A B C D E F G H I J K L M N O P Q R S T U V W X Y Z

A

a - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator

final semi major axis.

a - Variable in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution

a.

A - Variable in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution

A = sqrt(μ * a).

a0dp - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator

original recovered semi major axis.

AbsoluteDate - Class in org.orekit.time

This class represents a specific instant in time.

AbsoluteDate() - Constructor for class org.orekit.time.AbsoluteDate

Create an instance with a default value (AbsoluteDate.J2000_EPOCH).

AbsoluteDate(String, TimeScale) - Constructor for class org.orekit.time.AbsoluteDate

Build an instance from a location (parsed from a string) in a time scale.

AbsoluteDate(DateTimeComponents, TimeScale) - Constructor for class org.orekit.time.AbsoluteDate

Build an instance from a location in a time scale.

AbsoluteDate(DateComponents, TimeComponents, TimeScale) - Constructor for class org.orekit.time.AbsoluteDate

Build an instance from a location in a time scale.

AbsoluteDate(int, int, int, int, int, double, TimeScale) - Constructor for class org.orekit.time.AbsoluteDate

Build an instance from a location in a time scale.

AbsoluteDate(int, Month, int, int, int, double, TimeScale) - Constructor for class org.orekit.time.AbsoluteDate

Build an instance from a location in a time scale.

AbsoluteDate(DateComponents, TimeScale) - Constructor for class org.orekit.time.AbsoluteDate

Build an instance from a location in a time scale.

AbsoluteDate(int, int, int, TimeScale) - Constructor for class org.orekit.time.AbsoluteDate

Build an instance from a location in a time scale.

AbsoluteDate(int, Month, int, TimeScale) - Constructor for class org.orekit.time.AbsoluteDate

Build an instance from a location in a time scale.

AbsoluteDate(Date, TimeScale) - Constructor for class org.orekit.time.AbsoluteDate

Build an instance from a location in a time scale.

AbsoluteDate(AbsoluteDate, double) - Constructor for class org.orekit.time.AbsoluteDate

Build an instance from an elapsed duration since to another instant.

AbsoluteDate(AbsoluteDate, double, TimeScale) - Constructor for class org.orekit.time.AbsoluteDate

Build an instance from an apparent clock offset with respect to another instant in the perspective of a specific time scale.

ABSORPTION_COEFFICIENT - Static variable in interface org.orekit.forces.radiation.RadiationSensitive

Parameter name for absorption coefficient.

AbstractAnalyticalPropagator - Class in org.orekit.propagation.analytical

Common handling of Propagator methods for analytical propagators.

AbstractAnalyticalPropagator(AttitudeProvider) - Constructor for class org.orekit.propagation.analytical.AbstractAnalyticalPropagator

Build a new instance.

AbstractDetector<T extends EventDetector> - Class in org.orekit.propagation.events

Common parts shared by several orbital events finders.

AbstractDetector(double, double, int, EventHandler<T>) - Constructor for class org.orekit.propagation.events.AbstractDetector

Build a new instance.

AbstractGaussianContribution - Class in org.orekit.propagation.semianalytical.dsst.forces

Common handling of DSSTForceModel methods for Gaussian contributions to DSST propagation.

AbstractGaussianContribution(double, ForceModel) - Constructor for class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution

Build a new instance.

AbstractIntegratedPropagator - Class in org.orekit.propagation.integration

Common handling of Propagator methods for both numerical and semi-analytical propagators.

AbstractIntegratedPropagator(AbstractIntegrator, boolean) - Constructor for class org.orekit.propagation.integration.AbstractIntegratedPropagator

Build a new instance.

AbstractIntegratedPropagator.MainStateEquations - Interface in org.orekit.propagation.integration

Differential equations for the main state (orbit, attitude and mass).

AbstractPropagator - Class in org.orekit.propagation

Common handling of Propagator methods for analytical propagators.

AbstractPropagator() - Constructor for class org.orekit.propagation.AbstractPropagator

Build a new instance.

AbstractPropagatorConverter - Class in org.orekit.propagation.conversion

Common handling of PropagatorConverter methods for propagators conversions.

AbstractPropagatorConverter(PropagatorBuilder, double, int) - Constructor for class org.orekit.propagation.conversion.AbstractPropagatorConverter

Build a new instance.

accelerationDerivatives(AbsoluteDate, Frame, FieldVector3D<DerivativeStructure>, FieldVector3D<DerivativeStructure>, FieldRotation<DerivativeStructure>, DerivativeStructure) - Method in class org.orekit.forces.drag.DragForce

Compute acceleration derivatives with respect to state parameters.

accelerationDerivatives(SpacecraftState, String) - Method in class org.orekit.forces.drag.DragForce

Compute acceleration derivatives with respect to additional parameters.

accelerationDerivatives(AbsoluteDate, Frame, FieldVector3D<DerivativeStructure>, FieldVector3D<DerivativeStructure>, FieldRotation<DerivativeStructure>, DerivativeStructure) - Method in interface org.orekit.forces.ForceModel

Compute acceleration derivatives with respect to state parameters.

accelerationDerivatives(SpacecraftState, String) - Method in interface org.orekit.forces.ForceModel

Compute acceleration derivatives with respect to additional parameters.

accelerationDerivatives(AbsoluteDate, Frame, FieldVector3D<DerivativeStructure>, FieldVector3D<DerivativeStructure>, FieldRotation<DerivativeStructure>, DerivativeStructure) - Method in class org.orekit.forces.gravity.CunninghamAttractionModel

Compute acceleration derivatives with respect to state parameters.

accelerationDerivatives(SpacecraftState, String) - Method in class org.orekit.forces.gravity.CunninghamAttractionModel

Compute acceleration derivatives with respect to additional parameters.

accelerationDerivatives(AbsoluteDate, Frame, FieldVector3D<DerivativeStructure>, FieldVector3D<DerivativeStructure>, FieldRotation<DerivativeStructure>, DerivativeStructure) - Method in class org.orekit.forces.gravity.DrozinerAttractionModel

Compute acceleration derivatives with respect to state parameters.

accelerationDerivatives(SpacecraftState, String) - Method in class org.orekit.forces.gravity.DrozinerAttractionModel

Compute acceleration derivatives with respect to additional parameters.

accelerationDerivatives(AbsoluteDate, Frame, FieldVector3D<DerivativeStructure>, FieldVector3D<DerivativeStructure>, FieldRotation<DerivativeStructure>, DerivativeStructure) - Method in class org.orekit.forces.gravity.HolmesFeatherstoneAttractionModel

Compute acceleration derivatives with respect to state parameters.

accelerationDerivatives(SpacecraftState, String) - Method in class org.orekit.forces.gravity.HolmesFeatherstoneAttractionModel

Compute acceleration derivatives with respect to additional parameters.

accelerationDerivatives(AbsoluteDate, Frame, FieldVector3D<DerivativeStructure>, FieldVector3D<DerivativeStructure>, FieldRotation<DerivativeStructure>, DerivativeStructure) - Method in class org.orekit.forces.gravity.NewtonianAttraction

Compute acceleration derivatives with respect to state parameters.

accelerationDerivatives(SpacecraftState, String) - Method in class org.orekit.forces.gravity.NewtonianAttraction

Compute acceleration derivatives with respect to additional parameters.

accelerationDerivatives(AbsoluteDate, Frame, FieldVector3D<DerivativeStructure>, FieldVector3D<DerivativeStructure>, FieldRotation<DerivativeStructure>, DerivativeStructure) - Method in class org.orekit.forces.gravity.OceanTides

Compute acceleration derivatives with respect to state parameters.

accelerationDerivatives(SpacecraftState, String) - Method in class org.orekit.forces.gravity.OceanTides

Compute acceleration derivatives with respect to additional parameters.

accelerationDerivatives(AbsoluteDate, Frame, FieldVector3D<DerivativeStructure>, FieldVector3D<DerivativeStructure>, FieldRotation<DerivativeStructure>, DerivativeStructure) - Method in class org.orekit.forces.gravity.Relativity

accelerationDerivatives(SpacecraftState, String) - Method in class org.orekit.forces.gravity.Relativity

accelerationDerivatives(AbsoluteDate, Frame, FieldVector3D<DerivativeStructure>, FieldVector3D<DerivativeStructure>, FieldRotation<DerivativeStructure>, DerivativeStructure) - Method in class org.orekit.forces.gravity.SolidTides

Compute acceleration derivatives with respect to state parameters.

accelerationDerivatives(SpacecraftState, String) - Method in class org.orekit.forces.gravity.SolidTides

Compute acceleration derivatives with respect to additional parameters.

accelerationDerivatives(AbsoluteDate, Frame, FieldVector3D<DerivativeStructure>, FieldVector3D<DerivativeStructure>, FieldRotation<DerivativeStructure>, DerivativeStructure) - Method in class org.orekit.forces.gravity.ThirdBodyAttraction

Compute acceleration derivatives with respect to state parameters.

accelerationDerivatives(SpacecraftState, String) - Method in class org.orekit.forces.gravity.ThirdBodyAttraction

Compute acceleration derivatives with respect to additional parameters.

accelerationDerivatives(AbsoluteDate, Frame, FieldVector3D<DerivativeStructure>, FieldVector3D<DerivativeStructure>, FieldRotation<DerivativeStructure>, DerivativeStructure) - Method in class org.orekit.forces.maneuvers.ConstantThrustManeuver

Compute acceleration derivatives with respect to state parameters.

accelerationDerivatives(SpacecraftState, String) - Method in class org.orekit.forces.maneuvers.ConstantThrustManeuver

Compute acceleration derivatives with respect to additional parameters.

accelerationDerivatives(AbsoluteDate, Frame, FieldVector3D<DerivativeStructure>, FieldVector3D<DerivativeStructure>, FieldRotation<DerivativeStructure>, DerivativeStructure) - Method in class org.orekit.forces.radiation.SolarRadiationPressure

Compute acceleration derivatives with respect to state parameters.

accelerationDerivatives(SpacecraftState, String) - Method in class org.orekit.forces.radiation.SolarRadiationPressure

Compute acceleration derivatives with respect to additional parameters.

accelerationDerivatives(AbsoluteDate, Frame, FieldVector3D<DerivativeStructure>, FieldVector3D<DerivativeStructure>, FieldRotation<DerivativeStructure>, DerivativeStructure) - Method in class org.orekit.propagation.numerical.Jacobianizer

Compute acceleration and derivatives with respect to state.

accelerationDerivatives(SpacecraftState, String) - Method in class org.orekit.propagation.numerical.Jacobianizer

Compute acceleration and derivatives with respect to parameter.

acceptStep(AbsoluteDate, double) - Method in class org.orekit.propagation.analytical.AbstractAnalyticalPropagator

Accept a step, triggering events and step handlers.

AdamsBashforthIntegratorBuilder - Class in org.orekit.propagation.conversion

Builder for AdamsBashforthIntegrator.

AdamsBashforthIntegratorBuilder(int, double, double, double) - Constructor for class org.orekit.propagation.conversion.AdamsBashforthIntegratorBuilder

Build a new instance.

AdamsMoultonIntegratorBuilder - Class in org.orekit.propagation.conversion

Builder for AdamsMoultonIntegrator.

AdamsMoultonIntegratorBuilder(int, double, double, double) - Constructor for class org.orekit.propagation.conversion.AdamsMoultonIntegratorBuilder

Build a new instance.

AdapterPropagator - Class in org.orekit.propagation.analytical

Orbit propagator that adapts an underlying propagator, adding differential effects.

AdapterPropagator(Propagator) - Constructor for class org.orekit.propagation.analytical.AdapterPropagator

Build a propagator from an underlying reference propagator.

AdapterPropagator.DifferentialEffect - Interface in org.orekit.propagation.analytical

Interface for orbit differential effects.

add(OrekitStepHandler) - Method in class org.orekit.propagation.sampling.OrekitStepHandlerMultiplexer

Add a step handler.

add(PolynomialFunctionMatrix) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.PolynomialFunctionMatrix

Add the argument matrix with the current matrix.

addAcceleration(Vector3D, Frame) - Method in interface org.orekit.propagation.numerical.TimeDerivativesEquations

Add the contribution of an acceleration expressed in some inertial frame.

addAdditionalEquations(AdditionalEquations) - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator

Add a set of user-specified equations to be integrated along with the orbit propagation.

addAdditionalState(String, double...) - Method in class org.orekit.propagation.SpacecraftState

Add an additional state.

addAdditionalStateProvider(AdditionalStateProvider) - Method in class org.orekit.propagation.AbstractPropagator

Add a set of user-specified state parameters to be computed along with the orbit propagation.

addAdditionalStateProvider(AdditionalStateProvider) - Method in interface org.orekit.propagation.Propagator

Add a set of user-specified state parameters to be computed along with the orbit propagation.

addCelestialBodyLoader(String, CelestialBodyLoader) - Static method in class org.orekit.bodies.CelestialBodyFactory

Add a loader for celestial bodies.

addChild(OrphanFrame, Transform, boolean) - Method in class org.orekit.frames.OrphanFrame

Add a child.

addChild(OrphanFrame, TransformProvider, boolean) - Method in class org.orekit.frames.OrphanFrame

Add a child.

addContribution(SpacecraftState, TimeDerivativesEquations) - Method in class org.orekit.forces.drag.DragForce

Compute the contribution of the drag to the perturbing acceleration.

addContribution(SpacecraftState, TimeDerivativesEquations) - Method in interface org.orekit.forces.ForceModel

Compute the contribution of the force model to the perturbing acceleration.

addContribution(SpacecraftState, TimeDerivativesEquations) - Method in class org.orekit.forces.gravity.CunninghamAttractionModel

Compute the contribution of the force model to the perturbing acceleration.

addContribution(SpacecraftState, TimeDerivativesEquations) - Method in class org.orekit.forces.gravity.DrozinerAttractionModel

Compute the contribution of the force model to the perturbing acceleration.

addContribution(SpacecraftState, TimeDerivativesEquations) - Method in class org.orekit.forces.gravity.HolmesFeatherstoneAttractionModel

Compute the contribution of the force model to the perturbing acceleration.

addContribution(SpacecraftState, TimeDerivativesEquations) - Method in class org.orekit.forces.gravity.NewtonianAttraction

Compute the contribution of the force model to the perturbing acceleration.

addContribution(SpacecraftState, TimeDerivativesEquations) - Method in class org.orekit.forces.gravity.OceanTides

Compute the contribution of the force model to the perturbing acceleration.

addContribution(BodiesElements, double[][], double[][]) - Method in class org.orekit.forces.gravity.potential.OceanTidesWave

Add the contribution of the wave to Stokes coefficients.

addContribution(SpacecraftState, TimeDerivativesEquations) - Method in class org.orekit.forces.gravity.Relativity

addContribution(SpacecraftState, TimeDerivativesEquations) - Method in class org.orekit.forces.gravity.SolidTides

Compute the contribution of the force model to the perturbing acceleration.

addContribution(SpacecraftState, TimeDerivativesEquations) - Method in class org.orekit.forces.gravity.ThirdBodyAttraction

Compute the contribution of the force model to the perturbing acceleration.

addContribution(SpacecraftState, TimeDerivativesEquations) - Method in class org.orekit.forces.maneuvers.ConstantThrustManeuver

Compute the contribution of the force model to the perturbing acceleration.

addContribution(SpacecraftState, TimeDerivativesEquations) - Method in class org.orekit.forces.radiation.SolarRadiationPressure

Compute the contribution of the force model to the perturbing acceleration.

addDefaultCelestialBodyLoader(String) - Static method in class org.orekit.bodies.CelestialBodyFactory

Add the default loaders for all predefined celestial bodies.

addDefaultCelestialBodyLoader(String, String) - Static method in class org.orekit.bodies.CelestialBodyFactory

Add the default loaders for celestial bodies.

addDefaultEOP1980HistoryLoaders(String, String, String, String, String) - Static method in class org.orekit.frames.FramesFactory

Add the default loaders EOP history (IAU 1980 precession/nutation).

addDefaultEOP2000HistoryLoaders(String, String, String, String, String) - Static method in class org.orekit.frames.FramesFactory

Add the default loaders for EOP history (IAU 2000/2006 precession/nutation).

addDefaultOceanTidesReaders() - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory

Add the default READERS for ocean tides.

addDefaultPotentialCoefficientsReaders() - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory

Add the default readers for gravity fields.

addDefaultProviders() - Method in class org.orekit.data.DataProvidersManager

Add the default providers configuration.

addDefaultUTCTAILoader() - Static method in class org.orekit.time.TimeScalesFactory

Add the default loader for UTC-TAI offsets history files.

addEffect(AdapterPropagator.DifferentialEffect) - Method in class org.orekit.propagation.analytical.AdapterPropagator

Add a differential effect.

addEOPHistoryLoader(IERSConventions, EOPHistoryLoader) - Static method in class org.orekit.frames.FramesFactory

Add a loader for Earth Orientation Parameters history.

addEventDate(AbsoluteDate) - Method in class org.orekit.propagation.events.DateDetector

Add an event date.

addEventDetector(T) - Method in class org.orekit.propagation.AbstractPropagator

Add an event detector.

addEventDetector(T) - Method in class org.orekit.propagation.analytical.AbstractAnalyticalPropagator

Add an event detector.

addEventDetector(EventDetector) - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator

Add an event detector.

addEventDetector(T) - Method in interface org.orekit.propagation.Propagator

Add an event detector.

addForceModel(ForceModel) - Method in class org.orekit.propagation.conversion.NumericalPropagatorBuilder

Add a force model to the global perturbation model.

addForceModel(ForceModel) - Method in class org.orekit.propagation.numerical.NumericalPropagator

Add a force model to the global perturbation model.

addForceModel(DSSTForceModel) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator

Add a force model to the global perturbation model.

addGridPoint(AbsoluteDate, double) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.ShortPeriodicsInterpolatedCoefficient

Add a point to the interpolation grid.

AdditionalEquations - Interface in org.orekit.propagation.integration

This interface allows users to add their own differential equations to a numerical propagator.

AdditionalStateProvider - Interface in org.orekit.propagation

This interface represents providers for additional state data beyond SpacecraftState.

addKeplerContribution(PositionAngle, double, double[]) - Method in class org.orekit.orbits.CartesianOrbit

Add the contribution of the Keplerian motion to parameters derivatives

addKeplerContribution(PositionAngle, double, double[]) - Method in class org.orekit.orbits.CircularOrbit

Add the contribution of the Keplerian motion to parameters derivatives

addKeplerContribution(PositionAngle, double, double[]) - Method in class org.orekit.orbits.EquinoctialOrbit

Add the contribution of the Keplerian motion to parameters derivatives

addKeplerContribution(PositionAngle, double, double[]) - Method in class org.orekit.orbits.KeplerianOrbit

Add the contribution of the Keplerian motion to parameters derivatives

addKeplerContribution(PositionAngle, double, double[]) - Method in class org.orekit.orbits.Orbit

Add the contribution of the Keplerian motion to parameters derivatives

addKeplerContribution(double) - Method in interface org.orekit.propagation.numerical.TimeDerivativesEquations

Add the contribution of the Kepler evolution.

addMassDerivative(double) - Method in interface org.orekit.propagation.numerical.TimeDerivativesEquations

Add the contribution of the flow rate (dm/dt).

addOceanTidesReader(OceanTidesReader) - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory

Add a reader for ocean tides.

addOffset(AngularCoordinates) - Method in class org.orekit.utils.AngularCoordinates

Add an offset from the instance.

addOffset(FieldAngularCoordinates<T>) - Method in class org.orekit.utils.FieldAngularCoordinates

Add an offset from the instance.

addOffset(AngularCoordinates) - Method in class org.orekit.utils.TimeStampedAngularCoordinates

Add an offset from the instance.

addOffset(FieldAngularCoordinates<T>) - Method in class org.orekit.utils.TimeStampedFieldAngularCoordinates

Add an offset from the instance.

addPoint(AbsoluteDate, double) - Method in class org.orekit.utils.SecularAndHarmonic

Add a fitting point.

addPotentialCoefficientsReader(PotentialCoefficientsReader) - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory

Add a reader for gravity fields.

addProvider(DataProvider) - Method in class org.orekit.data.DataProvidersManager

Add a data provider to the supported list.

addSatellite(String) - Method in class org.orekit.files.sp3.SP3File

Add a new satellite with a given identifier to the list of stored satellites.

addSatelliteCoordinate(String, SatelliteTimeCoordinate) - Method in class org.orekit.files.sp3.SP3File

Adds a new P/V coordinate for a given satellite.

addSwitchingCondition(AttitudeProvider, T, boolean, boolean, AttitudeProvider) - Method in class org.orekit.attitudes.AttitudesSequence

Add a switching condition between two attitude providers.

addUTCTAILoader(UTCTAILoader) - Static method in class org.orekit.time.TimeScalesFactory

Add a loader for UTC-TAI offsets history files.

addWaveCoefficients(int, int, int, double, double, double, double, int, String) - Method in class org.orekit.forces.gravity.potential.OceanTidesReader

Add parsed coefficients.

addXYZAcceleration(double, double, double) - Method in interface org.orekit.propagation.numerical.TimeDerivativesEquations

Add the contribution of an acceleration expressed in the inertial frame (it is important to make sure this acceleration is defined in the same frame as the orbit) .

afterIntegration() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator

Method called just after integration.

afterIntegration() - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator

Method called just after integration.

AlignmentDetector - Class in org.orekit.propagation.events

Finder for satellite/body alignment events.

AlignmentDetector(Orbit, PVCoordinatesProvider, double) - Constructor for class org.orekit.propagation.events.AlignmentDetector

Build a new alignment detector.

AlignmentDetector(double, Orbit, PVCoordinatesProvider, double) - Constructor for class org.orekit.propagation.events.AlignmentDetector

Build a new alignment detector.

AltitudeDetector - Class in org.orekit.propagation.events

Finder for satellite altitude crossing events.

AltitudeDetector(double, BodyShape) - Constructor for class org.orekit.propagation.events.AltitudeDetector

Build a new altitude detector.

AltitudeDetector(double, double, BodyShape) - Constructor for class org.orekit.propagation.events.AltitudeDetector

Build a new altitude detector.

AltitudeDetector(double, double, double, BodyShape) - Constructor for class org.orekit.propagation.events.AltitudeDetector

Build a new altitude detector.

AngularCoordinates - Class in org.orekit.utils

Simple container for rotation/rotation rate/rotation acceleration triplets.

AngularCoordinates() - Constructor for class org.orekit.utils.AngularCoordinates

Simple constructor.

AngularCoordinates(Rotation, Vector3D) - Constructor for class org.orekit.utils.AngularCoordinates

Builds a rotation/rotation rate pair.

AngularCoordinates(Rotation, Vector3D, Vector3D) - Constructor for class org.orekit.utils.AngularCoordinates

Builds a rotation/rotation rate/rotation acceleration triplet.

AngularCoordinates(PVCoordinates, PVCoordinates, PVCoordinates, PVCoordinates, double) - Constructor for class org.orekit.utils.AngularCoordinates

Build the rotation that transforms a pair of pv coordinates into another one.

AngularCoordinates(PVCoordinates, PVCoordinates) - Constructor for class org.orekit.utils.AngularCoordinates

Build one of the rotations that transform one pv coordinates into another one.

AngularCoordinates(FieldRotation<DerivativeStructure>) - Constructor for class org.orekit.utils.AngularCoordinates

Builds a AngularCoordinates from a FieldRotation<DerivativeStructure>.

AngularDerivativesFilter - Enum in org.orekit.utils

Enumerate for selecting which derivatives to use in TimeStampedAngularCoordinates and TimeStampedFieldAngularCoordinates interpolation.

apply(Orbit) - Method in class org.orekit.forces.maneuvers.SmallManeuverAnalyticalModel

Compute the effect of the maneuver on an orbit.

apply(SpacecraftState) - Method in class org.orekit.forces.maneuvers.SmallManeuverAnalyticalModel

Compute the effect of the maneuver on a spacecraft state.

apply(SpacecraftState) - Method in interface org.orekit.propagation.analytical.AdapterPropagator.DifferentialEffect

Apply the effect to a spacecraft state.

apply(Orbit) - Method in class org.orekit.propagation.analytical.J2DifferentialEffect

Compute the effect of the maneuver on an orbit.

apply(SpacecraftState) - Method in class org.orekit.propagation.analytical.J2DifferentialEffect

Apply the effect to a spacecraft state.

applyTo(PVCoordinates) - Method in class org.orekit.utils.AngularCoordinates

Apply the rotation to a pv coordinates.

applyTo(TimeStampedPVCoordinates) - Method in class org.orekit.utils.AngularCoordinates

Apply the rotation to a pv coordinates.

approximateAsPolynomialOnly(int, AbsoluteDate, int, int, AbsoluteDate, AbsoluteDate, double) - Method in class org.orekit.utils.SecularAndHarmonic

Approximate an already fitted model to polynomial only terms.

ApsideDetector - Class in org.orekit.propagation.events

Finder for apside crossing events.

ApsideDetector(Orbit) - Constructor for class org.orekit.propagation.events.ApsideDetector

Build a new instance.

ApsideDetector(double, Orbit) - Constructor for class org.orekit.propagation.events.ApsideDetector

Build a new instance.

ARC_SECONDS_TO_RADIANS - Static variable in interface org.orekit.utils.Constants

Conversion factor from arc seconds to radians: 2*PI/(360*60*60).

AstronomicalAmplitudeReader - Class in org.orekit.forces.gravity.potential

Parser for tides astronomical amplitude H_f.

AstronomicalAmplitudeReader(String, int, int, int, double) - Constructor for class org.orekit.forces.gravity.potential.AstronomicalAmplitudeReader

Simple constructor.

Atmosphere - Interface in org.orekit.forces.drag

Interface for atmospheric models.

AtmosphericRefractionModel - Interface in org.orekit.models

Defines an refraction model that can be used to correct for the apparent position of an object due to atmospheric effects.

ATOMIC_NITROGEN - Static variable in class org.orekit.forces.drag.DTM2000

Identifier for atomic nitrogen.

ATOMIC_OXYGEN - Static variable in class org.orekit.forces.drag.DTM2000

Identifier for atomic oxygen.

attachTo(Frame, Transform, boolean) - Method in class org.orekit.frames.OrphanFrame

Attach the instance (and all its children down to leafs) to the main tree.

attachTo(Frame, TransformProvider, boolean) - Method in class org.orekit.frames.OrphanFrame

Attach the instance (and all its children down to leafs) to the main tree.

Attitude - Class in org.orekit.attitudes

This class handles attitude definition at a given date.

Attitude(Frame, TimeStampedAngularCoordinates) - Constructor for class org.orekit.attitudes.Attitude

Creates a new instance.

Attitude(AbsoluteDate, Frame, AngularCoordinates) - Constructor for class org.orekit.attitudes.Attitude

Creates a new instance.

Attitude(AbsoluteDate, Frame, Rotation, Vector3D, Vector3D) - Constructor for class org.orekit.attitudes.Attitude

Creates a new instance.

AttitudeProvider - Interface in org.orekit.attitudes

This interface represents an attitude provider model set.

AttitudeProviderModifier - Interface in org.orekit.attitudes

This interface represents an attitude provider that modifies/wraps another underlying provider.

AttitudesSequence - Class in org.orekit.attitudes

This classes manages a sequence of different attitude providers that are activated in turn according to switching events.

AttitudesSequence() - Constructor for class org.orekit.attitudes.AttitudesSequence

Constructor for an initially empty sequence.

ATTRACTION_COEFFICIENT_SUFFIX - Static variable in class org.orekit.forces.gravity.ThirdBodyAttraction

Suffix for parameter name for attraction coefficient enabling jacobian processing.

AuxiliaryElements - Class in org.orekit.propagation.semianalytical.dsst.utilities

Container class for common parameters used by all DSST forces.

AuxiliaryElements(Orbit, int) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements

Simple constructor.

B

B - Variable in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution

B = sqrt(1 - h² - k²).

B_STAR - Static variable in class org.orekit.propagation.conversion.TLEPropagatorBuilder

Parameter name for B* coefficient.

basicPropagate(AbsoluteDate) - Method in class org.orekit.propagation.analytical.AbstractAnalyticalPropagator

Propagate an orbit without any fancy features.

basicPropagate(AbsoluteDate) - Method in class org.orekit.propagation.analytical.AdapterPropagator

Propagate an orbit without any fancy features.

basicPropagate(AbsoluteDate) - Method in class org.orekit.propagation.analytical.Ephemeris

basicPropagate(AbsoluteDate) - Method in class org.orekit.propagation.integration.IntegratedEphemeris

Propagate an orbit without any fancy features.

beforeIntegration(SpacecraftState, AbsoluteDate) - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator

Method called just before integration.

beforeIntegration(SpacecraftState, AbsoluteDate) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator

Method called just before integration.

BESSELIAN_YEAR - Static variable in interface org.orekit.utils.Constants

Duration of a Besselian year: 365.242198781 Constants.JULIAN_DAY.

beta0 - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator

sqrt (1 - e2).

beta02 - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator

1 - e2.

BodiesElements - Class in org.orekit.data

Elements of the bodies having an effect on nutation.

BodiesElements(AbsoluteDate, double, double, double, double, double, double, double, double, double, double, double, double, double, double, double, double) - Constructor for class org.orekit.data.BodiesElements

Simple constructor.

BodyCenterPointing - Class in org.orekit.attitudes

This class handles body center pointing attitude provider.

BodyCenterPointing(Frame) - Constructor for class org.orekit.attitudes.BodyCenterPointing

Creates new instance.

BodyShape - Interface in org.orekit.bodies

Interface representing the rigid surface shape of a natural body.

BoundedPropagator - Interface in org.orekit.propagation

This interface is intended for ephemerides valid only during a time range.

BoxAndSolarArraySpacecraft - Class in org.orekit.forces

experimental class representing the features of a classical satellite with a convex body shape and rotating flat solar arrays.

BoxAndSolarArraySpacecraft(double, double, double, PVCoordinatesProvider, double, Vector3D, double, double, double) - Constructor for class org.orekit.forces.BoxAndSolarArraySpacecraft

Build a spacecraft model with best lightning of solar array.

BoxAndSolarArraySpacecraft(BoxAndSolarArraySpacecraft.Facet[], PVCoordinatesProvider, double, Vector3D, double, double, double) - Constructor for class org.orekit.forces.BoxAndSolarArraySpacecraft

Build a spacecraft model with best lightning of solar array.

BoxAndSolarArraySpacecraft(double, double, double, PVCoordinatesProvider, double, Vector3D, AbsoluteDate, Vector3D, double, double, double, double) - Constructor for class org.orekit.forces.BoxAndSolarArraySpacecraft

Build a spacecraft model with linear rotation of solar array.

BoxAndSolarArraySpacecraft(BoxAndSolarArraySpacecraft.Facet[], PVCoordinatesProvider, double, Vector3D, AbsoluteDate, Vector3D, double, double, double, double) - Constructor for class org.orekit.forces.BoxAndSolarArraySpacecraft

Build a spacecraft model with linear rotation of solar array.

BoxAndSolarArraySpacecraft.Facet - Class in org.orekit.forces

Class representing a single facet of a convex spacecraft body.

BoxAndSolarArraySpacecraft.Facet(Vector3D, double) - Constructor for class org.orekit.forces.BoxAndSolarArraySpacecraft.Facet

Simple constructor.

buildIdentityMatrix2() - Static method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenUtilities

Build the identity matrix of order 2.

buildIdentityMatrix4() - Static method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenUtilities

Build the identity matrix of order 4.

buildIntegrator(Orbit) - Method in class org.orekit.propagation.conversion.AdamsBashforthIntegratorBuilder

Build a first order integrator.

buildIntegrator(Orbit) - Method in class org.orekit.propagation.conversion.AdamsMoultonIntegratorBuilder

Build a first order integrator.

buildIntegrator(Orbit) - Method in class org.orekit.propagation.conversion.ClassicalRungeKuttaIntegratorBuilder

Build a first order integrator.

buildIntegrator(Orbit) - Method in class org.orekit.propagation.conversion.DormandPrince54IntegratorBuilder

Build a first order integrator.

buildIntegrator(Orbit) - Method in class org.orekit.propagation.conversion.DormandPrince853IntegratorBuilder

Build a first order integrator.

buildIntegrator(Orbit) - Method in class org.orekit.propagation.conversion.EulerIntegratorBuilder

Build a first order integrator.

buildIntegrator(Orbit) - Method in interface org.orekit.propagation.conversion.FirstOrderIntegratorBuilder

Build a first order integrator.

buildIntegrator(Orbit) - Method in class org.orekit.propagation.conversion.GillIntegratorBuilder

Build a first order integrator.

buildIntegrator(Orbit) - Method in class org.orekit.propagation.conversion.GraggBulirschStoerIntegratorBuilder

Build a first order integrator.

buildIntegrator(Orbit) - Method in class org.orekit.propagation.conversion.HighamHall54IntegratorBuilder

Build a first order integrator.

buildIntegrator(Orbit) - Method in class org.orekit.propagation.conversion.MidpointIntegratorBuilder

Build a first order integrator.

buildIntegrator(Orbit) - Method in class org.orekit.propagation.conversion.ThreeEighthesIntegratorBuilder

Build a first order integrator.

buildPropagator(AbsoluteDate, double[]) - Method in class org.orekit.propagation.conversion.EcksteinHechlerPropagatorBuilder

Build a propagator.

buildPropagator(AbsoluteDate, double[]) - Method in class org.orekit.propagation.conversion.KeplerianPropagatorBuilder

Build a propagator.

buildPropagator(AbsoluteDate, double[]) - Method in class org.orekit.propagation.conversion.NumericalPropagatorBuilder

Build a propagator.

buildPropagator(AbsoluteDate, double[]) - Method in interface org.orekit.propagation.conversion.PropagatorBuilder

Build a propagator.

buildPropagator(AbsoluteDate, double[]) - Method in class org.orekit.propagation.conversion.TLEPropagatorBuilder

Build a propagator.

buildRow(int, int, double) - Static method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader

Build a coefficients row.

buildTriangularArray(int, int, double) - Static method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader

Build a coefficients triangular array.

buildZeroMatrix2() - Static method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenUtilities

Build the empty matrix of order 2.

buildZeroMatrix4() - Static method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenUtilities

Build the empty matrix of order 4.

BULLETINA_FILENAME - Static variable in class org.orekit.frames.FramesFactory

Default regular expression for the BulletinA files (IAU1980 and IAU2000 compatibles).

BULLETINB_1980_FILENAME - Static variable in class org.orekit.frames.FramesFactory

Default regular expression for the BulletinB files (IAU1980 compatibles).

BULLETINB_2000_FILENAME - Static variable in class org.orekit.frames.FramesFactory

Default regular expression for the BulletinB files (IAU2000 compatibles).

C

C - Variable in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution

C = 1 + p² + q².

c1 - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator

C1 from SPTRCK #3.

c2 - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator

C2 from SPTRCK #3.

c4 - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator

C4 from SPTRCK #3.

CachedNormalizedSphericalHarmonicsProvider - Class in org.orekit.forces.gravity.potential

Caching wrapper for NormalizedSphericalHarmonicsProvider.

CachedNormalizedSphericalHarmonicsProvider(NormalizedSphericalHarmonicsProvider, double, int, int, double, double) - Constructor for class org.orekit.forces.gravity.potential.CachedNormalizedSphericalHarmonicsProvider

Simple constructor.

calculateField(double, double, double) - Method in class org.orekit.models.earth.GeoMagneticField

Calculate the magnetic field at the specified geodetic point identified by latitude, longitude and altitude.

calculatePathDelay(double, double) - Method in class org.orekit.models.earth.FixedTroposphericDelay

Calculates the tropospheric path delay for the signal path from a ground station to a satellite.

calculatePathDelay(double, double) - Method in class org.orekit.models.earth.SaastamoinenModel

Calculates the tropospheric path delay for the signal path from a ground station to a satellite.

calculatePathDelay(double, double) - Method in interface org.orekit.models.earth.TroposphericDelayModel

Calculates the tropospheric path delay for the signal path from a ground station to a satellite.

calculateSignalDelay(double, double) - Method in class org.orekit.models.earth.FixedTroposphericDelay

Calculates the tropospheric signal delay for the signal path from a ground station to a satellite.

calculateSignalDelay(double, double) - Method in class org.orekit.models.earth.SaastamoinenModel

Calculates the tropospheric signal delay for the signal path from a ground station to a satellite.

calculateSignalDelay(double, double) - Method in interface org.orekit.models.earth.TroposphericDelayModel

Calculates the tropospheric signal delay for the signal path from a ground station to a satellite.

canAdd(int, int) - Method in class org.orekit.forces.gravity.potential.OceanTidesReader

Check if coefficients can be added.

CartesianDerivativesFilter - Enum in org.orekit.utils

Enumerate for selecting which derivatives to use in TimeStampedPVCoordinates and TimeStampedFieldPVCoordinates interpolation.

CartesianOrbit - Class in org.orekit.orbits

This class holds cartesian orbital parameters.

CartesianOrbit(TimeStampedPVCoordinates, Frame, double) - Constructor for class org.orekit.orbits.CartesianOrbit

Constructor from Cartesian parameters.

CartesianOrbit(PVCoordinates, Frame, AbsoluteDate, double) - Constructor for class org.orekit.orbits.CartesianOrbit

Constructor from Cartesian parameters.

CartesianOrbit(Orbit) - Constructor for class org.orekit.orbits.CartesianOrbit

Constructor from any kind of orbital parameters.

CCSDS_EPOCH - Static variable in class org.orekit.time.AbsoluteDate

Reference epoch for CCSDS Time Code Format (CCSDS 301.0-B-4): 1958-01-01T00:00:00 International Atomic Time (not UTC).

CCSDS_EPOCH - Static variable in class org.orekit.time.DateComponents

Reference epoch for CCSDS Time Code Format (CCSDS 301.0-B-4): 1958-01-01.

CCSDSFrame - Enum in org.orekit.files.ccsds

Frames used in CCSDS Orbit Data Messages.

CelestialBody - Interface in org.orekit.bodies

Interface for celestial bodies like Sun, Moon or solar system planets.

CelestialBodyFactory - Class in org.orekit.bodies

Factory class for bodies of the solar system.

CelestialBodyLoader - Interface in org.orekit.bodies

Interface for loading celestial bodies.

CelestialBodyPointed - Class in org.orekit.attitudes

This class handles a celestial body pointed attitude provider.

CelestialBodyPointed(Frame, PVCoordinatesProvider, Vector3D, Vector3D, Vector3D) - Constructor for class org.orekit.attitudes.CelestialBodyPointed

Creates new instance.

CenterName - Enum in org.orekit.files.ccsds

Orbit central bodies for which a Celestial body can be created.

CENTRAL_ATTRACTION_COEFFICIENT - Static variable in class org.orekit.forces.gravity.NewtonianAttraction

Name of the single parameter of this model: the central attraction coefficient.

checkEOPContinuity(double) - Method in class org.orekit.frames.EOPHistory

Check Earth orientation parameters continuity.

ChronologicalComparator - Class in org.orekit.time

Comparator for TimeStamped instance.

ChronologicalComparator() - Constructor for class org.orekit.time.ChronologicalComparator

Simple constructor.

CircularFieldOfViewDetector - Class in org.orekit.propagation.events

Finder for target entry/exit events with respect to a satellite sensor Field Of View.

CircularFieldOfViewDetector(double, PVCoordinatesProvider, Vector3D, double) - Constructor for class org.orekit.propagation.events.CircularFieldOfViewDetector

Build a new instance.

CircularOrbit - Class in org.orekit.orbits

This class handles circular orbital parameters.

CircularOrbit(double, double, double, double, double, double, PositionAngle, Frame, AbsoluteDate, double) - Constructor for class org.orekit.orbits.CircularOrbit

Creates a new instance.

CircularOrbit(double, double, double, double, double, double, PositionAngle, TimeStampedPVCoordinates, Frame, double) - Constructor for class org.orekit.orbits.CircularOrbit

Creates a new instance.

CircularOrbit(TimeStampedPVCoordinates, Frame, double) - Constructor for class org.orekit.orbits.CircularOrbit

Constructor from cartesian parameters.

CircularOrbit(PVCoordinates, Frame, AbsoluteDate, double) - Constructor for class org.orekit.orbits.CircularOrbit

Constructor from cartesian parameters.

CircularOrbit(Orbit) - Constructor for class org.orekit.orbits.CircularOrbit

Constructor from any kind of orbital parameters.

CjSjCoefficient - Class in org.orekit.propagation.semianalytical.dsst.utilities

Compute the S_j(k, h) and the C_j(k, h) series and their partial derivatives with respect to k and h.

CjSjCoefficient(double, double) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.CjSjCoefficient

C_j(k, h) and S_j(k, h) constructor.

ClassicalRungeKuttaIntegratorBuilder - Class in org.orekit.propagation.conversion

Builder for ClassicalRungeKuttaIntegrator.

ClassicalRungeKuttaIntegratorBuilder(double) - Constructor for class org.orekit.propagation.conversion.ClassicalRungeKuttaIntegratorBuilder

Build a new instance.

ClasspathCrawler - Class in org.orekit.data

Provider for data files stored as resources in the classpath.

ClasspathCrawler(String...) - Constructor for class org.orekit.data.ClasspathCrawler

Build a data classpath crawler.

ClasspathCrawler(ClassLoader, String...) - Constructor for class org.orekit.data.ClasspathCrawler

Build a data classpath crawler.

clearCelestialBodyCache(String) - Static method in class org.orekit.bodies.CelestialBodyFactory

Clear the specified celestial body from the internal cache.

clearCelestialBodyCache() - Static method in class org.orekit.bodies.CelestialBodyFactory

Clear all loaded celestial bodies.

clearCelestialBodyLoaders(String) - Static method in class org.orekit.bodies.CelestialBodyFactory

Clear loaders for one celestial body.

clearCelestialBodyLoaders() - Static method in class org.orekit.bodies.CelestialBodyFactory

Clear loaders for all celestial bodies.

clearEOPHistoryLoaders() - Static method in class org.orekit.frames.FramesFactory

Clear loaders for Earth Orientation Parameters history.

clearEventsDetectors() - Method in class org.orekit.propagation.AbstractPropagator

Remove all events detectors.

clearEventsDetectors() - Method in class org.orekit.propagation.analytical.AbstractAnalyticalPropagator

Remove all events detectors.

clearEventsDetectors() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator

Remove all events detectors.

clearEventsDetectors() - Method in interface org.orekit.propagation.Propagator

Remove all events detectors.

clearHistory() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.ShortPeriodicsInterpolatedCoefficient

Clear the recorded values from the interpolation grid.

clearLoadedDataNames() - Method in class org.orekit.data.DataProvidersManager

Clear the set of data file names that have been loaded.

clearLoggedEvents() - Method in class org.orekit.propagation.events.EventsLogger

Clear the logged events.

clearOceanTidesReaders() - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory

Clear ocean tides readers.

clearPotentialCoefficientsReaders() - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory

Clear gravity field readers.

clearProviders() - Method in class org.orekit.data.DataProvidersManager

Remove all data providers.

clearUTCTAILoaders() - Static method in class org.orekit.time.TimeScalesFactory

Clear loaders for UTC-TAI offsets history files.

co2AB - Variable in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution

C / (2 * A * B) .

coef - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator

coef for SGP C3 computation.

coef1 - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator

coef for SGP C5 computation.

CoefficientsFactory - Class in org.orekit.propagation.semianalytical.dsst.utilities

This class is designed to provide coefficient from the DSST theory.

CoefficientsFactory.MNSKey - Class in org.orekit.propagation.semianalytical.dsst.utilities

MNS couple's key.

CoefficientsFactory.MNSKey(int, int, int) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.CoefficientsFactory.MNSKey

Simpleconstructor.

CoefficientsFactory.NSKey - Class in org.orekit.propagation.semianalytical.dsst.utilities

Key formed by two integer values.

CoefficientsFactory.NSKey(int, int) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.CoefficientsFactory.NSKey

Simple constructor.

compare(TimeStamped, TimeStamped) - Method in class org.orekit.time.ChronologicalComparator

Compare two time-stamped instances.

compareTo(CoefficientsFactory.MNSKey) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.CoefficientsFactory.MNSKey

compareTo(CoefficientsFactory.NSKey) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.CoefficientsFactory.NSKey

compareTo(AbsoluteDate) - Method in class org.orekit.time.AbsoluteDate

Compare the instance with another date.

compareTo(DateComponents) - Method in class org.orekit.time.DateComponents

compareTo(DateTimeComponents) - Method in class org.orekit.time.DateTimeComponents

compareTo(TimeComponents) - Method in class org.orekit.time.TimeComponents

compile(PoissonSeries<S>...) - Static method in class org.orekit.data.PoissonSeries

Join several nutation series, for fast simultaneous evaluation.

computeDerivatives(SpacecraftState) - Method in interface org.orekit.propagation.integration.AbstractIntegratedPropagator.MainStateEquations

Compute differential equations for main state.

computeDerivatives(SpacecraftState, double[]) - Method in interface org.orekit.propagation.integration.AdditionalEquations

Compute the derivatives related to the additional state parameters.

computeDerivatives(SpacecraftState, double[]) - Method in class org.orekit.propagation.numerical.PartialDerivativesEquations

Compute the derivatives related to the additional state parameters.

computeGsHs(double, double, double, double, int) - Static method in class org.orekit.propagation.semianalytical.dsst.utilities.CoefficientsFactory

Compute recursively G_s and H_s polynomials from equation 3.1-(5).

computeInitValues(double, double, double) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenTesseralLinear

Compute the values for the first four coefficients and their derivatives by means of series.

computeInitValues(double, double, double) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenThirdBodyLinear

Compute the initial values (see Collins, 4-255, 4-256 and 4.259)

computeInitValues(double) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenZonalLinear

Compute the roots for the Hansen coefficients and their derivatives.

computeJacobianEccentricWrtCartesian() - Method in class org.orekit.orbits.CartesianOrbit

computeJacobianEccentricWrtCartesian() - Method in class org.orekit.orbits.CircularOrbit

Compute the Jacobian of the orbital parameters with eccentric angle with respect to the Cartesian parameters.

computeJacobianEccentricWrtCartesian() - Method in class org.orekit.orbits.EquinoctialOrbit

Compute the Jacobian of the orbital parameters with eccentric angle with respect to the Cartesian parameters.

computeJacobianEccentricWrtCartesian() - Method in class org.orekit.orbits.KeplerianOrbit

Compute the Jacobian of the orbital parameters with eccentric angle with respect to the Cartesian parameters.

computeJacobianEccentricWrtCartesian() - Method in class org.orekit.orbits.Orbit

Compute the Jacobian of the orbital parameters with eccentric angle with respect to the Cartesian parameters.

computeJacobianMeanWrtCartesian() - Method in class org.orekit.orbits.CartesianOrbit

computeJacobianMeanWrtCartesian() - Method in class org.orekit.orbits.CircularOrbit

Compute the Jacobian of the orbital parameters with mean angle with respect to the Cartesian parameters.

computeJacobianMeanWrtCartesian() - Method in class org.orekit.orbits.EquinoctialOrbit

Compute the Jacobian of the orbital parameters with mean angle with respect to the Cartesian parameters.

computeJacobianMeanWrtCartesian() - Method in class org.orekit.orbits.KeplerianOrbit

Compute the Jacobian of the orbital parameters with mean angle with respect to the Cartesian parameters.

computeJacobianMeanWrtCartesian() - Method in class org.orekit.orbits.Orbit

Compute the Jacobian of the orbital parameters with mean angle with respect to the Cartesian parameters.

computeJacobianTrueWrtCartesian() - Method in class org.orekit.orbits.CartesianOrbit

computeJacobianTrueWrtCartesian() - Method in class org.orekit.orbits.CircularOrbit

Compute the Jacobian of the orbital parameters with true angle with respect to the Cartesian parameters.

computeJacobianTrueWrtCartesian() - Method in class org.orekit.orbits.EquinoctialOrbit

Compute the Jacobian of the orbital parameters with true angle with respect to the Cartesian parameters.

computeJacobianTrueWrtCartesian() - Method in class org.orekit.orbits.KeplerianOrbit

Compute the Jacobian of the orbital parameters with true angle with respect to the Cartesian parameters.

computeJacobianTrueWrtCartesian() - Method in class org.orekit.orbits.Orbit

Compute the Jacobian of the orbital parameters with true angle with respect to the Cartesian parameters.

computeLimitVisibilityPoint(double, double, double) - Method in class org.orekit.frames.TopocentricFrame

Compute the limit visibility point for a satellite in a given direction.

computeMeanState(SpacecraftState, Collection<DSSTForceModel>) - Static method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator

Conversion from osculating to mean, orbit.

computeOsculatingState(SpacecraftState, Collection<DSSTForceModel>) - Static method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator

Conversion from mean to osculating orbit.

computeQns(double, int, int) - Static method in class org.orekit.propagation.semianalytical.dsst.utilities.CoefficientsFactory

Compute the Q_n,s coefficients evaluated at γ from the recurrence formula 2.8.3-(2).

computeShortPeriodicsCoefficients(SpacecraftState) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution

Compute the coefficients used for short periodic variations.

computeShortPeriodicsCoefficients(SpacecraftState) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTCentralBody

Compute the coefficients used for short periodic variations.

computeShortPeriodicsCoefficients(SpacecraftState) - Method in interface org.orekit.propagation.semianalytical.dsst.forces.DSSTForceModel

Compute the coefficients used for short periodic variations.

computeShortPeriodicsCoefficients(SpacecraftState) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBody

Compute the coefficients used for short periodic variations.

computeVns(int) - Static method in class org.orekit.propagation.semianalytical.dsst.utilities.CoefficientsFactory

Compute the V_n,s coefficients from 2.8.2-(1)(2).

configureOceanLoadDeformationCoefficients(OceanLoadDeformationCoefficients) - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory

Configure ocean load deformation coefficients.

Constants - Interface in org.orekit.utils

Set of useful physical constants.

ConstantThrustManeuver - Class in org.orekit.forces.maneuvers

This class implements a simple maneuver with constant thrust.

ConstantThrustManeuver(AbsoluteDate, double, double, double, Vector3D) - Constructor for class org.orekit.forces.maneuvers.ConstantThrustManeuver

Simple constructor for a constant direction and constant thrust.

containsSatellite(String) - Method in class org.orekit.files.ccsds.ODMFile

Tests whether a satellite with the given id is contained in this orbit file.

containsSatellite(String) - Method in interface org.orekit.files.general.OrbitFile

Tests whether a satellite with the given id is contained in this orbit file.

containsSatellite(String) - Method in class org.orekit.files.sp3.SP3File

Tests whether a satellite with the given id is contained in this orbit file.

ContinueOnEvent<T extends EventDetector> - Class in org.orekit.propagation.events.handlers

Event handler which will always return continue as a state.

ContinueOnEvent() - Constructor for class org.orekit.propagation.events.handlers.ContinueOnEvent

convert(double[]) - Method in interface org.orekit.data.SimpleTimeStampedTableParser.RowConverter

Convert a row.

convert(Propagator, double, int, Collection<String>) - Method in class org.orekit.propagation.conversion.AbstractPropagatorConverter

Convert a propagator to another.

convert(Propagator, double, int, String...) - Method in class org.orekit.propagation.conversion.AbstractPropagatorConverter

Convert a propagator to another.

convert(List<SpacecraftState>, boolean, Collection<String>) - Method in class org.orekit.propagation.conversion.AbstractPropagatorConverter

Find the propagator that minimize the mean square error for a sample of states.

convert(List<SpacecraftState>, boolean, String...) - Method in class org.orekit.propagation.conversion.AbstractPropagatorConverter

Find the propagator that minimize the mean square error for a sample of states.

convert() - Method in class org.orekit.propagation.conversion.OsculatingToMeanElementsConverter

Convert an osculating orbit into a mean orbit, in DSST sense.

convert(Propagator, double, int, Collection<String>) - Method in interface org.orekit.propagation.conversion.PropagatorConverter

Convert a propagator into another one.

convert(Propagator, double, int, String...) - Method in interface org.orekit.propagation.conversion.PropagatorConverter

Convert a propagator into another one.

convert(List<SpacecraftState>, boolean, Collection<String>) - Method in interface org.orekit.propagation.conversion.PropagatorConverter

Find the propagator that minimize the mean square error for a sample of states.

convert(List<SpacecraftState>, boolean, String...) - Method in interface org.orekit.propagation.conversion.PropagatorConverter

Find the propagator that minimize the mean square error for a sample of states.

convertType(Orbit) - Method in enum org.orekit.orbits.OrbitType

Convert an orbit to the instance type.

cosi0 - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator

cosinus original inclination.

create(double, double, int, EventHandler<ImpulseManeuver<T>>) - Method in class org.orekit.forces.maneuvers.ImpulseManeuver

Build a new instance.

create(double, double, int, EventHandler<T>) - Method in class org.orekit.propagation.events.AbstractDetector

Build a new instance.

create(double, double, int, EventHandler<AlignmentDetector>) - Method in class org.orekit.propagation.events.AlignmentDetector

Build a new instance.

create(double, double, int, EventHandler<AltitudeDetector>) - Method in class org.orekit.propagation.events.AltitudeDetector

Build a new instance.

create(double, double, int, EventHandler<ApsideDetector>) - Method in class org.orekit.propagation.events.ApsideDetector

Build a new instance.

create(double, double, int, EventHandler<CircularFieldOfViewDetector>) - Method in class org.orekit.propagation.events.CircularFieldOfViewDetector

Build a new instance.

create(double, double, int, EventHandler<DateDetector>) - Method in class org.orekit.propagation.events.DateDetector

Build a new instance.

create(double, double, int, EventHandler<DihedralFieldOfViewDetector>) - Method in class org.orekit.propagation.events.DihedralFieldOfViewDetector

Build a new instance.

create(double, double, int, EventHandler<EclipseDetector>) - Method in class org.orekit.propagation.events.EclipseDetector

Build a new instance.

create(double, double, int, EventHandler<ElevationDetector>) - Method in class org.orekit.propagation.events.ElevationDetector

Build a new instance.

create(double, double, int, EventHandler<EventFilter<T>>) - Method in class org.orekit.propagation.events.EventFilter

Build a new instance.

create(double, double, int, EventHandler<EventShifter<T>>) - Method in class org.orekit.propagation.events.EventShifter

Build a new instance.

create(double, double, int, EventHandler<GeographicZoneDetector>) - Method in class org.orekit.propagation.events.GeographicZoneDetector

Build a new instance.

create(double, double, int, EventHandler<NodeDetector>) - Method in class org.orekit.propagation.events.NodeDetector

Build a new instance.

createBesselianEpoch(double) - Static method in class org.orekit.time.AbsoluteDate

Build an instance corresponding to a Besselian Epoch (BE).

createFromModifiedRodrigues(double[][]) - Static method in class org.orekit.utils.AngularCoordinates

Convert a modified Rodrigues vector and derivatives to angular coordinates.

createFromWeekComponents(int, int, int) - Static method in class org.orekit.time.DateComponents

Build a date from week components.

createGPSDate(int, double) - Static method in class org.orekit.time.AbsoluteDate

Build an instance corresponding to a GPS date.

createIllegalArgumentException(Localizable, Object...) - Static method in exception org.orekit.errors.OrekitException

Create an IllegalArgumentException with localized message.

createIllegalStateException(Localizable, Object...) - Static method in exception org.orekit.errors.OrekitException

Create an IllegalStateException with localized message.

createInternalError(Throwable) - Static method in exception org.orekit.errors.OrekitException

Create an RuntimeException for an internal error.

createJulianEpoch(double) - Static method in class org.orekit.time.AbsoluteDate

Build an instance corresponding to a Julian Epoch (JE).

createMapper(AbsoluteDate, double, OrbitType, PositionAngle, AttitudeProvider, Frame) - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator

Create a mapper between raw double components and spacecraft state.

createMapper(AbsoluteDate, double, OrbitType, PositionAngle, AttitudeProvider, Frame) - Method in class org.orekit.propagation.numerical.NumericalPropagator

Create a mapper between raw double components and spacecraft state.

createMapper(AbsoluteDate, double, OrbitType, PositionAngle, AttitudeProvider, Frame) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator

Create a mapper between raw double components and spacecraft state.

createParseException(Localizable, Object...) - Static method in exception org.orekit.errors.OrekitException

Create an ParseException with localized message.

createTransformedITRF(Frame, String) - Method in enum org.orekit.frames.HelmertTransformation.Predefined

Create an ITRF frame by transforming another ITRF frame.

crossProduct(PVCoordinates, PVCoordinates) - Static method in class org.orekit.utils.PVCoordinates

Compute the cross-product of two instances.

CunninghamAttractionModel - Class in org.orekit.forces.gravity

This class represents the gravitational field of a celestial body.

CunninghamAttractionModel(Frame, UnnormalizedSphericalHarmonicsProvider) - Constructor for class org.orekit.forces.gravity.CunninghamAttractionModel

Creates a new instance.

D

DataLoader - Interface in org.orekit.data

Interface for loading data files from data providers.

DataProvider - Interface in org.orekit.data

Interface for providing data files to file loaders.

DataProvidersManager - Class in org.orekit.data

Singleton class managing all supported data providers.

DateComponents - Class in org.orekit.time

Class representing a date broken up as year, month and day components.

DateComponents(int, int, int) - Constructor for class org.orekit.time.DateComponents

Build a date from its components.

DateComponents(int, Month, int) - Constructor for class org.orekit.time.DateComponents

Build a date from its components.

DateComponents(int, int) - Constructor for class org.orekit.time.DateComponents

Build a date from a year and day number.

DateComponents(int) - Constructor for class org.orekit.time.DateComponents

Build a date from its offset with respect to a DateComponents.J2000_EPOCH.

DateComponents(DateComponents, int) - Constructor for class org.orekit.time.DateComponents

Build a date from its offset with respect to a reference epoch.

DateDetector - Class in org.orekit.propagation.events

Finder for date events.

DateDetector(double, double, TimeStamped...) - Constructor for class org.orekit.propagation.events.DateDetector

Build a new instance.

DateDetector(AbsoluteDate) - Constructor for class org.orekit.propagation.events.DateDetector

Build a new instance.

DateTimeComponents - Class in org.orekit.time

Holder for date and time components.

DateTimeComponents(DateComponents, TimeComponents) - Constructor for class org.orekit.time.DateTimeComponents

Build a new instance from its components.

DateTimeComponents(int, int, int, int, int, double) - Constructor for class org.orekit.time.DateTimeComponents

Build an instance from raw level components.

DateTimeComponents(int, Month, int, int, int, double) - Constructor for class org.orekit.time.DateTimeComponents

Build an instance from raw level components.

DateTimeComponents(int, int, int) - Constructor for class org.orekit.time.DateTimeComponents

Build an instance from raw level components.

DateTimeComponents(int, Month, int) - Constructor for class org.orekit.time.DateTimeComponents

Build an instance from raw level components.

DateTimeComponents(DateTimeComponents, double) - Constructor for class org.orekit.time.DateTimeComponents

Build an instance from a seconds offset with respect to another one.

DEFAULT - Static variable in class org.orekit.propagation.analytical.tle.TLE

Identifier for default type of ephemeris (SGP4/SDP4).

DEFAULT_CACHED_SLOTS_NUMBER - Static variable in class org.orekit.utils.GenericTimeStampedCache

Default number of independent cached time slots.

DEFAULT_CORRECTION_FACTOR - Static variable in class org.orekit.models.earth.EarthStandardAtmosphereRefraction

Default correction factor value.

DEFAULT_DE_SUPPORTED_NAMES - Static variable in class org.orekit.bodies.JPLEphemeridesLoader

Default supported files name pattern for JPL DE files.

DEFAULT_INPOP_SUPPORTED_NAMES - Static variable in class org.orekit.bodies.JPLEphemeridesLoader

Default supported files name pattern for IMCCE INPOP files.

DEFAULT_LAW - Static variable in interface org.orekit.propagation.Propagator

Default attitude provider.

DEFAULT_MASS - Static variable in interface org.orekit.propagation.Propagator

Default mass.

DEFAULT_MAX_ITER - Static variable in class org.orekit.propagation.events.AbstractDetector

Default cmaximum number of iterations in the event time search.

DEFAULT_MAXCHECK - Static variable in class org.orekit.propagation.events.AbstractDetector

Default maximum checking interval (s).

DEFAULT_POINTS - Static variable in class org.orekit.forces.gravity.OceanTides

Default number of points tides field sampling.

DEFAULT_POINTS - Static variable in class org.orekit.forces.gravity.SolidTides

Default number of points tides field sampling.

DEFAULT_PRESSURE - Static variable in class org.orekit.models.earth.EarthStandardAtmosphereRefraction

Default local pressure at viewpoint (Pa).

DEFAULT_STEP - Static variable in class org.orekit.forces.gravity.OceanTides

Default step for tides field sampling (seconds).

DEFAULT_STEP - Static variable in class org.orekit.forces.gravity.SolidTides

Default step for tides field sampling (seconds).

DEFAULT_TEMPERATURE - Static variable in class org.orekit.models.earth.EarthStandardAtmosphereRefraction

Default local temperature at viewpoint (K).

DEFAULT_THRESHOLD - Static variable in class org.orekit.propagation.events.AbstractDetector

Default convergence threshold (s).

DelaunayArguments - Class in org.orekit.data

Delaunay arguments used for nutation or tides.

DelaunayArguments(AbsoluteDate, double, double, double, double, double, double, double) - Constructor for class org.orekit.data.DelaunayArguments

Simple constructor.

DihedralFieldOfViewDetector - Class in org.orekit.propagation.events

Finder for body entering/exiting dihedral FOV events.

DihedralFieldOfViewDetector(double, PVCoordinatesProvider, Vector3D, Vector3D, double, Vector3D, double) - Constructor for class org.orekit.propagation.events.DihedralFieldOfViewDetector

Build a new instance.

DirectoryCrawler - Class in org.orekit.data

Provider for data files stored in a directories tree on filesystem.

DirectoryCrawler(File) - Constructor for class org.orekit.data.DirectoryCrawler

Build a data files crawler.

DormandPrince54IntegratorBuilder - Class in org.orekit.propagation.conversion

Builder for DormandPrince54Integrator.

DormandPrince54IntegratorBuilder(double, double, double) - Constructor for class org.orekit.propagation.conversion.DormandPrince54IntegratorBuilder

Build a new instance.

DormandPrince853IntegratorBuilder - Class in org.orekit.propagation.conversion

Builder for DormandPrince853Integrator.

DormandPrince853IntegratorBuilder(double, double, double) - Constructor for class org.orekit.propagation.conversion.DormandPrince853IntegratorBuilder

Build a new instance.

DRAG_COEFFICIENT - Static variable in interface org.orekit.forces.drag.DragSensitive

Parameter name for drag coefficient enabling jacobian processing.

dragAcceleration(AbsoluteDate, Frame, Vector3D, Rotation, double, double, Vector3D) - Method in class org.orekit.forces.BoxAndSolarArraySpacecraft

Compute the acceleration due to drag.

dragAcceleration(AbsoluteDate, Frame, FieldVector3D<DerivativeStructure>, FieldRotation<DerivativeStructure>, DerivativeStructure, double, FieldVector3D<DerivativeStructure>) - Method in class org.orekit.forces.BoxAndSolarArraySpacecraft

Compute the acceleration due to drag, with state derivatives.

dragAcceleration(AbsoluteDate, Frame, Vector3D, Rotation, double, double, Vector3D, String) - Method in class org.orekit.forces.BoxAndSolarArraySpacecraft

Compute acceleration due to drag, with parameters derivatives.

dragAcceleration(AbsoluteDate, Frame, Vector3D, Rotation, double, double, Vector3D) - Method in interface org.orekit.forces.drag.DragSensitive

Compute the acceleration due to drag.

dragAcceleration(AbsoluteDate, Frame, FieldVector3D<DerivativeStructure>, FieldRotation<DerivativeStructure>, DerivativeStructure, double, FieldVector3D<DerivativeStructure>) - Method in interface org.orekit.forces.drag.DragSensitive

Compute the acceleration due to drag, with state derivatives.

dragAcceleration(AbsoluteDate, Frame, Vector3D, Rotation, double, double, Vector3D, String) - Method in interface org.orekit.forces.drag.DragSensitive

Compute acceleration due to drag, with parameters derivatives.

dragAcceleration(AbsoluteDate, Frame, Vector3D, Rotation, double, double, Vector3D) - Method in class org.orekit.forces.SphericalSpacecraft

Compute the acceleration due to drag.

dragAcceleration(AbsoluteDate, Frame, FieldVector3D<DerivativeStructure>, FieldRotation<DerivativeStructure>, DerivativeStructure, double, FieldVector3D<DerivativeStructure>) - Method in class org.orekit.forces.SphericalSpacecraft

Compute the acceleration due to drag, with state derivatives.

dragAcceleration(AbsoluteDate, Frame, Vector3D, Rotation, double, double, Vector3D, String) - Method in class org.orekit.forces.SphericalSpacecraft

Compute acceleration due to drag, with parameters derivatives.

DragForce - Class in org.orekit.forces.drag

Atmospheric drag force model.

DragForce(Atmosphere, DragSensitive) - Constructor for class org.orekit.forces.drag.DragForce

Simple constructor.

DragSensitive - Interface in org.orekit.forces.drag

Interface for spacecraft that are sensitive to atmospheric drag forces.

DrozinerAttractionModel - Class in org.orekit.forces.gravity

This class represents the gravitational field of a celestial body.

DrozinerAttractionModel(Frame, UnnormalizedSphericalHarmonicsProvider) - Constructor for class org.orekit.forces.gravity.DrozinerAttractionModel

Creates a new instance.

dsEvaluateTC(AbsoluteDate) - Method in enum org.orekit.utils.IERSConventions

Evaluate the date offset between the current date and the reference date.

DSSTAtmosphericDrag - Class in org.orekit.propagation.semianalytical.dsst.forces

Atmospheric drag contribution to the DSSTPropagator.

DSSTAtmosphericDrag(Atmosphere, double, double) - Constructor for class org.orekit.propagation.semianalytical.dsst.forces.DSSTAtmosphericDrag

Simple constructor assuming spherical spacecraft.

DSSTAtmosphericDrag(Atmosphere, DragSensitive) - Constructor for class org.orekit.propagation.semianalytical.dsst.forces.DSSTAtmosphericDrag

Simple constructor with custom spacecraft.

DSSTCentralBody - Class in org.orekit.propagation.semianalytical.dsst.forces

Central body gravitational contribution to the DSSTPropagator.

DSSTCentralBody(Frame, double, UnnormalizedSphericalHarmonicsProvider, boolean) - Constructor for class org.orekit.propagation.semianalytical.dsst.forces.DSSTCentralBody

DSST Central body constructor.

DSSTCentralBody(Frame, double, UnnormalizedSphericalHarmonicsProvider) - Constructor for class org.orekit.propagation.semianalytical.dsst.forces.DSSTCentralBody

DSST Central body constructor.

DSSTForceModel - Interface in org.orekit.propagation.semianalytical.dsst.forces

This interface represents a force modifying spacecraft motion for a DSSTPropagator.

DSSTPropagator - Class in org.orekit.propagation.semianalytical.dsst

This class propagates orbits using the DSST theory.

DSSTPropagator(AbstractIntegrator, boolean) - Constructor for class org.orekit.propagation.semianalytical.dsst.DSSTPropagator

Create a new instance of DSSTPropagator.

DSSTPropagator(AbstractIntegrator) - Constructor for class org.orekit.propagation.semianalytical.dsst.DSSTPropagator

Create a new instance of DSSTPropagator.

DSSTSolarRadiationPressure - Class in org.orekit.propagation.semianalytical.dsst.forces

Solar radiation pressure contribution to the DSSTPropagator.

DSSTSolarRadiationPressure(double, double, PVCoordinatesProvider, double) - Constructor for class org.orekit.propagation.semianalytical.dsst.forces.DSSTSolarRadiationPressure

Simple constructor with default reference values and spherical spacecraft.

DSSTSolarRadiationPressure(PVCoordinatesProvider, double, RadiationSensitive) - Constructor for class org.orekit.propagation.semianalytical.dsst.forces.DSSTSolarRadiationPressure

Simple constructor with default reference values, but custom spacecraft.

DSSTSolarRadiationPressure(double, double, double, double, PVCoordinatesProvider, double) - Constructor for class org.orekit.propagation.semianalytical.dsst.forces.DSSTSolarRadiationPressure

Constructor with customizable reference values but spherical spacecraft.

DSSTSolarRadiationPressure(double, double, PVCoordinatesProvider, double, RadiationSensitive) - Constructor for class org.orekit.propagation.semianalytical.dsst.forces.DSSTSolarRadiationPressure

Complete constructor.

DSSTThirdBody - Class in org.orekit.propagation.semianalytical.dsst.forces

Third body attraction perturbation to the DSSTPropagator.

DSSTThirdBody(CelestialBody) - Constructor for class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBody

Complete constructor.

DTM2000 - Class in org.orekit.forces.drag

This atmosphere model is the realization of the DTM-2000 model.

DTM2000(DTM2000InputParameters, PVCoordinatesProvider, BodyShape) - Constructor for class org.orekit.forces.drag.DTM2000

Simple constructor for independent computation.

DTM2000InputParameters - Interface in org.orekit.forces.drag

Container for solar activity data, compatible with DTM2000 Atmosphere model.

durationFrom(AbsoluteDate) - Method in class org.orekit.time.AbsoluteDate

Compute the physically elapsed duration between two instants.

E

e - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator

final eccentricity.

e0sq - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator

original eccentricity squared.

EARTH - Static variable in class org.orekit.bodies.CelestialBodyFactory

Predefined name for Earth.

EARTH_MOON - Static variable in class org.orekit.bodies.CelestialBodyFactory

Predefined name for Earth-Moon barycenter.

EarthStandardAtmosphereRefraction - Class in org.orekit.models.earth

Implementation of refraction model for Earth standard atmosphere.

EarthStandardAtmosphereRefraction() - Constructor for class org.orekit.models.earth.EarthStandardAtmosphereRefraction

Creates a new default instance.

EarthStandardAtmosphereRefraction(double, double) - Constructor for class org.orekit.models.earth.EarthStandardAtmosphereRefraction

Creates an instance given a specific pressure and temperature.

ecc - Variable in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution

Eccentricity.

EcksteinHechlerPropagator - Class in org.orekit.propagation.analytical

This class propagates a SpacecraftState using the analytical Eckstein-Hechler model.

EcksteinHechlerPropagator(Orbit, UnnormalizedSphericalHarmonicsProvider) - Constructor for class org.orekit.propagation.analytical.EcksteinHechlerPropagator

Build a propagator from orbit and potential provider.

EcksteinHechlerPropagator(Orbit, AttitudeProvider, double, UnnormalizedSphericalHarmonicsProvider, UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics) - Constructor for class org.orekit.propagation.analytical.EcksteinHechlerPropagator

Private helper constructor.

EcksteinHechlerPropagator(Orbit, double, double, double, double, double, double, double) - Constructor for class org.orekit.propagation.analytical.EcksteinHechlerPropagator

Build a propagator from orbit and potential.

EcksteinHechlerPropagator(Orbit, double, UnnormalizedSphericalHarmonicsProvider) - Constructor for class org.orekit.propagation.analytical.EcksteinHechlerPropagator

Build a propagator from orbit, mass and potential provider.

EcksteinHechlerPropagator(Orbit, double, double, double, double, double, double, double, double) - Constructor for class org.orekit.propagation.analytical.EcksteinHechlerPropagator

Build a propagator from orbit, mass and potential.

EcksteinHechlerPropagator(Orbit, AttitudeProvider, UnnormalizedSphericalHarmonicsProvider) - Constructor for class org.orekit.propagation.analytical.EcksteinHechlerPropagator

Build a propagator from orbit, attitude provider and potential provider.

EcksteinHechlerPropagator(Orbit, AttitudeProvider, double, double, double, double, double, double, double) - Constructor for class org.orekit.propagation.analytical.EcksteinHechlerPropagator

Build a propagator from orbit, attitude provider and potential.

EcksteinHechlerPropagator(Orbit, AttitudeProvider, double, UnnormalizedSphericalHarmonicsProvider) - Constructor for class org.orekit.propagation.analytical.EcksteinHechlerPropagator

Build a propagator from orbit, attitude provider, mass and potential provider.

EcksteinHechlerPropagator(Orbit, AttitudeProvider, double, double, double, double, double, double, double, double) - Constructor for class org.orekit.propagation.analytical.EcksteinHechlerPropagator

Build a propagator from orbit, attitude provider, mass and potential.

EcksteinHechlerPropagatorBuilder - Class in org.orekit.propagation.conversion

Builder for Eckstein-Hechler propagator.

EcksteinHechlerPropagatorBuilder(Frame, UnnormalizedSphericalHarmonicsProvider) - Constructor for class org.orekit.propagation.conversion.EcksteinHechlerPropagatorBuilder

Build a new instance.

EcksteinHechlerPropagatorBuilder(Frame, double, double, TideSystem, double, double, double, double, double) - Constructor for class org.orekit.propagation.conversion.EcksteinHechlerPropagatorBuilder

Build a new instance.

EclipseDetector - Class in org.orekit.propagation.events

Finder for satellite eclipse related events.

EclipseDetector(PVCoordinatesProvider, double, PVCoordinatesProvider, double) - Constructor for class org.orekit.propagation.events.EclipseDetector

Build a new eclipse detector.

EclipseDetector(double, PVCoordinatesProvider, double, PVCoordinatesProvider, double) - Constructor for class org.orekit.propagation.events.EclipseDetector

Build a new eclipse detector.

EclipseDetector(double, double, PVCoordinatesProvider, double, PVCoordinatesProvider, double) - Constructor for class org.orekit.propagation.events.EclipseDetector

Build a new eclipse detector.

EclipticProvider - Class in org.orekit.frames

An inertial frame aligned with the ecliptic.

EclipticProvider(IERSConventions) - Constructor for class org.orekit.frames.EclipticProvider

Create a transform provider from MOD to an ecliptically aligned frame.

eeta - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator

original eccentricity * eta.

EGM96_EARTH_C20 - Static variable in interface org.orekit.utils.Constants

Earth un-normalized second zonal coefficient from EGM96 model: -1.08262668355315e-3.

EGM96_EARTH_C30 - Static variable in interface org.orekit.utils.Constants

Earth un-normalized third zonal coefficient from EGM96 model: 2.53265648533224e-6.

EGM96_EARTH_C40 - Static variable in interface org.orekit.utils.Constants

Earth un-normalized fourth zonal coefficient from EGM96 model: 1.619621591367e-6.

EGM96_EARTH_C50 - Static variable in interface org.orekit.utils.Constants

Earth un-normalized fifth zonal coefficient from EGM96 model: 2.27296082868698e-7.

EGM96_EARTH_C60 - Static variable in interface org.orekit.utils.Constants

Earth un-normalized sixth zonal coefficient from EGM96 model: -5.40681239107085e-7.

EGM96_EARTH_EQUATORIAL_RADIUS - Static variable in interface org.orekit.utils.Constants

Earth equatorial radius from EGM96 model: 6378136.3 m.

EGM96_EARTH_MU - Static variable in interface org.orekit.utils.Constants

Earth gravitational constant from EGM96 model: 3.986004415e14 m³/s².

EGM_FILENAME - Static variable in class org.orekit.forces.gravity.potential.GravityFieldFactory

Default regular expression for EGM files.

EGMFormatReader - Class in org.orekit.forces.gravity.potential

This reader is adapted to the EGM Format.

EGMFormatReader(String, boolean) - Constructor for class org.orekit.forces.gravity.potential.EGMFormatReader

Simple constructor.

EIGEN5C_EARTH_C20 - Static variable in interface org.orekit.utils.Constants

Earth un-normalized second zonal coefficient from EIGEN5C model: -1.082626457231767e-3.

EIGEN5C_EARTH_C30 - Static variable in interface org.orekit.utils.Constants

Earth un-normalized third zonal coefficient from EIGEN5C model: 2.532547231862799e-6.

EIGEN5C_EARTH_C40 - Static variable in interface org.orekit.utils.Constants

Earth un-normalized fourth zonal coefficient from EIGEN5C model: 1.619964434136e-6.

EIGEN5C_EARTH_C50 - Static variable in interface org.orekit.utils.Constants

Earth un-normalized fifth zonal coefficient from EIGEN5C model: 2.277928487005437e-7.

EIGEN5C_EARTH_C60 - Static variable in interface org.orekit.utils.Constants

Earth un-normalized sixth zonal coefficient from EIGEN5C model: -5.406653715879098e-7.

EIGEN5C_EARTH_EQUATORIAL_RADIUS - Static variable in interface org.orekit.utils.Constants

Earth equatorial radius from EIGEN5C model: 6378136.46 m.

EIGEN5C_EARTH_MU - Static variable in interface org.orekit.utils.Constants

Earth gravitational constant from EIGEN5C model: 3.986004415e14 m³/s².

ElevationDetector - Class in org.orekit.propagation.events

Finder for satellite raising/setting events that allows for the setting of azimuth and/or elevation bounds or a ground azimuth/elevation mask input.

ElevationDetector(TopocentricFrame) - Constructor for class org.orekit.propagation.events.ElevationDetector

Creates an instance of Elevation detector based on passed in topocentric frame and the minimum elevation angle.

ElevationDetector(double, double, TopocentricFrame) - Constructor for class org.orekit.propagation.events.ElevationDetector

Creates an instance of Elevation detector based on passed in topocentric frame and overrides of default maximal checking interval and convergence threshold values.

ElevationMask - Class in org.orekit.utils

Class for modeling the ground elevation values around a given point.

ElevationMask(double[][]) - Constructor for class org.orekit.utils.ElevationMask

Creates an instance of an Elevation mask based on the passed in parameter.

Ellipse - Class in org.orekit.bodies

Model of a 2D ellipse in 3D space.

Ellipse(Vector3D, Vector3D, Vector3D, double, double, Frame) - Constructor for class org.orekit.bodies.Ellipse

Simple constructor.

Ellipsoid - Class in org.orekit.bodies

Modeling of a general three-axes ellipsoid.

Ellipsoid(Frame, double, double, double) - Constructor for class org.orekit.bodies.Ellipsoid

Simple constructor.

EME2000_ALIGNED - Static variable in class org.orekit.attitudes.InertialProvider

Dummy attitude provider, perfectly aligned with the EME2000 frame.

emptyCache() - Static method in class org.orekit.utils.ImmutableTimeStampedCache

Get an empty immutable cache, cast to the correct type.

endParse() - Method in class org.orekit.forces.gravity.potential.OceanTidesReader

End parsing.

ensureCompatibleAdditionalStates(SpacecraftState) - Method in class org.orekit.propagation.SpacecraftState

Check if two instances have the same set of additional states available.

EOPC04_1980_FILENAME - Static variable in class org.orekit.frames.FramesFactory

Default regular expression for the EOPC04 files (IAU1980 compatibles).

EOPC04_2000_FILENAME - Static variable in class org.orekit.frames.FramesFactory

Default regular expression for the EOPC04 files (IAU2000 compatibles).

EOPEntry - Class in org.orekit.frames

This class holds an Earth Orientation Parameters entry.

EOPEntry(int, double, double, double, double, double, double, double, double) - Constructor for class org.orekit.frames.EOPEntry

Simple constructor.

EOPHistory - Class in org.orekit.frames

This class loads any kind of Earth Orientation Parameter data throughout a large time range.

EOPHistory(IERSConventions, Collection<EOPEntry>, boolean) - Constructor for class org.orekit.frames.EOPHistory

Simple constructor.

EOPHistoryLoader - Interface in org.orekit.frames

Interface for loading Earth Orientation Parameters history.

Ephemeris - Class in org.orekit.propagation.analytical

This class is designed to accept and handle tabulated orbital entries.

Ephemeris(List<SpacecraftState>, int) - Constructor for class org.orekit.propagation.analytical.Ephemeris

Constructor with tabulated states.

EPHEMERIS_GENERATION_MODE - Static variable in interface org.orekit.propagation.Propagator

Indicator for ephemeris generation mode.

equals(Object) - Method in class org.orekit.bodies.GeodeticPoint

equals(Object) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.CoefficientsFactory.MNSKey

equals(Object) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.CoefficientsFactory.NSKey

equals(Object) - Method in class org.orekit.time.AbsoluteDate

Check if the instance represent the same time as another instance.

equals(Object) - Method in class org.orekit.time.DateComponents

equals(Object) - Method in class org.orekit.time.DateTimeComponents

equals(Object) - Method in class org.orekit.time.TimeComponents

EquinoctialOrbit - Class in org.orekit.orbits

This class handles equinoctial orbital parameters, which can support both circular and equatorial orbits.

EquinoctialOrbit(double, double, double, double, double, double, PositionAngle, Frame, AbsoluteDate, double) - Constructor for class org.orekit.orbits.EquinoctialOrbit

Creates a new instance.

EquinoctialOrbit(TimeStampedPVCoordinates, Frame, double) - Constructor for class org.orekit.orbits.EquinoctialOrbit

Constructor from cartesian parameters.

EquinoctialOrbit(PVCoordinates, Frame, AbsoluteDate, double) - Constructor for class org.orekit.orbits.EquinoctialOrbit

Constructor from cartesian parameters.

EquinoctialOrbit(Orbit) - Constructor for class org.orekit.orbits.EquinoctialOrbit

Constructor from any kind of orbital parameters.

estimateRate(Rotation, Rotation, double) - Static method in class org.orekit.utils.AngularCoordinates

Estimate rotation rate between two orientations.

estimateRate(FieldRotation<T>, FieldRotation<T>, double) - Static method in class org.orekit.utils.FieldAngularCoordinates

Estimate FieldRotation rate between two orientations.

estimateVelocity(FieldVector3D<T>, FieldVector3D<T>, double) - Static method in class org.orekit.utils.FieldPVCoordinates

Estimate velocity between two positions.

estimateVelocity(Vector3D, Vector3D, double) - Static method in class org.orekit.utils.PVCoordinates

Estimate velocity between two positions.

eta - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator

eta from SPTRCK #3.

etasq - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator

eta squared.

EulerIntegratorBuilder - Class in org.orekit.propagation.conversion

Builder for EulerIntegrator.

EulerIntegratorBuilder(double) - Constructor for class org.orekit.propagation.conversion.EulerIntegratorBuilder

Build a new instance.

evaluateAll(AbsoluteDate) - Method in class org.orekit.data.FundamentalNutationArguments

Evaluate all fundamental arguments for the current date (Delaunay plus planetary).

evaluateDerivative(AbsoluteDate) - Method in class org.orekit.data.FundamentalNutationArguments

Evaluate all fundamental arguments for the current date (Delaunay plus planetary), including the first time derivative.

evaluateStep(OrekitStepInterpolator) - Method in class org.orekit.propagation.events.EventState

Evaluate the impact of the proposed step on the event detector.

evaluateTC(AbsoluteDate) - Method in enum org.orekit.utils.IERSConventions

Evaluate the date offset between the current date and the reference date.

EventDetector - Interface in org.orekit.propagation.events

This interface represents space-dynamics aware events detectors.

EventFilter<T extends EventDetector> - Class in org.orekit.propagation.events

Wrapper used to detect only increasing or decreasing events.

EventFilter(T, FilterType) - Constructor for class org.orekit.propagation.events.EventFilter

Wrap an event detector.

EventHandler<T extends EventDetector> - Interface in org.orekit.propagation.events.handlers

An interface defining how to override event handling behavior in the standard propagator eventing classes without requiring subclassing.

EventHandler.Action - Enum in org.orekit.propagation.events.handlers

Enumerate for actions to be performed when an event occurs.

eventOccurred(SpacecraftState, boolean) - Method in class org.orekit.propagation.events.AbstractDetector

Handle the event.

eventOccurred(SpacecraftState, boolean) - Method in interface org.orekit.propagation.events.EventDetector

Handle the event.

eventOccurred(SpacecraftState, T, boolean) - Method in class org.orekit.propagation.events.handlers.ContinueOnEvent

Specific implementation of the eventOccurred interface.

eventOccurred(SpacecraftState, T, boolean) - Method in interface org.orekit.propagation.events.handlers.EventHandler

eventOccurred method mirrors the same interface method as in EventDetector and its subclasses, but with an additional parameter that allows the calling method to pass in an object from the detector which would have potential additional data to allow the implementing class to determine the correct return state.

eventOccurred(SpacecraftState, T, boolean) - Method in class org.orekit.propagation.events.handlers.StopOnDecreasing

Handle a detection event and choose what to do next.

eventOccurred(SpacecraftState, T, boolean) - Method in class org.orekit.propagation.events.handlers.StopOnEvent

Specific implementation of the eventOccurred interface.

eventOccurred(SpacecraftState, T, boolean) - Method in class org.orekit.propagation.events.handlers.StopOnIncreasing

Handle a detection event and choose what to do next.

EventShifter<T extends EventDetector> - Class in org.orekit.propagation.events

Wrapper shifting events occurrences times.

EventShifter(T, boolean, double, double) - Constructor for class org.orekit.propagation.events.EventShifter

Build a new instance.

EventsLogger - Class in org.orekit.propagation.events

This class logs events detectors events during propagation.

EventsLogger() - Constructor for class org.orekit.propagation.events.EventsLogger

Simple constructor.

EventsLogger.LoggedEvent - Class in org.orekit.propagation.events

Class for logged events entries.

EventState<T extends EventDetector> - Class in org.orekit.propagation.events

This class handles the state for one event detector during integration steps.

EventState(T) - Constructor for class org.orekit.propagation.events.EventState

Simple constructor.

extendListOfLists(List<List<Double>>, int, int, double) - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader

Extend a list of lists of coefficients if needed.

F

f - Variable in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution

Equinoctial frame f vector.

FactoryManagedFrame - Class in org.orekit.frames

Base class for the predefined frames that are managed by FramesFactory.

FactoryManagedFrame(Frame, TransformProvider, boolean, Predefined) - Constructor for class org.orekit.frames.FactoryManagedFrame

Simple constructor.

feed(Pattern, DataLoader) - Method in class org.orekit.data.ClasspathCrawler

Feed a data file loader by browsing the data collection.

feed(Pattern, DataLoader) - Method in interface org.orekit.data.DataProvider

Feed a data file loader by browsing the data collection.

feed(String, DataLoader) - Method in class org.orekit.data.DataProvidersManager

Feed a data file loader by browsing all data providers.

feed(Pattern, DataLoader) - Method in class org.orekit.data.DirectoryCrawler

Feed a data file loader by browsing the data collection.

feed(Pattern, DataLoader) - Method in class org.orekit.data.NetworkCrawler

Feed a data file loader by browsing the data collection.

feed(Pattern, DataLoader) - Method in class org.orekit.data.ZipJarCrawler

Feed a data file loader by browsing the data collection.

FES_CHAT_EPSILON_FILENAME - Static variable in class org.orekit.forces.gravity.potential.GravityFieldFactory

Default regular expression for FES C hat and epsilon tides files.

FES_CNM_SNM_FILENAME - Static variable in class org.orekit.forces.gravity.potential.GravityFieldFactory

Default regular expression for FES Cnm, Snm tides files.

FES_HF_FILENAME - Static variable in class org.orekit.forces.gravity.potential.GravityFieldFactory

Default regular expression for FES Hf tides files.

FESCHatEpsilonReader - Class in org.orekit.forces.gravity.potential

Reader for ocean tides files following the fes2004.dat format.

FESCHatEpsilonReader(String, double, double, OceanLoadDeformationCoefficients, Map<Integer, Double>) - Constructor for class org.orekit.forces.gravity.potential.FESCHatEpsilonReader

Simple constructor.

FESCnmSnmReader - Class in org.orekit.forces.gravity.potential

Reader for ocean tides files following the fes2004_Cnm-Snm.dat format.

FESCnmSnmReader(String, double) - Constructor for class org.orekit.forces.gravity.potential.FESCnmSnmReader

Simple constructor.

FieldAngularCoordinates<T extends RealFieldElement<T>> - Class in org.orekit.utils

Simple container for FieldRotation/FieldRotation rate pairs, using RealFieldElement.

FieldAngularCoordinates(FieldRotation<T>, FieldVector3D<T>) - Constructor for class org.orekit.utils.FieldAngularCoordinates

Builds a rotation/rotation rate pair.

FieldAngularCoordinates(FieldRotation<T>, FieldVector3D<T>, FieldVector3D<T>) - Constructor for class org.orekit.utils.FieldAngularCoordinates

Builds a FieldRotation/FieldRotation rate/FieldRotation acceleration triplet.

FieldBodiesElements<T extends RealFieldElement<T>> - Class in org.orekit.data

Elements of the bodies having an effect on nutation.

FieldBodiesElements(AbsoluteDate, T, T, T, T, T, T, T, T, T, T, T, T, T, T, T, T) - Constructor for class org.orekit.data.FieldBodiesElements

Simple constructor.

FieldDelaunayArguments<T extends RealFieldElement<T>> - Class in org.orekit.data

Delaunay arguments used for nutation or tides.

FieldDelaunayArguments(AbsoluteDate, T, T, T, T, T, T, T) - Constructor for class org.orekit.data.FieldDelaunayArguments

Simple constructor.

FieldPVCoordinates<T extends RealFieldElement<T>> - Class in org.orekit.utils

Simple container for Position/Velocity pairs, using RealFieldElement.

FieldPVCoordinates(FieldVector3D<T>, FieldVector3D<T>) - Constructor for class org.orekit.utils.FieldPVCoordinates

Builds a PVCoordinates triplet with zero acceleration.

FieldPVCoordinates(FieldVector3D<T>, FieldVector3D<T>, FieldVector3D<T>) - Constructor for class org.orekit.utils.FieldPVCoordinates

Builds a PVCoordinates triplet.

FieldPVCoordinates(double, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.FieldPVCoordinates

Multiplicative constructor

FieldPVCoordinates(T, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.FieldPVCoordinates

Multiplicative constructor

FieldPVCoordinates(T, PVCoordinates) - Constructor for class org.orekit.utils.FieldPVCoordinates

Multiplicative constructor

FieldPVCoordinates(FieldPVCoordinates<T>, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.FieldPVCoordinates

Subtractive constructor

FieldPVCoordinates(double, FieldPVCoordinates<T>, double, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.FieldPVCoordinates

Linear constructor

FieldPVCoordinates(T, FieldPVCoordinates<T>, T, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.FieldPVCoordinates

Linear constructor

FieldPVCoordinates(T, PVCoordinates, T, PVCoordinates) - Constructor for class org.orekit.utils.FieldPVCoordinates

Linear constructor

FieldPVCoordinates(double, FieldPVCoordinates<T>, double, FieldPVCoordinates<T>, double, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.FieldPVCoordinates

Linear constructor

FieldPVCoordinates(T, FieldPVCoordinates<T>, T, FieldPVCoordinates<T>, T, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.FieldPVCoordinates

Linear constructor

FieldPVCoordinates(T, PVCoordinates, T, PVCoordinates, T, PVCoordinates) - Constructor for class org.orekit.utils.FieldPVCoordinates

Linear constructor

FieldPVCoordinates(double, FieldPVCoordinates<T>, double, FieldPVCoordinates<T>, double, FieldPVCoordinates<T>, double, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.FieldPVCoordinates

Linear constructor

FieldPVCoordinates(T, FieldPVCoordinates<T>, T, FieldPVCoordinates<T>, T, FieldPVCoordinates<T>, T, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.FieldPVCoordinates

Linear constructor

FieldPVCoordinates(T, PVCoordinates, T, PVCoordinates, T, PVCoordinates, T, PVCoordinates) - Constructor for class org.orekit.utils.FieldPVCoordinates

Linear constructor

FIFTIES_EPOCH - Static variable in class org.orekit.time.AbsoluteDate

Reference epoch for 1950 dates: 1950-01-01T00:00:00 Terrestrial Time.

FIFTIES_EPOCH - Static variable in class org.orekit.time.DateComponents

Reference epoch for 1950 dates: 1950-01-01.

fillHalfRow(double, Vector3D, double[], int) - Static method in class org.orekit.orbits.Orbit

Fill a Jacobian half row with a single vector.

fillHalfRow(double, Vector3D, double, Vector3D, double[], int) - Static method in class org.orekit.orbits.Orbit

Fill a Jacobian half row with a linear combination of vectors.

fillHalfRow(double, Vector3D, double, Vector3D, double, Vector3D, double[], int) - Static method in class org.orekit.orbits.Orbit

Fill a Jacobian half row with a linear combination of vectors.

fillHalfRow(double, Vector3D, double, Vector3D, double, Vector3D, double, Vector3D, double[], int) - Static method in class org.orekit.orbits.Orbit

Fill a Jacobian half row with a linear combination of vectors.

fillHalfRow(double, Vector3D, double, Vector3D, double, Vector3D, double, Vector3D, double, Vector3D, double[], int) - Static method in class org.orekit.orbits.Orbit

Fill a Jacobian half row with a linear combination of vectors.

fillHalfRow(double, Vector3D, double, Vector3D, double, Vector3D, double, Vector3D, double, Vector3D, double, Vector3D, double[], int) - Static method in class org.orekit.orbits.Orbit

Fill a Jacobian half row with a linear combination of vectors.

fillHistory(IERSConventions.NutationCorrectionConverter, SortedSet<EOPEntry>) - Method in interface org.orekit.frames.EOPHistoryLoader

Load celestial body.

FilterType - Enum in org.orekit.propagation.events

Enumerate for filtering events.

FiniteDifferencePropagatorConverter - Class in org.orekit.propagation.conversion

Propagator converter using finite differences to compute the jacobian.

FiniteDifferencePropagatorConverter(PropagatorBuilder, double, int) - Constructor for class org.orekit.propagation.conversion.FiniteDifferencePropagatorConverter

Simple constructor.

FirstOrderIntegratorBuilder - Interface in org.orekit.propagation.conversion

This interface is the top-level abstraction to build first order integrators for propagators conversion.

fit() - Method in class org.orekit.utils.SecularAndHarmonic

Fit parameters.

FixedRate - Class in org.orekit.attitudes

This class handles a simple attitude provider at constant rate around a fixed axis.

FixedRate(Attitude) - Constructor for class org.orekit.attitudes.FixedRate

Creates a new instance.

FixedTransformProvider - Class in org.orekit.frames

Transform provider using fixed transform.

FixedTransformProvider(Transform) - Constructor for class org.orekit.frames.FixedTransformProvider

Simple constructor.

FixedTroposphericDelay - Class in org.orekit.models.earth

A static tropospheric model that interpolates the actual tropospheric delay based on values read from a configuration file (tropospheric-delay.txt) via the DataProvidersManager.

FixedTroposphericDelay(double[], double[], double[][]) - Constructor for class org.orekit.models.earth.FixedTroposphericDelay

Creates a new FixedTroposphericDelay instance.

FixedTroposphericDelay(String) - Constructor for class org.orekit.models.earth.FixedTroposphericDelay

Creates a new FixedTroposphericDelay instance, and loads the delay values from the given resource via the DataProvidersManager.

ForceModel - Interface in org.orekit.forces

This interface represents a force modifying spacecraft motion.

Frame - Class in org.orekit.frames

Tridimensional references frames class.

Frame(Frame, Transform, String) - Constructor for class org.orekit.frames.Frame

Build a non-inertial frame from its transform with respect to its parent.

Frame(Frame, TransformProvider, String) - Constructor for class org.orekit.frames.Frame

Build a non-inertial frame from its transform with respect to its parent.

Frame(Frame, Transform, String, boolean) - Constructor for class org.orekit.frames.Frame

Build a frame from its transform with respect to its parent.

Frame(Frame, TransformProvider, String, boolean) - Constructor for class org.orekit.frames.Frame

Build a frame from its transform with respect to its parent.

FrameAncestorException - Exception in org.orekit.errors

This class is the base class for exception thrown by the UpdatableFrame.updateTransform method.

FrameAncestorException(Localizable, Object...) - Constructor for exception org.orekit.errors.FrameAncestorException

Simple constructor.

FramesFactory - Class in org.orekit.frames

Factory for predefined reference frames.

freeze() - Method in class org.orekit.frames.Transform

Get a frozen transform.

FundamentalNutationArguments - Class in org.orekit.data

Class computing the fundamental arguments for nutation and tides.

FundamentalNutationArguments(IERSConventions, TimeScale, InputStream, String) - Constructor for class org.orekit.data.FundamentalNutationArguments

Build a model of fundamental arguments from an IERS table file.

FundamentalNutationArguments(IERSConventions, TimeScale, List<double[]>) - Constructor for class org.orekit.data.FundamentalNutationArguments

Build a model of fundamental arguments from an IERS table file.

FUTURE_INFINITY - Static variable in class org.orekit.time.AbsoluteDate

Dummy date at infinity in the future direction.

G

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.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.ApsideDetector

Compute the value of the switching function.

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.DihedralFieldOfViewDetector

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 interface org.orekit.propagation.events.EventDetector

Compute the value of the switching function.

g(SpacecraftState) - Method in class org.orekit.propagation.events.EventFilter

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.GeographicZoneDetector

Compute the value of the detection function.

g(SpacecraftState) - Method in class org.orekit.propagation.events.NodeDetector

Compute the value of the switching function.

g - Variable in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution

Equinoctial frame g vector.

G0_STANDARD_GRAVITY - Static variable in interface org.orekit.utils.Constants

Standard gravity constant, used in maneuvers definition: 9.80665 m/s².

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 Γ^m_n,s(γ) function from equation 2.7.1-(13).

GammaMnsFunction(double[], double, int) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.GammaMnsFunction

Simple constructor.

generate(T, 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

Generate a CartesianOrbit from the KeplerianOrbit.

generateCartesianOrbit() - Method in class org.orekit.files.ccsds.OPMFile

Generate a CartesianOrbit from the OPM state vector data.

generateKeplerianOrbit() - Method in class org.orekit.files.ccsds.OMMFile

Generate a KeplerianOrbit based on the OMM mean keplerian elements.

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.

GenericTimeStampedCache<T extends TimeStamped> - Class in org.orekit.utils

Generic thread-safe cache for time-stamped data.

GenericTimeStampedCache(int, int, double, double, TimeStampedGenerator<T>, Class<T>) - Constructor for class org.orekit.utils.GenericTimeStampedCache

Simple constructor.

GeodeticPoint - Class in org.orekit.bodies

Point location relative to a 2D body surface.

GeodeticPoint(double, double, double) - Constructor for class org.orekit.bodies.GeodeticPoint

Build a new instance.

GeographicZoneDetector - Class in org.orekit.propagation.events

Detector for entry/exit of a zone defined by geographic boundaries.

GeographicZoneDetector(BodyShape, SphericalPolygonsSet, double) - Constructor for class org.orekit.propagation.events.GeographicZoneDetector

Build a new detector.

GeographicZoneDetector(double, double, BodyShape, SphericalPolygonsSet, double) - Constructor for class org.orekit.propagation.events.GeographicZoneDetector

Build a detector.

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

Factory for different GeoMagneticField models.

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

get24HoursKp(AbsoluteDate) - Method in interface org.orekit.forces.drag.DTM2000InputParameters

Get the last 24H mean geomagnetic index.

get24HoursKp(AbsoluteDate) - Method in class org.orekit.forces.drag.MarshallSolarActivityFutureEstimation

The Kp index is derived from the Ap 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.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.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.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.

getAbsorptionCoefficient() - Method in class org.orekit.forces.BoxAndSolarArraySpacecraft

Get the absorption coefficient.

getAbsorptionCoefficient() - Method in interface org.orekit.forces.radiation.RadiationSensitive

Get the absorption coefficient.

getAbsorptionCoefficient() - Method in class org.orekit.forces.SphericalSpacecraft

Get the absorption coefficient.

getAcceleration() - Method in class org.orekit.files.ccsds.OEMFile.EphemeridesDataLine

Get the ephemerides data line acceleration vector.

getAcceleration() - Method in class org.orekit.frames.Transform

Get the second time derivative of the translation.

getAcceleration(SpacecraftState) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution

Compute the acceleration due to the non conservative perturbing force.

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.general.SatelliteInformation

Returns the estimated accuracy of the orbit entries for this satellite (in m).

getAdaptedPropagator() - Method in class org.orekit.propagation.conversion.AbstractPropagatorConverter

Get the adapted propagator.

getAdditionalState(SpacecraftState) - Method in interface org.orekit.propagation.AdditionalStateProvider

Get the additional state.

getAdditionalState(String) - Method in class org.orekit.propagation.SpacecraftState

Get an 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 interface org.orekit.propagation.Propagator

Get an unmodifiable list of providers for additional state.

getAdditionalStates() - Method in class org.orekit.propagation.SpacecraftState

Get an unmodifiable map of additional states.

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.

getAgency() - Method in class org.orekit.files.sp3.SP3File

Returns the agency that prepared this SP3 file.

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.

getAlpha(PositionAngle) - Method in class org.orekit.orbits.CircularOrbit

Get the latitude argument.

getAlpha() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements

Get direction cosine α for central body.

getAlphaE() - Method in class org.orekit.orbits.CircularOrbit

Get the eccentric latitude argument.

getAlphaM() - Method in class org.orekit.orbits.CircularOrbit

Get the mean latitude argument.

getAlphaV() - Method in class org.orekit.orbits.CircularOrbit

Get the true latitude argument.

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.

getAncestor(int) - Method in class org.orekit.frames.Frame

Get the n^th ancestor of the frame.

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.KeplerianOrbit

Get the anomaly.

getAnomalyType() - Method in class org.orekit.files.ccsds.OGMFile

Get the type of anomaly (true or mean).

getAp(AbsoluteDate) - Method in interface org.orekit.forces.drag.JB2006InputParameters

Get the Geomagnetic planetary 3-hour index A_p.

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(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.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() - Method in class org.orekit.propagation.SpacecraftState

Get the attitude.

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.integration.StateMapper

Get the attitude provider.

getAttitudeProvider() - Method in interface org.orekit.propagation.Propagator

Get attitude provider.

getAvailableParameters() - Method in class org.orekit.propagation.conversion.AbstractPropagatorConverter

Get the available free parameters.

getAvailableParameters() - Method in class org.orekit.propagation.numerical.PartialDerivativesEquations

Get the names of the available parameters in the propagator.

getAvailableSatelliteNumbers() - Method in class org.orekit.propagation.analytical.tle.TLESeries

Get the available satellite numbers.

getAxis1() - Method in class org.orekit.propagation.events.DihedralFieldOfViewDetector

Get the direction of FOV 1st dihedral axis.

getAxis2() - Method in class org.orekit.propagation.events.DihedralFieldOfViewDetector

Get the direction of FOV 2nd dihedral axis.

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).

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.

getBasicDimension() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator

Get state vector dimension without additional parameters.

getBeta() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements

Get direction cosine β for central body.

getBody(String) - Static method in class org.orekit.bodies.CelestialBodyFactory

Get a celestial body.

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.semianalytical.dsst.forces.DSSTThirdBody

Get third body.

getBodyFrame() - Method in class org.orekit.attitudes.GroundPointing

Get the body frame.

getBodyFrame() - Method in interface org.orekit.bodies.BodyShape

Get body frame related to body shape.

getBodyFrame() - Method in class org.orekit.bodies.OneAxisEllipsoid

Get body frame related to body shape.

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.

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.

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.

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.

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.Transform

Get the underlying elementary cartesian part.

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.propagation.events.CircularFieldOfViewDetector

Get the direction of FOV center.

getCenter() - Method in class org.orekit.propagation.events.DihedralFieldOfViewDetector

Get the direction of FOV center.

getCenterBody() - Method in class org.orekit.files.ccsds.ODMMetaData

Get the CelestialBody corresponding to the center name.

getCenterName() - Method in class org.orekit.files.ccsds.ODMMetaData

Get the origin of reference frame.

getChildren() - Method in class org.orekit.frames.OrphanFrame

Get all children of the instance.

getCircularEx() - Method in class org.orekit.orbits.CircularOrbit

Get the first component of the circular eccentricity vector.

getCircularEy() - Method in class org.orekit.orbits.CircularOrbit

Get the second component of the circular eccentricity vector.

getCIRF(IERSConventions, boolean) - Static method in class org.orekit.frames.FramesFactory

Get the CIRF2000 reference frame.

getCj(int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.CjSjCoefficient

Get the C_j 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.

getClockCorrection() - Method in class org.orekit.files.general.SatelliteTimeCoordinate

Returns the clock correction value.

getClockRateChange() - Method in class org.orekit.files.general.SatelliteTimeCoordinate

Returns the clock rate change value.

getClosestTLE(AbsoluteDate) - Method in class org.orekit.propagation.analytical.tle.TLESeries

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.

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.

getComponents(TimeScale) - Method in class org.orekit.time.AbsoluteDate

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.frames.EOPHistory

Get the IERS conventions to which these EOP apply.

getCoordinate() - Method in class org.orekit.files.general.SatelliteTimeCoordinate

Returns the coordinate of this entry.

getCoordinateSystem() - Method in class org.orekit.files.ccsds.OEMFile

Returns the coordinate system of the entries in this orbit file.

getCoordinateSystem() - Method in class org.orekit.files.ccsds.OMMFile

Returns the coordinate system of the entries in this orbit file.

getCoordinateSystem() - Method in class org.orekit.files.ccsds.OPMFile

Returns the coordinate system of the entries in this orbit file.

getCoordinateSystem() - Method in interface org.orekit.files.general.OrbitFile

Returns the coordinate system of the entries in this orbit file.

getCoordinateSystem() - Method in class org.orekit.files.sp3.SP3File

Returns the coordinate system of the entries in this orbit file.

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.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.

getCreationDate() - Method in class org.orekit.files.ccsds.ODMFile

Get the file creation date and time in UTC.

getCurrentDate() - Method in interface org.orekit.propagation.sampling.OrekitStepInterpolator

Get the current grid date.

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.

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.data.DelaunayArguments

Get the date.

getDate() - Method in class org.orekit.data.FieldDelaunayArguments

Get the date.

getDate() - Method in class org.orekit.files.general.SatelliteTimeCoordinate

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.Transform

Get the date.

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.conversion.AbstractPropagatorConverter

Get the date of the initial state.

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.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 interface org.orekit.time.TimeStamped

Get the 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 dC_j / dh coefficient.

getDcjDk(int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.CjSjCoefficient

Get the dC_j / dk coefficient.

getDdEps() - Method in class org.orekit.frames.EOPEntry

Get the correction for nutation in obliquity δΔε.

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".

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(AbsoluteDate, Vector3D, Frame) - Method in interface org.orekit.forces.drag.Atmosphere

Get the local density.

getDensity(int, double, double, double, double, double, double, double, double) - Method in class org.orekit.forces.drag.DTM2000

Get the local density with initial entries.

getDensity(AbsoluteDate, Vector3D, Frame) - Method in class org.orekit.forces.drag.DTM2000

Get the local density.

getDensity(Vector3D, Vector3D) - Method in class org.orekit.forces.drag.HarrisPriester

Get the local density.

getDensity(AbsoluteDate, Vector3D, Frame) - Method in class org.orekit.forces.drag.HarrisPriester

Get the local density at some position.

getDensity(double, double, double, double, double, double, double, double, double, double, double, double, double) - Method in class org.orekit.forces.drag.JB2006

Get the local density with initial entries.

getDensity(AbsoluteDate, Vector3D, Frame) - Method in class org.orekit.forces.drag.JB2006

Get the local density.

getDensity(AbsoluteDate, Vector3D, Frame) - Method in class org.orekit.forces.drag.SimpleExponentialAtmosphere

Get the local density.

getDepth() - Method in class org.orekit.frames.Frame

Get the depth of the frame.

getDerivative(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GammaMnsFunction

Get Γ function derivative.

getDerivative(int, double) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenTesseralLinear

Compute the value of the derivative dK_j^{-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 dK₀^{n, 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.

getdGjsdAlpha(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials

Get the dG_js / dα coefficient.

getdGjsdBeta(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials

Get the dG_js / dβ coefficient.

getdGjsdh(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials

Get the dG_js / dh coefficient.

getdGjsdk(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials

Get the dG_js / dk coefficient.

getdGmsdAlpha(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHmsjPolynomials

Get the dG_ms^j / d_α coefficient.

getdGmsdBeta(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHmsjPolynomials

Get the dG_ms^j / d_β coefficient.

getdGmsdh(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHmsjPolynomials

Get the dG_ms^j / d_h coefficient.

getdGmsdk(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHmsjPolynomials

Get the dG_ms^j / d_k coefficient.

getdHjsdAlpha(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials

Get the dH_js / dα coefficient.

getdHjsdBeta(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials

Get the dH_js / dβ coefficient.

getdHjsdh(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials

Get the dH_js / dh coefficient.

getdHjsdk(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials

Get the dH_js / dk coefficient.

getdHmsdAlpha(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHmsjPolynomials

Get the dH_ms^j / d_α coefficient.

getdHmsdBeta(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHmsjPolynomials

Get the dH_ms^j / d_β coefficient.

getdHmsdh(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHmsjPolynomials

Get the dH_ms^j / d_h coefficient.

getdHmsdk(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHmsjPolynomials

Get the dH_ms^j / d_k coefficient.

getdIjsdAlpha(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials

Get the dI_js / dα coefficient.

getdIjsdBeta(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials

Get the dI_js / dβ coefficient.

getdIjsdh(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials

Get the dI_js / dh coefficient.

getdIjsdk(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials

Get the dI_js / dk coefficient.

getdJjsdAlpha(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials

Get the dJ_js / dα coefficient.

getdJjsdBeta(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials

Get the dJ_js / dβ coefficient.

getdJjsdh(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials

Get the dJ_js / dh coefficient.

getdJjsdk(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials

Get the dJ_js / dk coefficient.

getdLnsdGamma(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.LnsCoefficients

Get the value of dL_n^s / dγ (γ).

getDnl(double, double, int, int) - Static method in class org.orekit.propagation.semianalytical.dsst.utilities.UpperBounds

Get the upper bound value D_n^l(Χ).

getDoodson() - Method in class org.orekit.forces.gravity.potential.OceanTidesWave

Get the Doodson number for the wave.

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.

getDragCoefficient() - Method in class org.orekit.forces.BoxAndSolarArraySpacecraft

Get the drag coefficient.

getDragCoefficient() - Method in interface org.orekit.forces.drag.DragSensitive

Get the drag coefficient.

getDragCoefficient() - Method in class org.orekit.forces.SphericalSpacecraft

Get the drag coefficient.

getDsjDh(int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.CjSjCoefficient

Get the dS_j / dh coefficient.

getDsjDk(int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.CjSjCoefficient

Get the dS_j / dk coefficient.

getDuration() - Method in class org.orekit.files.ccsds.OPMFile.Maneuver

Get duration (value is 0 for impulsive maneuver).

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.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.KeplerianOrbit

Get the eccentricity.

getE() - Method in class org.orekit.orbits.Orbit

Get the eccentricity.

getE() - Method in class org.orekit.propagation.analytical.tle.TLE

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.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.

getEcc() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements

Get the eccentricity.

getEccentricAnomaly() - Method in class org.orekit.orbits.KeplerianOrbit

Get the eccentric anomaly.

getEcliptic(IERSConventions) - Static method in class org.orekit.frames.FramesFactory

Get the ecliptic frame.

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(Vector3D, Frame, AbsoluteDate) - Method in class org.orekit.frames.TopocentricFrame

Get the elevation of a point with regards to the local point.

getElevation(double) - Method in class org.orekit.utils.ElevationMask

Get the interpolated elevation for a given azimuth according to the mask.

getElevationMask() - Method in class org.orekit.propagation.events.ElevationDetector

Returns the currently configured elevation mask.

getEME2000() - Static method in class org.orekit.frames.FramesFactory

Get the unique EME2000 frame.

getEndDate() - Method in class org.orekit.frames.EOPHistory

Get the date of the last available Earth Orientation Parameters.

getEntries() - Method in class org.orekit.utils.GenericTimeStampedCache

Get the total number of entries cached.

getEOPHistory(IERSConventions, boolean) - Static method in class org.orekit.frames.FramesFactory

Get Earth Orientation Parameters history.

getEOPHistory() - Method in class org.orekit.time.UT1Scale

Get the EOP 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.

getEphemeridesDataLines() - Method in class org.orekit.files.ccsds.OEMFile.EphemeridesBlock

Get the list of Ephemerides data lines.

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.OEMFile

Returns the start epoch of the orbit file.

getEpoch() - Method in class org.orekit.files.ccsds.OGMFile

Get epoch of state vector, Keplerian elements and covariance matrix data.

getEpoch() - Method in interface org.orekit.files.general.OrbitFile

Returns the start epoch of the orbit file.

getEpoch() - Method in class org.orekit.files.general.SatelliteTimeCoordinate

Returns the epoch for this coordinate.

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.ccsds.ODMFile

Not supported by CCSDS orbit messages.

getEpochInterval() - Method in interface org.orekit.files.general.OrbitFile

Returns the time interval between epochs (in seconds).

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.

getEquinoctialEx() - Method in class org.orekit.orbits.CircularOrbit

Get the first component of the equinoctial eccentricity vector.

getEquinoctialEx() - Method in class org.orekit.orbits.EquinoctialOrbit

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.

getEquinoctialEx() - Method in class org.orekit.orbits.Orbit

Get the first component of the equinoctial eccentricity vector.

getEquinoctialEx() - Method in class org.orekit.propagation.SpacecraftState

Get the first component of the eccentricity vector (as per equinoctial parameters).

getEquinoctialEy() - Method in class org.orekit.orbits.CartesianOrbit

Get the second component of the equinoctial eccentricity vector.

getEquinoctialEy() - Method in class org.orekit.orbits.CircularOrbit

Get the second component of the equinoctial eccentricity vector.

getEquinoctialEy() - Method in class org.orekit.orbits.EquinoctialOrbit

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.

getEquinoctialEy() - Method in class org.orekit.orbits.Orbit

Get the second component of the equinoctial eccentricity vector.

getEquinoctialEy() - Method in class org.orekit.propagation.SpacecraftState

Get the second component of the eccentricity vector (as per equinoctial parameters).

getEquinoxNutationCorrection(AbsoluteDate) - Method in class org.orekit.frames.EOPHistory

Get the correction to the nutation parameters for equinox-based paradigm.

getEvaluations() - Method in class org.orekit.propagation.conversion.AbstractPropagatorConverter

Get the number of objective function evaluations.

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.

getEventsDetectors() - Method in class org.orekit.forces.drag.DragForce

There are no discrete events for this 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.CunninghamAttractionModel

Get the discrete events related to the model.

getEventsDetectors() - Method in class org.orekit.forces.gravity.DrozinerAttractionModel

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

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.integration.AbstractIntegratedPropagator

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 class org.orekit.propagation.semianalytical.dsst.forces.DSSTCentralBody

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.DSSTThirdBody

Get the discrete events related to the model.

getEventTime() - Method in class org.orekit.propagation.events.EventState

Get the occurrence time of the event triggered in the current step.

getException() - Method in exception org.orekit.errors.OrekitExceptionWrapper

Get the wrapped exception.

getExosphericTemp() - Method in class org.orekit.forces.drag.JB2006

Get the exospheric temperature above input position.

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.JB2006InputParameters

Get the value of the instantaneous solar flux index (1e^-22*Watt/(m²*Hertz)).

getF10B(AbsoluteDate) - Method in interface org.orekit.forces.drag.JB2006InputParameters

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.

getField(GeoMagneticFieldFactory.FieldModel, double) - Static method in class org.orekit.models.earth.GeoMagneticFieldFactory

Get the GeoMagneticField for the given model type and year.

getFieldVector() - Method in class org.orekit.models.earth.GeoMagneticElements

Returns the magnetic field vector in nTesla.

getFileDate(AbsoluteDate) - Method in class org.orekit.forces.drag.MarshallSolarActivityFutureEstimation

Get the date of the file from which data at the specified date comes from.

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

Get the first TLE.

getFirstDate() - Method in class org.orekit.propagation.analytical.tle.TLESeries

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.

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.NumericalPropagator

Get perturbing force models list.

getFormatVersion() - Method in class org.orekit.files.ccsds.ODMFile

Get the CCSDS ODM (OPM, OMM or OEM) 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(IERSConventions, boolean) - Method in enum org.orekit.files.ccsds.CCSDSFrame

Get the frame corresponding to the CCSDS constant.

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 interface org.orekit.forces.drag.Atmosphere

Get the frame of the central body.

getFrame() - Method in class org.orekit.forces.drag.DTM2000

Get the frame of the central body.

getFrame() - Method in class org.orekit.forces.drag.HarrisPriester

Get the frame of the central body.

getFrame() - Method in class org.orekit.forces.drag.JB2006

Get the frame of the central body.

getFrame() - Method in class org.orekit.forces.drag.SimpleExponentialAtmosphere

Get the frame of the central body.

getFrame(Predefined) - Static method in class org.orekit.frames.FramesFactory

Get one of the predefined frames.

getFrame() - Method in class org.orekit.frames.OrphanFrame

Get the associated frame.

getFrame() - Method in class org.orekit.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.tle.TLEPropagator

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 class org.orekit.propagation.conversion.EcksteinHechlerPropagatorBuilder

Get the frame in which the orbit is propagated.

getFrame() - Method in class org.orekit.propagation.conversion.KeplerianPropagatorBuilder

Get the frame in which the orbit is propagated.

getFrame() - Method in class org.orekit.propagation.conversion.NumericalPropagatorBuilder

Get the frame in which the orbit is propagated.

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.conversion.TLEPropagatorBuilder

Get the frame in which the orbit is propagated.

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.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.

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.

getFreeParameters() - Method in class org.orekit.propagation.conversion.AbstractPropagatorConverter

Get the free parameters.

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.

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.

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.

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.integration.AbstractIntegratedPropagator

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

Get the number of calls to the GenericTimeStampedCache.getNeighbors(AbsoluteDate) method.

getGjs(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials

Get the G_js coefficient.

getGM() - Method in interface org.orekit.bodies.CelestialBody

Get the attraction coefficient of the body.

getGmsj(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHmsjPolynomials

Get the G_ms^j 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.

getGPS() - Static method in class org.orekit.time.TimeScalesFactory

Get the Global Positioning System scale.

getGpsWeek() - Method in class org.orekit.files.sp3.SP3File

Returns the GPS week as contained in the SP3 file.

getGradient() - Method in class org.orekit.forces.gravity.HolmesFeatherstoneAttractionModel.GradientHessian

Get a reference to the gradient.

getGridPoints() - Method in class org.orekit.frames.InterpolatingTransformProvider

Get the number of interpolation grid points.

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.VariableStepInterpolationGrid

Get grid points that are within the current step.

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.

getHalfAperture1() - Method in class org.orekit.propagation.events.DihedralFieldOfViewDetector

Get the half aperture angle of FOV 1st dihedra.

getHalfAperture2() - Method in class org.orekit.propagation.events.DihedralFieldOfViewDetector

Get the half aperture angle of FOV 2nd dihedra.

getHandler() - Method in class org.orekit.propagation.events.AbstractDetector

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.

getHeaderComment() - Method in class org.orekit.files.ccsds.ODMFile

Get the header comment.

getHessian() - Method in class org.orekit.forces.gravity.HolmesFeatherstoneAttractionModel.GradientHessian

Get a reference to the Hessian.

getHjs(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials

Get the H_js coefficient.

getHmsj(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHmsjPolynomials

Get the H_ms^j 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.

getHP() - Method in class org.orekit.propagation.numerical.ParameterConfiguration

Get parameter step.

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.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.SpacecraftState

Get the first component of the inclination vector (as per equinoctial parameters).

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.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.SpacecraftState

Get the second component of the inclination vector (as per equinoctial parameters).

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.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.SpacecraftState

Get the inclination.

getICRF() - Static method in class org.orekit.frames.FramesFactory

Get the unique ICRF frame.

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 I_js 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.

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.Ephemeris

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.

getInstance() - Static method in class org.orekit.data.DataProvidersManager

Get the unique instance.

getInstantFlux(AbsoluteDate) - Method in interface org.orekit.forces.drag.DTM2000InputParameters

Get the value of the instantaneous solar flux.

getInstantFlux(AbsoluteDate) - Method in class org.orekit.forces.drag.MarshallSolarActivityFutureEstimation

Get the value of the instantaneous solar flux.

getIntegrator() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator

Get the integrator used by the propagator.

getInterpolatedDate() - Method in interface org.orekit.propagation.sampling.OrekitStepInterpolator

Get the interpolated date.

getInterpolatedState() - Method in interface org.orekit.propagation.sampling.OrekitStepInterpolator

Get the interpolated state.

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.

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.

getInverse() - Method in class org.orekit.frames.Transform

Get the inverse transform of the instance.

getISP() - Method in class org.orekit.forces.maneuvers.ConstantThrustManeuver

Get the specific impulse.

getIsp() - Method in class org.orekit.forces.maneuvers.ImpulseManeuver

Get the specific impulse.

getITRF(IERSConventions, boolean) - Static method in class org.orekit.frames.FramesFactory

Get the ITRF2008 reference frame, using IERS 2010 conventions.

getITRFEquinox(IERSConventions, boolean) - Static method in class org.orekit.frames.FramesFactory

Get the equinox-based ITRF reference frame.

getJ2000Day() - Method in class org.orekit.time.DateComponents

Get the day number with respect to J2000 epoch.

getJacobian(Orbit, PositionAngle, double[][]) - Method in class org.orekit.forces.maneuvers.SmallManeuverAnalyticalModel

Compute the Jacobian of the orbit with respect to maneuver parameters.

getJacobian(double[][]) - Method in class org.orekit.frames.Transform

Deprecated.

as of 7.0, replaced with Transform.getJacobian(CartesianDerivativesFilter, double[][])

getJacobian(CartesianDerivativesFilter, double[][]) - Method in class org.orekit.frames.Transform

Compute the Jacobian of the Transform.transformPVCoordinates(PVCoordinates) method of the transform.

getJacobianWrtCartesian(PositionAngle, double[][]) - Method in class org.orekit.orbits.CartesianOrbit

getJacobianWrtCartesian(PositionAngle, double[][]) - Method in class org.orekit.orbits.Orbit

Compute the Jacobian of the orbital parameters with respect to the Cartesian parameters.

getJacobianWrtParameters(PositionAngle, double[][]) - Method in class org.orekit.orbits.Orbit

Compute the Jacobian of the Cartesian parameters with respect to the orbital parameters.

getJjs(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials

Get the J_js coefficient.

getJulianDay() - Method in class org.orekit.files.sp3.SP3File

Returns the julian day for this SP3 file.

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.Orbit

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.Orbit

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.

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.

getLast() - Method in class org.orekit.propagation.analytical.tle.TLESeries

Get the last TLE.

getLastDate() - Method in class org.orekit.propagation.analytical.tle.TLESeries

Get the last date of the series.

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.GeodeticPoint

Get the latitude.

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.

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.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.SpacecraftState

Get the eccentric latitude argument (as per equinoctial parameters).

getLeap(AbsoluteDate) - Method in class org.orekit.time.UTCScale

Get the value of the previous leap.

getLf() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements

Get the eccentric longitude.

getLightningRatio(Vector3D, Frame, AbsoluteDate) - Method in class org.orekit.forces.radiation.SolarRadiationPressure

Get the lightning 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.

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.

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.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.semianalytical.dsst.utilities.AuxiliaryElements

Get the mean longitude.

getLM() - Method in class org.orekit.propagation.SpacecraftState

Get the mean latitude 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.

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.

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.

getLns(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.LnsCoefficients

Get the value of L_n^s(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

getLocalizedString(Locale) - Method in enum org.orekit.errors.OrekitMessages

getLocalTemp() - Method in class org.orekit.forces.drag.JB2006

Get the temperature at input position.

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.

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.

getLongitude() - Method in class org.orekit.bodies.GeodeticPoint

Get the longitude.

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.

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.

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.

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.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.semianalytical.dsst.utilities.AuxiliaryElements

Get the true longitude.

getLv() - Method in class org.orekit.propagation.SpacecraftState

Get the true latitude argument (as per equinoctial parameters).

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.

getMainStateEquations(AbstractIntegrator) - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator

Get the differential equations to integrate (for main state only).

getMainStateEquations(AbstractIntegrator) - Method in class org.orekit.propagation.numerical.NumericalPropagator

Get the differential equations to integrate (for main state only).

getMainStateEquations(AbstractIntegrator) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator

Get the differential equations to integrate (for main state only).

getMam() - Method in class org.orekit.forces.drag.DTM2000

Get the local mean atomic mass.

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.integration.AbstractIntegratedPropagator

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.GeographicZoneDetector

Get the angular margin to apply (radians).

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(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.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.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() - Method in class org.orekit.propagation.SpacecraftState

Gets the current mass.

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.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 interface org.orekit.propagation.events.EventDetector

Get maximal time interval between switching function checks.

getMaxChunksDuration() - Method in class org.orekit.bodies.JPLEphemeridesLoader

Get the maximal chunks duration.

getMaxDate() - Method in interface org.orekit.forces.drag.DTM2000InputParameters

Gets the available data range maximum date.

getMaxDate() - Method in interface org.orekit.forces.drag.JB2006InputParameters

Gets the available data range maximum date.

getMaxDate() - Method in class org.orekit.forces.drag.MarshallSolarActivityFutureEstimation

Gets the available data range maximum date.

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 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 interface org.orekit.propagation.events.EventDetector

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.

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.

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.

getMeanElementRate(SpacecraftState) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution

Computes the mean equinoctial elements rates da_i / dt.

getMeanElementRate(SpacecraftState) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTCentralBody

Computes the mean equinoctial elements rates da_i / dt.

getMeanElementRate(SpacecraftState) - Method in interface org.orekit.propagation.semianalytical.dsst.forces.DSSTForceModel

Computes the mean equinoctial elements rates da_i / dt.

getMeanElementRate(SpacecraftState) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBody

Computes the mean equinoctial elements rates da_i / dt.

getMeanElementTheory() - Method in class org.orekit.files.ccsds.OMMFile.OMMMetaData

Get the description of the Mean Element Theory.

getMeanFlux(AbsoluteDate) - Method in interface org.orekit.forces.drag.DTM2000InputParameters

Get the value of the mean solar flux.

getMeanFlux(AbsoluteDate) - Method in class org.orekit.forces.drag.MarshallSolarActivityFutureEstimation

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.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.

getMercury() - Static method in class org.orekit.bodies.CelestialBodyFactory

Get the Mercury singleton body.

getMessage(Locale) - Method in exception org.orekit.errors.OrekitException

Gets the message in a specified locale.

getMessage() - Method in exception org.orekit.errors.OrekitException

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.

getMetaDataComment() - Method in class org.orekit.files.ccsds.OPMFile

Get the comment for meta-data.

getMinAlt() - Method in class org.orekit.forces.drag.HarrisPriester

Get the minimal altitude for the model.

getMinDate() - Method in interface org.orekit.forces.drag.DTM2000InputParameters

Gets the available data range minimum date.

getMinDate() - Method in interface org.orekit.forces.drag.JB2006InputParameters

Gets the available data range minimum date.

getMinDate() - Method in class org.orekit.forces.drag.MarshallSolarActivityFutureEstimation

Gets the available data range minimum date.

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 class org.orekit.propagation.integration.IntegratedEphemeris

Get the first date of the range.

getMinElevation() - Method in class org.orekit.propagation.events.ElevationDetector

Returns the currently configured minimum valid elevation value.

getMinute() - Method in class org.orekit.time.TimeComponents

Get the minute number.

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.

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.

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.propagation.AbstractPropagator

Get the current operating mode of the propagator.

getMode() - Method in interface org.orekit.propagation.Propagator

Get the current operating mode of the propagator.

getModelName() - Method in class org.orekit.models.earth.GeoMagneticField

Returns the model name.

getModels() - Method in class org.orekit.models.earth.GeoMagneticModelLoader

Returns a Collection of the GeoMagneticField models that have been successfully loaded.

getModifiedRodrigues(double) - Method in class org.orekit.utils.AngularCoordinates

Convert rotation, rate and acceleration to modified Rodrigues vector and derivatives.

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.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.Orbit

Get the central acceleration constant.

getMU() - Static method in class org.orekit.propagation.analytical.tle.TLEPropagator

Get the Earth gravity coefficient used for TLE propagation.

getMu() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator

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.

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.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.frames.Frame

Get the name.

getName() - Method in enum org.orekit.frames.Predefined

Get the name of the frame.

getName() - Method in interface org.orekit.propagation.AdditionalStateProvider

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 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.GalileoScale

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.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.

getNbManeuvers() - Method in class org.orekit.files.ccsds.OPMFile

Get the number of maneuvers present in the OPM.

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

Get the fixed size of the arrays to be returned by GenericTimeStampedCache.getNeighbors(AbsoluteDate).

getNeighborsSize() - Method in class org.orekit.utils.ImmutableTimeStampedCache

getNeighborsSize() - Method in interface org.orekit.utils.TimeStampedCache

Get the fixed size of the lists returned by TimeStampedCache.getNeighbors(AbsoluteDate).

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.

getNewtonianAttractionForceModel() - Method in class org.orekit.propagation.numerical.NumericalPropagator

Get the Newtonian attraction from the central body force model.

getNonInterpolatingTransform(Frame, Frame, AbsoluteDate) - 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.

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, Vector3D, Rotation) - Method in class org.orekit.forces.BoxAndSolarArraySpacecraft

Get solar array normal in spacecraft frame.

getNormal(AbsoluteDate, Frame, FieldVector3D<DerivativeStructure>, FieldRotation<DerivativeStructure>) - Method in class org.orekit.forces.BoxAndSolarArraySpacecraft

Get solar array normal in spacecraft frame.

getNormalizedCnm(int, int) - Method in interface org.orekit.forces.gravity.potential.NormalizedSphericalHarmonicsProvider.NormalizedSphericalHarmonics

Get a spherical harmonic cosine coefficient.

getNormalizedProvider(int, int) - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory

Get the gravity field coefficients provider from the first supported file.

getNormalizedProvider(double, double, TideSystem, double[][], double[][]) - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory

Create a time-independent NormalizedSphericalHarmonicsProvider from canonical coefficients.

getNormalizedProvider(UnnormalizedSphericalHarmonicsProvider) - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory

Create a NormalizedSphericalHarmonicsProvider from an UnnormalizedSphericalHarmonicsProvider.

getNormalizedSnm(int, int) - Method in interface org.orekit.forces.gravity.potential.NormalizedSphericalHarmonicsProvider.NormalizedSphericalHarmonics

Get a spherical harmonic sine coefficient.

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.

getNumber() - Method in enum org.orekit.time.Month

Get the month number.

getNumberOfEpochs() - Method in class org.orekit.files.ccsds.ODMFile

Not supported by CCSDS orbit messages.

getNumberOfEpochs() - Method in interface org.orekit.files.general.OrbitFile

Returns the number of epochs contained in this orbit file.

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.

getObjectiveFunctionJacobian() - Method in class org.orekit.propagation.conversion.AbstractPropagatorConverter

Get the Jacobian of the function computing position/velocity at sample points.

getObjectiveFunctionJacobian() - Method in class org.orekit.propagation.conversion.FiniteDifferencePropagatorConverter

Get the Jacobian of the function computing position/velocity at sample points.

getObjectiveFunctionJacobian() - Method in class org.orekit.propagation.conversion.JacobianPropagatorConverter

Get the Jacobian of 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.

getOcculted() - Method in class org.orekit.propagation.events.EclipseDetector

Get the occulted body.

getOccultedRadius() - Method in class org.orekit.propagation.events.EclipseDetector

Get the occulted body radius (m).

getOcculting() - Method in class org.orekit.propagation.events.EclipseDetector

Get the occulting body.

getOccultingRadius() - Method in class org.orekit.propagation.events.EclipseDetector

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(AbsoluteDate) - Method in class org.orekit.forces.gravity.potential.CachedNormalizedSphericalHarmonicsProvider

Get the offset from reference date for the harmonics.

getOffset(AbsoluteDate) - Method in interface org.orekit.forces.gravity.potential.SphericalHarmonicsProvider

Get the offset from reference date for the harmonics.

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.

getOrbit() - Method in class org.orekit.files.ccsds.OEMFile.EphemeridesDataLine

Get the ephemerides data line orbit.

getOrbit() - Method in class org.orekit.propagation.SpacecraftState

Gets the current orbit.

getOrbitType() - Method in class org.orekit.files.sp3.SP3File

Returns the SP3File.SP3OrbitType for this SP3 file.

getOrbitType() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator

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.NumericalPropagator

Get propagation parameter type.

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.

getOriginator() - Method in class org.orekit.files.ccsds.ODMFile

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.

getParameter(String) - Method in class org.orekit.forces.drag.DragForce

getParameter(String) - Method in class org.orekit.forces.gravity.CunninghamAttractionModel

getParameter(String) - Method in class org.orekit.forces.gravity.DrozinerAttractionModel

getParameter(String) - Method in class org.orekit.forces.gravity.HolmesFeatherstoneAttractionModel

getParameter(String) - Method in class org.orekit.forces.gravity.NewtonianAttraction

getParameter(String) - Method in class org.orekit.forces.gravity.OceanTides

getParameter(String) - Method in class org.orekit.forces.gravity.Relativity

getParameter(String) - Method in class org.orekit.forces.gravity.SolidTides

getParameter(String) - Method in class org.orekit.forces.gravity.ThirdBodyAttraction

getParameter(String) - Method in class org.orekit.forces.maneuvers.ConstantThrustManeuver

getParameter(String) - Method in class org.orekit.forces.radiation.SolarRadiationPressure

getParameter(String) - Method in class org.orekit.propagation.conversion.EcksteinHechlerPropagatorBuilder

getParameter(String) - Method in class org.orekit.propagation.conversion.KeplerianPropagatorBuilder

getParameter(String) - Method in class org.orekit.propagation.conversion.NumericalPropagatorBuilder

getParameter(String) - Method in class org.orekit.propagation.conversion.TLEPropagatorBuilder

getParameterName() - Method in class org.orekit.propagation.numerical.ParameterConfiguration

Get parameter name.

getParameters() - Method in class org.orekit.propagation.numerical.JacobiansMapper

Get the number of 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.

getParametersNames() - Method in class org.orekit.propagation.conversion.NumericalPropagatorBuilder

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.

getPartialDensities(int) - Method in class org.orekit.forces.drag.DTM2000

Get the local partial density of the selected element.

getParts() - Method in exception org.orekit.errors.OrekitException

Get the variable parts of the error message.

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.

getPermanentTide() - Method in enum org.orekit.utils.IERSConventions

Get the permanent tide to be removed from ΔC₂₀ when zero-tide potentials are used.

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.

getPole(AbsoluteDate) - 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.

getPolynomial() - Method in class org.orekit.data.PoissonSeries

Get the polynomial part of the series.

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.

getPositionAngleType() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator

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.NumericalPropagator

Get propagation parameter type.

getPrecessionFunction() - Method in enum org.orekit.utils.IERSConventions

Get the function computing the precession angles.

getPressure() - Method in class org.orekit.models.earth.EarthStandardAtmosphereRefraction

Get the local pressure at the evaluation location.

getPreviousDate() - Method in interface org.orekit.propagation.sampling.OrekitStepInterpolator

Get the previous grid date.

getPrimeMeridianAngle(AbsoluteDate) - Method in interface org.orekit.bodies.IAUPole

Get the prime meridian angle.

getPropagator() - Method in class org.orekit.propagation.analytical.AdapterPropagator

Get the reference propagator.

getProvider(boolean, int, int) - Method in class org.orekit.forces.gravity.potential.EGMFormatReader

Get a provider for read spherical harmonics coefficients.

getProvider(boolean, int, int) - Method in class org.orekit.forces.gravity.potential.GRGSFormatReader

Get a provider for read spherical harmonics coefficients.

getProvider(boolean, int, int) - Method in class org.orekit.forces.gravity.potential.ICGEMFormatReader

Get a provider for read spherical harmonics coefficients.

getProvider(boolean, int, int) - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader

Get a provider for read spherical harmonics coefficients.

getProvider(boolean, int, int) - Method in class org.orekit.forces.gravity.potential.SHMFormatReader

Get a provider for read spherical harmonics coefficients.

getProvider() - Method in class org.orekit.propagation.numerical.ParameterConfiguration

Get the povider handling this parameter.

getProvider() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTCentralBody

Get the spherical harmonics provider.

getProviders() - Method in class org.orekit.data.DataProvidersManager

Get an unmodifiable view of the list of supported providers.

getPVCoordinates() - Method in class org.orekit.files.ccsds.OPMFile

Get the position/velocity coordinates contained in the OPM.

getPVCoordinates(AbsoluteDate, Frame) - Method in class org.orekit.frames.TopocentricFrame

Get the PVCoordinates of the topocentric frame origin in the selected frame.

getPVCoordinates(Frame) - Method in class org.orekit.orbits.Orbit

Get the TimeStampedPVCoordinates in a specified frame.

getPVCoordinates(AbsoluteDate, Frame) - Method in class org.orekit.orbits.Orbit

Get the PVCoordinates of the body in the selected frame.

getPVCoordinates() - Method in class org.orekit.orbits.Orbit

Get the TimeStampedPVCoordinates in definition frame.

getPVCoordinates(AbsoluteDate, Frame) - Method in class org.orekit.propagation.AbstractPropagator

Get the PVCoordinates of the body in the selected frame.

getPVCoordinates(AbsoluteDate, Frame) - Method in class org.orekit.propagation.analytical.Ephemeris

Get the PVCoordinates of the body in the selected frame.

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

Get the extrapolated position and velocity from an initial date.

getPVCoordinates(AbsoluteDate, Frame) - Method in class org.orekit.propagation.integration.IntegratedEphemeris

Get the PVCoordinates of the body in the selected frame.

getPVCoordinates(AbsoluteDate, Frame) - Method in class org.orekit.propagation.numerical.NumericalPropagator

Get the PVCoordinates of the body in the selected frame.

getPVCoordinates() - Method in class org.orekit.propagation.SpacecraftState

Get the TimeStampedPVCoordinates in orbit definition frame.

getPVCoordinates(Frame) - Method in class org.orekit.propagation.SpacecraftState

Get the TimeStampedPVCoordinates in given output frame.

getPVCoordinates(AbsoluteDate, Frame) - Method in interface org.orekit.utils.PVCoordinatesProvider

Get the PVCoordinates of the body in the selected frame.

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.

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.DihedralFieldOfViewDetector

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.

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.

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.

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.

getRawCnm(int, int) - Method in interface org.orekit.forces.gravity.potential.RawSphericalHarmonicsProvider.RawSphericalHarmonics

Get a spherical harmonic cosine coefficient.

getRawProvider() - Method in class org.orekit.frames.InterpolatingTransformProvider

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.

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.

getReal(int, int) - Method in class org.orekit.utils.LoveNumbers

Get the real part of a nominal Love numbers.

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.StateMapper

Get 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.

getRefFrame() - Method in class org.orekit.files.ccsds.OPMFile.Maneuver

Get Coordinate system for velocity increment vector, for absolute frames.

getReflectionCoefficient() - Method in class org.orekit.forces.BoxAndSolarArraySpacecraft

Get the specular reflection coefficient.

getReflectionCoefficient() - Method in interface org.orekit.forces.radiation.RadiationSensitive

Get the specular reflection coefficient.

getReflectionCoefficient() - Method in class org.orekit.forces.SphericalSpacecraft

Get the specular reflection coefficient.

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.EarthStandardAtmosphereRefraction

getRefractionModel() - Method in class org.orekit.propagation.events.ElevationDetector

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.

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.KeplerianOrbit

Get the right ascension of the ascending node.

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 R^ε_n,m,l(γ).

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.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 FieldRotation.

getRotationAcceleration() - Method in class org.orekit.attitudes.Attitude

Get the satellite rotation acceleration.

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.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 FieldRotation rate.

getS() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.CoefficientsFactory.NSKey

Get s.

getS10(AbsoluteDate) - Method in interface org.orekit.forces.drag.JB2006InputParameters

Get the EUV index (26-34 nm) scaled to F10.

getS10B(AbsoluteDate) - Method in interface org.orekit.forces.drag.JB2006InputParameters

Get the EUV 81-day averaged centered index.

getSample() - Method in class org.orekit.propagation.conversion.AbstractPropagatorConverter

Get the states sample.

getSatellite(String) - Method in class org.orekit.files.ccsds.OEMFile

Get additional information about a satellite.

getSatellite(String) - Method in class org.orekit.files.ccsds.OGMFile

Get additional information about a satellite.

getSatellite(String) - Method in interface org.orekit.files.general.OrbitFile

Get additional information about a satellite.

getSatellite(String) - Method in class org.orekit.files.sp3.SP3File

Get additional information about a satellite.

getSatellite(int) - Method in class org.orekit.files.sp3.SP3File

Returns the nth satellite as contained in the SP3 file.

getSatelliteCoordinates(String) - Method in class org.orekit.files.ccsds.ODMFile

Get the time coordinates for the given satellite.

getSatelliteCoordinates(String) - Method in class org.orekit.files.ccsds.OEMFile

Get the time coordinates for the given satellite.

getSatelliteCoordinates(String) - Method in class org.orekit.files.ccsds.OPMFile

Get the time coordinates for the given satellite.

getSatelliteCoordinates(String) - Method in interface org.orekit.files.general.OrbitFile

Get the time coordinates for the given satellite.

getSatelliteCoordinates(String) - Method in class org.orekit.files.sp3.SP3File

Get the time coordinates for the given satellite.

getSatelliteCoordinatesOPM() - Method in class org.orekit.files.ccsds.OPMFile

Get the SatelliteTimeCoordinate of the OPM.

getSatelliteCount() - Method in class org.orekit.files.ccsds.OEMFile

Get the number of satellites contained in this orbit file.

getSatelliteCount() - Method in class org.orekit.files.ccsds.OGMFile

Get the number of satellites contained in this orbit file.

getSatelliteCount() - Method in interface org.orekit.files.general.OrbitFile

Get the number of satellites contained in this orbit file.

getSatelliteCount() - Method in class org.orekit.files.sp3.SP3File

Get the number of satellites contained in this orbit file.

getSatelliteId() - Method in class org.orekit.files.general.SatelliteInformation

Returns the id for this satellite object.

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.files.ccsds.OEMFile

Returns a Collection of SatelliteInformation objects for all satellites contained in this orbit file.

getSatellites() - Method in class org.orekit.files.ccsds.OGMFile

Returns a Collection of SatelliteInformation objects for all satellites contained in this orbit file.

getSatellites() - Method in interface org.orekit.files.general.OrbitFile

Returns a Collection of SatelliteInformation objects for all satellites contained in this orbit file.

getSatellites() - Method in class org.orekit.files.sp3.SP3File

Returns a Collection of SatelliteInformation objects for all satellites contained in this orbit file.

getSaturn() - Static method in class org.orekit.bodies.CelestialBodyFactory

Get the Saturn singleton body.

getSecond() - Method in class org.orekit.time.TimeComponents

Get the seconds number.

getSecondsInDay() - Method in class org.orekit.time.TimeComponents

Get the second number within the day.

getSecondsOfWeek() - Method in class org.orekit.files.sp3.SP3File

Returns the seconds of the GPS week as contained in the SP3 file.

getShortPeriodicVariations(AbsoluteDate, double[]) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution

Computes the short periodic variations.

getShortPeriodicVariations(AbsoluteDate, double[]) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTCentralBody

Computes the short periodic variations.

getShortPeriodicVariations(AbsoluteDate, double[]) - Method in interface org.orekit.propagation.semianalytical.dsst.forces.DSSTForceModel

Computes the short periodic variations.

getShortPeriodicVariations(AbsoluteDate, double[]) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBody

Computes the short periodic variations.

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 S_j coefficient.

getSlots() - Method in class org.orekit.utils.GenericTimeStampedCache

Get the number of slots in use.

getSlotsEvictions() - Method in class org.orekit.utils.GenericTimeStampedCache

Get the number of slots evictions.

getSma() - Method in class org.orekit.propagation.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).

getSourceString() - Method in enum org.orekit.errors.OrekitMessages

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.

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.

getSpecifier() - Method in exception org.orekit.errors.OrekitException

Get the localizable specifier of the error message.

getSpin() - Method in class org.orekit.attitudes.Attitude

Get the satellite spin.

getStandardModel() - Static method in class org.orekit.models.earth.SaastamoinenModel

Create a new Saastamoinen model using a standard atmosphere model.

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.

getStartTime() - Method in class org.orekit.files.ccsds.OEMFile.EphemeridesBlock

Get start of total time span covered by ephemerides data and covariance data.

getState() - Method in class org.orekit.propagation.events.EventsLogger.LoggedEvent

Get the triggering state.

getStateDimension() - Method in class org.orekit.propagation.numerical.JacobiansMapper

Get the state vector dimension.

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.

getStep() - Method in class org.orekit.frames.InterpolatingTransformProvider

Get the grid points time step.

getStepHandler() - Method in class org.orekit.propagation.AbstractPropagator

Get the step handler.

getStopTime() - Method in class org.orekit.files.ccsds.OEMFile.EphemeridesBlock

Get end of total time span covered by ephemerides data and covariance data.

getStrengthLevel() - Method in class org.orekit.forces.drag.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.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 interface org.orekit.time.UTCTAILoader

Get the regular expression for supported UTC-TAI offsets files names.

getT() - Method in class org.orekit.forces.drag.DTM2000

Get the local temperature.

getTabDensity() - Method in class org.orekit.forces.drag.HarrisPriester

Get the current density table.

getTAI() - Static method in class org.orekit.time.TimeScalesFactory

Get the International Atomic Time scale.

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.

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.

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.

getThreeHourlyKP(AbsoluteDate) - Method in interface org.orekit.forces.drag.DTM2000InputParameters

Get the value of the 3 hours geomagnetic index.

getThreeHourlyKP(AbsoluteDate) - Method in class org.orekit.forces.drag.MarshallSolarActivityFutureEstimation

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 interface org.orekit.propagation.events.EventDetector

Get the convergence threshold in the event time search.

getThrust() - Method in class org.orekit.forces.maneuvers.ConstantThrustManeuver

Get the thrust.

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.CunninghamAttractionModel

Get the TideSystem used in the gravity field.

getTideSystem() - Method in class org.orekit.forces.gravity.DrozinerAttractionModel

Get the TideSystem used in the gravity field.

getTideSystem() - Method in class org.orekit.forces.gravity.HolmesFeatherstoneAttractionModel

Get the TideSystem used in the gravity field.

getTideSystem() - Method in class org.orekit.forces.gravity.potential.CachedNormalizedSphericalHarmonicsProvider

Get the TideSystem used in the gravity field.

getTideSystem() - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader

Get the TideSystem used in the gravity field.

getTideSystem() - Method in interface org.orekit.forces.gravity.potential.TideSystemProvider

Get the TideSystem used in the gravity field.

getTime() - Method in class org.orekit.time.DateTimeComponents

Get the time component.

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.OEMFile

Returns the OrbitFile.TimeSystem used to time-stamp position entries.

getTimeSystem() - Method in class org.orekit.files.ccsds.OMMFile

Returns the OrbitFile.TimeSystem used to time-stamp position entries.

getTimeSystem() - Method in class org.orekit.files.ccsds.OPMFile

Returns the OrbitFile.TimeSystem used to time-stamp position entries.

getTimeSystem() - Method in interface org.orekit.files.general.OrbitFile

Returns the OrbitFile.TimeSystem used to time-stamp position entries.

getTimeSystem() - Method in class org.orekit.files.sp3.SP3File

Returns the OrbitFile.TimeSystem used to time-stamp position entries.

getTinf() - Method in class org.orekit.forces.drag.DTM2000

Get the current exospheric temperature above input position.

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.

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.

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.

getTotalEclipse() - Method in class org.orekit.propagation.events.EclipseDetector

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.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 from TOD at specified date.

getTransform(AbsoluteDate) - Method in class org.orekit.frames.HelmertTransformation

Compute the transform at some date.

getTransform(AbsoluteDate) - Method in class org.orekit.frames.InterpolatingTransformProvider

Get the Transform corresponding to specified date.

getTransform(AbsoluteDate) - Method in interface org.orekit.frames.TransformProvider

Get the Transform corresponding to specified date.

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.

getTranslation() - Method in class org.orekit.frames.Transform

Get the underlying elementary translation.

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.KeplerianOrbit

Get the true anomaly.

getTT() - Static method in class org.orekit.time.TimeScalesFactory

Get the Terrestrial Time scale.

getType() - Method in class org.orekit.files.sp3.SP3File

Returns the SP3File.SP3FileType associated with this SP3 file.

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.KeplerianOrbit

Get the orbit type.

getType() - Method in class org.orekit.orbits.Orbit

Get the orbit type.

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.

getUnnormalizationFactors(int, int) - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory

Get a un-normalization factors array.

getUnnormalizedCnm(int, int) - Method in interface org.orekit.forces.gravity.potential.UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics

Get a spherical harmonic cosine coefficient.

getUnnormalizedProvider(int, int) - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory

Get the gravity field coefficients provider from the first supported file.

getUnnormalizedProvider(double, double, TideSystem, double[][], double[][]) - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory

Create a time-independent UnnormalizedSphericalHarmonicsProvider from canonical coefficients.

getUnnormalizedProvider(NormalizedSphericalHarmonicsProvider) - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory

Create an UnnormalizedSphericalHarmonicsProvider from a NormalizedSphericalHarmonicsProvider.

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.

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(IERSConventions, boolean) - Static method in class org.orekit.time.TimeScalesFactory

Get the Universal Time 1 scale.

getUT1(EOPHistory) - Static method in class org.orekit.time.TimeScalesFactory

Get the Universal Time 1 scale.

getUT1MinusUTC() - Method in class org.orekit.frames.EOPEntry

Get the UT1-UTC value.

getUT1MinusUTC(AbsoluteDate) - Method in class org.orekit.frames.EOPHistory

Get the UT1-UTC value.

getUTC() - Static method in class org.orekit.time.TimeScalesFactory

Get the Universal Time Coordinate scale.

getV() - Method in class org.orekit.bodies.Ellipse

Get the unit vector along the minor axis.

getValue(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GammaMnsFunction

Get Γ function value.

getValue(int, double) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenTesseralLinear

Compute the value of the Hansen coefficient K_j^{-n-1, s}.

getValue(int, double) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenThirdBodyLinear

Compute the value of the Hansen coefficient K₀^{n, 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, DerivativeStructure) - Static method in class org.orekit.propagation.semianalytical.dsst.utilities.JacobiPolynomials

Returns the value and derivatives of the Jacobi polynomial P_l^v,w evaluated at γ.

getValue(int, int, int, int) - Static method in class org.orekit.propagation.semianalytical.dsst.utilities.NewcombOperators

Get the Newcomb operator evaluated at n, s, ρ, σ.

getValuesSamples() - Method in class org.orekit.utils.InterpolationTableLoader

Returns a copy of the values samples for the interpolation function.

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.files.ccsds.OPMFile

Get velocity vector.

getVelocity(AbsoluteDate, Vector3D, Frame) - Method in interface org.orekit.forces.drag.Atmosphere

Get the inertial velocity of atmosphere molecules.

getVelocity(AbsoluteDate, Vector3D, Frame) - Method in class org.orekit.forces.drag.DTM2000

Get the inertial velocity of atmosphere molecules.

getVelocity(AbsoluteDate, Vector3D, Frame) - Method in class org.orekit.forces.drag.HarrisPriester

Get the inertial velocity of atmosphere molecules.

getVelocity(AbsoluteDate, Vector3D, Frame) - Method in class org.orekit.forces.drag.JB2006

Get the inertial velocity of atmosphere molecules.

getVelocity(AbsoluteDate, Vector3D, Frame) - Method in class org.orekit.forces.drag.SimpleExponentialAtmosphere

Get the inertial velocity of atmosphere molecules.

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.

getVenus() - Static method in class org.orekit.bodies.CelestialBodyFactory

Get the Venus singleton body.

getVmns(int, int, int, double, double) - Static method in class org.orekit.propagation.semianalytical.dsst.utilities.CoefficientsFactory

Get the V_n,s^m coefficient from V_n,s.

getWaves() - Method in class org.orekit.forces.gravity.potential.OceanTidesReader

Get the loaded waves.

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.

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.JB2006InputParameters

Get the MG2 index scaled to F10.

getXM10B(AbsoluteDate) - Method in interface org.orekit.forces.drag.JB2006InputParameters

Get the MG2 81-day average centered index.

getXp() - Method in class org.orekit.frames.PoleCorrection

Get the x_p 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.

getYawAngle(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.YawCompensation

Compute the yaw compensation angle at date.

getYear() - Method in class org.orekit.time.DateComponents

Get the year number.

getYp() - Method in class org.orekit.frames.PoleCorrection

Get the y_p parameter.

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.

getZone() - Method in class org.orekit.propagation.events.GeographicZoneDetector

Get the geographic zone.

GHIJjsPolynomials - Class in org.orekit.propagation.semianalytical.dsst.utilities

Compute the G_js, H_js, I_js and J_js 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 G_js, H_js, I_js and J_js polynomials.

GHmsjPolynomials - Class in org.orekit.propagation.semianalytical.dsst.utilities

Compute the G_ms^j and the H_ms^j 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 G_ms^j and H_ms^j 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.

GMSTScale - Class in org.orekit.time

Greenwich Mean Sidereal Time.

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.

GPSScale - Class in org.orekit.time

GPS time scale.

gradient(AbsoluteDate, Vector3D) - Method in class org.orekit.forces.gravity.HolmesFeatherstoneAttractionModel

Compute the gradient of the non-central part of the gravity field.

gradientHessian(AbsoluteDate, Vector3D) - Method in class org.orekit.forces.gravity.HolmesFeatherstoneAttractionModel

Compute both the gradient and the hessian 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.

GravityFieldFactory - Class in org.orekit.forces.gravity.potential

Factory used to read gravity field files in several supported formats.

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.

GroundPointing - Class in org.orekit.attitudes

Base class for ground pointing attitude providers.

GroundPointing(Frame) - Constructor for class org.orekit.attitudes.GroundPointing

Default constructor.

GRS80_EARTH_ANGULAR_VELOCITY - Static variable in interface org.orekit.utils.Constants

Earth angular velocity from GRS80 model: 7.292115e-5 rad/s.

GRS80_EARTH_C20 - Static variable in interface org.orekit.utils.Constants

Earth un-normalized second zonal coefficient from GRS80 model: -1.08263e-3.

GRS80_EARTH_EQUATORIAL_RADIUS - Static variable in interface org.orekit.utils.Constants

Earth equatorial radius from GRS80 model: 6378137.0 m.

GRS80_EARTH_FLATTENING - Static variable in interface org.orekit.utils.Constants

Earth flattening from GRS80 model: 1.0 / 298.257222101.

GRS80_EARTH_MU - Static variable in interface org.orekit.utils.Constants

Earth gravitational constant from GRS80 model: 3.986005e14 m³/s².

GTODProvider - Class in org.orekit.frames

Greenwich True Of Date Frame, also known as True of Date Rotating frame (TDR) or Greenwich Rotating Coordinate frame (GCR).

GTODProvider(IERSConventions, EOPHistory) - Constructor for class org.orekit.frames.GTODProvider

Simple constructor.

GZIP_FILE_PATTERN - Static variable in interface org.orekit.data.DataProvider

Pattern for name of gzip files.

H

h - Variable in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution

e_y.

H00 - Static variable in class org.orekit.time.TimeComponents

Constant for commonly used hour 00:00:00.

H12 - Static variable in class org.orekit.time.TimeComponents

Constant for commonly used hour 12:00:00.

handleStep(SpacecraftState, boolean) - Method in interface org.orekit.propagation.sampling.OrekitFixedStepHandler

Handle the current step.

handleStep(OrekitStepInterpolator, boolean) - Method in interface org.orekit.propagation.sampling.OrekitStepHandler

Handle the current step.

handleStep(OrekitStepInterpolator, boolean) - Method in class org.orekit.propagation.sampling.OrekitStepHandlerMultiplexer

Handle the current step.

handleStep(OrekitStepInterpolator, boolean) - Method in class org.orekit.propagation.sampling.OrekitStepNormalizer

Handle the last accepted step.

HansenTesseralLinear - Class in org.orekit.propagation.semianalytical.dsst.utilities.hansen

Hansen coefficients K(t,n,s) for t!=0 and n < 0.

HansenTesseralLinear(int, int, int, int, int) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenTesseralLinear

Constructor.

HansenThirdBodyLinear - Class in org.orekit.propagation.semianalytical.dsst.utilities.hansen

Hansen coefficients K(t,n,s) for t=0 and n > 0.

HansenThirdBodyLinear(int, int) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenThirdBodyLinear

Constructor.

HansenUtilities - Class in org.orekit.propagation.semianalytical.dsst.utilities.hansen

Utilities class.

HansenZonalLinear - Class in org.orekit.propagation.semianalytical.dsst.utilities.hansen

Hansen coefficients K(t,n,s) for t=0 and n < 0.

HansenZonalLinear(int, int) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenZonalLinear

Constructor.

HarrisPriester - Class in org.orekit.forces.drag

This atmosphere model is the realization of the Modified Harris-Priester model.

HarrisPriester(PVCoordinatesProvider, OneAxisEllipsoid) - Constructor for class org.orekit.forces.drag.HarrisPriester

Simple constructor for Modified Harris-Priester atmosphere model.

HarrisPriester(PVCoordinatesProvider, OneAxisEllipsoid, double) - Constructor for class org.orekit.forces.drag.HarrisPriester

Constructor for Modified Harris-Priester atmosphere model.

HarrisPriester(PVCoordinatesProvider, OneAxisEllipsoid, double[][]) - Constructor for class org.orekit.forces.drag.HarrisPriester

Constructor for Modified Harris-Priester atmosphere model.

HarrisPriester(PVCoordinatesProvider, OneAxisEllipsoid, double[][], double) - Constructor for class org.orekit.forces.drag.HarrisPriester

Constructor for Modified Harris-Priester atmosphere model.

hasAdditionalState(String) - Method in class org.orekit.propagation.SpacecraftState

Check if an additional state is available.

hasCovarianceMatrix() - Method in class org.orekit.files.ccsds.OGMFile

Check whether the OPM contains covariance matrix data.

hasDataFor(AbsoluteDate) - Method in class org.orekit.frames.EOPHistory

Check if the cache has data for the given date using EOPHistory.getStartDate() and EOPHistory.getEndDate().

hashCode() - Method in class org.orekit.bodies.GeodeticPoint

hashCode() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.CoefficientsFactory.MNSKey

hashCode() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.CoefficientsFactory.NSKey

hashCode() - Method in class org.orekit.time.AbsoluteDate

Get a hashcode for this date.

hashCode() - Method in class org.orekit.time.DateComponents

hashCode() - Method in class org.orekit.time.DateTimeComponents

hashCode() - Method in class org.orekit.time.TimeComponents

hasKeplerianElements() - Method in class org.orekit.files.ccsds.OGMFile

Check whether the OPM contains Keplerian elements data.

HELIUM - Static variable in class org.orekit.forces.drag.DTM2000

Identifier for helium.

HelmertTransformation - Class in org.orekit.frames

Transformation class for geodetic systems.

HelmertTransformation(AbsoluteDate, double, double, double, double, double, double, double, double, double, double, double, double) - Constructor for class org.orekit.frames.HelmertTransformation

Build a transform from its primitive operations.

HelmertTransformation.Predefined - Enum in org.orekit.frames

Enumerate for predefined Helmert transformations.

HighamHall54IntegratorBuilder - Class in org.orekit.propagation.conversion

Builder for HighamHall54Integrator.

HighamHall54IntegratorBuilder(double, double, double) - Constructor for class org.orekit.propagation.conversion.HighamHall54IntegratorBuilder

Build a new instance.

HolmesFeatherstoneAttractionModel - Class in org.orekit.forces.gravity

This class represents the gravitational field of a celestial body.

HolmesFeatherstoneAttractionModel(Frame, NormalizedSphericalHarmonicsProvider) - Constructor for class org.orekit.forces.gravity.HolmesFeatherstoneAttractionModel

Creates a new instance.

HolmesFeatherstoneAttractionModel.GradientHessian - Class in org.orekit.forces.gravity

Container for gradient and Hessian.

HolmesFeatherstoneAttractionModel.GradientHessian(double[], double[][]) - Constructor for class org.orekit.forces.gravity.HolmesFeatherstoneAttractionModel.GradientHessian

Simple constructor.

HYDROGEN - Static variable in class org.orekit.forces.drag.DTM2000

Identifier for hydrogen.

I

i - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator

final inclination.

I - Variable in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution

Retrograde factor.

IAU_2012_ASTRONOMICAL_UNIT - Static variable in interface org.orekit.utils.Constants

Astronomical unit as a conventional unit of length since IAU 2012 resolution B2: 149597870700.0 m.

IAUPole - Interface in org.orekit.bodies

Interface for IAU pole and primer meridian orientations.

ICGEM_FILENAME - Static variable in class org.orekit.forces.gravity.potential.GravityFieldFactory

Default regular expression for ICGEM files.

ICGEMFormatReader - Class in org.orekit.forces.gravity.potential

Reader for the ICGEM gravity field format.

ICGEMFormatReader(String, boolean) - Constructor for class org.orekit.forces.gravity.potential.ICGEMFormatReader

Simple constructor.

IDENTITY - Static variable in class org.orekit.frames.Transform

Identity transform.

IDENTITY - Static variable in class org.orekit.utils.AngularCoordinates

Fixed orientation parallel with reference frame (identity rotation, zero rotation rate and acceleration).

IERSConventions - Enum in org.orekit.utils

Supported IERS conventions.

IERSConventions.NutationCorrectionConverter - Interface in org.orekit.utils

Interface for functions converting nutation corrections between δΔψ/δΔε to δX/δY.

ImmutableTimeStampedCache<T extends TimeStamped> - Class in org.orekit.utils

A cache of TimeStamped data that provides concurrency through immutability.

ImmutableTimeStampedCache(int, Collection<? extends T>) - Constructor for class org.orekit.utils.ImmutableTimeStampedCache

Create a new cache with the given neighbors size and data.

ImpulseManeuver<T extends EventDetector> - Class in org.orekit.forces.maneuvers

Impulse maneuver model.

ImpulseManeuver(T, Vector3D, double) - Constructor for class org.orekit.forces.maneuvers.ImpulseManeuver

Build a new instance.

ImpulseManeuver(T, AttitudeProvider, Vector3D, double) - Constructor for class org.orekit.forces.maneuvers.ImpulseManeuver

Build a new instance.

InertialProvider - Class in org.orekit.attitudes

This class handles an inertial attitude provider.

InertialProvider(Rotation) - Constructor for class org.orekit.attitudes.InertialProvider

Creates new instance.

init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.forces.maneuvers.ImpulseManeuver

Initialize event handler at the start of a propagation.

init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.propagation.events.AbstractDetector

Initialize event handler at the start of a propagation.

init(SpacecraftState, AbsoluteDate) - Method in interface org.orekit.propagation.events.EventDetector

Initialize event handler at the start of a propagation.

init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.propagation.events.EventFilter

Initialize event handler at the start of a propagation.

init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.propagation.events.EventShifter

Initialize event handler at the start of a propagation.

init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.propagation.events.EventState

Initialize event handler at the start of a propagation.

init(SpacecraftState, AbsoluteDate) - Method in interface org.orekit.propagation.sampling.OrekitFixedStepHandler

Initialize step handler at the start of a propagation.

init(SpacecraftState, AbsoluteDate) - Method in interface org.orekit.propagation.sampling.OrekitStepHandler

Initialize step handler at the start of a propagation.

init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.propagation.sampling.OrekitStepHandlerMultiplexer

Initialize step handler at the start of a propagation.

init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.propagation.sampling.OrekitStepNormalizer

Initialize step handler at the start of a propagation.

initialIsOsculating() - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator

Check if the initial state is provided in osculating elements.

initialize(boolean) - Method in interface org.orekit.propagation.integration.ModeHandler

Initialize the mode handler.

initialize(AuxiliaryElements, boolean) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution

Performs initialization prior to propagation for the current force model.

initialize(AuxiliaryElements, boolean) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTCentralBody

Performs initialization prior to propagation for the current force model.

initialize(AuxiliaryElements, boolean) - Method in interface org.orekit.propagation.semianalytical.dsst.forces.DSSTForceModel

Performs initialization prior to propagation for the current force model.

initialize(AuxiliaryElements, boolean) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBody

Computes the highest power of the eccentricity and the highest power of a/R3 to appear in the truncated analytical power series expansion.

initializeStep(AuxiliaryElements) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution

Performs initialization at each integration step for the current force model.

initializeStep(AuxiliaryElements) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTCentralBody

Performs initialization at each integration step for the current force model.

initializeStep(AuxiliaryElements) - Method in interface org.orekit.propagation.semianalytical.dsst.forces.DSSTForceModel

Performs initialization at each integration step for the current force model.

initializeStep(AuxiliaryElements) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBody

Performs initialization at each integration step for the current force model.

initMapper() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator

Initialize the mapper.

initPVCoordinates() - Method in class org.orekit.orbits.CartesianOrbit

Compute the position/velocity coordinates from the canonical parameters.

initPVCoordinates() - Method in class org.orekit.orbits.CircularOrbit

Compute the position/velocity coordinates from the canonical parameters.

initPVCoordinates() - Method in class org.orekit.orbits.EquinoctialOrbit

Compute the position/velocity coordinates from the canonical parameters.

initPVCoordinates() - Method in class org.orekit.orbits.KeplerianOrbit

Compute the position/velocity coordinates from the canonical parameters.

initPVCoordinates() - Method in class org.orekit.orbits.Orbit

Compute the position/velocity coordinates from the canonical parameters.

insideLeap(AbsoluteDate) - Method in class org.orekit.time.UTCScale

Check if date is within a leap second introduction.

IntegratedEphemeris - Class in org.orekit.propagation.integration

This class stores sequentially generated orbital parameters for later retrieval.

IntegratedEphemeris(AbsoluteDate, AbsoluteDate, AbsoluteDate, StateMapper, boolean, ContinuousOutputModel, Map<String, double[]>, List<AdditionalStateProvider>, String[]) - Constructor for class org.orekit.propagation.integration.IntegratedEphemeris

Creates a new instance of IntegratedEphemeris.

interpolate(AbsoluteDate, Collection<Attitude>) - Method in class org.orekit.attitudes.Attitude

Get an interpolated instance.

interpolate(AbsoluteDate, Collection<Transform>) - Method in class org.orekit.frames.Transform

Get an interpolated instance.

interpolate(AbsoluteDate, boolean, boolean, Collection<Transform>) - Static method in class org.orekit.frames.Transform

Deprecated.

as of 7.0, replaced with Transform.interpolate(AbsoluteDate, CartesianDerivativesFilter, AngularDerivativesFilter, Collection)

interpolate(AbsoluteDate, CartesianDerivativesFilter, AngularDerivativesFilter, Collection<Transform>) - Static method in class org.orekit.frames.Transform

Interpolate a transform from a sample set of existing transforms.

interpolate(AbsoluteDate, Collection<Orbit>) - Method in class org.orekit.orbits.CartesianOrbit

Get an interpolated instance.

interpolate(AbsoluteDate, Collection<Orbit>) - Method in class org.orekit.orbits.CircularOrbit

Get an interpolated instance.

interpolate(AbsoluteDate, Collection<Orbit>) - Method in class org.orekit.orbits.EquinoctialOrbit

Get an interpolated instance.

interpolate(AbsoluteDate, Collection<Orbit>) - Method in class org.orekit.orbits.KeplerianOrbit

Get an interpolated instance.

interpolate(AbsoluteDate, Collection<SpacecraftState>) - Method in class org.orekit.propagation.SpacecraftState

Get an interpolated instance.

interpolate(AbsoluteDate, Collection<T>) - Method in interface org.orekit.time.TimeInterpolable

Get an interpolated instance.

interpolate(AbsoluteDate, boolean, Collection<Pair<AbsoluteDate, AngularCoordinates>>) - Static method in class org.orekit.utils.AngularCoordinates

Deprecated.

since 7.0 replaced with TimeStampedAngularCoordinates.interpolate(AbsoluteDate, AngularDerivativesFilter, Collection)

interpolate(AbsoluteDate, boolean, Collection<Pair<AbsoluteDate, FieldAngularCoordinates<T>>>) - Static method in class org.orekit.utils.FieldAngularCoordinates

Deprecated.

since 7.0 replaced with TimeStampedFieldAngularCoordinates.interpolate(AbsoluteDate, AngularDerivativesFilter, Collection)

interpolate(AbsoluteDate, boolean, Collection<Pair<AbsoluteDate, FieldPVCoordinates<T>>>) - Static method in class org.orekit.utils.FieldPVCoordinates

Deprecated.

as of 7.0, replaced with TimeStampedFieldPVCoordinates.interpolate(AbsoluteDate, CartesianDerivativesFilter, Collection)

interpolate(AbsoluteDate, boolean, Collection<Pair<AbsoluteDate, PVCoordinates>>) - Static method in class org.orekit.utils.PVCoordinates

Deprecated.

since 7.0 replaced with interpolate(AbsoluteDate, CartesianDerivativesFilter, Collection)

interpolate(AbsoluteDate, AngularDerivativesFilter, Collection<TimeStampedAngularCoordinates>) - Static method in class org.orekit.utils.TimeStampedAngularCoordinates

Interpolate angular coordinates.

interpolate(AbsoluteDate, AngularDerivativesFilter, Collection<TimeStampedFieldAngularCoordinates<T>>) - Static method in class org.orekit.utils.TimeStampedFieldAngularCoordinates

Interpolate angular coordinates.

interpolate(AbsoluteDate, CartesianDerivativesFilter, Collection<TimeStampedFieldPVCoordinates<T>>) - Static method in class org.orekit.utils.TimeStampedFieldPVCoordinates

Interpolate position-velocity.

interpolate(AbsoluteDate, CartesianDerivativesFilter, Collection<TimeStampedPVCoordinates>) - Static method in class org.orekit.utils.TimeStampedPVCoordinates

Interpolate position-velocity.

InterpolatingTransformProvider - Class in org.orekit.frames

Transform provider using thread-safe interpolation on transforms sample.

InterpolatingTransformProvider(TransformProvider, boolean, boolean, AbsoluteDate, AbsoluteDate, int, double, int, double, double) - Constructor for class org.orekit.frames.InterpolatingTransformProvider

Deprecated.

as of 7.0, replaced with InterpolatingTransformProvider.InterpolatingTransformProvider(TransformProvider, CartesianDerivativesFilter, AngularDerivativesFilter, AbsoluteDate, AbsoluteDate, int, double, int, double, double)

InterpolatingTransformProvider(TransformProvider, CartesianDerivativesFilter, AngularDerivativesFilter, AbsoluteDate, AbsoluteDate, int, double, int, double, double) - Constructor for class org.orekit.frames.InterpolatingTransformProvider

Simple constructor.

InterpolationGrid - Interface in org.orekit.propagation.semianalytical.dsst.utilities

Interface for interpolation grids.

InterpolationTableLoader - Class in org.orekit.utils

Used to read an interpolation table from a data file.

InterpolationTableLoader() - Constructor for class org.orekit.utils.InterpolationTableLoader

isAdditionalStateManaged(String) - Method in class org.orekit.propagation.AbstractPropagator

Check if an additional state is managed.

isAdditionalStateManaged(String) - Method in class org.orekit.propagation.analytical.Ephemeris

Check if an additional state is managed.

isAdditionalStateManaged(String) - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator

Check if an additional state is managed.

isAdditionalStateManaged(String) - Method in interface org.orekit.propagation.Propagator

Check if an additional state is managed.

isAvailable(String) - Method in class org.orekit.propagation.conversion.AbstractPropagatorConverter

Check if a parameter can be free.

isChildOf(Frame) - Method in class org.orekit.frames.Frame

Determine if a Frame is a child of another one.

isFormatOK(String, String) - Static method in class org.orekit.propagation.analytical.tle.TLE

Check the lines format validity.

isForward() - Method in interface org.orekit.propagation.sampling.OrekitStepInterpolator

Check is integration direction is forward in date.

isIncreasing() - Method in class org.orekit.propagation.events.EventsLogger.LoggedEvent

Get the Increasing/decreasing status of the event.

isLof() - Method in enum org.orekit.files.ccsds.CCSDSFrame

Check if the frame is a Local Orbital frame.

isMeanOrbit() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator

Check if only the mean elements should be used in a semianalitical propagation.

isOnlyPosition() - Method in class org.orekit.propagation.conversion.AbstractPropagatorConverter

Check if fitting uses only sample positions.

isPseudoInertial() - Method in class org.orekit.frames.Frame

Check if the frame is pseudo-inertial.

isSimpleEOP() - Method in class org.orekit.files.ccsds.ODMParser

Get EOP interpolation method.

isSupported(DataProvider) - Method in class org.orekit.data.DataProvidersManager

Check if some provider is supported.

isSupported(String) - Method in class org.orekit.propagation.conversion.NumericalPropagatorBuilder

J

J2000_EPOCH - Static variable in class org.orekit.time.AbsoluteDate

J2000.0 Reference epoch: 2000-01-01T12:00:00 Terrestrial Time (not UTC).

J2000_EPOCH - Static variable in class org.orekit.time.DateComponents

J2000.0 Reference epoch: 2000-01-01.

J2DifferentialEffect - Class in org.orekit.propagation.analytical

Analytical model for J2 effect.

J2DifferentialEffect(SpacecraftState, AdapterPropagator.DifferentialEffect, boolean, UnnormalizedSphericalHarmonicsProvider) - Constructor for class org.orekit.propagation.analytical.J2DifferentialEffect

Simple constructor.

J2DifferentialEffect(Orbit, Orbit, boolean, UnnormalizedSphericalHarmonicsProvider) - Constructor for class org.orekit.propagation.analytical.J2DifferentialEffect

Simple constructor.

J2DifferentialEffect(SpacecraftState, AdapterPropagator.DifferentialEffect, boolean, double, double, double) - Constructor for class org.orekit.propagation.analytical.J2DifferentialEffect

Simple constructor.

J2DifferentialEffect(Orbit, Orbit, boolean, double, double, double) - Constructor for class org.orekit.propagation.analytical.J2DifferentialEffect

Simple constructor.

Jacobianizer - Class in org.orekit.propagation.numerical

Class helping implementation of partial derivatives in force models implementations.

Jacobianizer(ForceModel, double, Collection<ParameterConfiguration>, double) - Constructor for class org.orekit.propagation.numerical.Jacobianizer

Simple constructor.

JacobianPropagatorConverter - Class in org.orekit.propagation.conversion

Propagator converter using the real jacobian.

JacobianPropagatorConverter(NumericalPropagatorBuilder, double, int) - Constructor for class org.orekit.propagation.conversion.JacobianPropagatorConverter

Simple constructor.

JacobiansMapper - Class in org.orekit.propagation.numerical

Mapper between two-dimensional Jacobian matrices and one-dimensional additional state arrays.

JacobiPolynomials - Class in org.orekit.propagation.semianalytical.dsst.utilities

Provider of the Jacobi polynomials P_l^v,w.

JAVA_EPOCH - Static variable in class org.orekit.time.AbsoluteDate

Java Reference epoch: 1970-01-01T00:00:00 Universal Time Coordinate.

JAVA_EPOCH - Static variable in class org.orekit.time.DateComponents

Java Reference epoch: 1970-01-01.

JB2006 - Class in org.orekit.forces.drag

This is the realization of the Jacchia-Bowman 2006 atmospheric model.

JB2006(JB2006InputParameters, PVCoordinatesProvider, BodyShape) - Constructor for class org.orekit.forces.drag.JB2006

Constructor with space environment information for internal computation.

JB2006InputParameters - Interface in org.orekit.forces.drag

Interface for solar activity and magnetic activity data.

JPL_SSD_ASTRONOMICAL_UNIT - Static variable in interface org.orekit.utils.Constants

Astronomical Unit: 149597870691 m.

JPL_SSD_EARTH_GM - Static variable in interface org.orekit.utils.Constants

Earth attraction coefficient (m³/s²).

JPL_SSD_EARTH_MOON_MASS_RATIO - Static variable in interface org.orekit.utils.Constants

Earth/Moon mass ratio: 81.30059.

JPL_SSD_EARTH_PLUS_MOON_GM - Static variable in interface org.orekit.utils.Constants

Sun/(Earth + Moon) attraction coefficient (m³/s²).

JPL_SSD_GAUSSIAN_GRAVITATIONAL_CONSTANT - Static variable in interface org.orekit.utils.Constants

Gaussian gravitational constant: 0.01720209895 √(AU³/d²).

JPL_SSD_JUPITER_SYSTEM_GM - Static variable in interface org.orekit.utils.Constants

Sun/(Jupiter system) ttraction coefficient (m³/s²).

JPL_SSD_MARS_SYSTEM_GM - Static variable in interface org.orekit.utils.Constants

Sun/(Mars system) attraction coefficient (m³/s²).

JPL_SSD_MERCURY_GM - Static variable in interface org.orekit.utils.Constants

Sun/Mercury attraction coefficient (m³/s²).

JPL_SSD_MOON_GM - Static variable in interface org.orekit.utils.Constants

Moon attraction coefficient (m³/s²).

JPL_SSD_NEPTUNE_SYSTEM_GM - Static variable in interface org.orekit.utils.Constants

Sun/(Neptune system) attraction coefficient (m³/s²).

JPL_SSD_PLUTO_SYSTEM_GM - Static variable in interface org.orekit.utils.Constants

Sun/(Pluto system) ttraction coefficient (m³/s²).

JPL_SSD_SATURN_SYSTEM_GM - Static variable in interface org.orekit.utils.Constants

Sun/(Saturn system) attraction coefficient (m³/s²).

JPL_SSD_SUN_EARTH_PLUS_MOON_MASS_RATIO - Static variable in interface org.orekit.utils.Constants

Sun/(Earth + Moon) mass ratio: 328900.56.

JPL_SSD_SUN_GM - Static variable in interface org.orekit.utils.Constants

Sun attraction coefficient (m³/s²).

JPL_SSD_SUN_JUPITER_SYSTEM_MASS_RATIO - Static variable in interface org.orekit.utils.Constants

Sun/(Jupiter system) mass ratio: 1047.3486.

JPL_SSD_SUN_MARS_SYSTEM_MASS_RATIO - Static variable in interface org.orekit.utils.Constants

Sun/(Mars system) mass ratio: 3098708.0.

JPL_SSD_SUN_MERCURY_MASS_RATIO - Static variable in interface org.orekit.utils.Constants

Sun/Mercury mass ratio: 6023600.

JPL_SSD_SUN_NEPTUNE_SYSTEM_MASS_RATIO - Static variable in interface org.orekit.utils.Constants

Sun/(Neptune system) mass ratio: 19412.24.

JPL_SSD_SUN_PLUTO_SYSTEM_MASS_RATIO - Static variable in interface org.orekit.utils.Constants

Sun/(Pluto system) mass ratio: 1.35e8.

JPL_SSD_SUN_SATURN_SYSTEM_MASS_RATIO - Static variable in interface org.orekit.utils.Constants

Sun/(Saturn system) mass ratio: 3497.898.

JPL_SSD_SUN_URANUS_SYSTEM_MASS_RATIO - Static variable in interface org.orekit.utils.Constants

Sun/(Uranus system) mass ratio: 22902.98.

JPL_SSD_SUN_VENUS_MASS_RATIO - Static variable in interface org.orekit.utils.Constants

Sun/Venus mass ratio: 408523.71.

JPL_SSD_URANUS_SYSTEM_GM - Static variable in interface org.orekit.utils.Constants

Sun/(Uranus system) attraction coefficient (m³/s²).

JPL_SSD_VENUS_GM - Static variable in interface org.orekit.utils.Constants

Sun/Venus attraction coefficient (m³/s²).

JPLEphemeridesLoader - Class in org.orekit.bodies

Loader for JPL ephemerides binary files (DE 4xx) and similar formats (INPOP 06/08/10).

JPLEphemeridesLoader(String, JPLEphemeridesLoader.EphemerisType) - Constructor for class org.orekit.bodies.JPLEphemeridesLoader

Create a loader for JPL ephemerides binary files.

JPLEphemeridesLoader.EphemerisType - Enum in org.orekit.bodies

List of supported ephemerides types.

JPLEphemeridesLoader.RawPVProvider - Interface in org.orekit.bodies

Interface for raw position-velocity retrieval.

JULIAN_CENTURY - Static variable in interface org.orekit.utils.Constants

Duration of a Julian century: 36525 Constants.JULIAN_DAY.

JULIAN_DAY - Static variable in interface org.orekit.utils.Constants

Duration of a mean solar day: 86400.0 s.

JULIAN_EPOCH - Static variable in class org.orekit.time.AbsoluteDate

Reference epoch for julian dates: -4712-01-01T12:00:00 Terrestrial Time.

JULIAN_EPOCH - Static variable in class org.orekit.time.DateComponents

Reference epoch for julian dates: -4712-01-01.

JULIAN_YEAR - Static variable in interface org.orekit.utils.Constants

Duration of a Julian year: 365.25 Constants.JULIAN_DAY.

JUPITER - Static variable in class org.orekit.bodies.CelestialBodyFactory

Predefined name for Jupiter.

K

k - Variable in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution

e_x.

KeplerianOrbit - Class in org.orekit.orbits

This class handles traditional keplerian orbital parameters.

KeplerianOrbit(double, double, double, double, double, double, PositionAngle, Frame, AbsoluteDate, double) - Constructor for class org.orekit.orbits.KeplerianOrbit

Creates a new instance.

KeplerianOrbit(TimeStampedPVCoordinates, Frame, double) - Constructor for class org.orekit.orbits.KeplerianOrbit

Constructor from cartesian parameters.

KeplerianOrbit(PVCoordinates, Frame, AbsoluteDate, double) - Constructor for class org.orekit.orbits.KeplerianOrbit

Constructor from cartesian parameters.

KeplerianOrbit(Orbit) - Constructor for class org.orekit.orbits.KeplerianOrbit

Constructor from any kind of orbital parameters.

KeplerianPropagator - Class in org.orekit.propagation.analytical

Simple keplerian orbit propagator.

KeplerianPropagator(Orbit) - Constructor for class org.orekit.propagation.analytical.KeplerianPropagator

Build a propagator from orbit only.

KeplerianPropagator(Orbit, double) - Constructor for class org.orekit.propagation.analytical.KeplerianPropagator

Build a propagator from orbit and central attraction coefficient μ.

KeplerianPropagator(Orbit, AttitudeProvider) - Constructor for class org.orekit.propagation.analytical.KeplerianPropagator

Build a propagator from orbit and attitude provider.

KeplerianPropagator(Orbit, AttitudeProvider, double) - Constructor for class org.orekit.propagation.analytical.KeplerianPropagator

Build a propagator from orbit, attitude provider and central attraction coefficient μ.

KeplerianPropagator(Orbit, AttitudeProvider, double, double) - Constructor for class org.orekit.propagation.analytical.KeplerianPropagator

Build propagator from orbit, attitude provider, central attraction coefficient μ and mass.

KeplerianPropagatorBuilder - Class in org.orekit.propagation.conversion

Builder for Keplerian propagator.

KeplerianPropagatorBuilder(double, Frame) - Constructor for class org.orekit.propagation.conversion.KeplerianPropagatorBuilder

Build a new instance.

Keyword - Enum in org.orekit.files.ccsds

Keywords for CCSDS orbit data messages.

L

lm - Variable in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution

Mean longitude.

LnsCoefficients - Class in org.orekit.propagation.semianalytical.dsst.utilities

Compute the L_n^s(γ).

LnsCoefficients(int, int, double[][], TreeMap<CoefficientsFactory.NSKey, Double>, double) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.LnsCoefficients

Create a set of L_n^s(γ) coefficients.

loadCelestialBody(String) - Method in interface org.orekit.bodies.CelestialBodyLoader

Load celestial body.

loadCelestialBody(String) - Method in class org.orekit.bodies.JPLEphemeridesLoader

Load celestial body.

loadData(InputStream, String) - Method in interface org.orekit.data.DataLoader

Load data from a stream.

loadData(InputStream, String) - Method in class org.orekit.forces.drag.MarshallSolarActivityFutureEstimation

Load data from a stream.

loadData(InputStream, String) - Method in class org.orekit.forces.gravity.potential.AstronomicalAmplitudeReader

Load data from a stream.

loadData(InputStream, String) - Method in class org.orekit.forces.gravity.potential.EGMFormatReader

Load data from a stream.

loadData(InputStream, String) - Method in class org.orekit.forces.gravity.potential.FESCHatEpsilonReader

Load data from a stream.

loadData(InputStream, String) - Method in class org.orekit.forces.gravity.potential.FESCnmSnmReader

Load data from a stream.

loadData(InputStream, String) - Method in class org.orekit.forces.gravity.potential.GRGSFormatReader

Load data from a stream.

loadData(InputStream, String) - Method in class org.orekit.forces.gravity.potential.ICGEMFormatReader

Load data from a stream.

loadData(InputStream, String) - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader

Load data from a stream.

loadData(InputStream, String) - Method in class org.orekit.forces.gravity.potential.SHMFormatReader

Load data from a stream.

loadData(InputStream, String) - Method in class org.orekit.models.earth.GeoMagneticModelLoader

Load data from a stream.

loadData(InputStream, String) - Method in class org.orekit.propagation.analytical.tle.TLESeries

Load data from a stream.

loadData(InputStream, String) - Method in class org.orekit.utils.InterpolationTableLoader

Loads an bi-variate interpolation table from the given InputStream.

loadLoveNumbers(String) - Method in enum org.orekit.utils.IERSConventions

Load the Love numbers.

loadTimeSteps() - Method in interface org.orekit.time.UTCTAILoader

Load UTC-TAI offsets entries.

loadTLEData() - Method in class org.orekit.propagation.analytical.tle.TLESeries

Load TLE data for a specified object.

loadTLEData(int) - Method in class org.orekit.propagation.analytical.tle.TLESeries

Load TLE data for a specified object.

loadTLEData(int, int, String) - Method in class org.orekit.propagation.analytical.tle.TLESeries

Load TLE data for a specified object.

LocalOrbitalFrame - Class in org.orekit.frames

Class for frames moving with an orbiting satellite.

LocalOrbitalFrame(Frame, LOFType, PVCoordinatesProvider, String) - Constructor for class org.orekit.frames.LocalOrbitalFrame

Build a new instance.

LofOffset - Class in org.orekit.attitudes

Attitude law defined by fixed Roll, Pitch and Yaw angles (in any order) with respect to a local orbital frame.

LofOffset(Frame, LOFType) - Constructor for class org.orekit.attitudes.LofOffset

Create a LOF-aligned attitude.

LofOffset(Frame, LOFType, RotationOrder, double, double, double) - Constructor for class org.orekit.attitudes.LofOffset

Creates new instance.

LofOffsetPointing - Class in org.orekit.attitudes

This class provides a default attitude provider.

LofOffsetPointing(BodyShape, AttitudeProvider, Vector3D) - Constructor for class org.orekit.attitudes.LofOffsetPointing

Creates new instance.

LOFType - Enum in org.orekit.frames

Enumerate for different types of Local Orbital Frames.

LoveNumbers - Class in org.orekit.utils

Container for Love numbers.

LoveNumbers(double[][], double[][], double[][]) - Constructor for class org.orekit.utils.LoveNumbers

Simple constructor.

M

mapArrayToOrbit(double[], PositionAngle, AbsoluteDate, double, Frame) - Method in enum org.orekit.orbits.OrbitType

Convert state array to orbital parameters.

mapArrayToState(double, double[], boolean) - Method in class org.orekit.propagation.integration.StateMapper

Map the raw double components to a spacecraft state.

mapDateToDouble(AbsoluteDate) - Method in class org.orekit.propagation.integration.StateMapper

Map a date to a raw double time offset.

mapDoubleToDate(double) - Method in class org.orekit.propagation.integration.StateMapper

Map the raw double time offset to a date.

mapOrbitToArray(Orbit, PositionAngle, double[]) - Method in enum org.orekit.orbits.OrbitType

Convert orbit to state array.

mapStateToArray(SpacecraftState, double[]) - Method in class org.orekit.propagation.integration.StateMapper

Map a spacecraft state to raw double components.

MARS - Static variable in class org.orekit.bodies.CelestialBodyFactory

Predefined name for Mars.

MarshallSolarActivityFutureEstimation - Class in org.orekit.forces.drag

This class reads and provides solar activity data needed by atmospheric models: F107 solar flux and Kp indexes.

MarshallSolarActivityFutureEstimation(String, MarshallSolarActivityFutureEstimation.StrengthLevel) - Constructor for class org.orekit.forces.drag.MarshallSolarActivityFutureEstimation

Simple constructor.

MarshallSolarActivityFutureEstimation.StrengthLevel - Enum in org.orekit.forces.drag

Strength level of activity.

MASTER_MODE - Static variable in interface org.orekit.propagation.Propagator

Indicator for master mode.

meanDerivative(AbsoluteDate, int, int) - Method in class org.orekit.utils.SecularAndHarmonic

Get mean derivative, truncated to first components.

meanSecondDerivative(AbsoluteDate, int, int) - Method in class org.orekit.utils.SecularAndHarmonic

Get mean second derivative, truncated to first components.

meanValue(AbsoluteDate, int, int) - Method in class org.orekit.utils.SecularAndHarmonic

Get mean value, truncated to first components.

MERCURY - Static variable in class org.orekit.bodies.CelestialBodyFactory

Predefined name for Mercury.

MidpointIntegratorBuilder - Class in org.orekit.propagation.conversion

Builder for MidpointIntegrator.

MidpointIntegratorBuilder(double) - Constructor for class org.orekit.propagation.conversion.MidpointIntegratorBuilder

Build a new instance.

missingCoefficientsAllowed() - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader

Check if missing coefficients are allowed in the input data.

ModeHandler - Interface in org.orekit.propagation.integration

Common interface for all propagator mode handlers initialization.

MODIFIED_JULIAN_EPOCH - Static variable in class org.orekit.time.AbsoluteDate

Reference epoch for modified julian dates: 1858-11-17T00:00:00 Terrestrial Time.

MODIFIED_JULIAN_EPOCH - Static variable in class org.orekit.time.DateComponents

Reference epoch for modified julian dates: 1858-11-17.

MOLECULAR_NITROGEN - Static variable in class org.orekit.forces.drag.DTM2000

Identifier for molecular nitrogen.

MOLECULAR_OXYGEN - Static variable in class org.orekit.forces.drag.DTM2000

Identifier for molecular oxygen.

monitorDetector(T) - Method in class org.orekit.propagation.events.EventsLogger

Monitor an event detector.

Month - Enum in org.orekit.time

Enumerate representing a calendar month.

MOON - Static variable in class org.orekit.bodies.CelestialBodyFactory

Predefined name for Moon.

MOON_EQUATORIAL_RADIUS - Static variable in interface org.orekit.utils.Constants

Moon equatorial radius: 1737400 m.

mu - Variable in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution

μ .

multiply(PolynomialFunctionMatrix) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.PolynomialFunctionMatrix

Multiply the argument matrix with the current matrix.

N

n - Variable in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution

Kepler mean motion: n = sqrt(μ / a³).

NadirPointing - Class in org.orekit.attitudes

This class handles nadir pointing attitude provider.

NadirPointing(BodyShape) - Constructor for class org.orekit.attitudes.NadirPointing

Creates new instance.

negate() - Method in class org.orekit.utils.FieldPVCoordinates

Get the opposite of the instance.

negate() - Method in class org.orekit.utils.PVCoordinates

Get the opposite of the instance.

NEPTUNE - Static variable in class org.orekit.bodies.CelestialBodyFactory

Predefined name for Neptune.

NetworkCrawler - Class in org.orekit.data

Provider for data files directly fetched from network.

NetworkCrawler(URL...) - Constructor for class org.orekit.data.NetworkCrawler

Build a data classpath crawler.

newBundle(String, Locale, String, ClassLoader, boolean) - Method in class org.orekit.errors.OrekitMessages.UTF8Control

NewcombOperators - Class in org.orekit.propagation.semianalytical.dsst.utilities

Implementation of the Modified Newcomb Operators.

NewtonianAttraction - Class in org.orekit.forces.gravity

Force model for Newtonian central body attraction.

NewtonianAttraction(double) - Constructor for class org.orekit.forces.gravity.NewtonianAttraction

Simple constructor.

NodeDetector - Class in org.orekit.propagation.events

Finder for node crossing events.

NodeDetector(Orbit, Frame) - Constructor for class org.orekit.propagation.events.NodeDetector

Build a new instance.

NodeDetector(double, Orbit, Frame) - Constructor for class org.orekit.propagation.events.NodeDetector

Build a new instance.

nonCentralPart(AbsoluteDate, Vector3D) - Method in class org.orekit.forces.gravity.HolmesFeatherstoneAttractionModel

Compute the non-central part of the gravity field.

normalize() - Method in class org.orekit.utils.FieldPVCoordinates

Normalize the position part of the instance.

normalize() - Method in class org.orekit.utils.PVCoordinates

Normalize the position part of the instance.

NormalizedSphericalHarmonicsProvider - Interface in org.orekit.forces.gravity.potential

Interface used to provide normalized spherical harmonics coefficients.

NormalizedSphericalHarmonicsProvider.NormalizedSphericalHarmonics - Interface in org.orekit.forces.gravity.potential

The normalized geopotential coefficients at a specific instance in time.

NULL_CORRECTION - Static variable in class org.orekit.frames.PoleCorrection

Null correction (xp = 0, yp = 0).

NumericalPropagator - Class in org.orekit.propagation.numerical

This class propagates orbits using numerical integration.

NumericalPropagator(AbstractIntegrator) - Constructor for class org.orekit.propagation.numerical.NumericalPropagator

Create a new instance of NumericalPropagator, based on orbit definition mu.

NumericalPropagatorBuilder - Class in org.orekit.propagation.conversion

Builder for numerical propagator.

NumericalPropagatorBuilder(double, Frame, FirstOrderIntegratorBuilder) - Constructor for class org.orekit.propagation.conversion.NumericalPropagatorBuilder

Build a new instance.

O

OceanLoadDeformationCoefficients - Enum in org.orekit.forces.gravity.potential

Supported Ocean load Deformation coefficients (Love numbers k'_i).

OceanTides - Class in org.orekit.forces.gravity

Ocean tides force model.

OceanTides(Frame, double, double, int, int, IERSConventions, UT1Scale) - Constructor for class org.orekit.forces.gravity.OceanTides

Simple constructor.

OceanTides(Frame, double, double, boolean, double, int, int, int, IERSConventions, UT1Scale) - Constructor for class org.orekit.forces.gravity.OceanTides

Simple constructor.

OceanTidesReader - Class in org.orekit.forces.gravity.potential

Reader for ocean tides coefficients.

OceanTidesReader(String) - Constructor for class org.orekit.forces.gravity.potential.OceanTidesReader

Simple constructor.

OceanTidesWave - Class in org.orekit.forces.gravity.potential

Container for ocen tides coefficients for one tide wave.

OceanTidesWave(int, int, int, double[][][]) - Constructor for class org.orekit.forces.gravity.potential.OceanTidesWave

Simple constructor.

ODMFile - Class in org.orekit.files.ccsds

The ODMFile (Orbit Data Message) class represents any of the three orbit messages used by the CCSDS, i.e.

ODMFile() - Constructor for class org.orekit.files.ccsds.ODMFile

ODMFile constructor.

ODMMetaData - Class in org.orekit.files.ccsds

This class gathers the meta-data present in the Orbital Data Message (ODM).

ODMParser - Class in org.orekit.files.ccsds

Base class for all CCSDS Orbit Data Message parsers.

ODMParser(AbsoluteDate, double, IERSConventions, boolean, int, int, String) - Constructor for class org.orekit.files.ccsds.ODMParser

Complete constructor.

OEMFile - Class in org.orekit.files.ccsds

This class stocks all the information of the OEM File parsed by OEMParser.

OEMFile() - Constructor for class org.orekit.files.ccsds.OEMFile

OEMFile constructor.

OEMFile.CovarianceMatrix - Class in org.orekit.files.ccsds

The CovarianceMatrix class represents a covariance matrix and its metadata: epoch and frame.

OEMFile.EphemeridesBlock - Class in org.orekit.files.ccsds

The Ephemerides Blocks class contain metadata, the list of ephemerides data lines and optional covariance matrices (and their metadata).

OEMFile.EphemeridesBlock() - Constructor for class org.orekit.files.ccsds.OEMFile.EphemeridesBlock

EphemeridesBlock constructor.

OEMFile.EphemeridesDataLine - Class in org.orekit.files.ccsds

The EphemeridesDataLine class represents the content of an OEM ephemerides data line and consists of a cartesian orbit and an optional acceleration vector.

OEMParser - Class in org.orekit.files.ccsds

A parser for the CCSDS OEM (Orbit Ephemeris Message).

OEMParser() - Constructor for class org.orekit.files.ccsds.OEMParser

Simple constructor.

offsetFrom(AbsoluteDate, TimeScale) - Method in class org.orekit.time.AbsoluteDate

Compute the apparent clock offset between two instant in the perspective of a specific time scale.

offsetFrom(DateTimeComponents) - Method in class org.orekit.time.DateTimeComponents

Compute the seconds offset between two instances.

offsetFromTAI(AbsoluteDate) - Method in class org.orekit.time.GalileoScale

Get the offset to convert locations from TAIScale to instance.

offsetFromTAI(AbsoluteDate) - Method in class org.orekit.time.GMSTScale

Get the offset to convert locations from TAIScale to instance.

offsetFromTAI(AbsoluteDate) - Method in class org.orekit.time.GPSScale

Get the offset to convert locations from TAIScale to instance.

offsetFromTAI(AbsoluteDate) - Method in class org.orekit.time.TAIScale

Get the offset to convert locations from TAIScale to instance.

offsetFromTAI(AbsoluteDate) - Method in class org.orekit.time.TCBScale

Get the offset to convert locations from TAIScale to instance.

offsetFromTAI(AbsoluteDate) - Method in class org.orekit.time.TCGScale

Get the offset to convert locations from TAIScale to instance.

offsetFromTAI(AbsoluteDate) - Method in class org.orekit.time.TDBScale

Get the offset to convert locations from TAIScale to instance.

offsetFromTAI(AbsoluteDate) - Method in interface org.orekit.time.TimeScale

Get the offset to convert locations from TAIScale to instance.

offsetFromTAI(AbsoluteDate) - Method in class org.orekit.time.TTScale

Get the offset to convert locations from TAIScale to instance.

offsetFromTAI(AbsoluteDate) - Method in class org.orekit.time.UT1Scale

Get the offset to convert locations from TAIScale to instance.

offsetFromTAI(AbsoluteDate) - Method in class org.orekit.time.UTCScale

Get the offset to convert locations from TAIScale to instance.

offsetToTAI(DateComponents, TimeComponents) - Method in class org.orekit.time.GalileoScale

Get the offset to convert locations from instance to TAIScale.

offsetToTAI(DateComponents, TimeComponents) - Method in class org.orekit.time.GMSTScale

Get the offset to convert locations from instance to TAIScale.

offsetToTAI(DateComponents, TimeComponents) - Method in class org.orekit.time.GPSScale

Get the offset to convert locations from instance to TAIScale.

offsetToTAI(DateComponents, TimeComponents) - Method in class org.orekit.time.TAIScale

Get the offset to convert locations from instance to TAIScale.

offsetToTAI(DateComponents, TimeComponents) - Method in class org.orekit.time.TCBScale

Get the offset to convert locations from instance to TAIScale.

offsetToTAI(DateComponents, TimeComponents) - Method in class org.orekit.time.TCGScale

Get the offset to convert locations from instance to TAIScale.

offsetToTAI(DateComponents, TimeComponents) - Method in class org.orekit.time.TDBScale

Get the offset to convert locations from instance to TAIScale.

offsetToTAI(DateComponents, TimeComponents) - Method in interface org.orekit.time.TimeScale

Get the offset to convert locations from instance to TAIScale.

offsetToTAI(DateComponents, TimeComponents) - Method in class org.orekit.time.TTScale

Get the offset to convert locations from instance to TAIScale.

offsetToTAI(DateComponents, TimeComponents) - Method in class org.orekit.time.UT1Scale

Get the offset to convert locations from instance to TAIScale.

offsetToTAI(DateComponents, TimeComponents) - Method in class org.orekit.time.UTCScale

Get the offset to convert locations from instance to TAIScale.

OGMFile - Class in org.orekit.files.ccsds

This class gathers the general state data present in both OPM and OMM files.

omega - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator

final perigee argument.

omgdot - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator

common parameter for perigee argument (omega) computation.

OMMFile - Class in org.orekit.files.ccsds

This class gathers the informations present in the Orbital Mean-Elements Message (OMM), and contains methods to generate a CartesianOrbit, a KeplerianOrbit, a SpacecraftState and, eventually, a TLE.

OMMFile.OMMMetaData - Class in org.orekit.files.ccsds

OMMParser - Class in org.orekit.files.ccsds

A parser for the CCSDS OMM (Orbiter Mean-Elements Message).

OMMParser() - Constructor for class org.orekit.files.ccsds.OMMParser

Simple constructor.

onDate(AbsoluteDate) - Method in class org.orekit.forces.gravity.potential.CachedNormalizedSphericalHarmonicsProvider

Get the normalized spherical harmonic coefficients at a specific instance in time.

onDate(AbsoluteDate) - Method in interface org.orekit.forces.gravity.potential.NormalizedSphericalHarmonicsProvider

Get the normalized spherical harmonic coefficients at a specific instance in time.

onDate(AbsoluteDate) - Method in interface org.orekit.forces.gravity.potential.RawSphericalHarmonicsProvider

Get the raw spherical harmonic coefficients on a specific date.

onDate(AbsoluteDate) - Method in interface org.orekit.forces.gravity.potential.UnnormalizedSphericalHarmonicsProvider

Get the un-normalized spherical harmonic coefficients at a specific instance in time.

ONE - Static variable in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenUtilities

1 represented as a polynomial.

OneAxisEllipsoid - Class in org.orekit.bodies

Modeling of a one-axis ellipsoid.

OneAxisEllipsoid(double, double, Frame) - Constructor for class org.orekit.bodies.OneAxisEllipsoid

Simple constructor.

ooA - Variable in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution

1 / A .

ooAB - Variable in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution

1 / (A * B) .

ooBpo - Variable in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution

1 / (1 + B) .

ooMu - Variable in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution

1 / μ .

OPMFile - Class in org.orekit.files.ccsds

This class gathers the informations present in the Orbital Parameter Message (OPM), and contains methods to generate CartesianOrbit, KeplerianOrbit or SpacecraftState.

OPMFile.Maneuver - Class in org.orekit.files.ccsds

Maneuver in an OPM file.

OPMFile.Maneuver() - Constructor for class org.orekit.files.ccsds.OPMFile.Maneuver

Simple constructor.

OPMParser - Class in org.orekit.files.ccsds

A parser for the CCSDS OPM (Orbit Parameter Message).

OPMParser() - Constructor for class org.orekit.files.ccsds.OPMParser

Simple constructor.

Orbit - Class in org.orekit.orbits

This class handles orbital parameters.

Orbit(Frame, AbsoluteDate, double) - Constructor for class org.orekit.orbits.Orbit

Default constructor.

Orbit(TimeStampedPVCoordinates, Frame, double) - Constructor for class org.orekit.orbits.Orbit

Set the orbit from Cartesian parameters.

OrbitFile - Interface in org.orekit.files.general

Interface for orbit file representations.

OrbitFile.TimeSystem - Enum in org.orekit.files.general

Time system used throughout this orbit file.

OrbitFileParser - Interface in org.orekit.files.general

Interface for orbit file parsers.

OrbitType - Enum in org.orekit.orbits

Enumerate for orbital parameters types.

OREKIT_DATA_PATH - Static variable in class org.orekit.data.DataProvidersManager

Name of the property defining the root directories or zip/jar files path for default configuration.

OrekitConfiguration - Class in org.orekit.utils

Utility class for setting global configuration parameters.

OrekitException - Exception in org.orekit.errors

This class is the base class for all specific exceptions thrown by the orekit classes.

OrekitException(Localizable, Object...) - Constructor for exception org.orekit.errors.OrekitException

Simple constructor.

OrekitException(OrekitException) - Constructor for exception org.orekit.errors.OrekitException

Copy constructor.

OrekitException(Localizable, Throwable) - Constructor for exception org.orekit.errors.OrekitException

Simple constructor.

OrekitException(Throwable, Localizable, Object...) - Constructor for exception org.orekit.errors.OrekitException

Simple constructor.

OrekitException(ExceptionContextProvider) - Constructor for exception org.orekit.errors.OrekitException

Simple constructor.

OrekitExceptionWrapper - Exception in org.orekit.errors

This class allows to wrap OrekitException instances in RuntimeException.

OrekitExceptionWrapper(OrekitException) - Constructor for exception org.orekit.errors.OrekitExceptionWrapper

Simple constructor.

OrekitFixedStepHandler - Interface in org.orekit.propagation.sampling

This interface is a space-dynamics aware fixed size step handler.

OrekitMessages - Enum in org.orekit.errors

Enumeration for localized messages formats.

OrekitMessages.UTF8Control - Class in org.orekit.errors

Control class loading properties in UTF-8 encoding.

OrekitMessages.UTF8Control() - Constructor for class org.orekit.errors.OrekitMessages.UTF8Control

OrekitStepHandler - Interface in org.orekit.propagation.sampling

This interface is a space-dynamics aware step handler.

OrekitStepHandlerMultiplexer - Class in org.orekit.propagation.sampling

This class gathers several OrekitStepHandler instances into one.

OrekitStepHandlerMultiplexer() - Constructor for class org.orekit.propagation.sampling.OrekitStepHandlerMultiplexer

Simple constructor.

OrekitStepInterpolator - Interface in org.orekit.propagation.sampling

This interface is a space-dynamics aware step interpolator.

OrekitStepNormalizer - Class in org.orekit.propagation.sampling

This class wraps an object implementing OrekitFixedStepHandler into a OrekitStepHandler.

OrekitStepNormalizer(double, OrekitFixedStepHandler) - Constructor for class org.orekit.propagation.sampling.OrekitStepNormalizer

Simple constructor.

org.orekit.attitudes - package org.orekit.attitudes

This package provides classes to represent simple attitudes.

org.orekit.bodies - package org.orekit.bodies

This package provides interface to represent the position and geometry of space objects such as stars, planets or asteroids.

org.orekit.data - package org.orekit.data

This package provide base classes for exploring the configured data directory tree and read external data that can be used by the library.

org.orekit.errors - package org.orekit.errors

This package provides classes to generate and handle exceptions.

org.orekit.files.ccsds - package org.orekit.files.ccsds

This package provides a parser for orbit data stored in CCSDS Orbit Data Message format.

org.orekit.files.general - package org.orekit.files.general

This package provides interfaces for orbit file representations and corresponding parsers.

org.orekit.files.sp3 - package org.orekit.files.sp3

This package provides a parser for orbit data stored in SP3 format.

org.orekit.forces - package org.orekit.forces

This package provides the interface for force models that will be used by the NumericalPropagator, as well as some classical spacecraft models for surface forces (spherical, box and solar array ...).

org.orekit.forces.drag - package org.orekit.forces.drag

org.orekit.forces.gravity - package org.orekit.forces.gravity

This package provides all gravity-related forces.

org.orekit.forces.gravity.potential - package org.orekit.forces.gravity.potential

This package provides classes to read gravity field files and supports several different formats.

org.orekit.forces.maneuvers - package org.orekit.forces.maneuvers

This package provides models of simple maneuvers.

org.orekit.forces.radiation - package org.orekit.forces.radiation

org.orekit.frames - package org.orekit.frames

This package provides classes to handle frames and transforms between them.

org.orekit.models - package org.orekit.models

org.orekit.models.earth - package org.orekit.models.earth

This package provides models that simulate certain physical phenomena experienced in the atmosphere of the earth.

org.orekit.orbits - package org.orekit.orbits

This package provides classes to represent orbits.

org.orekit.propagation - package org.orekit.propagation

This package provides tools to propagate orbital states with different methods.

org.orekit.propagation.analytical - package org.orekit.propagation.analytical

org.orekit.propagation.analytical.tle - package org.orekit.propagation.analytical.tle

This package provides classes to read and extrapolate tle's.

org.orekit.propagation.conversion - package org.orekit.propagation.conversion

This package provides tools to convert a given propagator or a set of SpacecraftState into another propagator.

org.orekit.propagation.events - package org.orekit.propagation.events

This package provides interfaces and classes dealing with events occurring during propagation.

org.orekit.propagation.events.handlers - package org.orekit.propagation.events.handlers

This package provides an interface and classes dealing with events occurrence only.

org.orekit.propagation.integration - package org.orekit.propagation.integration

org.orekit.propagation.numerical - package org.orekit.propagation.numerical

org.orekit.propagation.sampling - package org.orekit.propagation.sampling

This package provides interfaces and classes dealing with step handling during propagation.

org.orekit.propagation.semianalytical.dsst - package org.orekit.propagation.semianalytical.dsst

This package provides an implementation of the Draper Semi-analytical Satellite Theory (DSST).

org.orekit.propagation.semianalytical.dsst.forces - package org.orekit.propagation.semianalytical.dsst.forces

org.orekit.propagation.semianalytical.dsst.utilities - package org.orekit.propagation.semianalytical.dsst.utilities

org.orekit.propagation.semianalytical.dsst.utilities.hansen - package org.orekit.propagation.semianalytical.dsst.utilities.hansen

org.orekit.time - package org.orekit.time

This independent package provides classes to handle epochs, time scales, and to compare instants together.

org.orekit.utils - package org.orekit.utils

This package provides useful objects.

OrphanFrame - Class in org.orekit.frames

Prototype frame that can be built from leaf to roots and later attached to a tree.

OrphanFrame(String) - Constructor for class org.orekit.frames.OrphanFrame

Simple constructor.

osculatingDerivative(AbsoluteDate) - Method in class org.orekit.utils.SecularAndHarmonic

Get fitted osculating derivative.

osculatingSecondDerivative(AbsoluteDate) - Method in class org.orekit.utils.SecularAndHarmonic

Get fitted osculating second derivative.

OsculatingToMeanElementsConverter - Class in org.orekit.propagation.conversion

This class converts osculating orbital elements into mean elements.

OsculatingToMeanElementsConverter(SpacecraftState, int, Propagator) - Constructor for class org.orekit.propagation.conversion.OsculatingToMeanElementsConverter

Constructor.

osculatingValue(AbsoluteDate) - Method in class org.orekit.utils.SecularAndHarmonic

Get fitted osculating value.

P

p - Variable in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution

h_y.

ParameterConfiguration - Class in org.orekit.propagation.numerical

Simple container associating a parameter name with a step to compute its jacobian and the provider that manages it.

ParameterConfiguration(String, double) - Constructor for class org.orekit.propagation.numerical.ParameterConfiguration

Parameter name and step pair constructor.

parse(InputStream, String) - Method in class org.orekit.data.PoissonSeriesParser

Parse a stream.

parse(String) - Method in class org.orekit.data.PolynomialParser

Parse a polynomial expression.

parse(InputStream, String) - Method in class org.orekit.data.SimpleTimeStampedTableParser

Parse a stream.

parse(String) - Method in class org.orekit.files.ccsds.ODMParser

Parse a CCSDS Orbit Data Message.

parse(InputStream) - Method in class org.orekit.files.ccsds.ODMParser

Parse a CCSDS Orbit Data Message.

parse(InputStream, String) - Method in class org.orekit.files.ccsds.ODMParser

Parse a CCSDS Orbit Data Message.

parse(String) - Method in class org.orekit.files.ccsds.OEMParser

Parse a CCSDS Orbit Data Message.

parse(InputStream, String) - Method in class org.orekit.files.ccsds.OEMParser

Parse a CCSDS Orbit Data Message.

parse(String) - Method in class org.orekit.files.ccsds.OMMParser

Parse a CCSDS Orbit Data Message.

parse(InputStream, String) - Method in class org.orekit.files.ccsds.OMMParser

Parse a CCSDS Orbit Data Message.

parse(String) - Method in class org.orekit.files.ccsds.OPMParser

Parse a CCSDS Orbit Data Message.

parse(InputStream, String) - Method in class org.orekit.files.ccsds.OPMParser

Parse a CCSDS Orbit Data Message.

parse(InputStream) - Method in interface org.orekit.files.general.OrbitFileParser

Reads an orbit file from the given stream and returns a parsed OrbitFile.

parse(String) - Method in interface org.orekit.files.general.OrbitFileParser

Reads the orbit file and returns a parsed OrbitFile.

parse(String) - Method in class org.orekit.files.sp3.SP3Parser

Reads the orbit file and returns a parsed OrbitFile.

parse(InputStream) - Method in class org.orekit.files.sp3.SP3Parser

Reads an orbit file from the given stream and returns a parsed OrbitFile.

parseCCSDSCalendarSegmentedTimeCode(byte, byte[]) - Static method in class org.orekit.time.AbsoluteDate

Build an instance from a CCSDS Calendar Segmented Time Code (CCS).

parseCCSDSDaySegmentedTimeCode(byte, byte[], DateComponents) - Static method in class org.orekit.time.AbsoluteDate

Build an instance from a CCSDS Day Segmented Time Code (CDS).

parseCCSDSFrame(String) - Method in class org.orekit.files.ccsds.ODMParser

Parse a CCSDS frame.

parseCCSDSUnsegmentedTimeCode(byte, byte, byte[], AbsoluteDate) - Static method in class org.orekit.time.AbsoluteDate

Build an instance from a CCSDS Unsegmented Time Code (CUC).

parseCoefficient(String, List<List<Double>>, int, int, String, String) - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader

Parse a coefficient.

parseCoefficient(String, double[][], int, int, String, String) - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader

Parse a coefficient.

parseComment(KeyValue, List<String>) - Method in class org.orekit.files.ccsds.ODMParser

Parse a comment line.

parseDate(String, OrbitFile.TimeSystem) - Method in class org.orekit.files.ccsds.ODMParser

Parse a date.

parseDate(String) - Static method in class org.orekit.time.DateComponents

Parse a string in ISO-8601 format to build a date.

parseDateTime(String) - Static method in class org.orekit.time.DateTimeComponents

Parse a string in ISO-8601 format to build a date/time.

parseDouble(String) - Static method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader

Parse a double from a string.

parseGeneralStateDataEntry(KeyValue, OGMFile, List<String>) - Method in class org.orekit.files.ccsds.ODMParser

Parse a general state data key = value entry.

parseHeaderEntry(KeyValue, ODMFile, List<String>) - Method in class org.orekit.files.ccsds.ODMParser

Parse an entry from the header.

parseMetaDataEntry(KeyValue, ODMMetaData, List<String>) - Method in class org.orekit.files.ccsds.ODMParser

Parse a meta-data key = value entry.

parseMonth(String) - Static method in enum org.orekit.time.Month

Parse the string to get the month.

parseTime(String) - Static method in class org.orekit.time.TimeComponents

Parse a string in ISO-8601 format to build a time.

PartialDerivativesEquations - Class in org.orekit.propagation.numerical

Set of additional equations computing the partial derivatives of the state (orbit) with respect to initial state and force models parameters.

PartialDerivativesEquations(String, NumericalPropagator) - Constructor for class org.orekit.propagation.numerical.PartialDerivativesEquations

Simple constructor.

PAST_INFINITY - Static variable in class org.orekit.time.AbsoluteDate

Dummy date at infinity in the past direction.

perige - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator

perigee, expressed in KM and ALTITUDE.

PLUTO - Static variable in class org.orekit.bodies.CelestialBodyFactory

Predefined name for Pluto.

pointAt(double) - Method in class org.orekit.bodies.Ellipse

Get a point of the 2D ellipse.

pointAtDistance(double, double, double) - Method in class org.orekit.frames.TopocentricFrame

Compute the point observed from the station at some specified distance.

PoissonSeries<T extends RealFieldElement<T>> - Class in org.orekit.data

Class representing a Poisson series for nutation or ephemeris computations.

PoissonSeries(PolynomialNutation<T>, Map<Long, SeriesTerm<T>>) - Constructor for class org.orekit.data.PoissonSeries

Build a Poisson series from an IERS table file.

PoissonSeries.CompiledSeries<S extends RealFieldElement<S>> - Interface in org.orekit.data

This interface represents a fast evaluator for Poisson series.

PoissonSeriesParser<T extends RealFieldElement<T>> - Class in org.orekit.data

Parser for Poisson series files.

PoissonSeriesParser(int) - Constructor for class org.orekit.data.PoissonSeriesParser

Build a parser for a Poisson series from an IERS table file.

PoleCorrection - Class in org.orekit.frames

Simple container class for pole correction parameters.

PoleCorrection(double, double) - Constructor for class org.orekit.frames.PoleCorrection

Simple constructor.

PolynomialFunctionMatrix - Class in org.orekit.propagation.semianalytical.dsst.utilities.hansen

A quadratic matrix of PolynomialFunction.

PolynomialNutation<T extends RealFieldElement<T>> - Class in org.orekit.data

Polynomial nutation function.

PolynomialNutation(double...) - Constructor for class org.orekit.data.PolynomialNutation

Build a polynomial from its coefficients.

PolynomialParser - Class in org.orekit.data

Parser for polynomials in IERS tables.

PolynomialParser(char, PolynomialParser.Unit) - Constructor for class org.orekit.data.PolynomialParser

Simple constructor.

PolynomialParser.Unit - Enum in org.orekit.data

Unit for the coefficients.

PositionAngle - Enum in org.orekit.orbits

Enumerate for true, eccentric and mean position angles.

PotentialCoefficientsReader - Class in org.orekit.forces.gravity.potential

This abstract class represents a Gravitational Potential Coefficients file reader.

PotentialCoefficientsReader(String, boolean) - Constructor for class org.orekit.forces.gravity.potential.PotentialCoefficientsReader

Simple constructor.

Predefined - Enum in org.orekit.frames

Predefined frames provided by FramesFactory.

projectToEllipse(Vector2D) - Method in class org.orekit.bodies.Ellipse

Find the closest ellipse point.

projectToEllipse(TimeStampedPVCoordinates) - Method in class org.orekit.bodies.Ellipse

Project position-velocity-acceleration on an ellipse.

projectToGround(Vector3D, AbsoluteDate, Frame) - Method in interface org.orekit.bodies.BodyShape

Project a point to the ground.

projectToGround(TimeStampedPVCoordinates, Frame) - Method in interface org.orekit.bodies.BodyShape

Project a moving point to the ground.

projectToGround(Vector3D, AbsoluteDate, Frame) - Method in class org.orekit.bodies.OneAxisEllipsoid

Project a point to the ground.

projectToGround(TimeStampedPVCoordinates, Frame) - Method in class org.orekit.bodies.OneAxisEllipsoid

Project a moving point to the ground.

propagate(AbsoluteDate) - Method in class org.orekit.propagation.AbstractPropagator

Propagate towards a target date.

propagate(AbsoluteDate, AbsoluteDate) - Method in class org.orekit.propagation.analytical.AbstractAnalyticalPropagator

Propagate from a start date towards a target date.

propagate(AbsoluteDate) - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator

Propagate towards a target date.

propagate(AbsoluteDate, AbsoluteDate) - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator

Propagate from a start date towards a target date.

propagate(AbsoluteDate, boolean) - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator

Propagation with or without event detection.

propagate(AbsoluteDate) - Method in interface org.orekit.propagation.Propagator

Propagate towards a target date.

propagate(AbsoluteDate, AbsoluteDate) - Method in interface org.orekit.propagation.Propagator

Propagate from a start date towards a target date.

propagateOrbit(AbsoluteDate) - Method in class org.orekit.propagation.analytical.AbstractAnalyticalPropagator

Extrapolate an orbit up to a specific target date.

propagateOrbit(AbsoluteDate) - Method in class org.orekit.propagation.analytical.AdapterPropagator

Extrapolate an orbit up to a specific target date.

propagateOrbit(AbsoluteDate) - Method in class org.orekit.propagation.analytical.EcksteinHechlerPropagator

Extrapolate an orbit up to a specific target date.

propagateOrbit(AbsoluteDate) - Method in class org.orekit.propagation.analytical.Ephemeris

Extrapolate an orbit up to a specific target date.

propagateOrbit(AbsoluteDate) - Method in class org.orekit.propagation.analytical.KeplerianPropagator

Extrapolate an orbit up to a specific target date.

propagateOrbit(AbsoluteDate) - Method in class org.orekit.propagation.analytical.tle.TLEPropagator

Extrapolate an orbit up to a specific target date.

propagateOrbit(AbsoluteDate) - Method in class org.orekit.propagation.integration.IntegratedEphemeris

Extrapolate an orbit up to a specific target date.

PropagationException - Exception in org.orekit.errors

This class is the base class for all specific exceptions thrown by during the propagation computation.

PropagationException(Localizable, Object...) - Constructor for exception org.orekit.errors.PropagationException

Simple constructor.

PropagationException(Throwable, Localizable, Object...) - Constructor for exception org.orekit.errors.PropagationException

Simple constructor.

PropagationException(OrekitException) - Constructor for exception org.orekit.errors.PropagationException

Simple constructor.

PropagationException(ExceptionContextProvider) - Constructor for exception org.orekit.errors.PropagationException

Simple constructor.

Propagator - Interface in org.orekit.propagation

This interface provides a way to propagate an orbit at any time.

PropagatorBuilder - Interface in org.orekit.propagation.conversion

This interface is the top-level abstraction to build propagators for conversion.

PropagatorConverter - Interface in org.orekit.propagation.conversion

This interface is the top-level abstraction for propagators conversions.

PVCoordinates - Class in org.orekit.utils

Simple container for Position/Velocity/Acceleration triplets.

PVCoordinates() - Constructor for class org.orekit.utils.PVCoordinates

Simple constructor.

PVCoordinates(Vector3D, Vector3D) - Constructor for class org.orekit.utils.PVCoordinates

Builds a PVCoordinates triplet with zero acceleration.

PVCoordinates(Vector3D, Vector3D, Vector3D) - Constructor for class org.orekit.utils.PVCoordinates

Builds a PVCoordinates triplet.

PVCoordinates(double, PVCoordinates) - Constructor for class org.orekit.utils.PVCoordinates

Multiplicative constructor.

PVCoordinates(PVCoordinates, PVCoordinates) - Constructor for class org.orekit.utils.PVCoordinates

Subtractive constructor.

PVCoordinates(double, PVCoordinates, double, PVCoordinates) - Constructor for class org.orekit.utils.PVCoordinates

Linear constructor.

PVCoordinates(double, PVCoordinates, double, PVCoordinates, double, PVCoordinates) - Constructor for class org.orekit.utils.PVCoordinates

Linear constructor.

PVCoordinates(double, PVCoordinates, double, PVCoordinates, double, PVCoordinates, double, PVCoordinates) - Constructor for class org.orekit.utils.PVCoordinates

Linear constructor.

PVCoordinates(FieldVector3D<DerivativeStructure>) - Constructor for class org.orekit.utils.PVCoordinates

Builds a PVCoordinates triplet from a FieldVector3D<DerivativeStructure>.

PVCoordinatesProvider - Interface in org.orekit.utils

Interface for PV coordinates providers.

Q

q - Variable in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution

h_x.

R

radiationPressureAcceleration(AbsoluteDate, Frame, Vector3D, Rotation, double, Vector3D) - Method in class org.orekit.forces.BoxAndSolarArraySpacecraft

Compute the acceleration due to radiation pressure.

radiationPressureAcceleration(AbsoluteDate, Frame, FieldVector3D<DerivativeStructure>, FieldRotation<DerivativeStructure>, DerivativeStructure, FieldVector3D<DerivativeStructure>) - Method in class org.orekit.forces.BoxAndSolarArraySpacecraft

Compute the acceleration due to radiation pressure, with state derivatives.

radiationPressureAcceleration(AbsoluteDate, Frame, Vector3D, Rotation, double, Vector3D, String) - Method in class org.orekit.forces.BoxAndSolarArraySpacecraft

Compute the acceleration due to radiation pressure, with parameters derivatives.

radiationPressureAcceleration(AbsoluteDate, Frame, Vector3D, Rotation, double, Vector3D) - Method in interface org.orekit.forces.radiation.RadiationSensitive

Compute the acceleration due to radiation pressure.

radiationPressureAcceleration(AbsoluteDate, Frame, FieldVector3D<DerivativeStructure>, FieldRotation<DerivativeStructure>, DerivativeStructure, FieldVector3D<DerivativeStructure>) - Method in interface org.orekit.forces.radiation.RadiationSensitive

Compute the acceleration due to radiation pressure, with state derivatives.

radiationPressureAcceleration(AbsoluteDate, Frame, Vector3D, Rotation, double, Vector3D, String) - Method in interface org.orekit.forces.radiation.RadiationSensitive

Compute the acceleration due to radiation pressure, with parameters derivatives.

radiationPressureAcceleration(AbsoluteDate, Frame, Vector3D, Rotation, double, Vector3D) - Method in class org.orekit.forces.SphericalSpacecraft

Compute the acceleration due to radiation pressure.

radiationPressureAcceleration(AbsoluteDate, Frame, FieldVector3D<DerivativeStructure>, FieldRotation<DerivativeStructure>, DerivativeStructure, FieldVector3D<DerivativeStructure>) - Method in class org.orekit.forces.SphericalSpacecraft

Compute the acceleration due to radiation pressure, with state derivatives.

radiationPressureAcceleration(AbsoluteDate, Frame, Vector3D, Rotation, double, Vector3D, String) - Method in class org.orekit.forces.SphericalSpacecraft

Compute the acceleration due to radiation pressure, with parameters derivatives.

RadiationSensitive - Interface in org.orekit.forces.radiation

Interface for spacecraft that are sensitive to radiation pressure forces.

RAPID_DATA_PREDICITON_COLUMNS_2000_FILENAME - Static variable in class org.orekit.frames.FramesFactory

Default regular expression for the Rapid Data and Prediction EOP columns files (IAU2000 compatibles).

RAPID_DATA_PREDICITON_XML_2000_FILENAME - Static variable in class org.orekit.frames.FramesFactory

Default regular expression for the Rapid Data and Prediction EOP XML files (IAU2000 compatibles).

RAPID_DATA_PREDICTION_COLUMNS_1980_FILENAME - Static variable in class org.orekit.frames.FramesFactory

Default regular expression for the Rapid Data and Prediction EOP columns files (IAU1980 compatibles).

RAPID_DATA_PREDICTION_XML_1980_FILENAME - Static variable in class org.orekit.frames.FramesFactory

Default regular expression for the Rapid Data and Prediction EOP XML files (IAU1980 compatibles).

RawSphericalHarmonicsProvider - Interface in org.orekit.forces.gravity.potential

Interface used to provide raw spherical harmonics coefficients.

RawSphericalHarmonicsProvider.RawSphericalHarmonics - Interface in org.orekit.forces.gravity.potential

The raw spherical harmonics at a particular instant.

readGravityField(int, int) - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory

Read a gravity field coefficients provider from the first supported file.

REFLECTION_COEFFICIENT - Static variable in interface org.orekit.forces.radiation.RadiationSensitive

Parameter name for reflection coefficient.

registerAttitudeProvider(AttitudeProvider) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution

Register an attitude provider.

registerAttitudeProvider(AttitudeProvider) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTCentralBody

Register an attitude provider.

registerAttitudeProvider(AttitudeProvider) - Method in interface org.orekit.propagation.semianalytical.dsst.forces.DSSTForceModel

Register an attitude provider.

registerAttitudeProvider(AttitudeProvider) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBody

Register an attitude provider.

registerSwitchEvents(Propagator) - Method in class org.orekit.attitudes.AttitudesSequence

Register all wrapped switch events to the propagator.

reinitializeBegin(SpacecraftState, boolean) - Method in class org.orekit.propagation.events.EventState

Reinitialize the beginning of the step.

Relativity - Class in org.orekit.forces.gravity

Post-Newtonian correction force due to general relativity.

Relativity(double) - Constructor for class org.orekit.forces.gravity.Relativity

Create a force model to add post-Newtonian acceleration corrections to an Earth orbit.

removeForceModels() - Method in class org.orekit.propagation.numerical.NumericalPropagator

Remove all perturbing force models from the global perturbation model.

removeForceModels() - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator

Remove all perturbing force models from the global perturbation model.

removeProvider(DataProvider) - Method in class org.orekit.data.DataProvidersManager

Remove one provider.

requiresDenseOutput() - Method in class org.orekit.propagation.sampling.OrekitStepNormalizer

Determines whether this handler needs dense output.

rescale(double, boolean, double[][], double[][], boolean, double[][], double[][]) - Static method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader

Rescale coefficients arrays.

reset(SpacecraftState) - Method in class org.orekit.propagation.events.EventState

Let the event detector reset the state if it wants.

resetActiveProvider(AttitudeProvider) - Method in class org.orekit.attitudes.AttitudesSequence

Reset the active provider.

resetFitting(AbsoluteDate, double...) - Method in class org.orekit.utils.SecularAndHarmonic

Reset fitting.

resetInitialState(SpacecraftState) - Method in class org.orekit.propagation.AbstractPropagator

Reset the propagator initial state.

resetInitialState(SpacecraftState) - Method in class org.orekit.propagation.analytical.AdapterPropagator

Reset the propagator initial state.

resetInitialState(SpacecraftState) - Method in class org.orekit.propagation.analytical.EcksteinHechlerPropagator

Reset the propagator initial state.

resetInitialState(SpacecraftState) - Method in class org.orekit.propagation.analytical.Ephemeris

Try (and fail) to reset the initial state.

resetInitialState(SpacecraftState) - Method in class org.orekit.propagation.analytical.KeplerianPropagator

Reset the propagator initial state.

resetInitialState(SpacecraftState) - Method in class org.orekit.propagation.analytical.tle.TLEPropagator

Reset the propagator initial state.

resetInitialState(SpacecraftState) - Method in class org.orekit.propagation.integration.IntegratedEphemeris

Reset the propagator initial state.

resetInitialState(SpacecraftState) - Method in class org.orekit.propagation.numerical.NumericalPropagator

Reset the propagator initial state.

resetInitialState(SpacecraftState) - Method in interface org.orekit.propagation.Propagator

Reset the propagator initial state.

resetInitialState(SpacecraftState) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator

Reset the initial state.

resetShortPeriodicsCoefficients() - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution

Reset the coefficients used for short periodic variations.

resetShortPeriodicsCoefficients() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTCentralBody

Reset the coefficients used for short periodic variations.

resetShortPeriodicsCoefficients() - Method in interface org.orekit.propagation.semianalytical.dsst.forces.DSSTForceModel

Reset the coefficients used for short periodic variations.

resetShortPeriodicsCoefficients() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBody

resetState(SpacecraftState) - Method in class org.orekit.propagation.events.AbstractDetector

Reset the state prior to continue propagation.

resetState(SpacecraftState) - Method in interface org.orekit.propagation.events.EventDetector

Reset the state prior to continue propagation.

resetState(T, SpacecraftState) - Method in class org.orekit.propagation.events.handlers.ContinueOnEvent

Reset the state prior to continue propagation.

resetState(T, SpacecraftState) - Method in interface org.orekit.propagation.events.handlers.EventHandler

Reset the state prior to continue propagation.

resetState(T, SpacecraftState) - Method in class org.orekit.propagation.events.handlers.StopOnDecreasing

Reset the state prior to continue propagation.

resetState(T, SpacecraftState) - Method in class org.orekit.propagation.events.handlers.StopOnEvent

Reset the state prior to continue propagation.

resetState(T, SpacecraftState) - Method in class org.orekit.propagation.events.handlers.StopOnIncreasing

Reset the state prior to continue propagation.

revert() - Method in class org.orekit.utils.AngularCoordinates

Revert a rotation/rotation rate/ rotation acceleration triplet.

revert() - Method in class org.orekit.utils.FieldAngularCoordinates

Revert a FieldRotation/FieldRotation/FieldRotation acceleration triplet.

revert() - Method in class org.orekit.utils.TimeStampedAngularCoordinates

Revert a rotation/rotation rate pair.

revert() - Method in class org.orekit.utils.TimeStampedFieldAngularCoordinates

Revert a rotation/rotation rate pair.

rotationFromInertial(PVCoordinates) - Method in enum org.orekit.frames.LOFType

Get the rotation from inertial frame to local orbital frame.

S

s4 - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator

s* new value for the contant s.

SaastamoinenModel - Class in org.orekit.models.earth

The modified Saastamoinen model.

SaastamoinenModel(double, double, double) - Constructor for class org.orekit.models.earth.SaastamoinenModel

Create a new Saastamoinen model for the troposphere using the given environmental conditions.

SatelliteInformation - Class in org.orekit.files.general

Contains general information about a satellite as contained in an orbit file.

SatelliteInformation(String) - Constructor for class org.orekit.files.general.SatelliteInformation

Create a new SatelliteInformation object with a given satellite id.

SatelliteTimeCoordinate - Class in org.orekit.files.general

Contains the position/velocity of a satellite at an specific epoch.

SatelliteTimeCoordinate(AbsoluteDate, PVCoordinates) - Constructor for class org.orekit.files.general.SatelliteTimeCoordinate

Creates a new SatelliteTimeCoordinate instance with a given epoch and coordinate.

SatelliteTimeCoordinate(AbsoluteDate, Vector3D, double) - Constructor for class org.orekit.files.general.SatelliteTimeCoordinate

Creates a new SatelliteTimeCoordinate object with a given epoch and position coordinate.

SatelliteTimeCoordinate(AbsoluteDate, PVCoordinates, double, double) - Constructor for class org.orekit.files.general.SatelliteTimeCoordinate

Creates a new SatelliteTimeCoordinate instance with a given epoch, coordinate and clock value / rate change.

SATURN - Static variable in class org.orekit.bodies.CelestialBodyFactory

Predefined name for Saturn.

SDP4 - Static variable in class org.orekit.propagation.analytical.tle.TLE

Identifier for SDP4 type of ephemeris.

SDP8 - Static variable in class org.orekit.propagation.analytical.tle.TLE

Identifier for SDP8 type of ephemeris.

SecularAndHarmonic - Class in org.orekit.utils

Class for fitting evolution of osculating orbital parameters.

SecularAndHarmonic(int, double...) - Constructor for class org.orekit.utils.SecularAndHarmonic

Simple constructor.

selectExtrapolator(TLE) - Static method in class org.orekit.propagation.analytical.tle.TLEPropagator

Selects the extrapolator to use with the selected TLE.

selectExtrapolator(TLE, AttitudeProvider, double) - Static method in class org.orekit.propagation.analytical.tle.TLEPropagator

Selects the extrapolator to use with the selected TLE.

selectParamAndStep(String, double) - Method in class org.orekit.propagation.numerical.PartialDerivativesEquations

Select the parameters to consider for Jacobian processing.

selectParameters(String...) - Method in class org.orekit.propagation.numerical.PartialDerivativesEquations

Select the parameters to consider for Jacobian processing.

selectTransformer(Transformer, double, boolean) - Method in enum org.orekit.propagation.events.FilterType

Get next function transformer in the specified direction.

setAbsorptionCoefficient(double) - Method in class org.orekit.forces.BoxAndSolarArraySpacecraft

Set the absorption coefficient.

setAbsorptionCoefficient(double) - Method in interface org.orekit.forces.radiation.RadiationSensitive

Set the absorption coefficient.

setAbsorptionCoefficient(double) - Method in class org.orekit.forces.SphericalSpacecraft

Set the absorption coefficient.

setAccuracy(int) - Method in class org.orekit.files.general.SatelliteInformation

Set the accuracy for this satellite.

setAe(double) - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader

Set the central body reference radius.

setAgency(String) - Method in class org.orekit.files.sp3.SP3File

Set the agency string for this SP3 file.

setAngularThreshold(double) - Method in class org.orekit.bodies.OneAxisEllipsoid

Set the angular convergence threshold.

setAttitudeProvider(AttitudeProvider) - Method in class org.orekit.propagation.AbstractPropagator

Set attitude provider.

setAttitudeProvider(AttitudeProvider) - Method in class org.orekit.propagation.conversion.NumericalPropagatorBuilder

Set the attitude provider.

setAttitudeProvider(AttitudeProvider) - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator

Set attitude provider.

setAttitudeProvider(AttitudeProvider) - Method in interface org.orekit.propagation.Propagator

Set attitude provider.

setAttitudeProvider(AttitudeProvider) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator

Set attitude provider.

setCacheSlotsNumber(int) - Static method in class org.orekit.utils.OrekitConfiguration

Set the number of slots to use in caches.

setClockCorrection(double) - Method in class org.orekit.files.general.SatelliteTimeCoordinate

Set the clock correction to the given value.

setClockRateChange(double) - Method in class org.orekit.files.general.SatelliteTimeCoordinate

Set the clock rate change to the given value.

setComment(List<String>) - Method in class org.orekit.files.ccsds.OPMFile.Maneuver

Set the maneuvers data comment, each string in the list corresponds to one line of comment.

setCoordinate(PVCoordinates) - Method in class org.orekit.files.general.SatelliteTimeCoordinate

Set the coordinate for this entry.

setCoordinateSystem(String) - Method in class org.orekit.files.sp3.SP3File

Set the coordinate system used for the orbit entries.

setDataUsed(String) - Method in class org.orekit.files.sp3.SP3File

Set the data used indicator for this SP3 file.

setDayFraction(double) - Method in class org.orekit.files.sp3.SP3File

Set the day fraction for this SP3 file.

setDeltaMass(double) - Method in class org.orekit.files.ccsds.OPMFile.Maneuver

Set mass change during maneuver (value is < 0).

setDragCoefficient(double) - Method in class org.orekit.forces.BoxAndSolarArraySpacecraft

Set the drag coefficient.

setDragCoefficient(double) - Method in interface org.orekit.forces.drag.DragSensitive

Set the drag coefficient.

setDragCoefficient(double) - Method in class org.orekit.forces.SphericalSpacecraft

Set the drag coefficient.

setDuration(double) - Method in class org.orekit.files.ccsds.OPMFile.Maneuver

Set duration (value is 0 for impulsive maneuver).

setdV(Vector3D) - Method in class org.orekit.files.ccsds.OPMFile.Maneuver

Set velocity increment.

setElem(int, int, PolynomialFunction) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.PolynomialFunctionMatrix

Set an element of the matrix.

setEphemerisMode() - Method in class org.orekit.propagation.AbstractPropagator

Set the propagator to ephemeris generation mode.

setEphemerisMode() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator

Set the propagator to ephemeris generation mode.

setEphemerisMode() - Method in interface org.orekit.propagation.Propagator

Set the propagator to ephemeris generation mode.

setEpoch(AbsoluteDate) - Method in class org.orekit.files.general.SatelliteTimeCoordinate

Set the epoch for this coordinate.

setEpoch(AbsoluteDate) - Method in class org.orekit.files.sp3.SP3File

Set the epoch of the SP3 file.

setEpochInterval(double) - Method in class org.orekit.files.sp3.SP3File

Set the epoch interval for this SP3 file.

setFreeParameters(Collection<String>) - Method in class org.orekit.propagation.conversion.EcksteinHechlerPropagatorBuilder

Set the free parameters in order to build the propagator.

setFreeParameters(Collection<String>) - Method in class org.orekit.propagation.conversion.KeplerianPropagatorBuilder

Set the free parameters in order to build the propagator.

setFreeParameters(Collection<String>) - Method in class org.orekit.propagation.conversion.NumericalPropagatorBuilder

Set the free parameters in order to build the propagator.

setFreeParameters(Collection<String>) - Method in interface org.orekit.propagation.conversion.PropagatorBuilder

Set the free parameters in order to build the propagator.

setFreeParameters(Collection<String>) - Method in class org.orekit.propagation.conversion.TLEPropagatorBuilder

Set the free parameters in order to build the propagator.

setGpsWeek(int) - Method in class org.orekit.files.sp3.SP3File

Set the GPS week of the SP3 file.

setInitialJacobians(SpacecraftState, int, int) - Method in class org.orekit.propagation.numerical.PartialDerivativesEquations

Set the initial value of the Jacobian with respect to state and parameter.

setInitialJacobians(SpacecraftState, double[][], double[][]) - Method in class org.orekit.propagation.numerical.PartialDerivativesEquations

Set the initial value of the Jacobian with respect to state and parameter.

setInitialState(SpacecraftState) - Method in class org.orekit.propagation.numerical.NumericalPropagator

Set the initial state.

setInitialState(SpacecraftState) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator

Set the initial state with osculating orbital elements.

setInitialState(SpacecraftState, boolean) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator

Set the initial state.

setInterpolatedDate(AbsoluteDate) - Method in interface org.orekit.propagation.sampling.OrekitStepInterpolator

Set the interpolated date.

setJulianDay(int) - Method in class org.orekit.files.sp3.SP3File

Set the julian day for this SP3 file.

setMainFieldCoefficients(int, int, double, double) - Method in class org.orekit.models.earth.GeoMagneticField

Set the given main field coefficients.

setMass(double) - Method in class org.orekit.propagation.conversion.NumericalPropagatorBuilder

Set the initial mass.

setMasterMode(double, OrekitFixedStepHandler) - Method in class org.orekit.propagation.AbstractPropagator

Set the propagator to master mode with fixed steps.

setMasterMode(OrekitStepHandler) - Method in class org.orekit.propagation.AbstractPropagator

Set the propagator to master mode with variable steps.

setMasterMode(OrekitStepHandler) - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator

Set the propagator to master mode with variable steps.

setMasterMode(double, OrekitFixedStepHandler) - Method in interface org.orekit.propagation.Propagator

Set the propagator to master mode with fixed steps.

setMasterMode(OrekitStepHandler) - Method in interface org.orekit.propagation.Propagator

Set the propagator to master mode with variable steps.

setMatrix(PolynomialFunction[][]) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.PolynomialFunctionMatrix

Set values for all elements.

setMatrixLine(int, PolynomialFunction[]) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.PolynomialFunctionMatrix

Set the value of a line of the matrix.

setMaxParseDegree(int) - Method in class org.orekit.forces.gravity.potential.OceanTidesReader

Set the degree limit for the next file parsing.

setMaxParseDegree(int) - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader

Set the degree limit for the next file parsing.

setMaxParseOrder(int) - Method in class org.orekit.forces.gravity.potential.OceanTidesReader

Set the order limit for the next file parsing.

setMaxParseOrder(int) - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader

Set the order limit for the next file parsing.

setMu(double) - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader

Set the central body attraction coefficient.

setMu(double) - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator

Set the central attraction coefficient μ.

setMu(double) - Method in class org.orekit.propagation.numerical.NumericalPropagator

Set the central attraction coefficient μ.

setMuUsed() - Method in class org.orekit.files.ccsds.ODMFile

Set the gravitational coefficient created from the knowledge of the central body.

setNumberOfEpochs(int) - Method in class org.orekit.files.sp3.SP3File

Set the number of epochs as contained in the SP3 file.

setOrbitType(SP3File.SP3OrbitType) - Method in class org.orekit.files.sp3.SP3File

Set the SP3File.SP3OrbitType for this SP3 file.

setOrbitType(OrbitType) - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator

Set propagation orbit type.

setOrbitType(OrbitType) - Method in class org.orekit.propagation.numerical.NumericalPropagator

Set propagation orbit type.

setParameter(String, double) - Method in class org.orekit.forces.drag.DragForce

setParameter(String, double) - Method in class org.orekit.forces.gravity.CunninghamAttractionModel

setParameter(String, double) - Method in class org.orekit.forces.gravity.DrozinerAttractionModel

setParameter(String, double) - Method in class org.orekit.forces.gravity.HolmesFeatherstoneAttractionModel

setParameter(String, double) - Method in class org.orekit.forces.gravity.NewtonianAttraction

setParameter(String, double) - Method in class org.orekit.forces.gravity.OceanTides

setParameter(String, double) - Method in class org.orekit.forces.gravity.Relativity

setParameter(String, double) - Method in class org.orekit.forces.gravity.SolidTides

setParameter(String, double) - Method in class org.orekit.forces.gravity.ThirdBodyAttraction

setParameter(String, double) - Method in class org.orekit.forces.maneuvers.ConstantThrustManeuver

setParameter(String, double) - Method in class org.orekit.forces.radiation.SolarRadiationPressure

setParameter(String, double) - Method in class org.orekit.propagation.conversion.EcksteinHechlerPropagatorBuilder

setParameter(String, double) - Method in class org.orekit.propagation.conversion.KeplerianPropagatorBuilder

setParameter(String, double) - Method in class org.orekit.propagation.conversion.NumericalPropagatorBuilder

setParameter(String, double) - Method in class org.orekit.propagation.conversion.TLEPropagatorBuilder

setPositionAngleType(PositionAngle) - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator

Set position angle type.

setPositionAngleType() - Method in class org.orekit.propagation.integration.StateMapper

Set position angle type.

setPositionAngleType(PositionAngle) - Method in class org.orekit.propagation.numerical.NumericalPropagator

Set position angle type.

setPressure(double) - Method in class org.orekit.models.earth.EarthStandardAtmosphereRefraction

Set the local pressure at the evaluation location

setProvider(ForceModel) - Method in class org.orekit.propagation.numerical.ParameterConfiguration

Set the povider handling this parameter.

setRawCoefficients(boolean, double[][], double[][], String) - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader

Set the tesseral-sectorial coefficients matrix.

setReadComplete(boolean) - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader

Set the indicator for completed read.

setRefFrame(Frame) - Method in class org.orekit.files.ccsds.OPMFile.Maneuver

Set Coordinate system for velocity increment vector, for absolute frames.

setReflectionCoefficient(double) - Method in class org.orekit.forces.BoxAndSolarArraySpacecraft

Set the specular reflection coefficient.

setReflectionCoefficient(double) - Method in interface org.orekit.forces.radiation.RadiationSensitive

Set the specular reflection coefficient.

setReflectionCoefficient(double) - Method in class org.orekit.forces.SphericalSpacecraft

Set the specular reflection coefficient.

setRefLofType(LOFType) - Method in class org.orekit.files.ccsds.OPMFile.Maneuver

Set coordinate system for velocity increment vector, for Local Orbital Frames.

setSatelliteId(String) - Method in class org.orekit.files.general.SatelliteInformation

Set the id of this satellite.

setSatelliteRevolution(int) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator

Override the default value of the parameter.

setSecondsOfWeek(double) - Method in class org.orekit.files.sp3.SP3File

Set the seconds of the GPS week for this SP3 file.

setSecularVariationCoefficients(int, int, double, double) - Method in class org.orekit.models.earth.GeoMagneticField

Set the given secular variation coefficients.

setSlaveMode() - Method in class org.orekit.propagation.AbstractPropagator

Set the propagator to slave mode.

setSlaveMode() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator

Set the propagator to slave mode.

setSlaveMode() - Method in interface org.orekit.propagation.Propagator

Set the propagator to slave mode.

setStartDate(AbsoluteDate) - Method in class org.orekit.propagation.AbstractPropagator

Set a start date.

setSteps(double, double) - Method in class org.orekit.forces.gravity.CunninghamAttractionModel

Set the step for finite differences with respect to spacecraft position.

setSteps(double, double) - Method in class org.orekit.forces.gravity.DrozinerAttractionModel

Set the step for finite differences with respect to spacecraft position.

setTemperature(double) - Method in class org.orekit.models.earth.EarthStandardAtmosphereRefraction

Set the local temperature at the evaluation location

setTideSystem(TideSystem) - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader

Set the TideSystem used in the gravity field.

setTimeout(int) - Method in class org.orekit.data.NetworkCrawler

Set the timeout for connection.

setTimeSystem(OrbitFile.TimeSystem) - Method in class org.orekit.files.sp3.SP3File

Set the time system used in this SP3 file.

setType(SP3File.SP3FileType) - Method in class org.orekit.files.sp3.SP3File

Set the file type for this SP3 file.

setUpEventDetector(AbstractIntegrator, EventDetector) - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator

Wrap an Orekit event detector and register it to the integrator.

setUpUserEventDetectors() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator

Set up all user defined event detectors.

SGP - Static variable in class org.orekit.propagation.analytical.tle.TLE

Identifier for SGP type of ephemeris.

SGP4 - Static variable in class org.orekit.propagation.analytical.tle.TLE

Identifier for SGP4 type of ephemeris.

SGP8 - Static variable in class org.orekit.propagation.analytical.tle.TLE

Identifier for SGP8 type of ephemeris.

shiftedBy(double) - Method in class org.orekit.attitudes.Attitude

Get a time-shifted attitude.

shiftedBy(double) - Method in class org.orekit.frames.Transform

Get a time-shifted instance.

shiftedBy(double) - Method in class org.orekit.orbits.CartesianOrbit

Get a time-shifted orbit.

shiftedBy(double) - Method in class org.orekit.orbits.CircularOrbit

Get a time-shifted orbit.

shiftedBy(double) - Method in class org.orekit.orbits.EquinoctialOrbit

Get a time-shifted orbit.

shiftedBy(double) - Method in class org.orekit.orbits.KeplerianOrbit

Get a time-shifted orbit.

shiftedBy(double) - Method in class org.orekit.orbits.Orbit

Get a time-shifted orbit.

shiftedBy(double) - Method in class org.orekit.propagation.SpacecraftState

Get a time-shifted state.

shiftedBy(double) - Method in class org.orekit.time.AbsoluteDate

Get a time-shifted date.

shiftedBy(double) - Method in interface org.orekit.time.TimeShiftable

Get a time-shifted instance.

shiftedBy(double) - Method in class org.orekit.utils.AngularCoordinates

Get a time-shifted state.

shiftedBy(double) - Method in class org.orekit.utils.FieldAngularCoordinates

Get a time-shifted state.

shiftedBy(double) - Method in class org.orekit.utils.FieldPVCoordinates

Get a time-shifted state.

shiftedBy(double) - Method in class org.orekit.utils.PVCoordinates

Get a time-shifted state.

shiftedBy(double) - Method in class org.orekit.utils.TimeStampedAngularCoordinates

Get a time-shifted state.

shiftedBy(double) - Method in class org.orekit.utils.TimeStampedFieldAngularCoordinates

Get a time-shifted state.

shiftedBy(double) - Method in class org.orekit.utils.TimeStampedFieldPVCoordinates

Get a time-shifted state.

shiftedBy(double) - Method in class org.orekit.utils.TimeStampedPVCoordinates

Get a time-shifted state.

SHM_FILENAME - Static variable in class org.orekit.forces.gravity.potential.GravityFieldFactory

Default regular expression for SHM files.

SHMFormatReader - Class in org.orekit.forces.gravity.potential

Reader for the SHM gravity field format.

SHMFormatReader(String, boolean) - Constructor for class org.orekit.forces.gravity.potential.SHMFormatReader

Simple constructor.

ShortPeriodicsInterpolatedCoefficient - Class in org.orekit.propagation.semianalytical.dsst.utilities

Interpolated short periodics coefficients.

ShortPeriodicsInterpolatedCoefficient(int) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.ShortPeriodicsInterpolatedCoefficient

Simple constructor.

SimpleExponentialAtmosphere - Class in org.orekit.forces.drag

Simple exponential atmospheric model.

SimpleExponentialAtmosphere(BodyShape, double, double, double) - Constructor for class org.orekit.forces.drag.SimpleExponentialAtmosphere

Create an exponential atmosphere.

SimpleTimeStampedTableParser<T extends TimeStamped> - Class in org.orekit.data

Parser for simple tables containing time stamped data.

SimpleTimeStampedTableParser(int, SimpleTimeStampedTableParser.RowConverter<T>) - Constructor for class org.orekit.data.SimpleTimeStampedTableParser

Simple constructor.

SimpleTimeStampedTableParser.RowConverter<S extends TimeStamped> - Interface in org.orekit.data

Interface for converting a table row into time-stamped data.

sini0 - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator

sinus original inclination.

SLAVE_MODE - Static variable in interface org.orekit.propagation.Propagator

Indicator for slave mode.

SmallManeuverAnalyticalModel - Class in org.orekit.forces.maneuvers

Analytical model for small maneuvers.

SmallManeuverAnalyticalModel(SpacecraftState, Vector3D, double) - Constructor for class org.orekit.forces.maneuvers.SmallManeuverAnalyticalModel

Build a maneuver defined in spacecraft frame.

SmallManeuverAnalyticalModel(SpacecraftState, Frame, Vector3D, double) - Constructor for class org.orekit.forces.maneuvers.SmallManeuverAnalyticalModel

Build a maneuver defined in user-specified frame.

SOLAR_SYSTEM_BARYCENTER - Static variable in class org.orekit.bodies.CelestialBodyFactory

Predefined name for solar system barycenter.

SolarRadiationPressure - Class in org.orekit.forces.radiation

Solar radiation pressure force model.

SolarRadiationPressure(PVCoordinatesProvider, double, RadiationSensitive) - Constructor for class org.orekit.forces.radiation.SolarRadiationPressure

Simple constructor with default reference values.

SolarRadiationPressure(double, double, PVCoordinatesProvider, double, RadiationSensitive) - Constructor for class org.orekit.forces.radiation.SolarRadiationPressure

Complete constructor.

SolidTides - Class in org.orekit.forces.gravity

Solid tides force model.

SolidTides(Frame, double, double, TideSystem, IERSConventions, UT1Scale, CelestialBody...) - Constructor for class org.orekit.forces.gravity.SolidTides

Simple constructor.

SolidTides(Frame, double, double, TideSystem, boolean, double, int, IERSConventions, UT1Scale, CelestialBody...) - Constructor for class org.orekit.forces.gravity.SolidTides

Simple constructor.

SP3File - Class in org.orekit.files.sp3

Represents a parsed SP3 orbit file.

SP3File() - Constructor for class org.orekit.files.sp3.SP3File

Create a new SP3 file object.

SP3File.SP3FileType - Enum in org.orekit.files.sp3

File type indicator.

SP3File.SP3OrbitType - Enum in org.orekit.files.sp3

Orbit type indicator.

SP3Parser - Class in org.orekit.files.sp3

A parser for the SP3 orbit file format.

SP3Parser() - Constructor for class org.orekit.files.sp3.SP3Parser

SpacecraftState - Class in org.orekit.propagation

This class is the representation of a complete state holding orbit, attitude and mass information at a given date.

SpacecraftState(Orbit) - Constructor for class org.orekit.propagation.SpacecraftState

Build a spacecraft state from orbit only.

SpacecraftState(Orbit, Attitude) - Constructor for class org.orekit.propagation.SpacecraftState

Build a spacecraft state from orbit and attitude provider.

SpacecraftState(Orbit, double) - Constructor for class org.orekit.propagation.SpacecraftState

Create a new instance from orbit and mass.

SpacecraftState(Orbit, Attitude, double) - Constructor for class org.orekit.propagation.SpacecraftState

Build a spacecraft state from orbit, attitude provider and mass.

SpacecraftState(Orbit, Map<String, double[]>) - Constructor for class org.orekit.propagation.SpacecraftState

Build a spacecraft state from orbit only.

SpacecraftState(Orbit, Attitude, Map<String, double[]>) - Constructor for class org.orekit.propagation.SpacecraftState

Build a spacecraft state from orbit and attitude provider.

SpacecraftState(Orbit, double, Map<String, double[]>) - Constructor for class org.orekit.propagation.SpacecraftState

Create a new instance from orbit and mass.

SpacecraftState(Orbit, Attitude, double, Map<String, double[]>) - Constructor for class org.orekit.propagation.SpacecraftState

Build a spacecraft state from orbit, attitude provider and mass.

SPEED_OF_LIGHT - Static variable in interface org.orekit.utils.Constants

Speed of light: 299792458.0 m/s.

SphericalHarmonicsProvider - Interface in org.orekit.forces.gravity.potential

Interface used to provide spherical harmonics coefficients.

SphericalSpacecraft - Class in org.orekit.forces

This class represents the features of a simplified spacecraft.

SphericalSpacecraft(double, double, double, double) - Constructor for class org.orekit.forces.SphericalSpacecraft

Simple constructor.

SpinStabilized - Class in org.orekit.attitudes

This class handles a spin stabilized attitude provider.

SpinStabilized(AttitudeProvider, AbsoluteDate, Vector3D, double) - Constructor for class org.orekit.attitudes.SpinStabilized

Creates a new instance.

STANDARD_ATM_PRESSURE - Static variable in class org.orekit.models.earth.EarthStandardAtmosphereRefraction

NIST standard atmospheric pressure (Pa).

STANDARD_ATM_TEMPERATURE - Static variable in class org.orekit.models.earth.EarthStandardAtmosphereRefraction

NIST standard atmospheric temperature (K).

startParse(String) - Method in class org.orekit.forces.gravity.potential.OceanTidesReader

Start parsing.

StateMapper - Class in org.orekit.propagation.integration

This class maps between raw double elements and SpacecraftState instances.

StateMapper(AbsoluteDate, double, OrbitType, PositionAngle, AttitudeProvider, Frame) - Constructor for class org.orekit.propagation.integration.StateMapper

Simple constructor.

stepAccepted(SpacecraftState) - Method in class org.orekit.propagation.events.EventState

Acknowledge the fact the step has been accepted by the propagator.

stillAcceptsData() - Method in interface org.orekit.data.DataLoader

Check if the loader still accepts new data.

stillAcceptsData() - Method in class org.orekit.forces.drag.MarshallSolarActivityFutureEstimation

Check if the loader still accepts new data.

stillAcceptsData() - Method in class org.orekit.forces.gravity.potential.AstronomicalAmplitudeReader

Check if the loader still accepts new data.

stillAcceptsData() - Method in class org.orekit.forces.gravity.potential.OceanTidesReader

Check if the loader still accepts new data.

stillAcceptsData() - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader

Check if the loader still accepts new data.

stillAcceptsData() - Method in class org.orekit.models.earth.GeoMagneticModelLoader

Check if the loader still accepts new data.

stillAcceptsData() - Method in class org.orekit.propagation.analytical.tle.TLESeries

Check if the loader still accepts new data.

stillAcceptsData() - Method in class org.orekit.utils.InterpolationTableLoader

Check if the loader still accepts new data.

stop() - Method in class org.orekit.propagation.events.EventState

Check if the propagation should be stopped at the end of the current step.

StopOnDecreasing<T extends EventDetector> - Class in org.orekit.propagation.events.handlers

Handle a detection event and choose what to do next.

StopOnDecreasing() - Constructor for class org.orekit.propagation.events.handlers.StopOnDecreasing

StopOnEvent<T extends EventDetector> - Class in org.orekit.propagation.events.handlers

Event handler which will always return stop as a state.

StopOnEvent() - Constructor for class org.orekit.propagation.events.handlers.StopOnEvent

StopOnIncreasing<T extends EventDetector> - Class in org.orekit.propagation.events.handlers

Handle a detection event and choose what to do next.

StopOnIncreasing() - Constructor for class org.orekit.propagation.events.handlers.StopOnIncreasing

subtractOffset(AngularCoordinates) - Method in class org.orekit.utils.AngularCoordinates

Subtract an offset from the instance.

subtractOffset(FieldAngularCoordinates<T>) - Method in class org.orekit.utils.FieldAngularCoordinates

Subtract an offset from the instance.

subtractOffset(AngularCoordinates) - Method in class org.orekit.utils.TimeStampedAngularCoordinates

Subtract an offset from the instance.

subtractOffset(FieldAngularCoordinates<T>) - Method in class org.orekit.utils.TimeStampedFieldAngularCoordinates

Subtract an offset from the instance.

SUN - Static variable in class org.orekit.bodies.CelestialBodyFactory

Predefined name for Sun.

SUN_RADIUS - Static variable in interface org.orekit.utils.Constants

Sun radius: 695500000 m.

supportsTimeTransform() - Method in class org.orekit.models.earth.GeoMagneticField

Indicates whether this model supports time transformation or not.

sxpInitialize() - Method in class org.orekit.propagation.analytical.tle.TLEPropagator

Initialization proper to each propagator (SGP or SDP).

sxpPropagate(double) - Method in class org.orekit.propagation.analytical.tle.TLEPropagator

Propagation proper to each propagator (SGP or SDP).

T

t2cof - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator

3/2 * C1.

TabulatedProvider - Class in org.orekit.attitudes

This class handles an attitude provider interpolating from a predefined table.

TabulatedProvider(List<Attitude>, int, boolean) - Constructor for class org.orekit.attitudes.TabulatedProvider

Deprecated.

as of 7.0, replaced with TabulatedProvider.TabulatedProvider(Frame, List, int, AngularDerivativesFilter)

TabulatedProvider(Frame, List<TimeStampedAngularCoordinates>, int, AngularDerivativesFilter) - Constructor for class org.orekit.attitudes.TabulatedProvider

Creates new instance.

TAIScale - Class in org.orekit.time

International Atomic Time.

TargetPointing - Class in org.orekit.attitudes

This class handles target pointing attitude provider.

TargetPointing(Frame, Vector3D) - Constructor for class org.orekit.attitudes.TargetPointing

Creates a new instance from body frame and target expressed in cartesian coordinates.

TargetPointing(GeodeticPoint, BodyShape) - Constructor for class org.orekit.attitudes.TargetPointing

Creates a new instance from body shape and target expressed in geodetic coordinates.

TCBScale - Class in org.orekit.time

Barycentric Coordinate Time.

TCGScale - Class in org.orekit.time

Geocentric Coordinate Time.

TDBScale - Class in org.orekit.time

Barycentric Dynamic Time.

theta2 - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator

cos io squared.

ThirdBodyAttraction - Class in org.orekit.forces.gravity

Third body attraction force model.

ThirdBodyAttraction(CelestialBody) - Constructor for class org.orekit.forces.gravity.ThirdBodyAttraction

Simple constructor.

ThreeEighthesIntegratorBuilder - Class in org.orekit.propagation.conversion

Builder for ThreeEighthesIntegrator.

ThreeEighthesIntegratorBuilder(double) - Constructor for class org.orekit.propagation.conversion.ThreeEighthesIntegratorBuilder

Build a new instance.

TideSystem - Enum in org.orekit.forces.gravity.potential

Enumerate for tie systems.

TideSystemProvider - Interface in org.orekit.forces.gravity.potential

Interface used to provide tide systems.

TimeComponents - Class in org.orekit.time

Class representing a time within the day broken up as hour, minute and second components.

TimeComponents(int, int, double) - Constructor for class org.orekit.time.TimeComponents

Build a time from its clock elements.

TimeComponents(double) - Constructor for class org.orekit.time.TimeComponents

Build a time from the second number within the day.

TimeComponents(int, double) - Constructor for class org.orekit.time.TimeComponents

Build a time from the second number within the day.

TimeDerivativesEquations - Interface in org.orekit.propagation.numerical

Interface summing up the contribution of several forces into orbit and mass derivatives.

TimeFunction<T> - Interface in org.orekit.time

This interface represents a scalar function of time.

TimeInterpolable<T extends TimeInterpolable<T>> - Interface in org.orekit.time

This interface represents objects that can be interpolated in time.

TimeScale - Interface in org.orekit.time

Interface for time scales.

TimeScalesFactory - Class in org.orekit.time

Factory for predefined time scales.

timeScalesOffset(TimeScale, TimeScale) - Method in class org.orekit.time.AbsoluteDate

Compute the offset between two time scales at the current instant.

TimeShiftable<T extends TimeShiftable<T>> - Interface in org.orekit.time

This interface represents objects that can be shifted in time.

TimeStamped - Interface in org.orekit.time

This interface represents objects that have a AbsoluteDate date attached to them.

TimeStampedAngularCoordinates - Class in org.orekit.utils

time-stamped version of AngularCoordinates.

TimeStampedAngularCoordinates(AbsoluteDate, Rotation, Vector3D, Vector3D) - Constructor for class org.orekit.utils.TimeStampedAngularCoordinates

Builds a rotation/rotation rate pair.

TimeStampedAngularCoordinates(AbsoluteDate, PVCoordinates, PVCoordinates, PVCoordinates, PVCoordinates, double) - Constructor for class org.orekit.utils.TimeStampedAngularCoordinates

Build the rotation that transforms a pair of pv coordinates into another pair.

TimeStampedAngularCoordinates(AbsoluteDate, PVCoordinates, PVCoordinates) - Constructor for class org.orekit.utils.TimeStampedAngularCoordinates

Build one of the rotations that transform one pv coordinates into another one.

TimeStampedAngularCoordinates(AbsoluteDate, FieldRotation<DerivativeStructure>) - Constructor for class org.orekit.utils.TimeStampedAngularCoordinates

Builds a TimeStampedAngularCoordinates from a FieldRotation<DerivativeStructure>.

TimeStampedCache<T extends TimeStamped> - Interface in org.orekit.utils

Interface for a data structure that can provide concurrent access to TimeStamped data surrounding a given date.

TimeStampedCacheException - Exception in org.orekit.errors

This class is the base class for all specific exceptions thrown by during the GenericTimeStampedCache.

TimeStampedCacheException(Localizable, Object...) - Constructor for exception org.orekit.errors.TimeStampedCacheException

Simple constructor.

TimeStampedCacheException(Throwable, Localizable, Object...) - Constructor for exception org.orekit.errors.TimeStampedCacheException

Simple constructor.

TimeStampedCacheException(OrekitException) - Constructor for exception org.orekit.errors.TimeStampedCacheException

Simple constructor.

TimeStampedCacheException(ExceptionContextProvider) - Constructor for exception org.orekit.errors.TimeStampedCacheException

Simple constructor.

TimeStampedFieldAngularCoordinates<T extends RealFieldElement<T>> - Class in org.orekit.utils

time-stamped version of FieldAngularCoordinates.

TimeStampedFieldAngularCoordinates(AbsoluteDate, FieldRotation<T>, FieldVector3D<T>, FieldVector3D<T>) - Constructor for class org.orekit.utils.TimeStampedFieldAngularCoordinates

Builds a rotation/rotation rate pair.

TimeStampedFieldPVCoordinates<T extends RealFieldElement<T>> - Class in org.orekit.utils

time-stamped version of FieldPVCoordinates.

TimeStampedFieldPVCoordinates(AbsoluteDate, FieldVector3D<T>, FieldVector3D<T>, FieldVector3D<T>) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates

Builds a PVCoordinates pair.

TimeStampedFieldPVCoordinates(AbsoluteDate, double, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates

Multiplicative constructor

TimeStampedFieldPVCoordinates(AbsoluteDate, T, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates

Multiplicative constructor

TimeStampedFieldPVCoordinates(AbsoluteDate, T, PVCoordinates) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates

Multiplicative constructor

TimeStampedFieldPVCoordinates(AbsoluteDate, FieldPVCoordinates<T>, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates

Subtractive constructor

TimeStampedFieldPVCoordinates(AbsoluteDate, double, FieldPVCoordinates<T>, double, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates

Linear constructor

TimeStampedFieldPVCoordinates(AbsoluteDate, T, FieldPVCoordinates<T>, T, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates

Linear constructor

TimeStampedFieldPVCoordinates(AbsoluteDate, T, PVCoordinates, T, PVCoordinates) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates

Linear constructor

TimeStampedFieldPVCoordinates(AbsoluteDate, double, FieldPVCoordinates<T>, double, FieldPVCoordinates<T>, double, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates

Linear constructor

TimeStampedFieldPVCoordinates(AbsoluteDate, T, FieldPVCoordinates<T>, T, FieldPVCoordinates<T>, T, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates

Linear constructor

TimeStampedFieldPVCoordinates(AbsoluteDate, T, PVCoordinates, T, PVCoordinates, T, PVCoordinates) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates

Linear constructor

TimeStampedFieldPVCoordinates(AbsoluteDate, double, FieldPVCoordinates<T>, double, FieldPVCoordinates<T>, double, FieldPVCoordinates<T>, double, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates

Linear constructor

TimeStampedFieldPVCoordinates(AbsoluteDate, T, FieldPVCoordinates<T>, T, FieldPVCoordinates<T>, T, FieldPVCoordinates<T>, T, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates

Linear constructor

TimeStampedFieldPVCoordinates(AbsoluteDate, T, PVCoordinates, T, PVCoordinates, T, PVCoordinates, T, PVCoordinates) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates

Linear constructor

TimeStampedGenerator<T extends TimeStamped> - Interface in org.orekit.utils

Generator to use for creating entries in time stamped caches.

TimeStampedPVCoordinates - Class in org.orekit.utils

time-stamped version of PVCoordinates.

TimeStampedPVCoordinates(AbsoluteDate, Vector3D, Vector3D, Vector3D) - Constructor for class org.orekit.utils.TimeStampedPVCoordinates

Builds a TimeStampedPVCoordinates pair.

TimeStampedPVCoordinates(AbsoluteDate, Vector3D, Vector3D) - Constructor for class org.orekit.utils.TimeStampedPVCoordinates

Build from position and velocity.

TimeStampedPVCoordinates(AbsoluteDate, PVCoordinates) - Constructor for class org.orekit.utils.TimeStampedPVCoordinates

Build from position velocity acceleration coordinates.

TimeStampedPVCoordinates(AbsoluteDate, double, PVCoordinates) - Constructor for class org.orekit.utils.TimeStampedPVCoordinates

Multiplicative constructor

TimeStampedPVCoordinates(AbsoluteDate, PVCoordinates, PVCoordinates) - Constructor for class org.orekit.utils.TimeStampedPVCoordinates

Subtractive constructor

TimeStampedPVCoordinates(AbsoluteDate, double, PVCoordinates, double, PVCoordinates) - Constructor for class org.orekit.utils.TimeStampedPVCoordinates

Linear constructor

TimeStampedPVCoordinates(AbsoluteDate, double, PVCoordinates, double, PVCoordinates, double, PVCoordinates) - Constructor for class org.orekit.utils.TimeStampedPVCoordinates

Linear constructor

TimeStampedPVCoordinates(AbsoluteDate, double, PVCoordinates, double, PVCoordinates, double, PVCoordinates, double, PVCoordinates) - Constructor for class org.orekit.utils.TimeStampedPVCoordinates

Linear constructor

TimeStampedPVCoordinates(AbsoluteDate, FieldVector3D<DerivativeStructure>) - Constructor for class org.orekit.utils.TimeStampedPVCoordinates

Builds a TimeStampedPVCoordinates triplet from a FieldVector3D<DerivativeStructure>.

TLE - Class in org.orekit.propagation.analytical.tle

This class is a container for a single set of TLE data.

TLE(String, String) - Constructor for class org.orekit.propagation.analytical.tle.TLE

Simple constructor from unparsed two lines.

TLE(int, char, int, int, String, int, int, AbsoluteDate, double, double, double, double, double, double, double, double, int, double) - Constructor for class org.orekit.propagation.analytical.tle.TLE

Simple constructor from already parsed elements.

tle - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator

Initial state.

TLEPropagator - Class in org.orekit.propagation.analytical.tle

This class provides elements to propagate TLE's.

TLEPropagator(TLE, AttitudeProvider, double) - Constructor for class org.orekit.propagation.analytical.tle.TLEPropagator

Protected constructor for derived classes.

TLEPropagatorBuilder - Class in org.orekit.propagation.conversion

Builder for TLEPropagator.

TLEPropagatorBuilder(int, char, int, int, String, int, int) - Constructor for class org.orekit.propagation.conversion.TLEPropagatorBuilder

Build a new instance.

TLESeries - Class in org.orekit.propagation.analytical.tle

This class reads and handles series of TLEs for one space object.

TLESeries(String, boolean) - Constructor for class org.orekit.propagation.analytical.tle.TLESeries

Simple constructor with a TLE file.

toAngularCoordinates() - Method in class org.orekit.utils.FieldAngularCoordinates

Convert to a regular angular coordinates.

toArray(List<List<Double>>) - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader

Convert a list of list into an array.

toDate(TimeScale) - Method in class org.orekit.time.AbsoluteDate

Convert the instance to a Java Date.

toDerivativeStructureRotation(int) - Method in class org.orekit.utils.AngularCoordinates

Transform the instance to a FieldRotation<DerivativeStructure>.

toDerivativeStructureVector(int) - Method in class org.orekit.utils.PVCoordinates

Transform the instance to a FieldVector3D<DerivativeStructure>.

toEquinox(AbsoluteDate, double, double) - Method in interface org.orekit.utils.IERSConventions.NutationCorrectionConverter

Convert nutation corrections.

tolerances(double, Orbit, OrbitType) - Static method in class org.orekit.propagation.numerical.NumericalPropagator

Estimate tolerance vectors for integrators.

tolerances(double, Orbit) - Static method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator

Estimate tolerance vectors for an AdaptativeStepsizeIntegrator.

ton2a - Variable in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution

2 / (n² * a) .

toNonRotating(AbsoluteDate, double, double) - Method in interface org.orekit.utils.IERSConventions.NutationCorrectionConverter

Convert nutation corrections.

toPlane(Vector3D) - Method in class org.orekit.bodies.Ellipse

Project a point to the ellipse plane.

TopocentricFrame - Class in org.orekit.frames

Topocentric frame.

TopocentricFrame(BodyShape, GeodeticPoint, String) - Constructor for class org.orekit.frames.TopocentricFrame

Simple constructor.

toPVCoordinates() - Method in class org.orekit.utils.FieldPVCoordinates

Convert to a constant position-velocity without derivatives.

toSI(double) - Method in enum org.orekit.data.PolynomialParser.Unit

Convert value from instance unit to corresponding SI unit.

toSpace(Vector2D) - Method in class org.orekit.bodies.Ellipse

Create a point from its ellipse-relative coordinates.

toString() - Method in class org.orekit.bodies.GeodeticPoint

toString() - Method in class org.orekit.frames.Frame

New definition of the java.util toString() method.

toString() - Method in class org.orekit.frames.OrphanFrame

toString() - Method in class org.orekit.models.earth.GeoMagneticElements

toString() - Method in class org.orekit.orbits.CartesianOrbit

Returns a string representation of this Orbit object.

toString() - Method in class org.orekit.orbits.CircularOrbit

Returns a string representation of this Orbit object.

toString() - Method in class org.orekit.orbits.EquinoctialOrbit

Returns a string representation of this equinoctial parameters object.

toString() - Method in class org.orekit.orbits.KeplerianOrbit

Returns a string representation of this keplerian parameters object.

toString() - Method in class org.orekit.propagation.analytical.tle.TLE

Get a string representation of this TLE set.

toString() - Method in class org.orekit.time.AbsoluteDate

Get a String representation of the instant location in UTC time scale.

toString(TimeScale) - Method in class org.orekit.time.AbsoluteDate

Get a String representation of the instant location.

toString() - Method in class org.orekit.time.DateComponents

Get a string representation (ISO-8601) of the date.

toString() - Method in class org.orekit.time.DateTimeComponents

Return a string representation of this pair.

toString() - Method in class org.orekit.time.GalileoScale

toString() - Method in class org.orekit.time.GMSTScale

toString() - Method in class org.orekit.time.GPSScale

toString() - Method in class org.orekit.time.TAIScale

toString() - Method in class org.orekit.time.TCBScale

toString() - Method in class org.orekit.time.TCGScale

toString() - Method in class org.orekit.time.TDBScale

toString() - Method in class org.orekit.time.TimeComponents

Get a string representation of the time.

toString() - Method in class org.orekit.time.TTScale

toString() - Method in class org.orekit.time.UT1Scale

toString() - Method in class org.orekit.time.UTCScale

toString() - Method in class org.orekit.utils.FieldPVCoordinates

Return a string representation of this position/velocity pair.

toString() - Method in class org.orekit.utils.ImmutableTimeStampedCache

toString() - Method in class org.orekit.utils.PVCoordinates

Return a string representation of this position/velocity pair.

toString() - Method in class org.orekit.utils.TimeStampedFieldPVCoordinates

Return a string representation of this position/velocity pair.

toString() - Method in class org.orekit.utils.TimeStampedPVCoordinates

Return a string representation of this position/velocity pair.

toTaylorProvider(Frame) - Method in class org.orekit.utils.TimeStampedPVCoordinates

Create a local provider using simply Taylor expansion through shiftedBy(double).

toTransform() - Method in class org.orekit.propagation.SpacecraftState

Compute the transform from orbite/attitude reference frame to spacecraft frame.

transform(Vector3D, Frame, AbsoluteDate) - Method in interface org.orekit.bodies.BodyShape

Transform a cartesian point to a surface-relative point.

transform(GeodeticPoint) - Method in interface org.orekit.bodies.BodyShape

Transform a surface-relative point to a cartesian point.

transform(GeodeticPoint) - Method in class org.orekit.bodies.OneAxisEllipsoid

Transform a surface-relative point to a cartesian point.

transform(Vector3D, Frame, AbsoluteDate) - Method in class org.orekit.bodies.OneAxisEllipsoid

Transform a cartesian point to a surface-relative point.

Transform - Class in org.orekit.frames

Transformation class in three dimensional space.

Transform(AbsoluteDate, Vector3D) - Constructor for class org.orekit.frames.Transform

Build a translation transform.

Transform(AbsoluteDate, Rotation) - Constructor for class org.orekit.frames.Transform

Build a rotation transform.

Transform(AbsoluteDate, Vector3D, Vector3D) - Constructor for class org.orekit.frames.Transform

Build a translation transform, with its first time derivative.

Transform(AbsoluteDate, Vector3D, Vector3D, Vector3D) - Constructor for class org.orekit.frames.Transform

Build a translation transform, with its first and second time derivatives.

Transform(AbsoluteDate, PVCoordinates) - Constructor for class org.orekit.frames.Transform

Build a translation transform, with its first time derivative.

Transform(AbsoluteDate, Rotation, Vector3D) - Constructor for class org.orekit.frames.Transform

Build a rotation transform.

Transform(AbsoluteDate, Rotation, Vector3D, Vector3D) - Constructor for class org.orekit.frames.Transform

Build a rotation transform.

Transform(AbsoluteDate, AngularCoordinates) - Constructor for class org.orekit.frames.Transform

Build a rotation transform.

Transform(AbsoluteDate, Transform, Transform) - Constructor for class org.orekit.frames.Transform

Build a transform by combining two existing ones.

transformFromInertial(AbsoluteDate, PVCoordinates) - Method in enum org.orekit.frames.LOFType

Get the transform from an inertial frame defining position-velocity and the local orbital frame.

transformLine(Line) - Method in class org.orekit.frames.Transform

Transform a line.

transformModel(double) - Method in class org.orekit.models.earth.GeoMagneticField

Time transform the model coefficients from the base year of the model using secular variation coefficients.

transformModel(GeoMagneticField, double) - Method in class org.orekit.models.earth.GeoMagneticField

Time transform the model coefficients from the base year of the model using a linear interpolation with a second model.

transformPosition(Vector3D) - Method in class org.orekit.frames.Transform

Transform a position vector (including translation effects).

transformPosition(FieldVector3D<T>) - Method in class org.orekit.frames.Transform

Transform a position vector (including translation effects).

TransformProvider - Interface in org.orekit.frames

Interface for Transform providers.

transformPVCoordinates(PVCoordinates) - Method in class org.orekit.frames.Transform

Transform PVCoordinates including kinematic effects.

transformPVCoordinates(TimeStampedPVCoordinates) - Method in class org.orekit.frames.Transform

Transform TimeStampedPVCoordinates including kinematic effects.

transformPVCoordinates(FieldPVCoordinates<T>) - Method in class org.orekit.frames.Transform

Transform FieldPVCoordinates including kinematic effects.

transformPVCoordinates(TimeStampedFieldPVCoordinates<T>) - Method in class org.orekit.frames.Transform

Transform TimeStampedFieldPVCoordinates including kinematic effects.

transformVector(Vector3D) - Method in class org.orekit.frames.Transform

Transform a vector (ignoring translation effects).

transformVector(FieldVector3D<T>) - Method in class org.orekit.frames.Transform

Transform a vector (ignoring translation effects).

TroposphericDelayModel - Interface in org.orekit.models.earth

Defines a tropospheric model, used to calculate the path delay imposed to electro-magnetic signals between an orbital satellite and a ground station.

tsi - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator

tsi from SPTRCK #3.

TTScale - Class in org.orekit.time

Terrestrial Time as defined by IAU(1991) recommendation IV.

U

UnnormalizedSphericalHarmonicsProvider - Interface in org.orekit.forces.gravity.potential

Interface used to provide un-normalized spherical harmonics coefficients.

UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics - Interface in org.orekit.forces.gravity.potential

Un-normalized spherical harmonics coefficients evaluated at a specific instant.

unwrap(OrekitException) - Static method in exception org.orekit.errors.PropagationException

Recover a PropagationException, possibly embedded in a OrekitException.

unwrap(ExceptionContextProvider) - Static method in exception org.orekit.errors.PropagationException

Recover a PropagationException, possibly embedded in an ExceptionContextProvider.

unwrap(OrekitException) - Static method in exception org.orekit.errors.TimeStampedCacheException

Recover a PropagationException, possibly embedded in a OrekitException.

unwrap(ExceptionContextProvider) - Static method in exception org.orekit.errors.TimeStampedCacheException

Recover a PropagationException, possibly embedded in an ExceptionContextProvider.

UpdatableFrame - Class in org.orekit.frames

Frame whose transform from its parent can be updated.

UpdatableFrame(Frame, Transform, String) - Constructor for class org.orekit.frames.UpdatableFrame

Build a non-inertial frame from its transform with respect to its parent.

UpdatableFrame(Frame, Transform, String, boolean) - Constructor for class org.orekit.frames.UpdatableFrame

Build a frame from its transform with respect to its parent.

updateAdditionalStates(SpacecraftState) - Method in class org.orekit.propagation.AbstractPropagator

Update state by adding all additional states.

updateMass(double) - Method in class org.orekit.forces.maneuvers.SmallManeuverAnalyticalModel

Update a spacecraft mass due to maneuver.

updateTransform(Frame, Frame, Transform, AbsoluteDate) - Method in class org.orekit.frames.UpdatableFrame

Update the transform from parent frame implicitly according to two other frames.

UpperBounds - Class in org.orekit.propagation.semianalytical.dsst.utilities

Utility class to compute upper bounds for truncation algorithms.

URANUS - Static variable in class org.orekit.bodies.CelestialBodyFactory

Predefined name for Uranus.

UT1Scale - Class in org.orekit.time

Universal Time 1.

UTCScale - Class in org.orekit.time

Coordinated Universal Time.

UTCTAILoader - Interface in org.orekit.time

Interface for loading UTC-TAI offsets data files.

V

validFrom() - Method in class org.orekit.models.earth.GeoMagneticField

Returns the start of the validity period for this model.

validTo() - Method in class org.orekit.models.earth.GeoMagneticField

Returns the end of the validity period for this model.

value(BodiesElements) - Method in interface org.orekit.data.PoissonSeries.CompiledSeries

Evaluate a set of Poisson series.

value(FieldBodiesElements<S>) - Method in interface org.orekit.data.PoissonSeries.CompiledSeries

Evaluate a set of Poisson series.

value(BodiesElements) - Method in class org.orekit.data.PoissonSeries

Evaluate the value of the series.

value(FieldBodiesElements<T>) - Method in class org.orekit.data.PoissonSeries

Evaluate the value of the series.

value(double) - Method in class org.orekit.data.PolynomialNutation

Evaluate the value of the polynomial.

value(T) - Method in class org.orekit.data.PolynomialNutation

Evaluate the value of the polynomial.

value(AbsoluteDate, Vector3D) - Method in class org.orekit.forces.gravity.HolmesFeatherstoneAttractionModel

Compute the value of the gravity field.

value(AbsoluteDate) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.ShortPeriodicsInterpolatedCoefficient

Compute the value of the coefficient.

value(AbsoluteDate) - Method in interface org.orekit.time.TimeFunction

Compute a function of time.

valueOf(String) - Static method in enum org.orekit.bodies.JPLEphemeridesLoader.EphemerisType

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.data.PolynomialParser.Unit

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.errors.OrekitMessages

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.files.ccsds.CCSDSFrame

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.files.ccsds.CenterName

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.files.ccsds.Keyword

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.files.general.OrbitFile.TimeSystem

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.files.sp3.SP3File.SP3FileType

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.files.sp3.SP3File.SP3OrbitType

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.forces.drag.MarshallSolarActivityFutureEstimation.StrengthLevel

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.forces.gravity.potential.OceanLoadDeformationCoefficients

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.forces.gravity.potential.TideSystem

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.frames.HelmertTransformation.Predefined

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.frames.LOFType

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.frames.Predefined

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.models.earth.GeoMagneticFieldFactory.FieldModel

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.orbits.OrbitType

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.orbits.PositionAngle

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.propagation.events.FilterType

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.propagation.events.handlers.EventHandler.Action

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.time.Month

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.utils.AngularDerivativesFilter

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.utils.CartesianDerivativesFilter

Returns the enum constant of this type with the specified name.

valueOf(String) - Static method in enum org.orekit.utils.IERSConventions

Returns the enum constant of this type with the specified name.

values() - Static method in enum org.orekit.bodies.JPLEphemeridesLoader.EphemerisType

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.data.PolynomialParser.Unit

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.errors.OrekitMessages

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.files.ccsds.CCSDSFrame

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.files.ccsds.CenterName

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.files.ccsds.Keyword

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.files.general.OrbitFile.TimeSystem

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.files.sp3.SP3File.SP3FileType

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.files.sp3.SP3File.SP3OrbitType

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.forces.drag.MarshallSolarActivityFutureEstimation.StrengthLevel

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.forces.gravity.potential.OceanLoadDeformationCoefficients

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.forces.gravity.potential.TideSystem

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.frames.HelmertTransformation.Predefined

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.frames.LOFType

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.frames.Predefined

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.models.earth.GeoMagneticFieldFactory.FieldModel

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.orbits.OrbitType

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.orbits.PositionAngle

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.propagation.events.FilterType

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.propagation.events.handlers.EventHandler.Action

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.time.Month

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.utils.AngularDerivativesFilter

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.utils.CartesianDerivativesFilter

Returns an array containing the constants of this enum type, in the order they are declared.

values() - Static method in enum org.orekit.utils.IERSConventions

Returns an array containing the constants of this enum type, in the order they are declared.

VariableStepInterpolationGrid - Class in org.orekit.propagation.semianalytical.dsst.utilities

Interpolation grid where points are evenly spaced between the start and the end of the integration step.

VariableStepInterpolationGrid(int) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.VariableStepInterpolationGrid

Constructor.

VENUS - Static variable in class org.orekit.bodies.CelestialBodyFactory

Predefined name for Venus.

W

w - Variable in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution

Equinoctial frame w vector.

WGS84_EARTH_ANGULAR_VELOCITY - Static variable in interface org.orekit.utils.Constants

Earth angular velocity from WGS84 model: 7.292115e-5 rad/s.

WGS84_EARTH_C20 - Static variable in interface org.orekit.utils.Constants

Earth un-normalized second zonal coefficient from WGS84 model: .

WGS84_EARTH_EQUATORIAL_RADIUS - Static variable in interface org.orekit.utils.Constants

Earth equatorial radius from WGS84 model: 6378137.0 m.

WGS84_EARTH_FLATTENING - Static variable in interface org.orekit.utils.Constants

Earth flattening from WGS84 model: 1.0 / 298.257223563.

WGS84_EARTH_MU - Static variable in interface org.orekit.utils.Constants

Earth gravitational constant from WGS84 model: 3.986004418e14 m³/s².

withConstantElevation(double) - Method in class org.orekit.propagation.events.ElevationDetector

Setup the minimum elevation for detection.

withConventions(IERSConventions) - Method in class org.orekit.files.ccsds.ODMParser

Set IERS conventions.

withConventions(IERSConventions) - Method in class org.orekit.files.ccsds.OEMParser

Set IERS conventions.

withConventions(IERSConventions) - Method in class org.orekit.files.ccsds.OMMParser

Set IERS conventions.

withConventions(IERSConventions) - Method in class org.orekit.files.ccsds.OPMParser

Set IERS conventions.

withDoodson(int, int) - Method in class org.orekit.data.PoissonSeriesParser

Set up columns for Doodson multiplers and Doodson number.

withElevationMask(ElevationMask) - Method in class org.orekit.propagation.events.ElevationDetector

Setup the elevation mask for detection using the passed in mask object.

withFirstDelaunay(int) - Method in class org.orekit.data.PoissonSeriesParser

Set up first column of Delaunay multiplier.

withFirstPlanetary(int) - Method in class org.orekit.data.PoissonSeriesParser

Set up first column of planetary multiplier.

withGamma(int) - Method in class org.orekit.data.PoissonSeriesParser

Set up column of GMST tide multiplier.

withHandler(EventHandler<T>) - Method in class org.orekit.propagation.events.AbstractDetector

Setup the event handler to call at event occurrences.

withInternationalDesignator(int, int, String) - Method in class org.orekit.files.ccsds.ODMParser

Set international designator.

withInternationalDesignator(int, int, String) - Method in class org.orekit.files.ccsds.OEMParser

Set international designator.

withInternationalDesignator(int, int, String) - Method in class org.orekit.files.ccsds.OMMParser

Set international designator.

withInternationalDesignator(int, int, String) - Method in class org.orekit.files.ccsds.OPMParser

Set international designator.

withMargin(double) - Method in class org.orekit.propagation.events.GeographicZoneDetector

Setup the detector margin.

withMaxCheck(double) - Method in class org.orekit.propagation.events.AbstractDetector

Setup the maximum checking interval.

withMaxIter(int) - Method in class org.orekit.propagation.events.AbstractDetector

Setup the maximum number of iterations in the event time search.

withMissionReferenceDate(AbsoluteDate) - Method in class org.orekit.files.ccsds.ODMParser

Set initial date.

withMissionReferenceDate(AbsoluteDate) - Method in class org.orekit.files.ccsds.OEMParser

Set initial date.

withMissionReferenceDate(AbsoluteDate) - Method in class org.orekit.files.ccsds.OMMParser

Set initial date.

withMissionReferenceDate(AbsoluteDate) - Method in class org.orekit.files.ccsds.OPMParser

Set initial date.

withMu(double) - Method in class org.orekit.files.ccsds.ODMParser

Set gravitational coefficient.

withMu(double) - Method in class org.orekit.files.ccsds.OEMParser

Set gravitational coefficient.

withMu(double) - Method in class org.orekit.files.ccsds.OMMParser

Set gravitational coefficient.

withMu(double) - Method in class org.orekit.files.ccsds.OPMParser

Set gravitational coefficient.

withOptionalColumn(int) - Method in class org.orekit.data.PoissonSeriesParser

Set up optional column.

withPenumbra() - Method in class org.orekit.propagation.events.EclipseDetector

Setup the detector to penumbra detection.

withPolynomialPart(char, PolynomialParser.Unit) - Method in class org.orekit.data.PoissonSeriesParser

Set up polynomial part parsing.

withReferenceFrame(Frame) - Method in class org.orekit.attitudes.Attitude

Get a similar attitude with a specific reference frame.

withRefraction(AtmosphericRefractionModel) - Method in class org.orekit.propagation.events.ElevationDetector

Setup the elevation detector to use an atmospheric refraction model in its calculations.

withSimpleEOP(boolean) - Method in class org.orekit.files.ccsds.ODMParser

Set EOP interpolation method.

withSimpleEOP(boolean) - Method in class org.orekit.files.ccsds.OEMParser

Set EOP interpolation method.

withSimpleEOP(boolean) - Method in class org.orekit.files.ccsds.OMMParser

Set EOP interpolation method.

withSimpleEOP(boolean) - Method in class org.orekit.files.ccsds.OPMParser

Set EOP interpolation method.

withSinCos(int, int, double, int, double) - Method in class org.orekit.data.PoissonSeriesParser

Set up columns of the sine and cosine coefficients.

withThreshold(double) - Method in class org.orekit.propagation.events.AbstractDetector

Setup the convergence threshold.

withUmbra() - Method in class org.orekit.propagation.events.EclipseDetector

Setup the detector to full umbra detection.

X

xl - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator

L from SPTRCK #3.

xmdot - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator

common parameter for mean anomaly (M) computation.

xn0dp - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator

original recovered mean motion.

xnodcf - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator

common parameter for raan (OMEGA) computation.

xnode - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator

final RAAN.

xnodot - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator

common parameter for raan (OMEGA) computation.

Y

YawCompensation - Class in org.orekit.attitudes

This class handles yaw compensation attitude provider.

YawCompensation(GroundPointing) - Constructor for class org.orekit.attitudes.YawCompensation

Creates a new instance.

YawSteering - Class in org.orekit.attitudes

This class handles yaw steering law.

YawSteering(GroundPointing, PVCoordinatesProvider, Vector3D) - Constructor for class org.orekit.attitudes.YawSteering

Creates a new instance.

Z

ZERO - Static variable in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenUtilities

0 represented as a polynomial.

ZERO - Static variable in class org.orekit.utils.PVCoordinates

Fixed position/velocity at origin (both p, v and a are zero vectors).

ZIP_ARCHIVE_PATTERN - Static variable in interface org.orekit.data.DataProvider

Pattern for name of zip/jar archives.

ZipJarCrawler - Class in org.orekit.data

Helper class for loading data files from a zip/jar archive.

ZipJarCrawler(File) - Constructor for class org.orekit.data.ZipJarCrawler

Build a zip crawler for an archive file on filesystem.

ZipJarCrawler(String) - Constructor for class org.orekit.data.ZipJarCrawler

Build a zip crawler for an archive file in classpath.

ZipJarCrawler(ClassLoader, String) - Constructor for class org.orekit.data.ZipJarCrawler

Build a zip crawler for an archive file in classpath.

ZipJarCrawler(URL) - Constructor for class org.orekit.data.ZipJarCrawler

Build a zip crawler for an archive file on network.

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