- g - Variable in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution
-
Equinoctial frame g vector.
- 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.FieldNodeDetector
-
Compute the value of the switching function.
- 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.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.CircularFieldOfViewDetector
-
Compute the value of the switching function.
- 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(SpacecraftState) - Method in class org.orekit.propagation.events.FieldOfViewDetector
-
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.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.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.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.
- G01 - org.orekit.gnss.Frequency
-
GPS L1 (1575.42 MHz).
- G02 - org.orekit.gnss.Frequency
-
GPS L2 (1227.6 MHz).
- G05 - org.orekit.gnss.Frequency
-
GPS L5 (1176.45 MHz).
- GAL - org.orekit.files.sp3.SP3File.TimeSystem
-
GALILEO.
- 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 - org.orekit.files.sp3.SP3File.SP3FileType
-
Galileo only file.
- GALILEO - org.orekit.gnss.SatelliteSystem
-
Galileo system.
- GALILEO_0A - org.orekit.gnss.antenna.SatelliteAntennaCode
-
Deprecated.
Galileo In-Orbit Validation Element A (GIOVE-A).
- GALILEO_0A - org.orekit.gnss.antenna.SatelliteType
-
Galileo In-Orbit Validation Element A (GIOVE-A).
- GALILEO_0B - org.orekit.gnss.antenna.SatelliteAntennaCode
-
Deprecated.
Galileo In-Orbit Validation Element B (GIOVE-B).
- GALILEO_0B - org.orekit.gnss.antenna.SatelliteType
-
Galileo In-Orbit Validation Element B (GIOVE-B).
- GALILEO_1 - org.orekit.gnss.antenna.SatelliteAntennaCode
-
Deprecated.
Galileo IOV : GSAT 0101-0104.
- GALILEO_1 - org.orekit.gnss.antenna.SatelliteType
-
Galileo IOV : GSAT 0101-0104.
- GALILEO_2 - org.orekit.gnss.antenna.SatelliteAntennaCode
-
Deprecated.
Galileo FOC : GSAT 0201-0222.
- GALILEO_2 - org.orekit.gnss.antenna.SatelliteType
-
Galileo FOC : GSAT 0201-0222.
- GALILEO_EPOCH - Static variable in class org.orekit.time.AbsoluteDate
-
Reference epoch for Galileo System Time: 1999-08-22T00:00:00 UTC.
- GALILEO_EPOCH - Static variable in class org.orekit.time.DateComponents
-
Reference epoch for Galileo System Time: 1999-08-22.
- 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.
- GCRF - org.orekit.files.ccsds.CCSDSFrame
-
Geocentric Celestial Reference Frame.
- GCRF - org.orekit.frames.Predefined
-
GCRF frame.
- GEGOUT - org.orekit.forces.gravity.potential.OceanLoadDeformationCoefficients
-
Coefficients computed by Pascal Gégout, CNRS / UMR5563 (GET).
- 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(List<OrekitStepInterpolator>) - Method in interface org.orekit.estimation.measurements.generation.Scheduler
-
Generate a sequence of measurements.
- generate(AbsoluteDate, AbsoluteDate) - Method in class org.orekit.estimation.measurements.generation.Generator
-
Generate 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.OMMFile
-
- generateCartesianOrbit() - Method in class org.orekit.files.ccsds.OPMFile
-
- generateKeplerianOrbit() - Method in class org.orekit.files.ccsds.OMMFile
-
- generateKeplerianOrbit() - Method in class org.orekit.files.ccsds.OPMFile
-
Generate a
KeplerianOrbit
from the OPM Keplerian elements if hasKeplerianElements is true,
or from the state vector data otherwise.
- generateSpacecraftState() - Method in class org.orekit.files.ccsds.OMMFile
-
Generate spacecraft state from the
KeplerianOrbit
generated by generateKeplerianOrbit.
- generateSpacecraftState() - Method in class org.orekit.files.ccsds.OPMFile
-
Generate spacecraft state from the
CartesianOrbit
generated by generateCartesianOrbit.
- generateTLE() - Method in class org.orekit.files.ccsds.OMMFile
-
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.
- 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(double, double, BodyShape, SphericalPolygonsSet, double) - Constructor for class org.orekit.propagation.events.GeographicZoneDetector
-
Build a detector.
- GeographicZoneDetector(BodyShape, SphericalPolygonsSet, double) - Constructor for class org.orekit.propagation.events.GeographicZoneDetector
-
Build a new 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.
- 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
-
- get(AbsoluteDate) - Method in class org.orekit.utils.TimeSpanMap
-
Get the entry valid at a specified date.
- get(FieldAbsoluteDate<D>) - Method in class org.orekit.utils.FieldTimeSpanMap
-
Get the entry valid at a specified date.
- get24HoursKp(AbsoluteDate) - Method in class org.orekit.forces.drag.atmosphere.data.MarshallSolarActivityFutureEstimation
-
The Kp index is derived from the Ap index.
- get24HoursKp(AbsoluteDate) - Method in interface org.orekit.forces.drag.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.OGMFile
-
Get the orbit semi-major axis.
- getA() - Method in class org.orekit.models.earth.GlobalPressureTemperature2Model
-
Returns the a coefficients array.
- getA() - Method in class org.orekit.models.earth.ViennaModelCoefficientsLoader
-
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.utilities.AuxiliaryElements
-
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.
- 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.
- getAccuracy() - Method in class org.orekit.files.sp3.SP3File.SP3Ephemeris
-
Get the formal accuracy for this satellite.
- 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.
- getAdaptedPropagator() - Method in class org.orekit.propagation.conversion.AbstractPropagatorConverter
-
Get the adapted propagator.
- 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.
- getAdditionalState(FieldSpacecraftState<T>) - Method in interface org.orekit.propagation.FieldAdditionalStateProvider
-
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.
- getAdditionalStateDimension() - Method in class org.orekit.propagation.numerical.JacobiansMapper
-
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
-
Get an unmodifiable map of additional states.
- getAdditionalStates() - Method in class org.orekit.propagation.SpacecraftState
-
Get an unmodifiable map of additional states.
- 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.gnss.GPSAlmanac
-
- getAf0() - Method in interface org.orekit.propagation.analytical.gnss.GPSOrbitalElements
-
Gets the Zeroth Order Clock Correction.
- getAf1() - Method in class org.orekit.gnss.GPSAlmanac
-
- getAf1() - Method in interface org.orekit.propagation.analytical.gnss.GPSOrbitalElements
-
Gets the First Order Clock Correction.
- getAf2() - Method in interface org.orekit.propagation.analytical.gnss.GPSOrbitalElements
-
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.SP3File
-
Returns the agency that prepared this SP3 file.
- getAgencyName() - Method in class org.orekit.gnss.RinexHeader
-
Get name of the agency.
- 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.
- 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.
- getAlmanacs() - Method in class org.orekit.gnss.SEMParser
-
- getAlmanacs() - Method in class org.orekit.gnss.YUMAParser
-
- getAlpha() - Method in class org.orekit.models.earth.KlobucharIonoCoefficientsLoader
-
Returns the alpha coefficients array.
- getAlpha() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
-
Get direction cosine α for central body.
- 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.
- 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.
- 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.
- 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).
- getAngleType() - Method in class org.orekit.files.ccsds.TDMFile.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.
- 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.OGMFile
-
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.OGMFile
-
Get the type of anomaly (true or mean).
- getAntennaAzimuth() - Method in class org.orekit.gnss.RinexHeader
-
Get the azimuth of the zero direction of a fixed antenna.
- getAntennaBSight() - Method in class org.orekit.gnss.RinexHeader
-
Get the antenna B.Sight.
- getAntennaHeight() - Method in class org.orekit.gnss.RinexHeader
-
Get the antenna height.
- getAntennaNumber() - Method in class org.orekit.gnss.RinexHeader
-
Get the number of the antenna.
- getAntennaPhaseCenter() - Method in class org.orekit.gnss.RinexHeader
-
Get the antenna phasecenter.
- getAntennaReferencePoint() - Method in class org.orekit.gnss.RinexHeader
-
Get the position of antenna reference point for antenna on vehicle.
- getAntennaType() - Method in class org.orekit.gnss.RinexHeader
-
Get the type of the antenna.
- getAntennaZeroDirection() - Method in class org.orekit.gnss.RinexHeader
-
Get the zero direction of antenna.
- getAp(AbsoluteDate) - Method in class org.orekit.forces.drag.atmosphere.data.MarshallSolarActivityFutureEstimation
-
Get the Ap geomagnetic indices.
- getAp(AbsoluteDate) - Method in interface org.orekit.forces.drag.atmosphere.NRLMSISE00InputParameters
-
Get the Ap geomagnetic indices.
- getApproxPos() - Method in class org.orekit.gnss.RinexHeader
-
Get the Approximate Marker Position.
- 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.propagation.semianalytical.dsst.forces.DSSTAtmosphericDrag
-
Get the atmospheric model.
- getAttitude() - Method in class org.orekit.propagation.FieldSpacecraftState
-
Get the attitude.
- getAttitude() - Method in class org.orekit.propagation.SpacecraftState
-
Get the attitude.
- getAttitude(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in interface org.orekit.attitudes.AttitudeProvider
-
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(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, 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.FixedRate
-
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(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, 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.LofOffset
-
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(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, 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.TabulatedLofOffset
-
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(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, 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.YawSteering
-
Compute the attitude corresponding to an orbital state.
- getAttitude(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.gnss.attitude.AbstractGNSSAttitudeProvider
-
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(PVCoordinatesProvider, AbsoluteDate, 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(PVCoordinatesProvider, AbsoluteDate, 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(PVCoordinatesProvider, AbsoluteDate, 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(PVCoordinatesProvider, AbsoluteDate, 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(PVCoordinatesProvider, AbsoluteDate, 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(PVCoordinatesProvider, AbsoluteDate, 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(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.gnss.attitude.AbstractGNSSAttitudeProvider
-
Compute the attitude corresponding to an orbital state.
- getAttitudeOverride() - Method in class org.orekit.forces.maneuvers.ConstantThrustManeuver
-
Get the attitude override used for the maneuver.
- getAttitudeOverride() - Method in class org.orekit.forces.maneuvers.ImpulseManeuver
-
Get the Attitude Provider to use during maneuver.
- getAttitudeProvider() - Method in class org.orekit.propagation.AbstractPropagator
-
Get attitude provider.
- getAttitudeProvider() - Method in class org.orekit.propagation.conversion.NumericalPropagatorBuilder
-
Get the attitudeProvider.
- 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.
- getAvailableDerivatives() - Method in class org.orekit.files.ccsds.OEMFile.EphemeridesBlock
-
- 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.OrekitEphemerisFile.OrekitEphemerisSegment
-
- getAvailableDerivatives() - Method in class org.orekit.files.sp3.SP3File.SP3Ephemeris
-
- getAvailableSatelliteNumbers() - Method in class org.orekit.propagation.analytical.tle.TLESeries
-
Deprecated.
Get the available satellite numbers.
- getAverageFlux(AbsoluteDate) - Method in class org.orekit.forces.drag.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.forces.drag.atmosphere.NRLMSISE00InputParameters
-
Get the value of the 81 day average of F10.7 solar flux centered on current day.
- 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.
- 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.
- 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.utilities.AuxiliaryElements
-
Get B = sqrt(1 - e²).
- getBaseFrame() - Method in class org.orekit.estimation.measurements.GroundStation
-
Get the base frame associated with the station.
- getBaseState(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, 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.YawSteering
-
Compute the base system state at given date, without compensation.
- getBaseState(PVCoordinatesProvider, AbsoluteDate, 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.
- 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.
- 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.
- 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.
- getBeta() - Method in class org.orekit.models.earth.KlobucharIonoCoefficientsLoader
-
Returns the beta coefficients array.
- getBeta() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
-
Get direction cosine β for central body.
- 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.
- getBody(String) - Static method in class org.orekit.bodies.CelestialBodyFactory
-
Get a celestial 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.
- getBStar() - Method in class org.orekit.files.ccsds.OMMFile
-
Get the SGP/SGP4 drag-like 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.
- 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.
- 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.
- 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(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.
- 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.
- getCCSDSEpoch(Field<T>) - Static method in class org.orekit.time.FieldAbsoluteDate
-
Reference epoch for CCSDS Time Code Format (CCSDS 301.0-B-4):
1958-01-01T00:00:00 International Atomic Time (not UTC).
- getCelestialBody() - Method in enum org.orekit.files.ccsds.CenterName
-
Get the celestial body corresponding to the CCSDS constant.
- getCenter() - Method in class org.orekit.bodies.Ellipse
-
Get the center of the 2D ellipse.
- getCenter() - Method in class org.orekit.models.earth.tessellation.Tile
-
Get the center point.
- getCenter() - Method in class org.orekit.propagation.events.CircularFieldOfViewDetector
-
Get the direction of FOV center.
- getCenterBody() - Method in class org.orekit.files.ccsds.ODMMetaData
-
- getCenterMass() - Method in class org.orekit.gnss.RinexHeader
-
Get the current center of mass of vehicle in body fixed coordinate system.
- getCenterName() - Method in class org.orekit.files.ccsds.CcsdsModifiedFrame
-
Get the CCSDS center name.
- getCenterName() - Method in class org.orekit.files.ccsds.ODMMetaData
-
Get the origin of reference frame.
- getCenterOfCurvature(Vector2D) - Method in class org.orekit.bodies.Ellipse
-
Find the center of curvature (point on the evolute) at the nadir of a point.
- getCentralBody() - Method in class org.orekit.propagation.events.InterSatDirectViewDetector
-
Get the central body.
- getChildren() - Method in class org.orekit.frames.OrphanFrame
-
Get all children of the instance.
- getCic() - Method in class org.orekit.gnss.GPSAlmanac
-
- getCic() - Method in interface org.orekit.propagation.analytical.gnss.GPSOrbitalElements
-
Gets the Amplitude of the Cosine Harmonic Correction Term to the Angle of Inclination.
- 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) - Static method in class org.orekit.frames.FramesFactory
-
Get the CIRF2000 reference frame.
- getCis() - Method in class org.orekit.gnss.GPSAlmanac
-
- getCis() - Method in interface org.orekit.propagation.analytical.gnss.GPSOrbitalElements
-
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.
- getClassification() - Method in class org.orekit.propagation.analytical.tle.TLE
-
Get the classification.
- getClassificationType() - Method in class org.orekit.files.ccsds.OMMFile
-
Get the classification type.
- getClkOffset() - Method in class org.orekit.gnss.RinexHeader
-
Get the realtime-derived receiver clock offset.
- getClockCorrection() - Method in class org.orekit.files.sp3.SP3File.SP3Coordinate
-
Returns the clock correction value.
- 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.
- getClockRateChange() - Method in class org.orekit.files.sp3.SP3File.SP3Coordinate
-
Returns the clock rate.
- getClosestTLE(AbsoluteDate) - Method in class org.orekit.propagation.analytical.tle.TLESeries
-
Deprecated.
Get the closest TLE to the selected date.
- 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(AbsoluteDate, Set<String>) - Method in interface org.orekit.propagation.semianalytical.dsst.forces.ShortPeriodTerms
-
Computes the coefficients involved in the contributions.
- getCoefficientsKeyPrefix() - Method in interface org.orekit.propagation.semianalytical.dsst.forces.ShortPeriodTerms
-
Get the prefix for short period coefficients keys.
- getCombinedProvider(TransformProvider, TransformProvider) - Static method in class org.orekit.frames.TransformProviderUtils
-
Combine two transform providers.
- getComment() - Method in class org.orekit.files.ccsds.ODMMetaData
-
Get the meta-data comment.
- getComment() - Method in class org.orekit.files.ccsds.OPMFile.Maneuver
-
Get the maneuvers data comment, each string in the list corresponds to one line of comment.
- getComment() - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData
-
Get the meta-data comment.
- getComponents(int) - Method in class org.orekit.time.AbsoluteDate
-
Split the instance into date/time components for a local time.
- getComponents(int) - 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.AbsoluteDate
-
Split the instance into date/time components for a time zone.
- getComponents(TimeZone) - Method in class org.orekit.time.FieldAbsoluteDate
-
Split the instance into date/time components for a time zone.
- getComponents(TimeScale) - Method in class org.orekit.time.AbsoluteDate
-
Split the instance into date/time components.
- getComponents(TimeScale) - Method in class org.orekit.time.FieldAbsoluteDate
-
Split the instance into date/time components.
- 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.
- getConstantProvider(boolean, int, int) - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
-
Get a time-independent provider for read spherical harmonics coefficients.
- 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.
- getConventions() - Method in class org.orekit.files.ccsds.ODMFile
-
Get IERS conventions.
- getConventions() - Method in class org.orekit.files.ccsds.ODMParser
-
Get IERS conventions.
- getConventions() - Method in class org.orekit.files.ccsds.TDMParser
-
Get IERS conventions.
- getConventions() - Method in class org.orekit.frames.EOPHistory
-
Get the IERS conventions to which these EOP apply.
- getConverter(ITRFVersion, ITRFVersion) - Static method in enum org.orekit.frames.ITRFVersion
-
Find a converter between specified ITRF frames.
- getCoordinates() - Method in class org.orekit.files.ccsds.OEMFile.EphemeridesBlock
-
- getCoordinates() - Method in interface org.orekit.files.general.EphemerisFile.EphemerisSegment
-
Get the coordinates for this ephemeris segment.
- getCoordinates() - Method in class org.orekit.files.general.OrekitEphemerisFile.OrekitEphemerisSegment
-
- getCoordinates() - Method in class org.orekit.files.sp3.SP3File.SP3Ephemeris
-
- getCoordinates(SpacecraftState, int, DSFactory) - Static method in class org.orekit.estimation.measurements.AbstractMeasurement
-
Get Cartesian coordinates as derivatives.
- getCoordinateSystem() - Method in class org.orekit.files.sp3.SP3File
-
Returns the coordinate system of the entries in this orbit file.
- getCorrectedMeasurement() - Method in interface org.orekit.estimation.sequential.KalmanEstimation
-
Get the estimated measurement.
- getCorrectedMeasurement() - Method in class org.orekit.estimation.sequential.Model
-
Get the estimated measurement.
- getCorrectedSpacecraftStates() - Method in interface org.orekit.estimation.sequential.KalmanEstimation
-
Get the corrected spacecraft states.
- getCorrectedSpacecraftStates() - Method in class org.orekit.estimation.sequential.Model
-
Get the corrected spacecraft states.
- getCorrection() - Method in class org.orekit.gnss.RinexLoader.Parser.PhaseShiftCorrection
-
Get the Phase Shift Corrections.
- getCorrection() - Method in class org.orekit.gnss.RinexLoader.Parser.ScaleFactorCorrection
-
Get the Scale Factor.
- getCorrectionAngle1() - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData
-
Getter for the correctionAngle1.
- getCorrectionAngle2() - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData
-
Getter for the correctionAngle2.
- getCorrectionDoppler() - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData
-
Getter for the correctionDoppler.
- getCorrectionRange() - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData
-
Getter for the correctionRange.
- getCorrectionReceive() - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData
-
Getter for the correctionReceive.
- getCorrectionsApplied() - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData
-
Getter for the correctionApplied.
- getCorrectionTransmit() - Method in class org.orekit.files.ccsds.TDMFile.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.
- getCovariance() - Method in class org.orekit.estimation.sequential.MeasurementDecorator
- getCovarianceComment() - Method in class org.orekit.files.ccsds.OGMFile
-
Get the comment for covariance.
- getCovarianceMatrices() - Method in class org.orekit.files.ccsds.OEMFile.EphemeridesBlock
-
Get the list 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.OGMFile
-
Get the Position/Velocity covariance matrix.
- getCovRefFrame() - Method in class org.orekit.files.ccsds.OGMFile
-
Get coordinate system for covariance matrix, for absolute frames.
- getCovRefLofType() - Method in class org.orekit.files.ccsds.OGMFile
-
Get coordinate system for covariance matrix, for Local Orbital Frames.
- getCrc() - Method in class org.orekit.gnss.GPSAlmanac
-
- getCrc() - Method in interface org.orekit.propagation.analytical.gnss.GPSOrbitalElements
-
Gets the Amplitude of the Cosine Harmonic Correction Term to the Orbit Radius.
- getCreationDate() - Method in class org.orekit.files.ccsds.ODMFile
-
Get the file creation date and time in UTC.
- getCreationDate() - Method in class org.orekit.files.ccsds.TDMFile
-
Get the file creation date and time in UTC.
- getCrs() - Method in class org.orekit.gnss.GPSAlmanac
-
- getCrs() - Method in interface org.orekit.propagation.analytical.gnss.GPSOrbitalElements
-
Gets the Amplitude of the Sine Harmonic Correction Term to the Orbit Radius.
- getCuc() - Method in class org.orekit.gnss.GPSAlmanac
-
- getCuc() - Method in interface org.orekit.propagation.analytical.gnss.GPSOrbitalElements
-
Gets the Amplitude of the Cosine Harmonic Correction Term to the Argument of Latitude.
- 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.Model
-
Get the current date.
- 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.Model
-
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.
- getCurrentWeight() - Method in class org.orekit.estimation.measurements.EstimatedMeasurement
-
- getCus() - Method in class org.orekit.gnss.GPSAlmanac
-
- getCus() - Method in interface org.orekit.propagation.analytical.gnss.GPSOrbitalElements
-
Gets the Amplitude of the Sine Harmonic Correction Term to the Argument of Latitude.
- 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.forces.drag.atmosphere.data.MarshallSolarActivityFutureEstimation
-
Get the value of the daily F10.7 solar flux for previous day.
- getDailyFlux(AbsoluteDate) - Method in interface org.orekit.forces.drag.atmosphere.NRLMSISE00InputParameters
-
Get the value of the daily F10.7 solar flux for previous day.
- getData() - Method in class org.orekit.utils.TimeSpanMap.Span
-
Get the data valid during this time span.
- getDataQuality() - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData
-
Getter for the dataQuality.
- getDataUsed() - Method in class org.orekit.files.sp3.SP3File
-
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.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.DOP
-
Gets the calculation date of the DOP.
- getDate() - Method in class org.orekit.gnss.GPSAlmanac
-
- getDate() - Method in class org.orekit.gnss.ObservationDataSet
-
Get the date.
- 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.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.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.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.GPSDate
-
Get the date.
- getDate() - Method in interface org.orekit.time.TimeStamped
-
Get the 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.
- getDay() - Method in class org.orekit.time.DateComponents
-
Get the day.
- getDayFraction() - Method in class org.orekit.files.sp3.SP3File
-
Returns the day fraction for this SP3 file.
- 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.
- getDcjDh(int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.CjSjCoefficient
-
Get the dCj / dh coefficient.
- getDcjDk(int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.CjSjCoefficient
-
Get the dCj / dk coefficient.
- getDdEps() - Method in class org.orekit.frames.EOPEntry
-
Get the correction for nutation in obliquity δΔε.
- 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 degrees.
- getDecreasingTimeShift() - Method in class org.orekit.propagation.events.EventShifter
-
Get the decreasing events time shift.
- getDefaultModel() - Static method in class org.orekit.models.earth.FixedTroposphericDelay
-
Returns the default model, loading delay values from the file
"tropospheric-delay.txt".
- getDelaunayMultipliers() - Method in class org.orekit.models.earth.displacement.Tide
-
Get the multipliers for Delaunay arguments (l, l', F, D, Ω).
- getDeltaMass() - Method in class org.orekit.files.ccsds.OPMFile.Maneuver
-
Get mass change during maneuver (value is < 0).
- getDeltaVSat() - Method in class org.orekit.forces.maneuvers.ImpulseManeuver
-
Get the velocity increment in satellite frame.
- getDensity(double, double, double, double, double, double, double, double, double, double, double, double, double, double, double) - Method in class org.orekit.forces.drag.atmosphere.JB2008
-
Get the local density with initial entries.
- getDensity(int) - Method in class org.orekit.forces.drag.atmosphere.NRLMSISE00.FieldOutput
-
Get one of the stored densities.
- getDensity(int, double, double, double, double, double, double, double, double) - Method in class org.orekit.forces.drag.atmosphere.DTM2000
-
Get the local density with initial entries.
- getDensity(int, T, T, T, T, double, double, double, double) - Method in class org.orekit.forces.drag.atmosphere.DTM2000
-
Get the local density with initial entries.
- getDensity(Vector3D, FieldVector3D<T>) - Method in class org.orekit.forces.drag.atmosphere.HarrisPriester
-
Get the local density.
- getDensity(Vector3D, Vector3D) - Method in class org.orekit.forces.drag.atmosphere.HarrisPriester
-
Get the local density.
- getDensity(AbsoluteDate, Vector3D, Frame) - Method in interface org.orekit.forces.drag.atmosphere.Atmosphere
-
Get the local density.
- getDensity(AbsoluteDate, Vector3D, Frame) - Method in class org.orekit.forces.drag.atmosphere.DTM2000
-
Get the local density.
- getDensity(AbsoluteDate, Vector3D, Frame) - Method in class org.orekit.forces.drag.atmosphere.HarrisPriester
-
Get the local density at some position.
- getDensity(AbsoluteDate, Vector3D, Frame) - Method in class org.orekit.forces.drag.atmosphere.JB2008
-
Get the local density.
- getDensity(AbsoluteDate, Vector3D, Frame) - Method in class org.orekit.forces.drag.atmosphere.NRLMSISE00
-
Get the local density.
- getDensity(AbsoluteDate, Vector3D, Frame) - Method in class org.orekit.forces.drag.atmosphere.SimpleExponentialAtmosphere
-
Get the local density.
- getDensity(FieldAbsoluteDate<T>, FieldVector3D<T>, Frame) - Method in interface org.orekit.forces.drag.atmosphere.Atmosphere
-
Get the local density.
- getDensity(FieldAbsoluteDate<T>, FieldVector3D<T>, Frame) - Method in class org.orekit.forces.drag.atmosphere.DTM2000
-
Get the local density.
- getDensity(FieldAbsoluteDate<T>, FieldVector3D<T>, Frame) - Method in class org.orekit.forces.drag.atmosphere.HarrisPriester
-
Get the local density at some position.
- getDensity(FieldAbsoluteDate<T>, FieldVector3D<T>, Frame) - Method in class org.orekit.forces.drag.atmosphere.JB2008
-
Get the local density.
- getDensity(FieldAbsoluteDate<T>, FieldVector3D<T>, Frame) - Method in class org.orekit.forces.drag.atmosphere.NRLMSISE00
-
Get the local density.
- getDensity(FieldAbsoluteDate<T>, FieldVector3D<T>, Frame) - Method in class org.orekit.forces.drag.atmosphere.SimpleExponentialAtmosphere
-
- getDensity(T, T, T, T, T, T, double, double, double, double, double, double, double, double, double) - Method in class org.orekit.forces.drag.atmosphere.JB2008
-
Get the local density with initial entries.
- getDepth() - Method in class org.orekit.frames.Frame
-
Get the depth of the frame.
- 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.
- getDerivative(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GammaMnsFunction
-
Get Γ function derivative.
- getDerivativesDrivers() - Method in class org.orekit.estimation.measurements.EstimatedMeasurement
-
Get all the drivers with set derivatives.
- 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.handlers.RecordAndContinue.Event
-
Get the detector.
- 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.GHIJjsPolynomials
-
Get the dGjs / dβ 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.GHIJjsPolynomials
-
Get the dGjs / dk 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.GHmsjPolynomials
-
Get the dGmsj / dβ 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.GHmsjPolynomials
-
Get the dGmsj / dk 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.GHIJjsPolynomials
-
Get the dHjs / dβ 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.GHIJjsPolynomials
-
Get the dHjs / dk 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.GHmsjPolynomials
-
Get the dHmsj / dβ 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.GHmsjPolynomials
-
Get the dHmsj / dk 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.GHIJjsPolynomials
-
Get the dIjs / dβ 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.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.
- getDirection() - Method in class org.orekit.forces.maneuvers.ConstantThrustManeuver
-
Get the direction.
- 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.GHIJjsPolynomials
-
Get the dJjs / dα 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.GHIJjsPolynomials
-
Get the dJjs / dh 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.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).
- 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.
- getDragArea() - Method in class org.orekit.files.ccsds.OGMFile
-
Get the drag area.
- getDragCoeff() - Method in class org.orekit.files.ccsds.OGMFile
-
Get the drag coefficient.
- 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.
- getDrivers() - Method in class org.orekit.utils.ParameterDriversList
-
Get delegating drivers for all parameters.
- getDrivers(double, Orbit, PositionAngle) - Method in enum org.orekit.orbits.OrbitType
-
Get parameters drivers initialized from a reference orbit.
- getDsjDh(int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.CjSjCoefficient
-
Get the dSj / dh coefficient.
- getDsjDk(int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.CjSjCoefficient
-
Get the dSj / dk coefficient.
- getDSTDTC(AbsoluteDate) - Method in interface org.orekit.forces.drag.atmosphere.JB2008InputParameters
-
Get the temperature change computed from Dst index.
- getDuration() - Method in class org.orekit.files.ccsds.OPMFile.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).
- getDV() - Method in class org.orekit.files.ccsds.OPMFile.Maneuver
-
Get velocity increment.
- 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.OGMFile
-
Get the orbit eccentricity.
- getE() - Method in class org.orekit.gnss.GPSAlmanac
-
- 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 interface org.orekit.propagation.analytical.gnss.GPSOrbitalElements
-
Gets 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.
- getEarliest() - Method in class org.orekit.utils.GenericTimeStampedCache
-
Get the earliest cached entry.
- getEarliest() - Method in class org.orekit.utils.ImmutableTimeStampedCache
-
- getEarliest() - Method in interface org.orekit.utils.TimeStampedCache
-
Get the earliest entry in this cache.
- getEarth() - Static method in class org.orekit.bodies.CelestialBodyFactory
-
Get the Earth singleton body.
- getEarthMoonBarycenter() - Static method in class org.orekit.bodies.CelestialBodyFactory
-
Get the Earth-Moon barycenter singleton bodies pair.
- getEarthOrientationAngleFunction(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.
- 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.gnss.antenna.FrequencyPattern
-
Get the phase center eccentricities.
- getEccentricities() - Method in class org.orekit.gnss.RinexHeader
-
Get the eccentricities of antenna center.
- getEccentricities(Frequency) - Method in class org.orekit.gnss.antenna.Antenna
-
Get the phase center eccentricities.
- getECEF() - Method in class org.orekit.propagation.analytical.gnss.GPSPropagator
-
- getECI() - Method in class org.orekit.propagation.analytical.gnss.GPSPropagator
-
Gets the Earth Centered Inertial frame used to propagate the orbit.
- 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.TLE
-
Get the element number.
- getElementSetNumber() - Method in class org.orekit.files.ccsds.OMMFile
-
Get the element set number for this satellite.
- getElevation(double) - Method in class org.orekit.utils.ElevationMask
-
Get the interpolated elevation for a given azimuth according to the mask.
- 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(Vector3D, Frame, AbsoluteDate) - 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.
- 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.
- 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() - Static method in class org.orekit.frames.FramesFactory
-
Get the unique EME2000 frame.
- 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() - Method in class org.orekit.forces.maneuvers.ConstantThrustManeuver
-
Get the end date.
- getEndDate() - Method in class org.orekit.frames.EOPHistory
-
Get the date of the last available Earth Orientation Parameters.
- 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.
- getEOPHistory() - Method in interface org.orekit.frames.EOPBasedTransformProvider
-
Get the EOP history.
- getEOPHistory() - Method in class org.orekit.frames.GTODProvider
-
Get the EOP history.
- getEOPHistory() - Method in class org.orekit.time.UT1Scale
-
Get the EOP history.
- getEOPHistory(IERSConventions, boolean) - Static method in class org.orekit.frames.FramesFactory
-
Get Earth Orientation Parameters history.
- getEOPTidalCorrection() - Method in enum org.orekit.utils.IERSConventions
-
Get the function computing tidal corrections for Earth Orientation Parameters.
- getEphemeridesBlocks() - Method in class org.orekit.files.ccsds.OEMFile
-
Get the list of ephemerides blocks as an unmodifiable list.
- getEphemeridesDataLinesComment() - Method in class org.orekit.files.ccsds.OEMFile.EphemeridesBlock
-
Get the ephemerides data lines comment.
- getEphemerisType() - Method in class org.orekit.files.ccsds.OMMFile
-
Get the ephemeris type.
- getEphemerisType() - Method in class org.orekit.propagation.analytical.tle.TLE
-
Get the type of ephemeris.
- getEpoch() - Method in class org.orekit.files.ccsds.OEMFile.CovarianceMatrix
-
Get the epoch relative to the covariance matrix.
- getEpoch() - Method in class org.orekit.files.ccsds.OGMFile
-
Get epoch of state vector, Keplerian elements and covariance matrix data.
- getEpoch() - Method in class org.orekit.files.ccsds.TDMFile.Observation
-
Getter for the epoch.
- getEpoch() - Method in class org.orekit.files.sp3.SP3File
-
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.models.earth.GeoMagneticField
-
Returns the epoch for this magnetic field model.
- getEpochComment() - Method in class org.orekit.files.ccsds.OGMFile
-
Get the comment for epoch.
- getEpochIgnition() - Method in class org.orekit.files.ccsds.OPMFile.Maneuver
-
Get epoch ignition.
- getEpochInterval() - Method in class org.orekit.files.sp3.SP3File
-
Returns the time interval between epochs (in seconds).
- getEquatorialRadius() - Method in class org.orekit.bodies.OneAxisEllipsoid
-
Get the equatorial radius of the body.
- 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.Model
-
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.
- 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.Model
-
Get the list of estimated measurements 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.Model
-
Get the list of estimated orbital 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.Model
-
Get the list of estimated propagation parameters.
- getEstimatedPropagators() - Method in class org.orekit.estimation.sequential.Model
-
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.
- getEvaluations() - Method in class org.orekit.propagation.conversion.AbstractPropagatorConverter
-
Get the number of objective function evaluations.
- 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.RecordAndContinue
-
Get the events passed to this handler.
- getEventsDetectors() - Method in class org.orekit.forces.AbstractParametricAcceleration
-
Get the discrete events related to the model.
- getEventsDetectors() - Method in class org.orekit.forces.drag.DragForce
-
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.HolmesFeatherstoneAttractionModel
-
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.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.maneuvers.ConstantThrustManeuver
-
Get the discrete events related to the model.
- getEventsDetectors() - Method in class org.orekit.forces.radiation.SolarRadiationPressure
-
Get the discrete events related to the model.
- getEventsDetectors() - Method in class org.orekit.propagation.AbstractPropagator
-
Get all the events detectors that have been added.
- 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 class org.orekit.propagation.FieldAbstractPropagator
-
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 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.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.Model
- getException() - Method in exception org.orekit.errors.OrekitExceptionWrapper
-
Deprecated.
Get the wrapped exception.
- 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.forces.drag.atmosphere.JB2008InputParameters
-
Get the value of the instantaneous solar flux index
(1e-22*Watt/(m²*Hertz)).
- getF10B(AbsoluteDate) - Method in interface org.orekit.forces.drag.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.
- 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() - Method in class org.orekit.propagation.FieldAbstractPropagator
-
Field getter.
- getField() - Method in class org.orekit.time.FieldAbsoluteDate
-
Get the field.
- getField(GeoMagneticFieldFactory.FieldModel, double) - Static method in class org.orekit.models.earth.GeoMagneticFieldFactory
-
- getFieldDate() - Method in class org.orekit.frames.FieldTransform
-
Get the date.
- getFieldEventsDetectors(Field<T>) - Method in class org.orekit.forces.AbstractParametricAcceleration
-
Get the discrete events related to the model.
- getFieldEventsDetectors(Field<T>) - Method in class org.orekit.forces.drag.DragForce
-
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.HolmesFeatherstoneAttractionModel
-
- 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.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.maneuvers.ConstantThrustManeuver
-
Get the discrete events related to the model.
- getFieldEventsDetectors(Field<T>) - Method in class org.orekit.forces.radiation.SolarRadiationPressure
-
Get the discrete events related to the model.
- getFieldOfView() - Method in class org.orekit.propagation.events.FieldOfViewDetector
-
Get the Field Of View.
- getFieldOfView() - Method in class org.orekit.propagation.events.FootprintOverlapDetector
-
Get the Field Of View.
- getFieldOfView() - Method in class org.orekit.propagation.events.GroundFieldOfViewDetector
-
Get the Field Of View.
- getFieldVector() - Method in class org.orekit.models.earth.GeoMagneticElements
-
Returns the magnetic field vector in nTesla.
- getFiftiesEpoch(Field<T>) - Static method in class org.orekit.time.FieldAbsoluteDate
-
Reference epoch for 1950 dates: 1950-01-01T00:00:00 Terrestrial Time.
- getFileDate(AbsoluteDate) - Method in class org.orekit.forces.drag.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.TDMParser
-
Get file format.
- 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.
- getFirst() - Method in class org.orekit.propagation.analytical.tle.TLESeries
-
Deprecated.
Get the first TLE.
- getFirstDate() - Method in class org.orekit.propagation.analytical.tle.TLESeries
-
Deprecated.
Get the start date of the series.
- getFirstKnownLeapSecond() - Method in class org.orekit.time.UTCScale
-
Get the date of the first known leap second.
- getFittedParameters() - Method in class org.orekit.utils.SecularAndHarmonic
-
Get a copy of the last fitted parameters.
- getFixedStepSize() - Method in class org.orekit.propagation.AbstractPropagator
-
Get the fixed step size.
- getFixedStepSize() - Method in class org.orekit.propagation.FieldAbstractPropagator
-
Get the fixed step size.
- 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.
- getForceModels() - Method in class org.orekit.propagation.numerical.FieldNumericalPropagator
-
- getFormatVersion() - Method in class org.orekit.files.ccsds.ODMFile
-
Get the CCSDS ODM (OPM, OMM or OEM) format version.
- getFormatVersion() - Method in class org.orekit.files.ccsds.TDMFile
-
Get the CCSDS TDM format version.
- 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() - Method in class org.orekit.files.ccsds.ODMMetaData
-
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.OEMFile.CovarianceMatrix
-
Get coordinate system for covariance matrix, for absolute frames.
- getFrame() - Method in class org.orekit.files.ccsds.OEMFile.EphemeridesBlock
-
- 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
-
- getFrame() - Method in class org.orekit.files.sp3.SP3File.SP3Ephemeris
-
- getFrame() - Method in interface org.orekit.forces.drag.atmosphere.Atmosphere
-
Get the frame of the central body.
- getFrame() - Method in class org.orekit.forces.drag.atmosphere.DTM2000
-
Get the frame of the central body.
- getFrame() - Method in class org.orekit.forces.drag.atmosphere.HarrisPriester
-
Get the frame of the central body.
- getFrame() - Method in class org.orekit.forces.drag.atmosphere.JB2008
-
Get the frame of the central body.
- getFrame() - Method in class org.orekit.forces.drag.atmosphere.NRLMSISE00
-
Get the frame of the central body.
- getFrame() - Method in class org.orekit.forces.drag.atmosphere.SimpleExponentialAtmosphere
-
Get the frame of the central body.
- getFrame() - Method in class org.orekit.frames.OrphanFrame
-
Get the associated
frame
.
- 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.GPSPropagator
-
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 inertial 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.SpacecraftState
-
Get the inertial frame.
- getFrame(Predefined) - Static method in class org.orekit.frames.FramesFactory
-
Get one of the predefined frames.
- getFrame(IERSConventions, boolean) - Method in enum org.orekit.files.ccsds.CCSDSFrame
-
Get the frame corresponding to the CCSDS constant.
- getFrameCenterString() - Method in class org.orekit.files.ccsds.OEMFile.EphemeridesBlock
-
- getFrameCenterString() - Method in interface org.orekit.files.general.EphemerisFile.EphemerisSegment
-
Get the name of the center of the coordinate system the ephemeris is provided
in.
- getFrameCenterString() - Method in class org.orekit.files.general.OrekitEphemerisFile.OrekitEphemerisSegment
-
- getFrameCenterString() - Method in class org.orekit.files.sp3.SP3File.SP3Ephemeris
-
- getFrameEpoch() - Method in class org.orekit.files.ccsds.ODMMetaData
-
Get epoch of reference frame, if not intrinsic to the definition of the
reference frame.
- getFrameEpochString() - Method in class org.orekit.files.ccsds.ODMMetaData
-
Get epoch of reference frame, if not intrinsic to the definition of the
reference frame.
- getFrameString() - Method in class org.orekit.files.ccsds.ODMMetaData
-
Get the reference frame specifier as it appeared in the file.
- getFrameString() - Method in class org.orekit.files.ccsds.OEMFile.EphemeridesBlock
-
- getFrameString() - Method in interface org.orekit.files.general.EphemerisFile.EphemerisSegment
-
Get the defining frame for this ephemeris segment.
- getFrameString() - Method in class org.orekit.files.general.OrekitEphemerisFile.OrekitEphemerisSegment
-
- getFrameString() - Method in class org.orekit.files.sp3.SP3File.SP3Ephemeris
-
- getFreeStateParameters() - Method in class org.orekit.estimation.measurements.modifiers.TroposphericDSConverter
-
Get the number of free state parameters.
- getFreqOffset() - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData
-
Getter for the freqOffset.
- getFrequency(SatelliteSystem) - Method in enum org.orekit.gnss.ObservationType
-
Get the frequency for a specified satellite system.
- 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.
- getFunction() - Method in class org.orekit.propagation.events.FunctionalDetector
-
Get the switching function.
- getFutureInfinity(Field<T>) - Static method in class org.orekit.time.FieldAbsoluteDate
-
Dummy date at infinity in the future direction.
- getGalileoEpoch(Field<T>) - Static method in class org.orekit.time.FieldAbsoluteDate
-
Reference epoch for Galileo System Time: 1999-08-22T00:00:00 UTC.
- 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.utilities.AuxiliaryElements
-
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.
- getGASTFunction(TimeScale, EOPHistory) - Method in enum org.orekit.utils.IERSConventions
-
Get the function computing Greenwich apparent sidereal time, in radians.
- getGCRF() - Static method in class org.orekit.frames.FramesFactory
-
Get the unique GCRF frame.
- getGdop() - Method in class org.orekit.gnss.DOP
-
Gets the geometric dilution of precision.
- getGenerateCalls() - Method in class org.orekit.utils.GenericTimeStampedCache
-
Get the number of calls to the generate method.
- getGeneratedEphemeris() - Method in class org.orekit.propagation.AbstractPropagator
-
Get the ephemeris generated during propagation.
- getGeneratedEphemeris() - Method in class org.orekit.propagation.analytical.AbstractAnalyticalPropagator
-
Get the ephemeris generated during propagation.
- getGeneratedEphemeris() - Method in class org.orekit.propagation.analytical.FieldAbstractAnalyticalPropagator
-
Get the ephemeris generated during propagation.
- getGeneratedEphemeris() - Method in class org.orekit.propagation.FieldAbstractPropagator
-
Get the ephemeris generated during propagation.
- getGeneratedEphemeris() - Method in interface org.orekit.propagation.FieldPropagator
-
Get the ephemeris generated during propagation.
- getGeneratedEphemeris() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
-
Get the ephemeris generated during propagation.
- getGeneratedEphemeris() - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator
-
Get the ephemeris generated during propagation.
- getGeneratedEphemeris() - Method in interface org.orekit.propagation.Propagator
-
Get the ephemeris generated during propagation.
- getGenerator() - Method in class org.orekit.utils.GenericTimeStampedCache
-
Get the generator.
- getGetNeighborsCalls() - Method in class org.orekit.utils.GenericTimeStampedCache
-
- getGFunction() - Method in class org.orekit.propagation.events.FunctionalDetector
-
- getGjs(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
-
Get the Gjs coefficient.
- getGLONASS() - Static method in class org.orekit.time.TimeScalesFactory
-
Get the GLObal NAvigation Satellite System time scale.
- getGM() - Method in interface org.orekit.bodies.CelestialBody
-
Get the attraction coefficient of the body.
- getGM() - Method in class org.orekit.models.earth.ReferenceEllipsoid
-
Gets the gravitational parameter that is part of the definition of the
reference ellipsoid.
- getGmsj(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHmsjPolynomials
-
Get the Gmsj coefficient.
- 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.
- getGMSTRateFunction(TimeScale) - Method in enum org.orekit.utils.IERSConventions
-
Get the function computing Greenwich mean sidereal time rate, in radians per second.
- getGnssNb() - Method in class org.orekit.gnss.DOP
-
Gets the number of GNSS satellites taken into account for DOP computation.
- getGPS() - Static method in class org.orekit.time.TimeScalesFactory
-
Get the Global Positioning System scale.
- getGPSEpoch(Field<T>) - Static method in class org.orekit.time.FieldAbsoluteDate
-
Reference epoch for GPS weeks: 1980-01-06T00:00:00 GPS time.
- getGPSOrbitalElements() - Method in class org.orekit.propagation.analytical.gnss.GPSPropagator
-
Gets the underlying GPS orbital elements.
- getGpsWeek() - Method in class org.orekit.files.sp3.SP3File
-
Returns the GPS week as contained in the SP3 file.
- 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(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() - Static method in class org.orekit.time.TimeScalesFactory
-
Get the Galileo System Time scale.
- 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.
- getHalfAperture() - Method in class org.orekit.propagation.events.CircularFieldOfViewDetector
-
Get FOV half aperture angle.
- getHandler() - Method in class org.orekit.propagation.events.AbstractDetector
-
Get the handler.
- getHandler() - Method in class org.orekit.propagation.events.FieldAbstractDetector
-
Get the handler.
- getHarmonicAmplitude() - Method in class org.orekit.utils.SecularAndHarmonic
-
Get an upper bound of the fitted harmonic amplitude.
- getHasCreatableBody() - Method in class org.orekit.files.ccsds.ODMMetaData
-
Get boolean testing whether the body corresponding to the centerName
attribute can be created through the
CelestialBodyFactory
.
- getHasManeuver() - Method in class org.orekit.files.ccsds.OPMFile
-
Get boolean testing whether the OPM contains at least one maneuver.
- getHasRefFrameEpoch() - Method in class org.orekit.files.ccsds.OEMFile.EphemeridesBlock
-
Get boolean testing whether the reference frame has an epoch associated to it.
- getHdop() - Method in class org.orekit.gnss.DOP
-
Gets the horizontal dilution of precision.
- getHeader() - Method in class org.orekit.gnss.ObservationDataSet
-
Get the Rinex header associated with this data set.
- getHeaderComment() - Method in class org.orekit.files.ccsds.ODMFile
-
Get the header comment.
- getHeaderComment() - Method in class org.orekit.files.ccsds.TDMFile
-
Get the header comment.
- getHealth() - Method in class org.orekit.gnss.GPSAlmanac
-
Gets the Health status.
- getHjs(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
-
Get the Hjs 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).
- getHour() - Method in class org.orekit.time.TimeComponents
-
Get the hour 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.
- 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.OGMFile
-
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.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.gnss.GPSAlmanac
-
- getI0() - Method in interface org.orekit.propagation.analytical.gnss.GPSOrbitalElements
-
Gets the Inclination Angle at Reference Time.
- getICRF() - Static method in class org.orekit.frames.FramesFactory
-
Get the unique ICRF frame.
- getId() - Method in class org.orekit.files.ccsds.OEMFile.OemSatelliteEphemeris
-
- getId() - Method in interface org.orekit.files.general.EphemerisFile.SatelliteEphemeris
-
Get the satellite ID.
- getId() - Method in class org.orekit.files.general.OrekitEphemerisFile.OrekitSatelliteEphemeris
-
- getId() - Method in class org.orekit.files.sp3.SP3File.SP3Ephemeris
-
- 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.gnss.GPSAlmanac
-
- 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 interface org.orekit.propagation.analytical.gnss.GPSOrbitalElements
-
Gets the Rate of Inclination Angle.
- getIGRF(double) - Static method in class org.orekit.models.earth.GeoMagneticFieldFactory
-
Get the IGRF model for the given year.
- getIjs(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
-
Get the Ijs coefficient.
- 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 degrees.
- getIncreasingTimeShift() - Method in class org.orekit.propagation.events.EventShifter
-
Get the increasing events time shift.
- getInertialDV() - Method in class org.orekit.forces.maneuvers.SmallManeuverAnalyticalModel
-
Get the inertial velocity increment of the maneuver.
- 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.
- 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.
- 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.
- 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.
- 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.
- getInnovation(MeasurementDecorator, NonLinearEvolution, RealMatrix) - Method in class org.orekit.estimation.sequential.Model
- getInstance() - Static method in class org.orekit.data.DataProvidersManager
-
Get the unique instance.
- getInstantFlux(AbsoluteDate) - Method in class org.orekit.forces.drag.atmosphere.data.MarshallSolarActivityFutureEstimation
-
Get the value of the instantaneous solar flux.
- getInstantFlux(AbsoluteDate) - Method in interface org.orekit.forces.drag.atmosphere.DTM2000InputParameters
-
Get the value of the instantaneous solar flux.
- getIntegrationInterval() - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData
-
Getter for the integrationInterval.
- getIntegrationRef() - Method in class org.orekit.files.ccsds.TDMFile.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.NumericalPropagatorBuilder
-
Get the integrator builder.
- getInterpolatedPoint(double, double) - Method in class org.orekit.models.earth.tessellation.Tile
-
Get an interpolated point inside the tile.
- getInterpolatedState(AbsoluteDate) - Method in interface org.orekit.propagation.sampling.OrekitStepInterpolator
-
Get the state at interpolated date.
- getInterpolatedState(FieldAbsoluteDate<T>) - Method in interface org.orekit.propagation.sampling.FieldOrekitStepInterpolator
-
Get the state at interpolated date.
- getInterpolationDegree() - Method in class org.orekit.files.ccsds.OEMFile.EphemeridesBlock
-
Get the interpolation degree.
- getInterpolationMethod() - Method in class org.orekit.files.ccsds.OEMFile.EphemeridesBlock
-
Get the interpolation method to be used.
- getInterpolationSamples() - Method in class org.orekit.files.ccsds.OEMFile.EphemeridesBlock
-
- 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.OrekitEphemerisFile.OrekitEphemerisSegment
-
- getInterpolationSamples() - Method in class org.orekit.files.sp3.SP3File.SP3Ephemeris
-
- 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(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(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.
- 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(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(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.
- getInterval() - Method in class org.orekit.gnss.RinexHeader
-
Get the observation interval in seconds.
- 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.
- getIODC() - Method in interface org.orekit.propagation.analytical.gnss.GPSOrbitalElements
-
Gets the Issue Of Data Clock (IODC).
- getIODE() - Method in interface org.orekit.propagation.analytical.gnss.GPSOrbitalElements
-
Gets the Issue Of Data Ephemeris (IODE).
- getIRNSS() - Static method in class org.orekit.time.TimeScalesFactory
-
Get the Indian Regional Navigation Satellite System time scale.
- getIsp() - Method in class org.orekit.forces.maneuvers.ImpulseManeuver
-
Get the specific impulse.
- getISP() - Method in class org.orekit.forces.maneuvers.ConstantThrustManeuver
-
Get the specific impulse.
- getIteration() - Method in class org.orekit.estimation.measurements.EstimatedMeasurement
-
Get the iteration number.
- getIterationsCount() - Method in class org.orekit.estimation.leastsquares.BatchLSEstimator
-
Get the number of iterations used for last estimation.
- getITRF(ITRFVersion, IERSConventions, boolean) - Static method in class org.orekit.frames.FramesFactory
-
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.
- 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() - Method in class org.orekit.frames.VersionedITRF
-
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(AbsoluteDate) - Method in class org.orekit.frames.EOPHistory
-
Get the ITRF version.
- getJ2000Day() - Method in class org.orekit.time.DateComponents
-
Get the day number with respect to J2000 epoch.
- getJ2000Epoch(Field<T>) - Static method in class org.orekit.time.FieldAbsoluteDate
-
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, double[][]) - Method in class org.orekit.frames.Transform
-
- getJacobian(CartesianDerivativesFilter, T[][]) - Method in class org.orekit.frames.FieldTransform
-
- getJacobianWrtCartesian(PositionAngle, double[][]) - Method in class org.orekit.orbits.Orbit
-
Compute the Jacobian of the orbital parameters with respect to the Cartesian parameters.
- getJacobianWrtCartesian(PositionAngle, T[][]) - Method in class org.orekit.orbits.FieldOrbit
-
Compute the Jacobian of the orbital parameters with respect to the Cartesian parameters.
- getJacobianWrtParameters(PositionAngle, double[][]) - Method in class org.orekit.orbits.Orbit
-
Compute the Jacobian of the Cartesian parameters with respect to the orbital parameters.
- getJacobianWrtParameters(PositionAngle, T[][]) - Method in class org.orekit.orbits.FieldOrbit
-
Compute the Jacobian of the Cartesian parameters with respect to the orbital parameters.
- getJavaEpoch(Field<T>) - Static method in class org.orekit.time.FieldAbsoluteDate
-
Java Reference epoch: 1970-01-01T00:00:00 Universal Time Coordinate.
- 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.SP3File
-
Returns the julian day for this SP3 file.
- getJulianEpoch(Field<T>) - Static method in class org.orekit.time.FieldAbsoluteDate
-
Reference epoch for julian dates: -4712-01-01T12:00:00 Terrestrial Time.
- getJupiter() - Static method in class org.orekit.bodies.CelestialBodyFactory
-
Get the Jupiter singleton body.
- getK() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
-
Get the x component of eccentricity vector.
- getKeplerianElementsComment() - Method in class org.orekit.files.ccsds.OGMFile
-
Get the comment for Keplerian elements.
- 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.SpacecraftState
-
Get the Keplerian period.
- getKey() - Method in enum org.orekit.gnss.SatelliteSystem
-
Get the key for the system.
- getKeyword() - Method in class org.orekit.files.ccsds.TDMFile.Observation
-
Getter for the keyword.
- 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.
- getLast() - Method in class org.orekit.propagation.analytical.tle.TLESeries
-
Deprecated.
Get the last TLE.
- getLastDate() - Method in class org.orekit.propagation.analytical.tle.TLESeries
-
Deprecated.
Get the last date of the series.
- 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.
- getLatest() - Method in class org.orekit.utils.GenericTimeStampedCache
-
Get the latest cached entry.
- getLatest() - Method in class org.orekit.utils.ImmutableTimeStampedCache
-
- 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.propagation.events.LatitudeCrossingDetector
-
Get the fixed latitude to be crossed (radians).
- getLaunchNumber() - Method in class org.orekit.files.ccsds.ODMMetaData
-
Get the launch number.
- getLaunchNumber() - Method in class org.orekit.files.ccsds.ODMParser
-
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.ODMMetaData
-
Get the piece of launch.
- getLaunchPiece() - Method in class org.orekit.files.ccsds.ODMParser
-
Get the piece of launch.
- getLaunchPiece() - Method in class org.orekit.propagation.analytical.tle.TLE
-
Get the launch piece.
- getLaunchYear() - Method in class org.orekit.files.ccsds.ODMMetaData
-
Get the launch year.
- getLaunchYear() - Method in class org.orekit.files.ccsds.ODMParser
-
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.SpacecraftState
-
Get the eccentric longitude argument (as per equinoctial parameters).
- getLeap(AbsoluteDate) - 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(AbsoluteDate) - Method in class org.orekit.time.UTCScale
-
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(FieldAbsoluteDate<T>) - Method in interface org.orekit.time.TimeScale
-
Get the value of the previous leap.
- getLeap(FieldAbsoluteDate<T>) - Method in class org.orekit.time.UTCScale
-
Get the value of the previous leap.
- getLeapSeconds() - Method in class org.orekit.gnss.RinexHeader
-
Get the Number of leap seconds since 6-Jan-1980.
- getLeapSecondsDayNum() - Method in class org.orekit.gnss.RinexHeader
-
Get the respective leap second day number.
- getLeapSecondsFuture() - Method in class org.orekit.gnss.RinexHeader
-
Get the future or past leap seconds.
- getLeapSecondsWeekNum() - Method in class org.orekit.gnss.RinexHeader
-
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.
- getLf() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
-
Get the eccentric longitude.
- getLightingRatio(FieldVector3D<T>, Frame, FieldAbsoluteDate<T>) - Method in class org.orekit.forces.radiation.SolarRadiationPressure
-
Get the lighting ratio ([0-1]).
- getLightingRatio(Vector3D, Frame, AbsoluteDate) - Method in class org.orekit.forces.radiation.SolarRadiationPressure
-
Get the lighting ratio ([0-1]).
- getLine1() - Method in class org.orekit.propagation.analytical.tle.TLE
-
Get the first line.
- getLine2() - Method in class org.orekit.propagation.analytical.tle.TLE
-
Get the second line.
- getListAppliedDCBS() - Method in class org.orekit.gnss.RinexHeader
-
Get the list of applied differential code bias corrections.
- getListAppliedPCVS() - Method in class org.orekit.gnss.RinexHeader
-
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) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution
-
Compute the limits in L, the true longitude, for integration.
- getLLimits(SpacecraftState) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTAtmosphericDrag
-
Compute the limits in L, the true longitude, for integration.
- getLLimits(SpacecraftState) - 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 latitude 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.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.
- getLns(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.LnsCoefficients
-
Get the value of Lns(γ).
- 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
- 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.CCSDSFrame
-
Get the type of Local Orbital frame.
- getLofType() - Method in class org.orekit.files.ccsds.OEMFile.CovarianceMatrix
-
Get coordinate system for covariance matrix, for Local Orbital Frames.
- 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.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.
- 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.
- 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.
- 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.SpacecraftState
-
Get the true longitude 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.
- getM0() - Method in class org.orekit.gnss.GPSAlmanac
-
- getM0() - Method in interface org.orekit.propagation.analytical.gnss.GPSOrbitalElements
-
Gets the Mean Anomaly at Reference Time.
- 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.integration.AbstractIntegratedPropagator
-
Get the differential equations to integrate (for main state only).
- 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).
- 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.
- getManeuver(int) - Method in class org.orekit.files.ccsds.OPMFile
-
Get a maneuver.
- getManeuvers() - Method in class org.orekit.files.ccsds.OPMFile
-
Get a list of all maneuvers.
- getMapper() - Method in class org.orekit.propagation.numerical.PartialDerivativesEquations
-
Get a mapper between two-dimensional Jacobians and one-dimensional additional state.
- getMargin() - Method in class org.orekit.propagation.events.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.RinexHeader
-
Get name of the antenna marker.
- getMarkerNumber() - Method in class org.orekit.gnss.RinexHeader
-
Get number of the antenna marker.
- getMarkerType() - Method in class org.orekit.gnss.RinexHeader
-
Get type of the antenna marker.
- getMars() - Static method in class org.orekit.bodies.CelestialBodyFactory
-
Get the Mars singleton body.
- getMass() - Method in class org.orekit.files.ccsds.OGMFile
-
Get the spacecraft 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() - Method in class org.orekit.propagation.SpacecraftState
-
Gets the current 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.EcksteinHechlerPropagator
-
Get the mass.
- getMass(AbsoluteDate) - Method in class org.orekit.propagation.analytical.Ephemeris
-
Get the mass.
- getMass(AbsoluteDate) - Method in class org.orekit.propagation.analytical.gnss.GPSPropagator
-
Get the mass.
- getMass(AbsoluteDate) - Method in class org.orekit.propagation.analytical.KeplerianPropagator
-
Get the mass.
- getMass(AbsoluteDate) - Method in class org.orekit.propagation.analytical.tle.TLEPropagator
-
Get the mass.
- getMass(AbsoluteDate) - Method in class org.orekit.propagation.integration.IntegratedEphemeris
-
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.FieldEcksteinHechlerPropagator
-
Get the mass.
- getMass(FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.analytical.FieldKeplerianPropagator
-
Get the mass.
- getMass(FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.integration.FieldIntegratedEphemeris
-
Get the mass.
- getMasterStation() - Method in class org.orekit.estimation.measurements.TurnAroundRange
-
Get the master ground station from which measurement is performed.
- getMatrix() - Method in class org.orekit.files.ccsds.OEMFile.CovarianceMatrix
-
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.forces.drag.atmosphere.HarrisPriester
-
Get the maximal altitude for the model.
- 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.forces.drag.atmosphere.data.MarshallSolarActivityFutureEstimation
-
Gets the available data range maximum date.
- getMaxDate() - Method in interface org.orekit.forces.drag.atmosphere.DTM2000InputParameters
-
Gets the available data range maximum date.
- getMaxDate() - Method in interface org.orekit.forces.drag.atmosphere.JB2008InputParameters
-
Gets the available data range maximum date.
- getMaxDate() - Method in interface org.orekit.forces.drag.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.
- 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.
- 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.
- getMaxSpan() - Method in class org.orekit.utils.GenericTimeStampedCache
-
Get the maximum duration span in seconds of one slot.
- getMaxValue() - Method in class org.orekit.utils.ParameterDriver
-
Get maximum parameter value.
- 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.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) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution
-
Computes the mean equinoctial elements rates dai / dt.
- getMeanElementRate(SpacecraftState) - Method in interface org.orekit.propagation.semianalytical.dsst.forces.DSSTForceModel
-
Computes the mean equinoctial elements rates dai / dt.
- getMeanElementRate(SpacecraftState) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseral
-
Computes the mean equinoctial elements rates dai / dt.
- getMeanElementRate(SpacecraftState) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBody
-
Computes the mean equinoctial elements rates dai / dt.
- getMeanElementRate(SpacecraftState) - 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.OMMFile.OMMMetaData
-
Get the description of the Mean Element Theory.
- getMeanFlux(AbsoluteDate) - Method in class org.orekit.forces.drag.atmosphere.data.MarshallSolarActivityFutureEstimation
-
Get the value of the mean solar flux.
- getMeanFlux(AbsoluteDate) - Method in interface org.orekit.forces.drag.atmosphere.DTM2000InputParameters
-
Get the value of the mean solar flux.
- getMeanMotion() - Method in class org.orekit.files.ccsds.OMMFile
-
Get the orbit mean motion.
- getMeanMotion() - Method in class org.orekit.gnss.GPSAlmanac
-
- getMeanMotion() - Method in interface org.orekit.propagation.analytical.gnss.GPSOrbitalElements
-
Gets 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.utilities.AuxiliaryElements
-
Get the Keplerian mean motion.
- getMeanMotionDot() - Method in class org.orekit.files.ccsds.OMMFile
-
Get the first time derivative of the mean motion.
- getMeanMotionDotDot() - Method in class org.orekit.files.ccsds.OMMFile
-
Get the second time derivative of the mean motion.
- 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.TLE
-
Get the mean motion second derivative.
- getMeanObliquityFunction() - Method in enum org.orekit.utils.IERSConventions
-
Get the function computing mean obliquity of the ecliptic.
- getMeasurement() - Method in class org.orekit.files.ccsds.TDMFile.Observation
-
Getter for the measurement.
- getMeasurementsParametersDrivers(boolean) - Method in class org.orekit.estimation.leastsquares.BatchLSEstimator
-
Get the measurements parameters supported by this estimator (including measurements and modifiers).
- getMeasurementType() - Method in enum org.orekit.gnss.ObservationType
-
Get the measurement type.
- getMercury() - Static method in class org.orekit.bodies.CelestialBodyFactory
-
Get the Mercury singleton body.
- getMessage() - Method in exception org.orekit.errors.OrekitException
- getMessage() - Method in exception org.orekit.errors.OrekitIllegalArgumentException
- getMessage() - Method in exception org.orekit.errors.OrekitIllegalStateException
- getMessage() - Method in exception org.orekit.errors.OrekitInternalError
- getMessage() - Method in exception org.orekit.errors.OrekitIOException
- getMessage() - Method in exception org.orekit.errors.OrekitParseException
- 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(Locale) - Method in exception org.orekit.errors.OrekitIllegalArgumentException
-
Gets the message in a specified locale.
- getMessage(Locale) - Method in exception org.orekit.errors.OrekitIllegalStateException
-
Gets the message in a specified locale.
- getMessage(Locale) - Method in exception org.orekit.errors.OrekitInternalError
-
Gets the message in a specified locale.
- getMessage(Locale) - Method in exception org.orekit.errors.OrekitIOException
-
Gets the message in a specified locale.
- getMessage(Locale) - Method in exception org.orekit.errors.OrekitParseException
-
Gets the message in a specified locale.
- getMetaData() - Method in class org.orekit.files.ccsds.OEMFile.EphemeridesBlock
-
Get the meta-data for the block.
- getMetaData() - Method in class org.orekit.files.ccsds.OGMFile
-
Get the meta data.
- getMetaData() - Method in class org.orekit.files.ccsds.OMMFile
-
Get the meta data.
- getMetaData() - Method in class org.orekit.files.ccsds.OPMFile
-
Get the meta data.
- getMetaData() - Method in class org.orekit.files.ccsds.TDMFile.ObservationsBlock
-
Get the meta-data for the block.
- getMetaDataComment() - Method in class org.orekit.files.ccsds.OPMFile
-
Get the comment for meta-data.
- getMHzFrequency() - Method in enum org.orekit.gnss.Frequency
-
Get the value of the frequency in MHz.
- getMilliInWeek() - Method in class org.orekit.time.GPSDate
-
Get the number of milliseconds since week start.
- getMinAlt() - Method in class org.orekit.forces.drag.atmosphere.HarrisPriester
-
Get the minimal altitude for the model.
- getMinDate() - Method in class org.orekit.forces.drag.atmosphere.data.MarshallSolarActivityFutureEstimation
-
Gets the available data range minimum date.
- getMinDate() - Method in interface org.orekit.forces.drag.atmosphere.DTM2000InputParameters
-
Gets the available data range minimum date.
- getMinDate() - Method in interface org.orekit.forces.drag.atmosphere.JB2008InputParameters
-
Gets the available data range minimum date.
- getMinDate() - Method in interface org.orekit.forces.drag.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.
- 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.
- getMissionReferenceDate() - Method in class org.orekit.files.ccsds.ODMFile
-
Get reference date for Mission Elapsed Time and Mission Relative Time time systems.
- getMissionReferenceDate() - Method in class org.orekit.files.ccsds.ODMParser
-
Get initial date.
- getMissionReferenceDate() - Method in class org.orekit.files.ccsds.TDMParser
-
Get initial date.
- 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.
- getMJDRef() - Method in class org.orekit.time.OffsetModel
-
Get the reference date of the linear model as a modified julian day.
- 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.TDMFile.TDMMetaData
-
Getter for the mode.
- getMode() - Method in class org.orekit.propagation.AbstractPropagator
-
Get the current operating mode of the propagator.
- getMode() - Method in class org.orekit.propagation.FieldAbstractPropagator
-
Get the current operating mode of the propagator.
- getMode() - Method in interface org.orekit.propagation.FieldPropagator
-
Get the current operating mode of the propagator.
- getMode() - Method in interface org.orekit.propagation.Propagator
-
Get the current operating mode of the propagator.
- 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(Field<T>) - Static method in class org.orekit.time.FieldAbsoluteDate
-
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() - Static method in class org.orekit.bodies.CelestialBodyFactory
-
Get the Moon singleton body.
- getMu() - Method in class org.orekit.files.ccsds.ODMParser
-
Get gravitational coefficient.
- getMu() - Method in class org.orekit.files.ccsds.OEMFile.EphemeridesBlock
-
- getMu() - Method in class org.orekit.files.ccsds.OEMFile.OemSatelliteEphemeris
-
- 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
-
- getMu() - Method in class org.orekit.files.general.OrekitEphemerisFile.OrekitSatelliteEphemeris
-
- getMu() - Method in class org.orekit.files.sp3.SP3File.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() - 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
-
- getMu() - Method in class org.orekit.orbits.Orbit
-
Get the central acceleration constant.
- 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.utilities.AuxiliaryElements
-
Get the central body attraction coefficient.
- getMu() - Method in class org.orekit.propagation.SpacecraftState
-
Get the central attraction coefficient.
- getMU() - Static method in class org.orekit.propagation.analytical.gnss.GPSPropagator
-
Get the Earth gravity coefficient used for GPS propagation.
- getMU() - Static method in class org.orekit.propagation.analytical.tle.TLEPropagator
-
Get the Earth gravity coefficient used for TLE propagation.
- getMuCreated() - Method in class org.orekit.files.ccsds.ODMFile
-
Get the gravitational coefficient created from the knowledge of the central body.
- getMuParsed() - Method in class org.orekit.files.ccsds.ODMFile
-
Get the gravitational coefficient parsed in the ODM File.
- getMuSet() - Method in class org.orekit.files.ccsds.ODMFile
-
Get the gravitational coefficient set by the user.
- getMuUsed() - Method in class org.orekit.files.ccsds.ODMFile
-
Get the used gravitational coefficient.
- getN() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.CoefficientsFactory.NSKey
-
Get n.
- 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.data.NamedData
-
Get the name of the data.
- getName() - Method in class org.orekit.forces.maneuvers.ConstantThrustManeuver
-
Get the 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.SatelliteAntennaCode
-
Deprecated.
Get the IGS name for the antenna code.
- getName() - Method in enum org.orekit.gnss.antenna.SatelliteType
-
Get the IGS name for the antenna code.
- 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 interface org.orekit.propagation.FieldAdditionalStateProvider
-
Get the name of the additional state.
- getName() - Method in interface org.orekit.propagation.integration.AdditionalEquations
-
Get the name of the additional state.
- getName() - Method in interface org.orekit.propagation.integration.FieldAdditionalEquations
-
Get the name of the additional state.
- getName() - Method in class org.orekit.propagation.numerical.JacobiansMapper
-
Get the name of the partial Jacobians.
- getName() - Method in class org.orekit.propagation.numerical.PartialDerivativesEquations
-
Get the name of the additional state.
- 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.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.
- getNbManeuvers() - Method in class org.orekit.files.ccsds.OPMFile
-
Get the number of maneuvers present in the OPM.
- 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() - Static method in class org.orekit.bodies.CelestialBodyFactory
-
Get the Neptune singleton body.
- 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.
- getNewtonianAttractionForceModel() - Method in class org.orekit.propagation.numerical.FieldNumericalPropagator
-
- 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.
- 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.OMMFile
-
Get the NORAD Catalog Number ("Satellite Number").
- getNormal() - Method in class org.orekit.forces.BoxAndSolarArraySpacecraft.Facet
-
Get unit normal vector.
- getNormal(AbsoluteDate, Frame, FieldVector3D<DerivativeStructure>, FieldRotation<DerivativeStructure>) - Method in class org.orekit.forces.BoxAndSolarArraySpacecraft
-
Get solar array normal in spacecraft frame.
- 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(double, double, TideSystem, double[][], double[][]) - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory
-
- 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(UnnormalizedSphericalHarmonicsProvider) - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory
-
- 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.
- 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.
- getNumberOfEpochs() - Method in class org.orekit.files.sp3.SP3File
-
Returns the number of epochs contained in this orbit file.
- getNutationArguments(TimeScale) - 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.
- getNutationFunction() - Method in enum org.orekit.utils.IERSConventions
-
Get the function computing the nutation angles.
- getNutationReferenceEpoch() - Method in enum org.orekit.utils.IERSConventions
-
Get the reference epoch for fundamental nutation arguments.
- getObjectID() - Method in class org.orekit.files.ccsds.ODMMetaData
-
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.ODMMetaData
-
Get the spacecraft name for which the orbit state is provided.
- getObservationCode() - Method in class org.orekit.gnss.RinexHeader
-
Get the observation code of the average phasecenter position w/r to antenna reference point.
- getObservationData() - Method in class org.orekit.gnss.ObservationDataSet
-
Get list of observation data.
- getObservationDataSets() - Method in class org.orekit.gnss.RinexLoader
-
Get parsed rinex observations data sets.
- getObservations() - Method in class org.orekit.files.ccsds.TDMFile.ObservationsBlock
-
Get the list of Observations data lines.
- getObservations() - Method in class org.orekit.gnss.RinexLoader
-
- getObservationsBlocks() - Method in class org.orekit.files.ccsds.TDMFile
-
Get the list of observations blocks as an unmodifiable list.
- getObservationsComment() - Method in class org.orekit.files.ccsds.TDMFile.ObservationsBlock
-
Get the observations data lines comment.
- 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.propagation.events.AngularSeparationDetector
-
Get the observer for the spacecraft.
- getObserverName() - Method in class org.orekit.gnss.RinexHeader
-
Get name of the observer.
- getObservers() - Method in class org.orekit.utils.ParameterDriver
-
Get the observers for this driver.
- getOcculted() - Method in class org.orekit.propagation.events.EclipseDetector
-
Get 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
-
Get the occulted body radius (m).
- getOccultedRadius() - Method in class org.orekit.propagation.events.FieldEclipseDetector
-
Get the occulted body radius (m).
- getOcculting() - Method in class org.orekit.propagation.events.EclipseDetector
-
Get the occulting body.
- getOcculting() - Method in class org.orekit.propagation.events.FieldEclipseDetector
-
Get the occulting body.
- getOccultingRadius() - Method in class org.orekit.propagation.events.EclipseDetector
-
Get the occulting body radius (m).
- 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.
- getOceanPoleTide(EOPHistory) - Method in enum org.orekit.utils.IERSConventions
-
Get the function computing ocean pole tide (ΔC₂₁, ΔS₂₁).
- getOceanTidesWaves(int, int) - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory
-
Get the ocean tides waves from the first supported file.
- getODMFile() - Method in class org.orekit.files.ccsds.ODMMetaData
-
Get the ODM file to which these meta-data belong.
- getOffset() - Method in class org.orekit.time.OffsetModel
-
Offset at reference date in seconds (TAI minus UTC).
- getOffset(AbsoluteDate) - Method in class org.orekit.forces.gravity.potential.CachedNormalizedSphericalHarmonicsProvider
-
- getOffset(AbsoluteDate) - Method in interface org.orekit.forces.gravity.potential.SphericalHarmonicsProvider
-
- getOffsetGeodeticPoint() - Method in class org.orekit.estimation.measurements.GroundStation
-
- 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, DSFactory, 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<DerivativeStructure>, DSFactory, 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.gnss.GPSAlmanac
-
- getOmega0() - Method in interface org.orekit.propagation.analytical.gnss.GPSOrbitalElements
-
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.gnss.GPSAlmanac
-
- getOmegaDot() - Method in interface org.orekit.propagation.analytical.gnss.GPSOrbitalElements
-
Gets the Rate of Right Ascension.
- getOptimum() - Method in class org.orekit.estimation.leastsquares.BatchLSEstimator
-
Get the optimum found.
- getOrbit() - Method in class org.orekit.propagation.FieldSpacecraftState
-
Gets the current orbit.
- getOrbit() - Method in class org.orekit.propagation.SpacecraftState
-
Gets the current orbit.
- 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.
- 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.
- getOrbitType() - Method in class org.orekit.files.sp3.SP3File
-
- 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.
- getOrbitTypeKey() - Method in class org.orekit.files.sp3.SP3File
-
Returns the orbit type key for this SP3 file.
- 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.
- getOriginator() - Method in class org.orekit.files.ccsds.ODMFile
-
Get the file originator.
- getOriginator() - Method in class org.orekit.files.ccsds.TDMFile
-
Get the file originator.
- getP() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
-
Get the y component of inclination vector.
- 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.OGMFile
-
Get the orbit argument of pericenter.
- getPa() - Method in class org.orekit.gnss.GPSAlmanac
-
- getPa() - Method in interface org.orekit.propagation.analytical.gnss.GPSOrbitalElements
-
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.
- getParameters() - Method in interface org.orekit.forces.ForceModel
-
Get force model parameters.
- getParameters() - Method in interface org.orekit.models.earth.MappingFunction
-
Get tropospheric model parameters.
- getParameters() - Method in class org.orekit.propagation.numerical.JacobiansMapper
-
Get the number of parameters.
- getParameters(Field<T>) - Method in interface org.orekit.forces.ForceModel
-
Get force model parameters.
- getParameters(Field<T>) - Method in interface org.orekit.models.earth.MappingFunction
-
Get tropospheric model parameters.
- getParameters(FieldSpacecraftState<DerivativeStructure>, DiscreteTroposphericModel) - Method in class org.orekit.estimation.measurements.modifiers.TroposphericDSConverter
-
Get the tropospheric 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.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.OnBoardAntennaInterSatellitesRangeModifier
-
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.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.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.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 interface org.orekit.forces.ForceModel
-
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.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.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.HarmonicParametricAcceleration
-
Get the drivers for force model parameters.
- getParametersDrivers() - Method in class org.orekit.forces.maneuvers.ConstantThrustManeuver
-
Get the drivers for force model parameters.
- getParametersDrivers() - Method in class org.orekit.forces.PolynomialParametricAcceleration
-
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.EstimatedTroposphericModel
-
- getParametersDrivers() - Method in class org.orekit.models.earth.GlobalMappingFunctionModel
-
Get the drivers for tropospheric model parameters.
- getParametersDrivers() - Method in interface org.orekit.models.earth.MappingFunction
-
Get the drivers for tropospheric model parameters.
- getParametersDrivers() - Method in class org.orekit.models.earth.MendesPavlisModel
-
Get the drivers for tropospheric model parameters.
- getParametersDrivers() - Method in class org.orekit.models.earth.NiellMappingFunctionModel
-
- getParametersDrivers() - Method in interface org.orekit.models.earth.TroposphericModel
-
Get the drivers for tropospheric model parameters.
- getParametersDrivers() - Method in class org.orekit.models.earth.ViennaOneModel
-
Get the drivers for tropospheric model parameters.
- getParametersDrivers() - Method in class org.orekit.models.earth.ViennaThreeModel
-
Get the drivers for tropospheric model parameters.
- getParametersJacobian(SpacecraftState, double[][]) - Method in class org.orekit.propagation.numerical.JacobiansMapper
-
Get theJacobian 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.
- 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.TDMFile.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(Field<T>) - Static method in class org.orekit.time.FieldAbsoluteDate
-
Dummy date at infinity in the past direction.
- getPath() - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData
-
Getter for the path.
- getPath1() - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData
-
Getter for the path1.
- getPath2() - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData
-
Getter for the path2.
- 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.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.
- getPhase(BodiesElements) - Method in class org.orekit.models.earth.displacement.Tide
-
Get the phase of the tide.
- getPhaseCenterVariation(Vector3D) - Method in class org.orekit.gnss.antenna.FrequencyPattern
-
Get the value of the phase center variation in a signal direction.
- getPhaseCenterVariation(Frequency, Vector3D) - Method in class org.orekit.gnss.antenna.Antenna
-
Get the value of the phase center variation in a signal direction.
- getPhaseShiftCorrections() - Method in class org.orekit.gnss.RinexHeader
-
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 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.Model
-
Get the "physical" estimated covariance matrix (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.Model
-
Get the "physical" estimated state (i.e.
- getPhysicalInnovationCovarianceMatrix() - Method in interface org.orekit.estimation.sequential.KalmanEstimation
-
Get the physical innovation covariance matrix.
- getPhysicalInnovationCovarianceMatrix() - Method in class org.orekit.estimation.sequential.Model
-
Get the physical innovation covariance matrix.
- getPhysicalKalmanGain() - Method in interface org.orekit.estimation.sequential.KalmanEstimation
-
Get the physical Kalman gain matrix.
- getPhysicalKalmanGain() - Method in class org.orekit.estimation.sequential.Model
-
Get the physical Kalman gain 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.Model
-
Get the physical Jacobian of the measurement with respect to the state (H matrix).
- 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.Model
-
Get physical state transition matrix between previous state and estimated (but not yet corrected) state.
- 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() - Static method in class org.orekit.bodies.CelestialBodyFactory
-
Get the Pluto singleton body.
- 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.
- 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.ccsds.OPMFile
-
Get position vector.
- 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.
- getPositionScale() - Method in class org.orekit.propagation.conversion.AbstractPropagatorBuilder
-
Get the position scale.
- getPrecessionFunction() - Method in enum org.orekit.utils.IERSConventions
-
Get the function computing the precession angles.
- getPredictedMeasurement() - Method in interface org.orekit.estimation.sequential.KalmanEstimation
-
Get the predicted measurement.
- getPredictedMeasurement() - Method in class org.orekit.estimation.sequential.Model
-
Get the predicted measurement.
- getPredictedSpacecraftStates() - Method in interface org.orekit.estimation.sequential.KalmanEstimation
-
Get the predicted spacecraft states.
- getPredictedSpacecraftStates() - Method in class org.orekit.estimation.sequential.Model
-
Get the predicted spacecraft states.
- 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.GlobalPressureTemperature2Model
-
Returns the pressure at the station [hPa].
- getPressure() - Method in class org.orekit.models.earth.GlobalPressureTemperatureModel
-
Get the atmospheric pressure of the station depending its position.
- 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.
- 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.
- getPRN() - Method in class org.orekit.gnss.GPSAlmanac
-
- getPRN() - Method in interface org.orekit.propagation.analytical.gnss.GPSOrbitalElements
-
Gets the PRN number of the GPS satellite.
- getPrnNumber() - Method in class org.orekit.gnss.antenna.SatelliteAntenna
-
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.
- 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.
- getProgDCBS() - Method in class org.orekit.gnss.RinexLoader.Parser.AppliedDCBS
-
Get the program name used to apply DCBs.
- getProgPCVS() - Method in class org.orekit.gnss.RinexLoader.Parser.AppliedPCVS
-
Get the program name used to apply PCVs.
- 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.
- getPropagationParametersDrivers(boolean) - Method in class org.orekit.estimation.sequential.KalmanEstimator
-
Get the propagator parameters supported by this estimator.
- getPropagationParametersEvolution() - Method in class org.orekit.estimation.sequential.UnivariateProcessNoise
-
Getter for the propagationParametersEvolution.
- 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.sp3.SP3File.SP3Ephemeris
-
- getPropagator() - Method in class org.orekit.propagation.analytical.AdapterPropagator
-
Get the reference propagator.
- getPropagator(ObservableSatellite) - Method in class org.orekit.estimation.measurements.generation.Generator
-
Get a registered propagator.
- getPropagatorIndex() - Method in class org.orekit.estimation.measurements.ObservableSatellite
-
Get the index of the propagator related to this satellite.
- 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.
- getPropagatorsIndices() - Method in class org.orekit.estimation.measurements.AbstractMeasurement
-
- getPropagatorsIndices() - Method in interface org.orekit.estimation.measurements.ObservedMeasurement
-
- getProvider() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonal
-
Get the spherical harmonics provider.
- 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.
- 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).
- getPVCoordinates() - Method in class org.orekit.files.ccsds.OPMFile
-
Get the position/velocity coordinates contained in the OPM.
- getPVCoordinates() - Method in class org.orekit.orbits.FieldOrbit
-
- getPVCoordinates() - Method in class org.orekit.orbits.Orbit
-
- getPVCoordinates() - Method in class org.orekit.propagation.FieldSpacecraftState
-
- getPVCoordinates() - Method in class org.orekit.propagation.SpacecraftState
-
- getPVCoordinates(Frame) - Method in class org.orekit.orbits.FieldOrbit
-
- getPVCoordinates(Frame) - Method in class org.orekit.orbits.Orbit
-
- getPVCoordinates(Frame) - Method in class org.orekit.propagation.FieldSpacecraftState
-
- getPVCoordinates(Frame) - Method in class org.orekit.propagation.SpacecraftState
-
- getPVCoordinates(AbsoluteDate) - Method in class org.orekit.propagation.analytical.tle.TLEPropagator
-
Get the extrapolated position and velocity from an initial TLE.
- getPVCoordinates(AbsoluteDate) - Method in class org.orekit.propagation.analytical.tle.TLESeries
-
Deprecated.
Get the extrapolated position and velocity from an initial date.
- getPVCoordinates(AbsoluteDate, Frame) - Method in class org.orekit.frames.TopocentricFrame
-
Get the
PVCoordinates
of the topocentric frame origin in the selected frame.
- getPVCoordinates(AbsoluteDate, Frame) - 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(AbsoluteDate, Frame) - Method in class org.orekit.propagation.integration.IntegratedEphemeris
-
- getPVCoordinates(AbsoluteDate, Frame) - Method in class org.orekit.propagation.numerical.NumericalPropagator
-
- getPVCoordinates(AbsoluteDate, Frame) - Method in interface org.orekit.utils.PVCoordinatesProvider
-
- getPVCoordinates(FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.orbits.FieldOrbit
-
- getPVCoordinates(FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.propagation.FieldAbstractPropagator
-
- getPVCoordinates(FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.propagation.integration.FieldIntegratedEphemeris
-
- getPVCoordinates(FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.propagation.numerical.FieldNumericalPropagator
-
- getPVCoordinates(FieldAbsoluteDate<T>, Frame) - Method in interface org.orekit.utils.ExtendedPVCoordinatesProvider
-
- getPVCoordinates(FieldAbsoluteDate<T>, Frame) - Method in interface org.orekit.utils.FieldPVCoordinatesProvider
-
- 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.CircularFieldOfViewDetector
-
Get the position/velocity provider of the target .
- getPVTarget() - Method in class org.orekit.propagation.events.FieldOfViewDetector
-
Get the position/velocity provider of the target .
- getQ() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
-
Get the x component of inclination vector.
- getQZSS() - Static method in class org.orekit.time.TimeScalesFactory
-
Get the Quasi-Zenith Satellite System time scale.
- getRaan() - Method in class org.orekit.files.ccsds.OGMFile
-
Get the orbit right ascension of 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(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.
- 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.
- 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).
- getRangeMode() - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData
-
Getter for the rangeMode.
- getRangeModulus() - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData
-
Getter for the rangeModulus.
- 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.
- 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.
- getRangeUnits() - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData
-
Getter for the rangeUnits.
- 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.
- getRawCnm(int, int) - Method in interface org.orekit.forces.gravity.potential.RawSphericalHarmonicsProvider.RawSphericalHarmonics
-
Get a spherical harmonic cosine coefficient.
- 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.
- 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.
- getRcvrClkOffset() - Method in class org.orekit.gnss.ObservationDataSet
-
Get receiver clock offset.
- getReal(int, int) - Method in class org.orekit.utils.LoveNumbers
-
Get the real part of a nominal Love numbers.
- getReceiveBand() - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData
-
Getter for the receiveBand.
- getReceiveDelays() - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData
-
Getter for receiveDelays.
- getReceiverNumber() - Method in class org.orekit.gnss.RinexHeader
-
Get the number of the receiver.
- getReceiversAntennas() - Method in class org.orekit.gnss.antenna.AntexLoader
-
Get parsed receivers antennas.
- getReceiverType() - Method in class org.orekit.gnss.RinexHeader
-
Get the type of the receiver.
- getReceiverVersion() - Method in class org.orekit.gnss.RinexHeader
-
Get the version of the receiver.
- getReferenceAttitude() - Method in class org.orekit.attitudes.FixedRate
-
Get the reference attitude.
- 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.TDMFile.TDMMetaData
-
Get the the value of
REFERENCE_FRAME
as an Orekit
Frame
.
- getReferenceFrameString() - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData
-
Get the reference frame specifier as it appeared in the file.
- getReferenceValue() - Method in class org.orekit.utils.ParameterDriver
-
Get reference parameter value.
- getRefFrame() - Method in class org.orekit.files.ccsds.CcsdsModifiedFrame
-
Get the name of the CCSDS reference frame.
- getRefFrame() - Method in class org.orekit.files.ccsds.ODMMetaData
-
Get the the value of
REF_FRAME
as an Orekit
Frame
.
- getRefFrame() - Method in class org.orekit.files.ccsds.OPMFile.Maneuver
-
Get Coordinate system for velocity increment vector, for absolute frames.
- getRefLofType() - Method in class org.orekit.files.ccsds.OPMFile.Maneuver
-
Get coordinate system for velocity increment vector, for Local Orbital Frames.
- 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.
- getRetrogradeFactor() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
-
Get the retrograde factor.
- getRevAtEpoch() - Method in class org.orekit.files.ccsds.OMMFile
-
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.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.RinexHeader
-
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).
- getRolloverReference() - Static method in class org.orekit.time.GPSDate
-
Get the reference date ensuring continuity across GPS week rollover.
- getRoot() - Static method in class org.orekit.frames.Frame
-
Get the unique root 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.
- 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.
- getS() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.CoefficientsFactory.NSKey
-
Get s.
- getS10(AbsoluteDate) - Method in interface org.orekit.forces.drag.atmosphere.JB2008InputParameters
-
Get the EUV index (26-34 nm) scaled to F10.
- getS10B(AbsoluteDate) - Method in interface org.orekit.forces.drag.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.gnss.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.SP3File
-
Get the number of satellites contained in this orbit file.
- 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.
- 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.OEMFile
-
- 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.OrekitEphemerisFile
-
- getSatellites() - Method in class org.orekit.files.sp3.SP3File
-
- 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 enum org.orekit.gnss.Frequency
-
Get the satellite system for which this frequency is defined.
- getSatelliteSystem() - Method in class org.orekit.gnss.ObservationDataSet
-
Get Satellite System.
- getSatelliteSystem() - Method in class org.orekit.gnss.RinexHeader
-
Get Satellite System.
- getSatelliteSystem() - Method in class org.orekit.gnss.RinexLoader.Parser.AppliedDCBS
-
Get the satellite system.
- getSatelliteSystem() - Method in class org.orekit.gnss.RinexLoader.Parser.AppliedPCVS
-
Get the satellite system.
- getSatelliteSystem() - Method in class org.orekit.gnss.RinexLoader.Parser.PhaseShiftCorrection
-
Get the Satellite System.
- getSatelliteSystem() - Method in class org.orekit.gnss.RinexLoader.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.RinexLoader.Parser.PhaseShiftCorrection
-
Get the list of satellites involved.
- getSaturn() - Static method in class org.orekit.bodies.CelestialBodyFactory
-
Get the Saturn singleton body.
- getScale() - Method in class org.orekit.utils.ParameterDriver
-
Get scale.
- getSecond() - Method in class org.orekit.time.TimeComponents
-
Get the seconds number.
- 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.SP3File
-
Returns the seconds of the GPS week as contained in the SP3 file.
- getSegments() - Method in class org.orekit.files.ccsds.OEMFile.OemSatelliteEphemeris
-
- getSegments() - Method in interface org.orekit.files.general.EphemerisFile.SatelliteEphemeris
-
Get the segments of the ephemeris.
- getSegments() - Method in class org.orekit.files.general.OrekitEphemerisFile.OrekitSatelliteEphemeris
-
- getSegments() - Method in class org.orekit.files.sp3.SP3File.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.
- 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.
- getSelectedParameters() - Method in class org.orekit.propagation.numerical.PartialDerivativesEquations
-
Get the selected parameters, in Jacobian matrix column order.
- getSelector() - Method in class org.orekit.estimation.measurements.generation.AbstractScheduler
-
Get the dates selector.
- getSerialNumber() - Method in class org.orekit.gnss.antenna.ReceiverAntenna
-
Get the serial number.
- getSigma() - Method in class org.orekit.estimation.measurements.modifiers.DynamicOutlierFilter
-
Get the current value of sigma.
- getSignalStrength() - Method in class org.orekit.gnss.ObservationData
-
Get the signal strength.
- getSignalStrengthUnit() - Method in class org.orekit.gnss.RinexHeader
-
Get the unit of the carrier to noise ratio observables.
- getSinexCode() - Method in class org.orekit.gnss.antenna.Antenna
-
Get the sinex code of the antenna.
- 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.utils.LoveNumbers
-
Get the size of the arrays.
- getSj(int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.CjSjCoefficient
-
Get the Sj coefficient.
- getSlave() - Method in class org.orekit.propagation.events.InterSatDirectViewDetector
-
Get the provider for the slave satellite.
- getSlaveStation() - Method in class org.orekit.estimation.measurements.TurnAroundRange
-
Get the slave ground station reflecting the signal.
- 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.gnss.GPSAlmanac
-
- getSma() - Method in interface org.orekit.propagation.analytical.gnss.GPSOrbitalElements
-
Gets the Semi-Major Axis.
- getSma() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
-
Get the semi-major axis.
- getSolarRadArea() - Method in class org.orekit.files.ccsds.OGMFile
-
Get the solar radiation pressure area.
- getSolarRadCoeff() - Method in class org.orekit.files.ccsds.OGMFile
-
Get the solar radiation pressure coefficient.
- getSolarSystemBarycenter() - Static method in class org.orekit.bodies.CelestialBodyFactory
-
Get the solar system barycenter aggregated body.
- getSolidPoleTide(EOPHistory) - Method in enum org.orekit.utils.IERSConventions
-
Get the function computing solid pole tide (ΔC₂₁, ΔS₂₁).
- getSource() - Method in class org.orekit.gnss.GPSAlmanac
-
Gets the source of this GPS almanac.
- getSourceDCBS() - Method in class org.orekit.gnss.RinexLoader.Parser.AppliedDCBS
-
Get the source of corrections.
- getSourcePCVS() - Method in class org.orekit.gnss.RinexLoader.Parser.AppliedPCVS
-
Get the source of corrections.
- getSourceString() - Method in enum org.orekit.errors.OrekitMessages
- 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.propagation.semianalytical.dsst.forces.DSSTAtmosphericDrag
-
Get spacecraft shape.
- getSpacecraft() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTSolarRadiationPressure
-
Get spacecraft shape.
- getSpacecraftComment() - Method in class org.orekit.files.ccsds.OGMFile
-
Get the comment for spacecraft.
- getSpan(AbsoluteDate) - Method in class org.orekit.utils.TimeSpanMap
-
Get the time span containing a specified date.
- 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.
- 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.
- getStandardModel() - Static method in class org.orekit.models.earth.SaastamoinenModel
-
Create a new Saastamoinen model using a standard atmosphere model.
- getStandardModel(double, double) - Static method in class org.orekit.models.earth.MariniMurrayModel
-
Create a new Marini-Murray model using a standard atmosphere model.
- getStandardModel(double, double) - Static method in class org.orekit.models.earth.MendesPavlisModel
-
Create a new Mendes-Pavlis 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.OEMFile.EphemeridesBlock
-
- getStart() - Method in class org.orekit.files.ccsds.OEMFile.OemSatelliteEphemeris
-
- 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.OrekitEphemerisFile.OrekitEphemerisSegment
-
- getStart() - Method in class org.orekit.files.general.OrekitEphemerisFile.OrekitSatelliteEphemeris
-
- getStart() - Method in class org.orekit.files.sp3.SP3File.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.frames.EOPHistory
-
Get the date of the first available Earth Orientation Parameters.
- getStartDate() - Method in class org.orekit.propagation.AbstractPropagator
-
Get the start date.
- getStartDate() - Method in class org.orekit.propagation.FieldAbstractPropagator
-
Get the start date.
- getStartTime() - Method in class org.orekit.files.ccsds.OEMFile.EphemeridesBlock
-
Get start of total time span covered by ephemerides data and
covariance data.
- getStartTime() - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData
-
Getter for the startTime.
- getStartTimeString() - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData
-
Getter for the startTime String.
- 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.RecordAndContinue.Event
-
Get the spacecraft's state at the event.
- getState(DiscreteTroposphericModel) - Method in class org.orekit.estimation.measurements.modifiers.TroposphericDSConverter
-
Get the state with the number of parameters consistent with tropospheric model.
- getStateDerivatives(int) - Method in class org.orekit.estimation.measurements.EstimatedMeasurement
-
- getStateDimension() - Method in class org.orekit.propagation.numerical.JacobiansMapper
-
- 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.
- getStates() - Method in class org.orekit.estimation.measurements.EstimatedMeasurement
-
Get the states of the spacecrafts.
- 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.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.
- getStatus() - Method in class org.orekit.estimation.measurements.EstimatedMeasurement
-
Get the status.
- 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.
- getStepHandler() - Method in class org.orekit.propagation.AbstractPropagator
-
Get the step handler.
- getStepHandler() - Method in class org.orekit.propagation.FieldAbstractPropagator
-
Get the step handler.
- getStop() - Method in class org.orekit.files.ccsds.OEMFile.EphemeridesBlock
-
- getStop() - Method in class org.orekit.files.ccsds.OEMFile.OemSatelliteEphemeris
-
- 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.OrekitEphemerisFile.OrekitEphemerisSegment
-
- getStop() - Method in class org.orekit.files.general.OrekitEphemerisFile.OrekitSatelliteEphemeris
-
- getStop() - Method in class org.orekit.files.sp3.SP3File.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.
- getStopTime() - Method in class org.orekit.files.ccsds.OEMFile.EphemeridesBlock
-
Get end of total time span covered by ephemerides data and covariance
data.
- getStopTime() - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData
-
Getter for the stopTime.
- getStopTimeString() - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData
-
Getter for the stopTime String.
- getStreamOpener() - Method in class org.orekit.data.NamedData
-
Get the data stream opener.
- getStrengthLevel() - Method in class org.orekit.forces.drag.atmosphere.data.MarshallSolarActivityFutureEstimation
-
Get the strength level for activity.
- getSun() - Static method in class org.orekit.bodies.CelestialBodyFactory
-
Get the Sun singleton body.
- getSupportedNames() - Method in class org.orekit.forces.drag.atmosphere.data.MarshallSolarActivityFutureEstimation
-
Get the supported names for data files.
- 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
-
Get the supported names for data files.
- getSupportedNames() - Method in class org.orekit.gnss.YUMAParser
-
Get the supported names for data files.
- getSupportedNames() - Method in class org.orekit.models.earth.KlobucharIonoCoefficientsLoader
-
Returns the supported names of the loader.
- getSupportedNames() - Method in class org.orekit.models.earth.ViennaModelCoefficientsLoader
-
Returns the supported names of the loader.
- getSVN() - Method in class org.orekit.gnss.GPSAlmanac
-
Gets the satellite "SVN" reference number.
- getTabDensity() - Method in class org.orekit.forces.drag.atmosphere.HarrisPriester
-
Get the current density table.
- getTable() - Method in class org.orekit.attitudes.TabulatedLofOffset
-
Get an unmodifiable view of the tabulated attitudes.
- getTAI() - Static method in class org.orekit.time.TimeScalesFactory
-
Get the International Atomic Time scale.
- getTargetPV(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, 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.GroundPointing
-
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(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, 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.TargetPointing
-
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(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.YawSteering
-
Compute the target point position/velocity in specified frame.
- getTargetPV(PVCoordinatesProvider, AbsoluteDate, 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(PVCoordinatesProvider, AbsoluteDate, 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(PVCoordinatesProvider, AbsoluteDate, 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(PVCoordinatesProvider, AbsoluteDate, 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.
- 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() - Static method in class org.orekit.time.TimeScalesFactory
-
Get the Barycentric Coordinate Time scale.
- getTCG() - Static method in class org.orekit.time.TimeScalesFactory
-
Get the Geocentric Coordinate Time scale.
- getTDB() - Static method in class org.orekit.time.TimeScalesFactory
-
Get the Barycentric Dynamic Time scale.
- getTdop() - Method in class org.orekit.gnss.DOP
-
Gets the time dilution of precision.
- getTEME() - Static method in class org.orekit.frames.FramesFactory
-
Get the TEME reference frame.
- 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.GlobalPressureTemperature2Model
-
Returns the temperature at the station [K].
- getTemperature() - Method in class org.orekit.models.earth.GlobalPressureTemperatureModel
-
Get the atmospheric temperature of the station depending its position.
- getTFirstObs() - Method in class org.orekit.gnss.RinexHeader
-
Get the time of First observation record.
- getTGD() - Method in interface org.orekit.propagation.analytical.gnss.GPSOrbitalElements
-
Gets the estimated group delay differential TGD for L1-L2 correction.
- 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.
- 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.
- getThreeHourlyKP(AbsoluteDate) - Method in class org.orekit.forces.drag.atmosphere.data.MarshallSolarActivityFutureEstimation
-
Get the value of the 3 hours geomagnetic index.
- getThreeHourlyKP(AbsoluteDate) - Method in interface org.orekit.forces.drag.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.forces.maneuvers.ConstantThrustManeuver
-
Get the thrust.
- 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).
- 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.gnss.GPSAlmanac
-
- getTime() - Method in interface org.orekit.propagation.analytical.gnss.GPSOrbitalElements
-
Gets the Reference Time of the GPS orbit as a duration from week start.
- getTime() - Method in class org.orekit.time.DateTimeComponents
-
Get the time component.
- getTimeOffset() - Method in class org.orekit.estimation.measurements.EstimatedMeasurement
-
Get the time offset from first state date to measurement date.
- getTimeScale() - Method in class org.orekit.files.ccsds.OEMFile.EphemeridesBlock
-
- getTimeScale() - Method in interface org.orekit.files.general.EphemerisFile.EphemerisSegment
-
Get the time scale for this ephemeris segment.
- getTimeScale() - Method in class org.orekit.files.general.OrekitEphemerisFile.OrekitEphemerisSegment
-
- getTimeScale() - Method in class org.orekit.files.sp3.SP3File.SP3Ephemeris
-
- getTimeScale(IERSConventions) - Method in enum org.orekit.files.ccsds.CcsdsTimeScale
-
- getTimeScaleString() - Method in class org.orekit.files.ccsds.OEMFile.EphemeridesBlock
-
- getTimeScaleString() - Method in interface org.orekit.files.general.EphemerisFile.EphemerisSegment
-
Get the time scale for this ephemeris segment.
- getTimeScaleString() - Method in class org.orekit.files.general.OrekitEphemerisFile.OrekitEphemerisSegment
-
- getTimeScaleString() - Method in class org.orekit.files.sp3.SP3File.SP3Ephemeris
-
- getTimeSystem() - Method in class org.orekit.files.ccsds.ODMMetaData
-
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.TDMFile.TDMMetaData
-
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.sp3.SP3File
-
- getTimetagRef() - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData
-
Getter for the timetagRef.
- 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.
- getTLastObs() - Method in class org.orekit.gnss.RinexHeader
-
Get the time of last observation record.
- getTLE() - Method in class org.orekit.propagation.analytical.tle.TLEPropagator
-
Get the underlying TLE.
- getTLERelatedParametersComment() - Method in class org.orekit.files.ccsds.OMMFile
-
Get the comment for TLE related parameters.
- getToc() - Method in interface org.orekit.propagation.analytical.gnss.GPSOrbitalElements
-
Gets the clock correction reference time toc.
- 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.
- 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.
- 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).
- getTransform(AbsoluteDate) - Method in class org.orekit.estimation.measurements.EstimatedEarthFrameProvider
-
Get the
Transform
corresponding to specified date.
- getTransform(AbsoluteDate) - Method in class org.orekit.frames.EclipticProvider
-
- getTransform(AbsoluteDate) - Method in class org.orekit.frames.FixedTransformProvider
-
Get the
Transform
corresponding to specified date.
- getTransform(AbsoluteDate) - Method in class org.orekit.frames.GTODProvider
-
Get the
Transform
corresponding to specified date.
- getTransform(AbsoluteDate) - Method in class org.orekit.frames.HelmertTransformation
-
Get the
Transform
corresponding to specified date.
- getTransform(AbsoluteDate) - Method in class org.orekit.frames.InterpolatingTransformProvider
-
Get the
Transform
corresponding to specified date.
- getTransform(AbsoluteDate) - Method in class org.orekit.frames.ITRFVersion.Converter
-
Get the
Transform
corresponding to specified date.
- getTransform(AbsoluteDate) - Method in class org.orekit.frames.L1TransformProvider
-
Get the
Transform
corresponding to specified date.
- getTransform(AbsoluteDate) - Method in class org.orekit.frames.ShiftingTransformProvider
-
Get the
Transform
corresponding to specified date.
- getTransform(AbsoluteDate) - Method in interface org.orekit.frames.TransformProvider
-
Get the
Transform
corresponding to specified date.
- getTransform(FieldAbsoluteDate<DerivativeStructure>, DSFactory, Map<String, Integer>) - Method in class org.orekit.estimation.measurements.EstimatedEarthFrameProvider
-
Get the transform with derivatives.
- getTransform(FieldAbsoluteDate<T>) - Method in class org.orekit.estimation.measurements.EstimatedEarthFrameProvider
-
- getTransform(FieldAbsoluteDate<T>) - Method in class org.orekit.frames.EclipticProvider
-
- getTransform(FieldAbsoluteDate<T>) - Method in class org.orekit.frames.FixedTransformProvider
-
- getTransform(FieldAbsoluteDate<T>) - Method in class org.orekit.frames.GTODProvider
-
- getTransform(FieldAbsoluteDate<T>) - Method in class org.orekit.frames.HelmertTransformation
-
- getTransform(FieldAbsoluteDate<T>) - Method in class org.orekit.frames.InterpolatingTransformProvider
-
- getTransform(FieldAbsoluteDate<T>) - Method in class org.orekit.frames.ITRFVersion.Converter
-
- getTransform(FieldAbsoluteDate<T>) - Method in class org.orekit.frames.L1TransformProvider
-
- getTransform(FieldAbsoluteDate<T>) - Method in class org.orekit.frames.ShiftingTransformProvider
-
- getTransform(FieldAbsoluteDate<T>) - Method in interface org.orekit.frames.TransformProvider
-
- getTransformation() - 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.utils.FieldTimeSpanMap
-
Get an unmodifiable view of the sorted transitions.
- getTransitions() - Method in class org.orekit.utils.TimeSpanMap
-
Get an unmodifiable view of the sorted transitions.
- 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.
- getTransmitBand() - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData
-
Getter for the transmitBand.
- getTransmitDelays() - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData
-
Getter for the transmitDelays.
- getTrigger() - Method in class org.orekit.forces.maneuvers.ImpulseManeuver
-
Get the triggering event.
- getTriggeredIncreasing() - Method in enum org.orekit.propagation.events.FilterType
-
Get the increasing status of triggered events.
- 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() - Static method in class org.orekit.time.TimeScalesFactory
-
Get the Terrestrial Time scale.
- getTurnaroundDenominator() - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData
-
Getter for the turnaroundDenominator.
- getTurnaroundNumerator() - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData
-
Getter for the turnaroundNumerator.
- getType() - Method in class org.orekit.files.sp3.SP3File
-
- 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.
- getTypeObs() - Method in class org.orekit.gnss.RinexLoader.Parser.PhaseShiftCorrection
-
Get the Carrier Phase Observation Code.
- getTypesObsScaled() - Method in class org.orekit.gnss.RinexLoader.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.
- 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.
- 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(double, double, TideSystem, double[][], double[][]) - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory
-
- 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(NormalizedSphericalHarmonicsProvider) - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory
-
- 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.gnss.GPSAlmanac
-
Gets the average URA number.
- getUranus() - Static method in class org.orekit.bodies.CelestialBodyFactory
-
Get the Uranus singleton body.
- getUseableStartTime() - Method in class org.orekit.files.ccsds.OEMFile.EphemeridesBlock
-
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.OEMFile.EphemeridesBlock
-
Get end of useable time span covered by ephemerides data, it may be
necessary to allow for proper interpolation.
- getUserDefinedParameters() - Method in class org.orekit.files.ccsds.OGMFile
-
Get the map of user defined parameter keywords and their corresponding values.
- getUT1(EOPHistory) - Static method in class org.orekit.time.TimeScalesFactory
-
Get the Universal Time 1 scale.
- getUT1(IERSConventions, boolean) - 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.
- 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.
- getV() - Method in class org.orekit.bodies.Ellipse
-
Get the unit vector along the minor axis.
- getValidFrom() - Method in class org.orekit.gnss.antenna.SatelliteAntenna
-
Get start of validity.
- getValidFUntil() - 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.ObservationData
-
Get the observed value.
- getValue() - Method in class org.orekit.utils.ParameterDriver
-
Get current parameter 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) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GammaMnsFunction
-
Get Γ function value.
- 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(int, int, int, DerivativeStructure) - 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(DSFactory, Map<String, Integer>) - Method in class org.orekit.utils.ParameterDriver
-
Get the value as a derivative structure.
- getValuesSamples() - Method in class org.orekit.utils.InterpolationTableLoader
-
Returns a copy of the values samples for the interpolation function.
- 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.
- getVectorG() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
-
Get equinoctial frame vector g.
- getVectorW() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
-
Get equinoctial frame vector w.
- 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.ccsds.OPMFile
-
Get velocity vector.
- 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() - Method in class org.orekit.utils.FieldPVCoordinates
-
Gets the velocity.
- getVelocity() - Method in class org.orekit.utils.PVCoordinates
-
Gets the velocity.
- getVelocity(AbsoluteDate, Vector3D, Frame) - Method in interface org.orekit.forces.drag.atmosphere.Atmosphere
-
Get the inertial velocity of atmosphere molecules.
- getVelocity(FieldAbsoluteDate<T>, FieldVector3D<T>, Frame) - Method in interface org.orekit.forces.drag.atmosphere.Atmosphere
-
Get the inertial velocity of atmosphere molecules.
- getVenus() - Static method in class org.orekit.bodies.CelestialBodyFactory
-
Get the Venus singleton body.
- getVertices() - Method in class org.orekit.models.earth.tessellation.Tile
-
Get the four vertices.
- getVmns(int, int, int) - Static method in class org.orekit.propagation.semianalytical.dsst.utilities.CoefficientsFactory
-
Get the Vn,sm coefficient from Vn,s.
- getWarmup() - Method in class org.orekit.estimation.measurements.modifiers.OutlierFilter
-
Get the value of warmup iterations.
- getWaterVaporPressure() - Method in class org.orekit.models.earth.GlobalPressureTemperature2Model
-
Returns the water vapor pressure at the station [hPa].
- getWaves() - Method in class org.orekit.forces.gravity.potential.OceanTidesReader
-
Get the loaded waves.
- getWeek() - Method in class org.orekit.gnss.GPSAlmanac
-
- getWeek() - Method in interface org.orekit.propagation.analytical.gnss.GPSOrbitalElements
-
Gets the Reference Week of the GPS orbit.
- getWeekNumber() - Method in class org.orekit.time.GPSDate
-
- 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.
- getWgs84(Frame) - Static method in class org.orekit.models.earth.ReferenceEllipsoid
-
Get the WGS84 ellipsoid, attached to the given body frame.
- getWMM(double) - Static method in class org.orekit.models.earth.GeoMagneticFieldFactory
-
Get the WMM model for the given year.
- getX() - Method in class org.orekit.frames.EOPEntry
-
Get the X component of the pole motion.
- getXM10(AbsoluteDate) - Method in interface org.orekit.forces.drag.atmosphere.JB2008InputParameters
-
Get the MG2 index scaled to F10.
- getXM10B(AbsoluteDate) - Method in interface org.orekit.forces.drag.atmosphere.JB2008InputParameters
-
Get the MG2 81-day average centered index.
- getXp() - Method in class org.orekit.frames.FieldPoleCorrection
-
Get the xp parameter.
- getXp() - Method in class org.orekit.frames.PoleCorrection
-
Get the xp parameter.
- getXYSpXY2Function() - 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.
- getY10(AbsoluteDate) - Method in interface org.orekit.forces.drag.atmosphere.JB2008InputParameters
-
Get the Solar X-Ray & Lya index scaled to F10.
- getY10B(AbsoluteDate) - Method in interface org.orekit.forces.drag.atmosphere.JB2008InputParameters
-
Get the Solar X-Ray & Lya 81-day ave.
- getYawAngle(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.YawCompensation
-
Compute the yaw compensation angle at date.
- getYawAngle(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.YawCompensation
-
Compute the yaw compensation angle at date.
- 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.
- getYp() - Method in class org.orekit.frames.FieldPoleCorrection
-
Get the yp parameter.
- getYp() - Method in class org.orekit.frames.PoleCorrection
-
Get the yp parameter.
- 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.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).
- getZone() - Method in class org.orekit.propagation.events.FieldOfView
-
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.
- GLO - org.orekit.files.sp3.SP3File.TimeSystem
-
GLONASS.
- GlobalMappingFunctionModel - Class in org.orekit.models.earth
-
The Global Mapping Function model for radio techniques.
- GlobalMappingFunctionModel(double, double) - Constructor for class org.orekit.models.earth.GlobalMappingFunctionModel
-
Build a new instance.
- GlobalPressureTemperature2Model - Class in org.orekit.models.earth
-
The Global Pressure and Temperature 2 (GPT2) model.
- GlobalPressureTemperature2Model(double, double, Geoid) - Constructor for class org.orekit.models.earth.GlobalPressureTemperature2Model
-
Constructor with default supported names.
- GlobalPressureTemperature2Model(String, double, double, Geoid) - Constructor for class org.orekit.models.earth.GlobalPressureTemperature2Model
-
Constructor with supported names given by user.
- GlobalPressureTemperatureModel - Class in org.orekit.models.earth
-
The Global Pressure and Temperature model.
- GlobalPressureTemperatureModel(double, double, Frame) - Constructor for class org.orekit.models.earth.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 - org.orekit.files.sp3.SP3File.SP3FileType
-
GLONASS only file.
- GLONASS - org.orekit.gnss.antenna.SatelliteAntennaCode
-
Deprecated.
GLONASS : GLONASS no.
- GLONASS - org.orekit.gnss.antenna.SatelliteType
-
GLONASS : GLONASS no.
- GLONASS - org.orekit.gnss.SatelliteSystem
-
GLONASS system.
- GLONASS_K1 - org.orekit.gnss.antenna.SatelliteAntennaCode
-
Deprecated.
GLONASS-K1 : IGS SVN R801-R802 (GLO no.
- GLONASS_K1 - org.orekit.gnss.antenna.SatelliteType
-
GLONASS-K1 : IGS SVN R801-R802 (GLO no.
- GLONASS_K2 - org.orekit.gnss.antenna.SatelliteAntennaCode
-
Deprecated.
GLONASS-K2.
- GLONASS_K2 - org.orekit.gnss.antenna.SatelliteType
-
GLONASS-K2.
- GLONASS_M - org.orekit.gnss.antenna.SatelliteAntennaCode
-
Deprecated.
GLONASS-M : GLONASS no.
- GLONASS_M - org.orekit.gnss.antenna.SatelliteType
-
GLONASS-M : GLONASS no.
- GLONASSScale - Class in org.orekit.time
-
GLONASS time scale.
- GM - org.orekit.files.ccsds.Keyword
-
Gravitational coefficient.
- GMST - org.orekit.files.ccsds.CcsdsTimeScale
-
Greenwich Mean Sidereal Time.
- GMSTScale - Class in org.orekit.time
-
Greenwich Mean Sidereal Time.
- GNSSAttitudeProvider - Interface in org.orekit.gnss.attitude
-
Attitude providers for navigation satellites.
- GPS - org.orekit.files.ccsds.CcsdsTimeScale
-
Global Positioning System.
- GPS - org.orekit.files.sp3.SP3File.SP3FileType
-
GPS only file.
- GPS - org.orekit.files.sp3.SP3File.TimeSystem
-
Global Positioning System.
- GPS - org.orekit.gnss.SatelliteSystem
-
GPS system.
- 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.GPSOrbitalElements
-
WGS 84 value of the Earth's universal gravitational parameter for GPS user in m³/s².
- GPS_PI - Static variable in interface org.orekit.propagation.analytical.gnss.GPSOrbitalElements
-
Value of Pi for conversion from semicircles to radian.
- GPS_WEEK_IN_SECONDS - Static variable in interface org.orekit.propagation.analytical.gnss.GPSOrbitalElements
-
Duration of the GPS week in seconds.
- GPS_WEEK_NB - Static variable in interface org.orekit.propagation.analytical.gnss.GPSOrbitalElements
-
Number of weeks in the GPS cycle.
- GPSAlmanac - Class in org.orekit.gnss
-
This class holds a GPS almanac as read from SEM or YUMA files.
- GPSAlmanac(String, int, int, int, double, double, double, double, double, double, double, double, double, double, int, int, int) - Constructor for class org.orekit.gnss.GPSAlmanac
-
Constructor.
- GPSBlockIIA - Class in org.orekit.gnss.attitude
-
Attitude providers for GPS block IIR navigation satellites.
- GPSBlockIIA(double, double, AbsoluteDate, AbsoluteDate, ExtendedPVCoordinatesProvider, Frame) - Constructor for class org.orekit.gnss.attitude.GPSBlockIIA
-
Simple constructor.
- GPSBlockIIA(double, double, AbsoluteDate, AbsoluteDate, ExtendedPVCoordinatesProvider, Frame, int) - Constructor for class org.orekit.gnss.attitude.GPSBlockIIA
-
- 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 IIF navigation satellites.
- GPSBlockIIR(double, AbsoluteDate, AbsoluteDate, ExtendedPVCoordinatesProvider, Frame) - Constructor for class org.orekit.gnss.attitude.GPSBlockIIR
-
Simple constructor.
- GPSDate - Class in org.orekit.time
-
Container for date in GPS form.
- GPSDate(int, double) - Constructor for class org.orekit.time.GPSDate
-
Build an instance corresponding to a GPS date.
- GPSDate(AbsoluteDate) - Constructor for class org.orekit.time.GPSDate
-
Build an instance from an absolute date.
- GPSOrbitalElements - Interface in org.orekit.propagation.analytical.gnss
-
This interface provides the minimal set of orbital elements needed by the
GPSPropagator
.
- GPSPropagator - Class in org.orekit.propagation.analytical.gnss
-
- GPSPropagator.Builder - Class in org.orekit.propagation.analytical.gnss
-
This nested class aims at building a GPSPropagator.
- 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.
- GRAVITY_FIELD_NORMALIZATION_UNDERFLOW - org.orekit.errors.OrekitMessages
-
- GravityFieldFactory - Class in org.orekit.forces.gravity.potential
-
Factory used to read gravity field files in several supported formats.
- GRC - org.orekit.files.ccsds.CCSDSFrame
-
Greenwich Rotating Coordinates.
- 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.
- 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.
- GTOD_CONVENTIONS_1996_ACCURATE_EOP - org.orekit.frames.Predefined
-
GTOD, IERS 1996 conventions, with accurate EOP interpolation.
- GTOD_CONVENTIONS_1996_SIMPLE_EOP - org.orekit.frames.Predefined
-
GTOD, IERS 1996 conventions, with simple EOP interpolation.
- GTOD_CONVENTIONS_2003_ACCURATE_EOP - org.orekit.frames.Predefined
-
GTOD, IERS 2003 conventions, with accurate EOP interpolation.
- GTOD_CONVENTIONS_2003_SIMPLE_EOP - org.orekit.frames.Predefined
-
GTOD, IERS 2003 conventions, with simple EOP interpolation.
- GTOD_CONVENTIONS_2010_ACCURATE_EOP - org.orekit.frames.Predefined
-
GTOD, IERS 2010 conventions, with accurate EOP interpolation.
- GTOD_CONVENTIONS_2010_SIMPLE_EOP - org.orekit.frames.Predefined
-
GTOD, IERS 2010 conventions, with simple EOP interpolation.
- GTOD_WITHOUT_EOP_CORRECTIONS - org.orekit.frames.Predefined
-
GTOD, IERS 1996 conventions without EOP corrections.
- 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) - Constructor for class org.orekit.frames.GTODProvider
-
Simple constructor.
- GZIP_FILE_PATTERN - Static variable in interface org.orekit.data.DataProvider
-
- GzipFilter - Class in org.orekit.data
-
Filter for gzip compressed data.
- GzipFilter() - Constructor for class org.orekit.data.GzipFilter
-