
- StreamingOemWriter - Class in org.orekit.files.ccsds.ndm.odm.oem
-
A writer for OEM files.
- StreamingOemWriter(Generator, OemWriter, Header, OemMetadata) - Constructor for class org.orekit.files.ccsds.ndm.odm.oem.StreamingOemWriter
-
Construct a writer that for each segment uses the reference frame of the
first state's attitude.
- StreamingOemWriter(Generator, OemWriter, Header, OemMetadata, boolean) - Constructor for class org.orekit.files.ccsds.ndm.odm.oem.StreamingOemWriter
-
Construct a writer that writes position, velocity, and acceleration at
each time step.
- StreamingOemWriter(Generator, OemWriter, Header, OemMetadata, boolean, boolean) - Constructor for class org.orekit.files.ccsds.ndm.odm.oem.StreamingOemWriter
-
Simple constructor.
- StreamingOemWriter.SegmentWriter - Class in org.orekit.files.ccsds.ndm.odm.oem
-
A writer for a segment of an OEM.
- StreamMonitor - Class in org.orekit.gnss.metric.ntrip
-
Monitor for retrieving streamed data from one mount point.
- StreamMonitor(NtripClient, String, Type, boolean, boolean, double, double, int) - Constructor for class org.orekit.gnss.metric.ntrip.StreamMonitor
-
Build a monitor for streaming data from a mount point.
- stringValue(EncodedMessage, int) - Method in interface org.orekit.gnss.metric.parser.DataField
-
Get the value of the field as a String.
- subtractOffset(AngularCoordinates) - Method in class org.orekit.utils.AngularCoordinates
-
Subtract an offset from the instance.
- subtractOffset(FieldAngularCoordinates<T>) - Method in class org.orekit.utils.FieldAngularCoordinates
-
Subtract an offset from the instance.
- subtractOffset(AngularCoordinates) - Method in class org.orekit.utils.TimeStampedAngularCoordinates
-
Subtract an offset from the instance.
- subtractOffset(FieldAngularCoordinates<T>) - Method in class org.orekit.utils.TimeStampedFieldAngularCoordinates
-
Subtract an offset from the instance.
- SUN - Static variable in class org.orekit.bodies.CelestialBodyFactory
-
Predefined name for Sun.
- SUN_RADIUS - Static variable in interface org.orekit.utils.Constants
-
Sun radius: 695500000 m.
- SUPPORTED_NAMES - Static variable in class org.orekit.frames.ITRFVersionLoader
-
Regular expression for supported files names.
- supportsTimeTransform() - Method in class org.orekit.models.earth.GeoMagneticField
-
Indicates whether this model supports time transformation or not.
- switchOccurred(AttitudeProvider, AttitudeProvider, SpacecraftState) - Method in interface org.orekit.attitudes.AttitudesSequence.SwitchHandler
-
Method called when attitude is switched from one law to another law.
- sxpInitialize(T[]) - Method in class org.orekit.propagation.analytical.tle.FieldSGP4
-
Initialization proper to each propagator (SGP or SDP).
- sxpInitialize(T[]) - Method in class org.orekit.propagation.analytical.tle.FieldTLEPropagator
-
Initialization proper to each propagator (SGP or SDP).
- sxpInitialize() - Method in class org.orekit.propagation.analytical.tle.SGP4
-
Initialization proper to each propagator (SGP or SDP).
- sxpInitialize() - Method in class org.orekit.propagation.analytical.tle.TLEPropagator
-
Initialization proper to each propagator (SGP or SDP).
- sxpPropagate(T, T[]) - Method in class org.orekit.propagation.analytical.tle.FieldSGP4
-
Propagation proper to each propagator (SGP or SDP).
- sxpPropagate(T, T[]) - Method in class org.orekit.propagation.analytical.tle.FieldTLEPropagator
-
Propagation proper to each propagator (SGP or SDP).
- sxpPropagate(double) - Method in class org.orekit.propagation.analytical.tle.SGP4
-
Propagation proper to each propagator (SGP or SDP).
- sxpPropagate(double) - Method in class org.orekit.propagation.analytical.tle.TLEPropagator
-
Propagation proper to each propagator (SGP or SDP).
- SystemConfiguration() - Constructor for class org.orekit.files.ilrs.CRDConfiguration.SystemConfiguration
-