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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<? super T>) - Constructor for class org.orekit.propagation.events.AbstractDetector
Build a new instance.
AbstractForceModel - Class in org.orekit.forces
Base class for force models.
AbstractForceModel() - Constructor for class org.orekit.forces.AbstractForceModel
 
AbstractGaussianContribution - Class in org.orekit.propagation.semianalytical.dsst.forces
Common handling of DSSTForceModel methods for Gaussian contributions to DSST propagation.
AbstractGaussianContribution(String, 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(ODEIntegrator, 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).
AbstractMeasurement<T extends ObservedMeasurement<T>> - Class in org.orekit.estimation.measurements
Abstract class handling measurements boilerplate.
AbstractMeasurement(AbsoluteDate, double, double, double, List<Integer>, ParameterDriver...) - Constructor for class org.orekit.estimation.measurements.AbstractMeasurement
Simple constructor for mono-dimensional measurements.
AbstractMeasurement(AbsoluteDate, double[], double[], double[], List<Integer>, ParameterDriver...) - Constructor for class org.orekit.estimation.measurements.AbstractMeasurement
Simple constructor, for multi-dimensional measurements.
AbstractParametricAcceleration - Class in org.orekit.forces
This class implements a parametric acceleration.
AbstractParametricAcceleration(Vector3D, boolean, AttitudeProvider) - Constructor for class org.orekit.forces.AbstractParametricAcceleration
Simple constructor.
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.
AbstractPropagatorBuilder - Class in org.orekit.propagation.conversion
Base class for propagator builders.
AbstractPropagatorBuilder(Orbit, PositionAngle, double, boolean) - Constructor for class org.orekit.propagation.conversion.AbstractPropagatorBuilder
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.
acceleration(SpacecraftState, double[]) - Method in class org.orekit.forces.AbstractParametricAcceleration
Compute acceleration.
acceleration(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.AbstractParametricAcceleration
Compute acceleration.
acceleration(SpacecraftState, double[]) - Method in class org.orekit.forces.drag.DragForce
Compute acceleration.
acceleration(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.drag.DragForce
Compute acceleration.
acceleration(SpacecraftState, double[]) - Method in interface org.orekit.forces.ForceModel
Compute acceleration.
acceleration(FieldSpacecraftState<T>, T[]) - Method in interface org.orekit.forces.ForceModel
Compute acceleration.
acceleration(SpacecraftState, double[]) - Method in class org.orekit.forces.gravity.HolmesFeatherstoneAttractionModel
Compute acceleration.
acceleration(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.gravity.HolmesFeatherstoneAttractionModel
Compute acceleration.
acceleration(SpacecraftState, double[]) - Method in class org.orekit.forces.gravity.NewtonianAttraction
Compute acceleration.
acceleration(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.gravity.NewtonianAttraction
Compute acceleration.
acceleration(SpacecraftState, double[]) - Method in class org.orekit.forces.gravity.OceanTides
Compute acceleration.
acceleration(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.gravity.OceanTides
Compute acceleration.
acceleration(SpacecraftState, double[]) - Method in class org.orekit.forces.gravity.Relativity
Compute acceleration.
acceleration(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.gravity.Relativity
Compute acceleration.
acceleration(SpacecraftState, double[]) - Method in class org.orekit.forces.gravity.SolidTides
Compute acceleration.
acceleration(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.gravity.SolidTides
Compute acceleration.
acceleration(SpacecraftState, double[]) - Method in class org.orekit.forces.gravity.ThirdBodyAttraction
Compute acceleration.
acceleration(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.gravity.ThirdBodyAttraction
Compute acceleration.
acceleration(SpacecraftState, double[]) - Method in class org.orekit.forces.maneuvers.ConstantThrustManeuver
Compute acceleration.
acceleration(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.maneuvers.ConstantThrustManeuver
Compute acceleration.
acceleration(SpacecraftState, double[]) - Method in class org.orekit.forces.radiation.SolarRadiationPressure
Compute acceleration.
acceleration(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.radiation.SolarRadiationPressure
Compute acceleration.
acceptStep(OrekitStepInterpolator, AbsoluteDate, double) - Method in class org.orekit.propagation.analytical.AbstractAnalyticalPropagator
Accept a step, triggering events and step handlers.
acceptStep(FieldAbstractAnalyticalPropagator<T>.FieldBasicStepInterpolator, FieldAbsoluteDate<T>, double) - Method in class org.orekit.propagation.analytical.FieldAbstractAnalyticalPropagator
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(FieldOrekitStepHandler<T>) - Method in class org.orekit.propagation.sampling.FieldOrekitStepHandlerMultiplexer
Add a step handler.
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.
add(ParameterDriver) - Method in class org.orekit.utils.ParameterDriversList
Add a driver.
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.
addAdditionalEquations(FieldAdditionalEquations<T>) - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator
Add a set of user-specified equations to be integrated along with the orbit propagation.
addAdditionalState(String, T...) - Method in class org.orekit.propagation.FieldSpacecraftState
Add an additional state.
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(FieldAdditionalStateProvider<T>) - Method in class org.orekit.propagation.FieldAbstractPropagator
Add a set of user-specified state parameters to be computed along with the orbit propagation.
addAdditionalStateProvider(FieldAdditionalStateProvider<T>) - Method in interface org.orekit.propagation.FieldPropagator
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 interface org.orekit.forces.ForceModel
Compute the contribution of the force model to the perturbing acceleration.
addContribution(FieldSpacecraftState<T>, FieldTimeDerivativesEquations<T>) - 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.NewtonianAttraction
Compute the contribution of the force model to the perturbing acceleration.
addContribution(FieldSpacecraftState<T>, FieldTimeDerivativesEquations<T>) - Method in class org.orekit.forces.gravity.NewtonianAttraction
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.maneuvers.ConstantThrustManeuver
Compute the contribution of the force model to the perturbing acceleration.
addContribution(FieldSpacecraftState<T>, FieldTimeDerivativesEquations<T>) - Method in class org.orekit.forces.maneuvers.ConstantThrustManeuver
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.
addDefaultUTCTAIOffsetsLoaders() - Static method in class org.orekit.time.TimeScalesFactory
Add the default loaders for UTC-TAI offsets history files (both IERS and USNO).
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.
addEventDate(FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.events.FieldDateDetector
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(D) - Method in class org.orekit.propagation.analytical.FieldAbstractAnalyticalPropagator
Add an event detector.
addEventDetector(D) - Method in class org.orekit.propagation.FieldAbstractPropagator
Add an event detector.
addEventDetector(D) - Method in interface org.orekit.propagation.FieldPropagator
Add an event detector.
addEventDetector(EventDetector) - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
Add an event detector.
addEventDetector(D) - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator
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.FieldNumericalPropagator
Add a force model to the global perturbation model.
addForceModel(ForceModel) - Method in class org.orekit.propagation.numerical.NumericalPropagator
Add a force 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, T[]) - Method in class org.orekit.orbits.FieldCartesianOrbit
Add the contribution of the Keplerian motion to parameters derivatives
addKeplerContribution(PositionAngle, double, T[]) - Method in class org.orekit.orbits.FieldCircularOrbit
Add the contribution of the Keplerian motion to parameters derivatives
addKeplerContribution(PositionAngle, double, T[]) - Method in class org.orekit.orbits.FieldEquinoctialOrbit
Add the contribution of the Keplerian motion to parameters derivatives
addKeplerContribution(PositionAngle, double, T[]) - Method in class org.orekit.orbits.FieldKeplerianOrbit
Add the contribution of the Keplerian motion to parameters derivatives
addKeplerContribution(PositionAngle, double, T[]) - Method in class org.orekit.orbits.FieldOrbit
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.FieldTimeDerivativesEquations
Add the contribution of the Kepler evolution.
addKeplerContribution(double) - Method in interface org.orekit.propagation.numerical.TimeDerivativesEquations
Add the contribution of the Kepler evolution.
addMassDerivative(T) - Method in interface org.orekit.propagation.numerical.FieldTimeDerivativesEquations
Add the contribution of the flow rate (dm/dt).
addMassDerivative(double) - Method in interface org.orekit.propagation.numerical.TimeDerivativesEquations
Add the contribution of the flow rate (dm/dt).
addMeasurement(ObservedMeasurement<?>) - Method in class org.orekit.estimation.leastsquares.BatchLSEstimator
Add a measurement.
addModifier(EstimationModifier<T>) - Method in class org.orekit.estimation.measurements.AbstractMeasurement
Add a modifier.
addModifier(EstimationModifier<T>) - Method in interface org.orekit.estimation.measurements.ObservedMeasurement
Add a modifier.
addNewSegment(List<SpacecraftState>) - Method in class org.orekit.files.general.OrekitEphemerisFile.OrekitSatelliteEphemeris
Injects pre-computed satellite states into this ephemeris file object, returning the generated OrekitEphemerisFile.OrekitEphemerisSegment that has been stored internally.
addNewSegment(List<SpacecraftState>, int) - Method in class org.orekit.files.general.OrekitEphemerisFile.OrekitSatelliteEphemeris
Injects pre-computed satellite states into this ephemeris file object, returning the generated OrekitEphemerisFile.OrekitEphemerisSegment that has been stored internally.
addNewSegment(List<SpacecraftState>, CelestialBody, int) - Method in class org.orekit.files.general.OrekitEphemerisFile.OrekitSatelliteEphemeris
Injects pre-computed satellite states into this ephemeris file object, returning the generated OrekitEphemerisFile.OrekitEphemerisSegment that has been stored internally.
addNonKeplerianAcceleration(FieldVector3D<T>) - Method in interface org.orekit.propagation.numerical.FieldTimeDerivativesEquations
Add the contribution of an acceleration expressed in some inertial frame.
addNonKeplerianAcceleration(Vector3D) - Method in interface org.orekit.propagation.numerical.TimeDerivativesEquations
Add the contribution of a non-Keplerian acceleration.
addObservation(TDMFile.Observation) - Method in class org.orekit.files.ccsds.TDMFile.ObservationsBlock
Adds an observation data line.
addObservation(String, AbsoluteDate, double) - Method in class org.orekit.files.ccsds.TDMFile.ObservationsBlock
Adds an observation data line.
addObservationComment(String) - Method in class org.orekit.files.ccsds.TDMFile.ObservationsBlock
Add an observation data line comment.
addObservationsBlock() - Method in class org.orekit.files.ccsds.TDMFile
Add a block to the list of observations blocks.
addObserver(ParameterObserver) - Method in class org.orekit.utils.ParameterDriver
Add an observer for this driver.
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.
addParticipant(int, String) - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData
Adds a participant to the list.
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.
addReceiveDelay(int, double) - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData
Adds a receive delay to the list.
addSatellite(String) - Method in class org.orekit.files.general.OrekitEphemerisFile
Adds a new satellite to this object.
addSatellite(String) - Method in class org.orekit.files.sp3.SP3File
Add a new satellite with a given identifier to the list of stored satellites.
addSupportedParameter(ParameterDriver) - Method in class org.orekit.propagation.conversion.AbstractPropagatorBuilder
Add a supported parameter.
addSwitchingCondition(AttitudeProvider, AttitudeProvider, T, boolean, boolean, double, AngularDerivativesFilter, AttitudesSequence.SwitchHandler) - Method in class org.orekit.attitudes.AttitudesSequence
Add a switching condition between two attitude providers.
addTransmitDelay(int, double) - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData
Adds a transmit delay to the list.
addUTCTAIOffsetsLoader(UTCTAIOffsetsLoader) - Static method in class org.orekit.time.TimeScalesFactory
Add a loader for UTC-TAI offsets history files.
addValidAfter(T, FieldAbsoluteDate<D>) - Method in class org.orekit.utils.FieldTimeSpanMap
Add an entry valid after a limit date.
addValidAfter(T, AbsoluteDate) - Method in class org.orekit.utils.TimeSpanMap
Add an entry valid after a limit date.
addValidBefore(T, FieldAbsoluteDate<D>) - Method in class org.orekit.utils.FieldTimeSpanMap
Add an entry valid before a limit date.
addValidBefore(T, AbsoluteDate) - Method in class org.orekit.utils.TimeSpanMap
Add an entry valid before a limit date.
addWaveCoefficients(int, int, int, double, double, double, double, int, String) - Method in class org.orekit.forces.gravity.potential.OceanTidesReader
Add parsed coefficients.
afterIntegration() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
Method called just after integration.
afterIntegration() - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator
Method called just after integration.
afterIntegration() - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator
Method called just after integration.
AggregateBoundedPropagator - Class in org.orekit.propagation.analytical
A BoundedPropagator that covers a larger time span from several constituent propagators that cover shorter time spans.
AggregateBoundedPropagator(Collection<? extends BoundedPropagator>) - Constructor for class org.orekit.propagation.analytical.AggregateBoundedPropagator
Create a propagator by concatenating several BoundedPropagators.
AlignmentDetector - Class in org.orekit.propagation.events
Finder for satellite/body alignment events in orbital plane.
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.
alongTileDirection(Vector3D, GeodeticPoint) - Method in class org.orekit.models.earth.tessellation.AlongTrackAiming
Find the along tile direction for tessellation at specified point.
alongTileDirection(Vector3D, GeodeticPoint) - Method in class org.orekit.models.earth.tessellation.ConstantAzimuthAiming
Find the along tile direction for tessellation at specified point.
alongTileDirection(Vector3D, GeodeticPoint) - Method in interface org.orekit.models.earth.tessellation.TileAiming
Find the along tile direction for tessellation at specified point.
AlongTrackAiming - Class in org.orekit.models.earth.tessellation
Class used to orient tiles along an orbit track.
AlongTrackAiming(OneAxisEllipsoid, Orbit, boolean) - Constructor for class org.orekit.models.earth.tessellation.AlongTrackAiming
Simple constructor.
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.
andCombine(EventDetector...) - Static method in class org.orekit.propagation.events.BooleanDetector
Create a new event detector that is the logical AND of the given event detectors.
andCombine(Collection<? extends EventDetector>) - Static method in class org.orekit.propagation.events.BooleanDetector
Create a new event detector that is the logical AND of the given event detectors.
AngularAzEl - Class in org.orekit.estimation.measurements
Class modeling an Azimuth-Elevation measurement from a ground station.
AngularAzEl(GroundStation, AbsoluteDate, double[], double[], double[]) - Constructor for class org.orekit.estimation.measurements.AngularAzEl
Simple constructor.
AngularAzEl(GroundStation, AbsoluteDate, double[], double[], double[], int) - Constructor for class org.orekit.estimation.measurements.AngularAzEl
Simple constructor.
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.
AngularIonosphericDelayModifier - Class in org.orekit.estimation.measurements.modifiers
Class modifying theoretical angular measurement with ionospheric delay.
AngularIonosphericDelayModifier(IonosphericModel) - Constructor for class org.orekit.estimation.measurements.modifiers.AngularIonosphericDelayModifier
Constructor.
AngularRaDec - Class in org.orekit.estimation.measurements
Class modeling an Right Ascension - Declination measurement from a ground point (station, telescope).
AngularRaDec(GroundStation, Frame, AbsoluteDate, double[], double[], double[]) - Constructor for class org.orekit.estimation.measurements.AngularRaDec
Simple constructor.
AngularRaDec(GroundStation, Frame, AbsoluteDate, double[], double[], double[], int) - Constructor for class org.orekit.estimation.measurements.AngularRaDec
Simple constructor.
AngularRadioRefractionModifier - Class in org.orekit.estimation.measurements.modifiers
Class modifying theoretical angular measurement with ionospheric radio refractive index.
AngularRadioRefractionModifier(AtmosphericRefractionModel) - Constructor for class org.orekit.estimation.measurements.modifiers.AngularRadioRefractionModifier
Constructor.
AngularSeparationDetector - Class in org.orekit.propagation.events
Detects when spacecraft comes close to a moving beacon, as seen from a moving observer.
AngularSeparationDetector(PVCoordinatesProvider, PVCoordinatesProvider, double) - Constructor for class org.orekit.propagation.events.AngularSeparationDetector
Build a new angular separation detector.
AngularTroposphericDelayModifier - Class in org.orekit.estimation.measurements.modifiers
Class modifying theoretical angular measurement with tropospheric delay.
AngularTroposphericDelayModifier(TroposphericModel) - Constructor for class org.orekit.estimation.measurements.modifiers.AngularTroposphericDelayModifier
Constructor.
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.
applyTo(FieldPVCoordinates<T>) - Method in class org.orekit.utils.AngularCoordinates
Apply the rotation to a pv coordinates.
applyTo(TimeStampedFieldPVCoordinates<T>) - Method in class org.orekit.utils.AngularCoordinates
Apply the rotation to a pv coordinates.
applyTo(PVCoordinates) - Method in class org.orekit.utils.FieldAngularCoordinates
Apply the rotation to a pv coordinates.
applyTo(TimeStampedPVCoordinates) - Method in class org.orekit.utils.FieldAngularCoordinates
Apply the rotation to a pv coordinates.
applyTo(FieldPVCoordinates<T>) - Method in class org.orekit.utils.FieldAngularCoordinates
Apply the rotation to a pv coordinates.
applyTo(TimeStampedFieldPVCoordinates<T>) - Method in class org.orekit.utils.FieldAngularCoordinates
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 Hf.
AstronomicalAmplitudeReader(String, int, int, int, double) - Constructor for class org.orekit.forces.gravity.potential.AstronomicalAmplitudeReader
Simple constructor.
Atmosphere - Interface in org.orekit.forces.drag.atmosphere
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.atmosphere.DTM2000
Identifier for atomic nitrogen.
ATOMIC_OXYGEN - Static variable in class org.orekit.forces.drag.atmosphere.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.
attitudeProvider(AttitudeProvider) - Method in class org.orekit.propagation.analytical.gnss.GPSPropagator.Builder
Sets the attitude provider.
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.
AttitudesSequence.SwitchHandler - Interface in org.orekit.attitudes
Interface for attitude switch notifications.
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(FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.analytical.FieldAbstractAnalyticalPropagator
Propagate an orbit without any fancy features.
basicPropagate(FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.integration.FieldIntegratedEphemeris
Propagate an orbit without any fancy features.
basicPropagate(AbsoluteDate) - Method in class org.orekit.propagation.integration.IntegratedEphemeris
Propagate an orbit without any fancy features.
BatchLSEstimator - Class in org.orekit.estimation.leastsquares
Least squares estimator for orbit determination.
BatchLSEstimator(LeastSquaresOptimizer, NumericalPropagatorBuilder...) - Constructor for class org.orekit.estimation.leastsquares.BatchLSEstimator
Simple constructor.
BatchLSObserver - Interface in org.orekit.estimation.leastsquares
Observer for batch least squares estimator iterations.
beforeIntegration(SpacecraftState, AbsoluteDate) - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
Method called just before integration.
beforeIntegration(FieldSpacecraftState<T>, FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator
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.
Bias<T extends ObservedMeasurement<T>> - Class in org.orekit.estimation.measurements.modifiers
Class modeling a measurement bias.
Bias(String[], double[], double[], double[], double[]) - Constructor for class org.orekit.estimation.measurements.modifiers.Bias
Simple constructor.
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, 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, Ellipsoid) - 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.
BooleanDetector - Class in org.orekit.propagation.events
This class provides AND and OR operations for event detectors.
BoundedPropagator - Interface in org.orekit.propagation
This interface is intended for ephemerides valid only during a time range.
BoxAndSolarArraySpacecraft - Class in org.orekit.forces
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 lighting of solar array.
BoxAndSolarArraySpacecraft(double, double, double, PVCoordinatesProvider, double, Vector3D, double, double, double, double) - Constructor for class org.orekit.forces.BoxAndSolarArraySpacecraft
Build a spacecraft model with best lighting 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 lighting of solar array.
BoxAndSolarArraySpacecraft(BoxAndSolarArraySpacecraft.Facet[], PVCoordinatesProvider, double, Vector3D, double, double, double, double) - Constructor for class org.orekit.forces.BoxAndSolarArraySpacecraft
Build a spacecraft model with best lighting 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(double, double, double, PVCoordinatesProvider, double, Vector3D, AbsoluteDate, Vector3D, double, 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(BoxAndSolarArraySpacecraft.Facet[], PVCoordinatesProvider, double, Vector3D, AbsoluteDate, Vector3D, double, 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.
build() - Method in class org.orekit.propagation.analytical.gnss.GPSPropagator.Builder
Finalizes the build.
Builder(GPSOrbitalElements) - Constructor for class org.orekit.propagation.analytical.gnss.GPSPropagator.Builder
Initializes the builder.
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, OrbitType) - Method in class org.orekit.propagation.conversion.AdamsBashforthIntegratorBuilder
Build a first order integrator.
buildIntegrator(Orbit, OrbitType) - Method in class org.orekit.propagation.conversion.AdamsMoultonIntegratorBuilder
Build a first order integrator.
buildIntegrator(Orbit, OrbitType) - Method in class org.orekit.propagation.conversion.ClassicalRungeKuttaIntegratorBuilder
Build a first order integrator.
buildIntegrator(Orbit, OrbitType) - Method in class org.orekit.propagation.conversion.DormandPrince54IntegratorBuilder
Build a first order integrator.
buildIntegrator(Orbit, OrbitType) - Method in class org.orekit.propagation.conversion.DormandPrince853IntegratorBuilder
Build a first order integrator.
buildIntegrator(Orbit, OrbitType) - Method in class org.orekit.propagation.conversion.EulerIntegratorBuilder
Build a first order integrator.
buildIntegrator(Orbit, OrbitType) - Method in class org.orekit.propagation.conversion.GillIntegratorBuilder
Build a first order integrator.
buildIntegrator(Orbit, OrbitType) - Method in class org.orekit.propagation.conversion.GraggBulirschStoerIntegratorBuilder
Build a first order integrator.
buildIntegrator(Orbit, OrbitType) - Method in class org.orekit.propagation.conversion.HighamHall54IntegratorBuilder
Build a first order integrator.
buildIntegrator(Orbit, OrbitType) - Method in class org.orekit.propagation.conversion.LutherIntegratorBuilder
Build a first order integrator.
buildIntegrator(Orbit, OrbitType) - Method in class org.orekit.propagation.conversion.MidpointIntegratorBuilder
Build a first order integrator.
buildIntegrator(Orbit, OrbitType) - Method in interface org.orekit.propagation.conversion.ODEIntegratorBuilder
Build a first order integrator.
buildIntegrator(Orbit, OrbitType) - Method in class org.orekit.propagation.conversion.ThreeEighthesIntegratorBuilder
Build a first order integrator.
buildPropagator(double[]) - Method in class org.orekit.propagation.conversion.EcksteinHechlerPropagatorBuilder
Build a propagator.
buildPropagator(double[]) - Method in class org.orekit.propagation.conversion.KeplerianPropagatorBuilder
Build a propagator.
buildPropagator(double[]) - Method in class org.orekit.propagation.conversion.NumericalPropagatorBuilder
Build a propagator.
buildPropagator(double[]) - Method in interface org.orekit.propagation.conversion.PropagatorBuilder
Build a propagator.
buildPropagator(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.
buildSimpleZone(double, double[]...) - Static method in class org.orekit.models.earth.tessellation.EllipsoidTessellator
Build a simple zone (connected zone without holes).
buildSimpleZone(double, GeodeticPoint...) - Static method in class org.orekit.models.earth.tessellation.EllipsoidTessellator
Build a simple zone (connected zone without holes).
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
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.
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.
CCSDS_OEM_VERS - Static variable in class org.orekit.files.ccsds.OEMWriter
Version number implemented.
CCSDS_OEM_VERS - Static variable in class org.orekit.files.ccsds.StreamingOemWriter
Version number implemented.
CCSDSFrame - Enum in org.orekit.files.ccsds
Frames used in CCSDS Orbit Data Messages.
CcsdsModifiedFrame - Class in org.orekit.files.ccsds
A reference frame created from the REF_FRAME and CENTER_NAME is a CCSDS OPM, OMM, or OEM file.
CcsdsTimeScale - Enum in org.orekit.files.ccsds
The set of time scales defined in Annex A of the ODM CCSDS standard 502.0-B-2.
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.
checkTimeSystems() - Method in class org.orekit.files.ccsds.TDMFile
Check that, according to the CCSDS standard, every ObservationsBlock has the same time system.
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, double, double, double, double, double, double, PositionAngle, Frame, AbsoluteDate, 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.
circularToPosition(T, T, T, T, T, T, double) - Static method in class org.orekit.orbits.FieldCircularOrbit
Compute position from circular parameters.
CjSjCoefficient - Class in org.orekit.propagation.semianalytical.dsst.utilities
Compute the Sj(k, h) and the Cj(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
Cj(k, h) and Sj(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.
clear() - Method in class org.orekit.propagation.events.handlers.RecordAndContinue
Clear all stored events.
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.analytical.FieldAbstractAnalyticalPropagator
Remove all events detectors.
clearEventsDetectors() - Method in class org.orekit.propagation.FieldAbstractPropagator
Remove all events detectors.
clearEventsDetectors() - Method in interface org.orekit.propagation.FieldPropagator
Remove all events detectors.
clearEventsDetectors() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
Remove all events detectors.
clearEventsDetectors() - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator
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.
clearLoggedEvents() - Method in class org.orekit.propagation.events.FieldEventsLogger
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.
clearUTCTAIOffsetsLoaders() - 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.NSKey - Class in org.orekit.propagation.semianalytical.dsst.utilities
Key formed by two integer values.
compare(TimeStamped, TimeStamped) - Method in class org.orekit.time.ChronologicalComparator
Compare two time-stamped instances.
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(FieldAbsoluteDate<T>) - Method in class org.orekit.time.FieldAbsoluteDate
Compare the instance with another date.
compareTo(TimeComponents) - Method in class org.orekit.time.TimeComponents
compile(PoissonSeries...) - Static method in class org.orekit.data.PoissonSeries
Join several nutation series, for fast simultaneous evaluation.
complainIfNotSupported(String) - Method in class org.orekit.forces.AbstractForceModel
Complain if a parameter is not supported.
compute(AbsoluteDate, List<Propagator>) - Method in class org.orekit.gnss.DOPComputer
Compute the DOP at a given date for a set of GNSS spacecrafts.
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(FieldSpacecraftState<T>) - Method in interface org.orekit.propagation.integration.FieldAbstractIntegratedPropagator.MainStateEquations
Compute differential equations for main state.
computeDerivatives(FieldSpacecraftState<T>, T[]) - Method in interface org.orekit.propagation.integration.FieldAdditionalEquations
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 Gs and Hs 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.FieldCartesianOrbit
 
computeJacobianEccentricWrtCartesian() - Method in class org.orekit.orbits.FieldCircularOrbit
Compute the Jacobian of the orbital parameters with eccentric angle with respect to the Cartesian parameters.
computeJacobianEccentricWrtCartesian() - Method in class org.orekit.orbits.FieldEquinoctialOrbit
Compute the Jacobian of the orbital parameters with eccentric angle with respect to the Cartesian parameters.
computeJacobianEccentricWrtCartesian() - Method in class org.orekit.orbits.FieldKeplerianOrbit
Compute the Jacobian of the orbital parameters with eccentric angle with respect to the Cartesian parameters.
computeJacobianEccentricWrtCartesian() - Method in class org.orekit.orbits.FieldOrbit
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.FieldCartesianOrbit
 
computeJacobianMeanWrtCartesian() - Method in class org.orekit.orbits.FieldCircularOrbit
Compute the Jacobian of the orbital parameters with mean angle with respect to the Cartesian parameters.
computeJacobianMeanWrtCartesian() - Method in class org.orekit.orbits.FieldEquinoctialOrbit
Compute the Jacobian of the orbital parameters with mean angle with respect to the Cartesian parameters.
computeJacobianMeanWrtCartesian() - Method in class org.orekit.orbits.FieldKeplerianOrbit
Compute the Jacobian of the orbital parameters with mean angle with respect to the Cartesian parameters.
computeJacobianMeanWrtCartesian() - Method in class org.orekit.orbits.FieldOrbit
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.FieldCartesianOrbit
 
computeJacobianTrueWrtCartesian() - Method in class org.orekit.orbits.FieldCircularOrbit
Compute the Jacobian of the orbital parameters with true angle with respect to the Cartesian parameters.
computeJacobianTrueWrtCartesian() - Method in class org.orekit.orbits.FieldEquinoctialOrbit
Compute the Jacobian of the orbital parameters with true angle with respect to the Cartesian parameters.
computeJacobianTrueWrtCartesian() - Method in class org.orekit.orbits.FieldKeplerianOrbit
Compute the Jacobian of the orbital parameters with true angle with respect to the Cartesian parameters.
computeJacobianTrueWrtCartesian() - Method in class org.orekit.orbits.FieldOrbit
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, AttitudeProvider, Collection<DSSTForceModel>) - Static method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator
Conversion from osculating to mean orbit.
computeOsculatingState(SpacecraftState, AttitudeProvider, 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 Qn,s coefficients evaluated at γ from the recurrence formula 2.8.3-(2).
computeVns(int) - Static method in class org.orekit.propagation.semianalytical.dsst.utilities.CoefficientsFactory
Compute the Vn,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.
ConstantAzimuthAiming - Class in org.orekit.models.earth.tessellation
Class used to orient tiles with respect to a geographic azimuth.
ConstantAzimuthAiming(OneAxisEllipsoid, double) - Constructor for class org.orekit.models.earth.tessellation.ConstantAzimuthAiming
Simple constructor.
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.
ConstantThrustManeuver(AbsoluteDate, double, double, double, Vector3D, String) - Constructor for class org.orekit.forces.maneuvers.ConstantThrustManeuver
Simple constructor for a constant direction and constant thrust.
contains(String) - Static method in enum org.orekit.files.ccsds.CcsdsTimeScale
Check if timeScale is one of the values supported by this enum.
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, List<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, List<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, List<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, List<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.
convertType(FieldOrbit<T>) - 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<? super ImpulseManeuver<T>>) - Method in class org.orekit.forces.maneuvers.ImpulseManeuver
Build a new instance.
create(OneAxisEllipsoid, GeodeticPoint) - Static method in class org.orekit.gnss.DOPComputer
Creates a DOP computer for one location.
create(double, double, int, EventHandler<? super T>) - Method in class org.orekit.propagation.events.AbstractDetector
Build a new instance.
create(double, double, int, EventHandler<? super AlignmentDetector>) - Method in class org.orekit.propagation.events.AlignmentDetector
Build a new instance.
create(double, double, int, EventHandler<? super AltitudeDetector>) - Method in class org.orekit.propagation.events.AltitudeDetector
Build a new instance.
create(double, double, int, EventHandler<? super AngularSeparationDetector>) - Method in class org.orekit.propagation.events.AngularSeparationDetector
Build a new instance.
create(double, double, int, EventHandler<? super ApsideDetector>) - Method in class org.orekit.propagation.events.ApsideDetector
Build a new instance.
create(double, double, int, EventHandler<? super BooleanDetector>) - Method in class org.orekit.propagation.events.BooleanDetector
 
create(double, double, int, EventHandler<? super CircularFieldOfViewDetector>) - Method in class org.orekit.propagation.events.CircularFieldOfViewDetector
Build a new instance.
create(double, double, int, EventHandler<? super DateDetector>) - Method in class org.orekit.propagation.events.DateDetector
Build a new instance.
create(double, double, int, EventHandler<? super EclipseDetector>) - Method in class org.orekit.propagation.events.EclipseDetector
Build a new instance.
create(double, double, int, EventHandler<? super ElevationDetector>) - Method in class org.orekit.propagation.events.ElevationDetector
Build a new instance.
create(double, double, int, EventHandler<? super ElevationExtremumDetector>) - Method in class org.orekit.propagation.events.ElevationExtremumDetector
Build a new instance.
create(double, double, int, EventHandler<? super EventEnablingPredicateFilter<T>>) - Method in class org.orekit.propagation.events.EventEnablingPredicateFilter
Build a new instance.
create(double, double, int, EventHandler<? super EventShifter<T>>) - Method in class org.orekit.propagation.events.EventShifter
Build a new instance.
create(double, double, int, EventHandler<? super EventSlopeFilter<T>>) - Method in class org.orekit.propagation.events.EventSlopeFilter
Build a new instance.
create(T, T, int, FieldEventHandler<? super D, T>) - Method in class org.orekit.propagation.events.FieldAbstractDetector
Build a new instance.
create(T, T, int, FieldEventHandler<? super FieldAltitudeDetector<T>, T>) - Method in class org.orekit.propagation.events.FieldAltitudeDetector
Build a new instance.
create(T, T, int, FieldEventHandler<? super FieldApsideDetector<T>, T>) - Method in class org.orekit.propagation.events.FieldApsideDetector
Build a new instance.
create(T, T, int, FieldEventHandler<? super FieldDateDetector<T>, T>) - Method in class org.orekit.propagation.events.FieldDateDetector
Build a new instance.
create(T, T, int, FieldEventHandler<? super FieldEclipseDetector<T>, T>) - Method in class org.orekit.propagation.events.FieldEclipseDetector
Build a new instance.
create(T, T, int, FieldEventHandler<? super FieldElevationDetector<T>, T>) - Method in class org.orekit.propagation.events.FieldElevationDetector
Build a new instance.
create(T, T, int, FieldEventHandler<? super FieldNodeDetector<T>, T>) - Method in class org.orekit.propagation.events.FieldNodeDetector
Build a new instance.
create(double, double, int, EventHandler<? super FieldOfViewDetector>) - Method in class org.orekit.propagation.events.FieldOfViewDetector
Build a new instance.
create(double, double, int, EventHandler<? super FootprintOverlapDetector>) - Method in class org.orekit.propagation.events.FootprintOverlapDetector
Build a new instance.
create(double, double, int, EventHandler<? super GeographicZoneDetector>) - Method in class org.orekit.propagation.events.GeographicZoneDetector
Build a new instance.
create(double, double, int, EventHandler<? super GroundFieldOfViewDetector>) - Method in class org.orekit.propagation.events.GroundFieldOfViewDetector
Build a new instance.
create(double, double, int, EventHandler<? super LatitudeCrossingDetector>) - Method in class org.orekit.propagation.events.LatitudeCrossingDetector
Build a new instance.
create(double, double, int, EventHandler<? super LatitudeExtremumDetector>) - Method in class org.orekit.propagation.events.LatitudeExtremumDetector
Build a new instance.
create(double, double, int, EventHandler<? super LongitudeCrossingDetector>) - Method in class org.orekit.propagation.events.LongitudeCrossingDetector
Build a new instance.
create(double, double, int, EventHandler<? super LongitudeExtremumDetector>) - Method in class org.orekit.propagation.events.LongitudeExtremumDetector
Build a new instance.
create(double, double, int, EventHandler<? super NegateDetector>) - Method in class org.orekit.propagation.events.NegateDetector
 
create(double, double, int, EventHandler<? super NodeDetector>) - Method in class org.orekit.propagation.events.NodeDetector
Build a new instance.
create(double, double, int, EventHandler<? super PositionAngleDetector>) - Method in class org.orekit.propagation.events.PositionAngleDetector
Build a new instance.
createBesselianEpoch(double) - Static method in class org.orekit.time.AbsoluteDate
Build an instance corresponding to a Besselian Epoch (BE).
createBesselianEpoch(T) - Static method in class org.orekit.time.FieldAbsoluteDate
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.
createFromModifiedRodrigues(T[][]) - Static method in class org.orekit.utils.FieldAngularCoordinates
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.
createGPSDate(int, T) - Static method in class org.orekit.time.FieldAbsoluteDate
Build an instance corresponding to a GPS date.
createInitialOrbit() - Method in class org.orekit.propagation.conversion.AbstractPropagatorBuilder
Build an initial orbit using the current selected parameters.
createJDDate(int, double, TimeScale) - Static method in class org.orekit.time.AbsoluteDate
Build an instance corresponding to a Julian Day date.
createJDDate(int, T, TimeScale) - Static method in class org.orekit.time.FieldAbsoluteDate
Build an instance corresponding to a Julian Day date.
createJulianEpoch(double) - Static method in class org.orekit.time.AbsoluteDate
Build an instance corresponding to a Julian Epoch (JE).
createJulianEpoch(T) - Static method in class org.orekit.time.FieldAbsoluteDate
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(FieldAbsoluteDate<T>, double, OrbitType, PositionAngle, AttitudeProvider, Frame) - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator
Create a mapper between raw double components and spacecraft state.
createMapper(FieldAbsoluteDate<T>, double, OrbitType, PositionAngle, AttitudeProvider, Frame) - Method in class org.orekit.propagation.numerical.FieldNumericalPropagator
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.
createMJDDate(int, double, TimeScale) - Static method in class org.orekit.time.AbsoluteDate
Build an instance corresponding to a Modified Julian Day date.
createMJDDate(int, T, TimeScale) - Static method in class org.orekit.time.FieldAbsoluteDate
Build an instance corresponding to a Modified Julian Day date.
createTransformedITRF(Frame, String) - Method in enum org.orekit.frames.HelmertTransformation.Predefined
Create an ITRF frame by transforming another ITRF frame.
crossProduct(FieldPVCoordinates<T>) - Method in class org.orekit.utils.FieldPVCoordinates
Compute the cross-product of two instances.
crossProduct(PVCoordinates, PVCoordinates) - Static method in class org.orekit.utils.PVCoordinates
Compute the cross-product of two instances.

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.
deepPeriodicEffects(double) - Method in class org.orekit.propagation.analytical.tle.DeepSDP4
Computes periodic terms from current coordinates and epoch.
DeepSDP4 - Class in org.orekit.propagation.analytical.tle
This class contains the methods that compute deep space perturbation terms.
DeepSDP4(TLE, AttitudeProvider, double) - Constructor for class org.orekit.propagation.analytical.tle.DeepSDP4
Constructor for a unique initial TLE.
deepSecularEffects(double) - Method in class org.orekit.propagation.analytical.tle.DeepSDP4
Computes secular terms from current coordinates and epoch.
DEFAULT - Static variable in class org.orekit.propagation.analytical.tle.TLE
Identifier for default type of ephemeris (SGP4/SDP4).
DEFAULT_BLQ_SUPPORTED_NAMES - Static variable in class org.orekit.models.earth.displacement.OceanLoadingCoefficientsBLQFactory
Default supported files name pattern for Onsala Space Observatory files in BLQ format.
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_EXTRAPOLATION_THRESHOLD_SEC - Static variable in class org.orekit.propagation.analytical.Ephemeris
Default extrapolation time threshold: 1ms.
DEFAULT_INPOP_SUPPORTED_NAMES - Static variable in class org.orekit.bodies.JPLEphemeridesLoader
Default supported files name pattern for IMCCE INPOP files.
DEFAULT_INTERPOLATION_METHOD - Static variable in class org.orekit.files.ccsds.OEMWriter
Default interpolation method if the user specifies none.
DEFAULT_INTERPOLATION_SIZE - Static variable in class org.orekit.files.general.OrekitEphemerisFile.OrekitSatelliteEphemeris
Defines the default interpolation sample size if it is not specified on a segment.
DEFAULT_LAW - Static variable in interface org.orekit.propagation.FieldPropagator
Default attitude provider.
DEFAULT_LAW - Static variable in interface org.orekit.propagation.Propagator
Default attitude provider.
DEFAULT_MASS - Static variable in interface org.orekit.propagation.FieldPropagator
Default mass.
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_MAX_ITER - Static variable in class org.orekit.propagation.events.FieldAbstractDetector
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_MAXCHECK - Static variable in class org.orekit.propagation.events.FieldAbstractDetector
Default maximum checking interval (s).
DEFAULT_ORIGINATOR - Static variable in class org.orekit.files.ccsds.OEMWriter
Default originator field value if user specifies none.
DEFAULT_ORIGINATOR - Static variable in class org.orekit.files.ccsds.StreamingOemWriter
Default value for Keyword.ORIGINATOR.
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_SUPPORTED_NAMES - Static variable in class org.orekit.models.earth.KlobucharIonoCoefficientsLoader
Default supported files name pattern.
DEFAULT_SUPPORTED_NAMES - Static variable in class org.orekit.time.TAIUTCDatFilesLoader
Default supported files name pattern.
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).
DEFAULT_THRESHOLD - Static variable in class org.orekit.propagation.events.FieldAbstractDetector
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, double, double, double, double, double, double) - Constructor for class org.orekit.data.DelaunayArguments
Simple constructor.
DELTA_R_FILE_NAME - Static variable in class org.orekit.models.earth.SaastamoinenModel
Default file name for δR correction term table.
dependsOnPositionOnly() - Method in class org.orekit.forces.drag.DragForce
Check if force models depends on position only.
dependsOnPositionOnly() - Method in interface org.orekit.forces.ForceModel
Check if force models depends on position only.
dependsOnPositionOnly() - Method in class org.orekit.forces.gravity.HolmesFeatherstoneAttractionModel
Check if force models depends on position only.
dependsOnPositionOnly() - Method in class org.orekit.forces.gravity.NewtonianAttraction
Check if force models depends on position only.
dependsOnPositionOnly() - Method in class org.orekit.forces.gravity.OceanTides
Check if force models depends on position only.
dependsOnPositionOnly() - Method in class org.orekit.forces.gravity.Relativity
Check if force models depends on position only.
dependsOnPositionOnly() - Method in class org.orekit.forces.gravity.SolidTides
Check if force models depends on position only.
dependsOnPositionOnly() - Method in class org.orekit.forces.gravity.ThirdBodyAttraction
Check if force models depends on position only.
dependsOnPositionOnly() - Method in class org.orekit.forces.HarmonicParametricAcceleration
Check if force models depends on position only.
dependsOnPositionOnly() - Method in class org.orekit.forces.maneuvers.ConstantThrustManeuver
Check if force models depends on position only.
dependsOnPositionOnly() - Method in class org.orekit.forces.PolynomialParametricAcceleration
Check if force models depends on position only.
dependsOnPositionOnly() - Method in class org.orekit.forces.radiation.SolarRadiationPressure
Check if force models depends on position only.
derivative(BodiesElements) - Method in interface org.orekit.data.PoissonSeries.CompiledSeries
Evaluate time derivative of a set of Poisson series.
derivative(FieldBodiesElements<S>) - Method in interface org.orekit.data.PoissonSeries.CompiledSeries
Evaluate time derivative of a set of Poisson series.
derivative(double) - Method in class org.orekit.data.PolynomialNutation
Evaluate the time derivative of the polynomial.
derivative(T) - Method in class org.orekit.data.PolynomialNutation
Evaluate the time derivative of the polynomial.
differentiate(ParameterFunction, ParameterDriver, int, double) - Static method in class org.orekit.utils.Differentiation
Differentiate a scalar function using finite differences.
differentiate(StateFunction, int, AttitudeProvider, OrbitType, PositionAngle, double, int) - Static method in class org.orekit.utils.Differentiation
Differentiate a vector function using finite differences.
Differentiation - Class in org.orekit.utils
Utility class for differentiating various kinds of functions.
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.
displacement(BodiesElements, Frame, Vector3D) - Method in class org.orekit.models.earth.displacement.OceanLoading
Compute displacement of a ground reference point.
displacement(BodiesElements, Frame, Vector3D) - Method in interface org.orekit.models.earth.displacement.StationDisplacement
Compute displacement of a ground reference point.
displacement(BodiesElements, Frame, Vector3D) - Method in class org.orekit.models.earth.displacement.TidalDisplacement
Compute displacement of a ground reference point.
doEvent(SpacecraftState) - Method in class org.orekit.propagation.events.EventState
Notify the user's listener of the event.
doEvent(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.events.FieldEventState
Notify the user's listener of the event.
DOP - Class in org.orekit.gnss
This class is a container for the result of a single DOP computation.
DOP(GeodeticPoint, AbsoluteDate, int, double, double, double, double, double) - Constructor for class org.orekit.gnss.DOP
Constructor.
DOP_MIN_ELEVATION - Static variable in class org.orekit.gnss.DOPComputer
Minimum elevation : 0°.
DOPComputer - Class in org.orekit.gnss
This class aims at computing the dilution of precision.
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, double[]) - Method in class org.orekit.forces.BoxAndSolarArraySpacecraft
Compute the acceleration due to drag.
dragAcceleration(AbsoluteDate, Frame, Vector3D, Rotation, double, double, Vector3D, double[], String) - Method in class org.orekit.forces.BoxAndSolarArraySpacecraft
Compute acceleration due to drag, with parameters derivatives.
dragAcceleration(FieldAbsoluteDate<T>, Frame, FieldVector3D<T>, FieldRotation<T>, T, T, FieldVector3D<T>, T[]) - Method in class org.orekit.forces.BoxAndSolarArraySpacecraft
Compute the acceleration due to drag.
dragAcceleration(AbsoluteDate, Frame, Vector3D, Rotation, double, double, Vector3D, double[]) - Method in interface org.orekit.forces.drag.DragSensitive
Compute the acceleration due to drag.
dragAcceleration(FieldAbsoluteDate<T>, Frame, FieldVector3D<T>, FieldRotation<T>, T, T, FieldVector3D<T>, T[]) - Method in interface org.orekit.forces.drag.DragSensitive
Compute the acceleration due to drag.
dragAcceleration(AbsoluteDate, Frame, Vector3D, Rotation, double, double, Vector3D, double[], 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, double[]) - Method in class org.orekit.forces.drag.IsotropicDrag
Compute the acceleration due to drag.
dragAcceleration(FieldAbsoluteDate<T>, Frame, FieldVector3D<T>, FieldRotation<T>, T, T, FieldVector3D<T>, T[]) - Method in class org.orekit.forces.drag.IsotropicDrag
Compute the acceleration due to drag.
dragAcceleration(AbsoluteDate, Frame, Vector3D, Rotation, double, double, Vector3D, double[], String) - Method in class org.orekit.forces.drag.IsotropicDrag
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.
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.
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(ODEIntegrator, boolean) - Constructor for class org.orekit.propagation.semianalytical.dsst.DSSTPropagator
Create a new instance of DSSTPropagator.
DSSTPropagator(ODEIntegrator) - 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.
DSSTTesseral - Class in org.orekit.propagation.semianalytical.dsst.forces
Tesseral contribution to the central body gravitational perturbation.
DSSTTesseral(Frame, double, UnnormalizedSphericalHarmonicsProvider, int, int, int, int, int, int, int) - Constructor for class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseral
Simple 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.
DSSTZonal - Class in org.orekit.propagation.semianalytical.dsst.forces
Zonal contribution to the central body gravitational perturbation.
DSSTZonal(UnnormalizedSphericalHarmonicsProvider, int, int, int) - Constructor for class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonal
Simple constructor.
DTM2000 - Class in org.orekit.forces.drag.atmosphere
This atmosphere model is the realization of the DTM-2000 model.
DTM2000(DTM2000InputParameters, PVCoordinatesProvider, BodyShape) - Constructor for class org.orekit.forces.drag.atmosphere.DTM2000
Simple constructor for independent computation.
DTM2000InputParameters - Interface in org.orekit.forces.drag.atmosphere
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.
durationFrom(FieldAbsoluteDate<T>) - Method in class org.orekit.time.FieldAbsoluteDate
Compute the physically elapsed duration between two instants.
durationFrom(AbsoluteDate) - Method in class org.orekit.time.FieldAbsoluteDate
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_ANGULAR_VELOCITY - Static variable in class org.orekit.estimation.measurements.EstimatedEarthFrameProvider
Earth Angular Velocity, in rad/s, from TIRF model.
EARTH_MOON - Static variable in class org.orekit.bodies.CelestialBodyFactory
Predefined name for Earth-Moon barycenter.
EarthITU453AtmosphereRefraction - Class in org.orekit.models.earth
Implementation of refraction model for Earth exponential atmosphere based on ITU-R P.834-7 recommendation.
EarthITU453AtmosphereRefraction(double) - Constructor for class org.orekit.models.earth.EarthITU453AtmosphereRefraction
Creates a new default instance.
EarthShape - Interface in org.orekit.models.earth
All models of Earth's shape have some common properties that are not shared with arbitrary BodyShapes.
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.
eccentricToMean(double, double, double) - Static method in class org.orekit.orbits.CircularOrbit
Computes the mean latitude argument from the eccentric latitude argument.
eccentricToMean(double, double, double) - Static method in class org.orekit.orbits.EquinoctialOrbit
Computes the mean longitude argument from the eccentric longitude argument.
eccentricToMean(T, T, T) - Static method in class org.orekit.orbits.FieldCircularOrbit
Computes the mean latitude argument from the eccentric latitude argument.
eccentricToMean(T, T, T) - Static method in class org.orekit.orbits.FieldEquinoctialOrbit
Computes the mean longitude argument from the eccentric longitude argument.
eccentricToTrue(double, double, double) - Static method in class org.orekit.orbits.CircularOrbit
Computes the true latitude argument from the eccentric latitude argument.
eccentricToTrue(double, double, double) - Static method in class org.orekit.orbits.EquinoctialOrbit
Computes the true longitude argument from the eccentric longitude argument.
eccentricToTrue(T, T, T) - Static method in class org.orekit.orbits.FieldCircularOrbit
Computes the true latitude argument from the eccentric latitude argument.
eccentricToTrue(T, T, T) - Static method in class org.orekit.orbits.FieldEquinoctialOrbit
Computes the true longitude argument from the eccentric longitude argument.
ecef(Frame) - Method in class org.orekit.propagation.analytical.gnss.GPSPropagator.Builder
Sets the Earth Centered Earth Fixed frame assimilated to the WGS84 ECEF.
eci(Frame) - Method in class org.orekit.propagation.analytical.gnss.GPSPropagator.Builder
Sets the Earth Centered Inertial frame used for propagation.
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(Orbit, UnnormalizedSphericalHarmonicsProvider, PositionAngle, double) - Constructor for class org.orekit.propagation.conversion.EcksteinHechlerPropagatorBuilder
Build a new instance.
EcksteinHechlerPropagatorBuilder(Orbit, double, double, TideSystem, double, double, double, double, double, OrbitType, PositionAngle, 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.
EGMFormatReader(String, boolean, boolean) - Constructor for class org.orekit.forces.gravity.potential.EGMFormatReader
Simple constructor that allows overriding 'standard' EGM96 ae and mu with WGS84 variants.
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.
ElevationExtremumDetector - Class in org.orekit.propagation.events
Detector for elevation extremum with respect to a ground point.
ElevationExtremumDetector(TopocentricFrame) - Constructor for class org.orekit.propagation.events.ElevationExtremumDetector
Build a new detector.
ElevationExtremumDetector(double, double, TopocentricFrame) - Constructor for class org.orekit.propagation.events.ElevationExtremumDetector
Build a detector.
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.
EllipsoidTessellator - Class in org.orekit.models.earth.tessellation
Class used to tessellate an interest zone on an ellipsoid in either tiles or grids of geodetic points.
EllipsoidTessellator(OneAxisEllipsoid, TileAiming, int) - Constructor for class org.orekit.models.earth.tessellation.EllipsoidTessellator
Simple constructor.
ellipticEccentricToMean(T, T) - Static method in class org.orekit.orbits.FieldKeplerianOrbit
Computes the mean anomaly from the elliptic eccentric anomaly.
ellipticEccentricToMean(double, double) - Static method in class org.orekit.orbits.KeplerianOrbit
Computes the mean anomaly from the elliptic eccentric anomaly.
ellipticEccentricToTrue(T, T) - Static method in class org.orekit.orbits.FieldKeplerianOrbit
Computes the true anomaly from the elliptic eccentric anomaly.
ellipticEccentricToTrue(double, double) - Static method in class org.orekit.orbits.KeplerianOrbit
Computes the true anomaly from the elliptic eccentric anomaly.
ellipticKeplerianToPosition(T, T, T, T, T, T, double) - Static method in class org.orekit.orbits.FieldKeplerianOrbit
Compute position from elliptic Keplerian parameters.
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.
EnablingPredicate<S extends EventDetector> - Interface in org.orekit.propagation.events
This interface represents an event enabling predicate function.
endParse() - Method in class org.orekit.forces.gravity.potential.OceanTidesReader
End parsing.
ensureCompatibleAdditionalStates(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.FieldSpacecraftState
Check if two instances have the same set of additional states available.
ensureCompatibleAdditionalStates(SpacecraftState) - Method in class org.orekit.propagation.SpacecraftState
Check if two instances have the same set of additional states available.
EOPBasedTransformProvider - Interface in org.orekit.frames
Interface for Transform providers that use Earth Orientation Parameters.
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.
EphemeridesBlock() - Constructor for class org.orekit.files.ccsds.OEMFile.EphemeridesBlock
EphemeridesBlock constructor.
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(List<SpacecraftState>, int, double) - Constructor for class org.orekit.propagation.analytical.Ephemeris
Constructor with tabulated states.
EPHEMERIS_GENERATION_MODE - Static variable in interface org.orekit.propagation.FieldPropagator
Indicator for ephemeris generation mode.
EPHEMERIS_GENERATION_MODE - Static variable in interface org.orekit.propagation.Propagator
Indicator for ephemeris generation mode.
EphemerisFile - Interface in org.orekit.files.general
An interface for accessing the data stored in an ephemeris file and using the data to create a working Propagator.
EphemerisFile.EphemerisSegment - Interface in org.orekit.files.general
A segment of an ephemeris for a satellite.
EphemerisFile.SatelliteEphemeris - Interface in org.orekit.files.general
Contains the information about a single satellite from an EphemerisFile.
EphemerisFileParser - Interface in org.orekit.files.general
Parse an ephemeris file.
EphemerisFileWriter - Interface in org.orekit.files.general
An interface for writing out ephemeris files to disk.
equals(Object) - Method in class org.orekit.bodies.FieldGeodeticPoint
 
equals(Object) - Method in class org.orekit.bodies.GeodeticPoint
 
equals(Object) - Method in class org.orekit.models.earth.displacement.Tide
 
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.FieldAbsoluteDate
Check if the instance represent the same time as another instance.
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(double, double, double, double, double, double, 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.
equinoctialToPosition(T, T, T, T, T, T, double) - Static method in class org.orekit.orbits.FieldEquinoctialOrbit
Compute position from equinoctial parameters.
estimate(Frame, PV, PV, PV) - Method in class org.orekit.estimation.iod.IodGibbs
Give an initial orbit estimation, assuming Keplerian motion.
estimate(Frame, Vector3D, AbsoluteDate, Vector3D, AbsoluteDate, Vector3D, AbsoluteDate) - Method in class org.orekit.estimation.iod.IodGibbs
Give an initial orbit estimation, assuming Keplerian motion.
estimate(Vector3D, Vector3D, Vector3D, Vector3D, AbsoluteDate, Vector3D, AbsoluteDate, Vector3D, AbsoluteDate, double, double) - Method in class org.orekit.estimation.iod.IodGooding
Orbit got from Observed Three Lines of Sight (angles only).
estimate(Frame, boolean, int, Vector3D, AbsoluteDate, Vector3D, AbsoluteDate) - Method in class org.orekit.estimation.iod.IodLambert
Estimate a Keplerian orbit given two position vectors and a duration.
estimate() - Method in class org.orekit.estimation.leastsquares.BatchLSEstimator
Estimate the orbital, propagation and measurements parameters.
estimate(int, int, SpacecraftState[]) - Method in class org.orekit.estimation.measurements.AbstractMeasurement
Estimate the theoretical value of the measurement.
estimate(int, int, SpacecraftState[]) - Method in interface org.orekit.estimation.measurements.ObservedMeasurement
Estimate the theoretical value of the measurement.
EstimatedEarthFrameProvider - Class in org.orekit.estimation.measurements
Class modeling an Earth frame whose Earth Orientation Parameters can be estimated.
EstimatedEarthFrameProvider(UT1Scale) - Constructor for class org.orekit.estimation.measurements.EstimatedEarthFrameProvider
Build an estimated Earth frame.
EstimatedMeasurement<T extends ObservedMeasurement<T>> - Class in org.orekit.estimation.measurements
Class holding an estimated theoretical value associated to an observed measurement.
EstimatedMeasurement(T, int, int, SpacecraftState[], TimeStampedPVCoordinates[]) - Constructor for class org.orekit.estimation.measurements.EstimatedMeasurement
Simple constructor.
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 rotation rate between two orientations.
estimateRate(FieldRotation<T>, FieldRotation<T>, T) - Static method in class org.orekit.utils.FieldAngularCoordinates
Estimate rotation 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.
EstimationModifier<T extends ObservedMeasurement<T>> - Interface in org.orekit.estimation.measurements
Interface for estimated measurements modifiers used for orbit determination.
EstimationsProvider - Interface in org.orekit.estimation.measurements
Interface for retrieving estimated measurements during orbit determination.
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).
evaluateAll(FieldAbsoluteDate<T>) - Method in class org.orekit.data.FundamentalNutationArguments
Evaluate all fundamental arguments for the current date (Delaunay plus planetary).
evaluateStep(OrekitStepInterpolator) - Method in class org.orekit.propagation.events.EventState
Evaluate the impact of the proposed step on the event detector.
evaluateStep(FieldOrekitStepInterpolator<T>) - Method in class org.orekit.propagation.events.FieldEventState
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.
evaluateTC(FieldAbsoluteDate<T>) - Method in enum org.orekit.utils.IERSConventions
Evaluate the date offset between the current date and the reference date.
evaluationPerformed(int, int, Orbit[], ParameterDriversList, ParameterDriversList, ParameterDriversList, EstimationsProvider, LeastSquaresProblem.Evaluation) - Method in interface org.orekit.estimation.leastsquares.BatchLSObserver
Notification callback for the end of each evaluation.
EventDetector - Interface in org.orekit.propagation.events
This interface represents space-dynamics aware events detectors.
EventEnablingPredicateFilter<T extends EventDetector> - Class in org.orekit.propagation.events
Wrapper used to detect events only when enabled by an external predicated function.
EventEnablingPredicateFilter(T, EnablingPredicate<T>) - Constructor for class org.orekit.propagation.events.EventEnablingPredicateFilter
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.
eventIsEnabled(SpacecraftState, S, double) - Method in interface org.orekit.propagation.events.EnablingPredicate
Compute an event enabling function of state.
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(FieldSpacecraftState<T>, boolean) - Method in class org.orekit.propagation.events.FieldAbstractDetector
Handle the event.
eventOccurred(FieldSpacecraftState<T>, boolean) - Method in interface org.orekit.propagation.events.FieldEventDetector
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(FieldSpacecraftState<T>, KK, boolean) - Method in class org.orekit.propagation.events.handlers.FieldContinueOnEvent
Specific implementation of the eventOccurred interface.
eventOccurred(FieldSpacecraftState<T>, KK, boolean) - Method in interface org.orekit.propagation.events.handlers.FieldEventHandler
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(FieldSpacecraftState<T>, KK, boolean) - Method in class org.orekit.propagation.events.handlers.FieldStopOnDecreasing
Handle a detection event and choose what to do next.
eventOccurred(FieldSpacecraftState<T>, KK, boolean) - Method in class org.orekit.propagation.events.handlers.FieldStopOnEvent
Specific implementation of the eventOccurred interface.
eventOccurred(FieldSpacecraftState<T>, KK, boolean) - Method in class org.orekit.propagation.events.handlers.FieldStopOnIncreasing
Handle a detection event and choose what to do next.
eventOccurred(SpacecraftState, T, boolean) - Method in class org.orekit.propagation.events.handlers.RecordAndContinue
 
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.
EventSlopeFilter<T extends EventDetector> - Class in org.orekit.propagation.events
Wrapper used to detect only increasing or decreasing events.
EventSlopeFilter(T, FilterType) - Constructor for class org.orekit.propagation.events.EventSlopeFilter
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.
EventState.EventOccurrence - Class in org.orekit.propagation.events
Class to hold the data related to an event occurrence that is needed to decide how to modify integration.
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.
Facet(Vector3D, double) - Constructor for class org.orekit.forces.BoxAndSolarArraySpacecraft.Facet
Simple constructor.
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.
FieldAbsoluteDate<T extends RealFieldElement<T>> - Class in org.orekit.time
This class represents a specific instant in time.
FieldAbsoluteDate(Field<T>, AbsoluteDate) - Constructor for class org.orekit.time.FieldAbsoluteDate
Build an instance from an AbsoluteDate.
FieldAbsoluteDate(Field<T>) - Constructor for class org.orekit.time.FieldAbsoluteDate
Create an instance with a default value (FieldAbsoluteDate.getJ2000Epoch(Field)).
FieldAbsoluteDate(FieldAbsoluteDate<T>, T) - Constructor for class org.orekit.time.FieldAbsoluteDate
Build an instance from an elapsed duration since to another instant.
FieldAbsoluteDate(Field<T>, String, TimeScale) - Constructor for class org.orekit.time.FieldAbsoluteDate
Build an instance from a location (parsed from a string) in a time scale.
FieldAbsoluteDate(Field<T>, DateTimeComponents, TimeScale) - Constructor for class org.orekit.time.FieldAbsoluteDate
Build an instance from a location in a time scale.
FieldAbsoluteDate(Field<T>, DateComponents, TimeComponents, TimeScale) - Constructor for class org.orekit.time.FieldAbsoluteDate
Build an instance from a location in a time scale.
FieldAbsoluteDate(Field<T>, int, int, int, int, int, double, TimeScale) - Constructor for class org.orekit.time.FieldAbsoluteDate
Build an instance from a location in a time scale.
FieldAbsoluteDate(Field<T>, int, Month, int, int, int, double, TimeScale) - Constructor for class org.orekit.time.FieldAbsoluteDate
Build an instance from a location in a time scale.
FieldAbsoluteDate(Field<T>, DateComponents, TimeScale) - Constructor for class org.orekit.time.FieldAbsoluteDate
Build an instance from a location in a time scale.
FieldAbsoluteDate(Field<T>, int, int, int, TimeScale) - Constructor for class org.orekit.time.FieldAbsoluteDate
Build an instance from a location in a time scale.
FieldAbsoluteDate(Field<T>, int, Month, int, TimeScale) - Constructor for class org.orekit.time.FieldAbsoluteDate
Build an instance from a location in a time scale.
FieldAbsoluteDate(Field<T>, Date, TimeScale) - Constructor for class org.orekit.time.FieldAbsoluteDate
Build an instance from a location in a time scale.
FieldAbsoluteDate(FieldAbsoluteDate<T>, double) - Constructor for class org.orekit.time.FieldAbsoluteDate
Build an instance from an elapsed duration since to another instant.
FieldAbsoluteDate(AbsoluteDate, T) - Constructor for class org.orekit.time.FieldAbsoluteDate
Build an instance from an elapsed duration since to another instant.
FieldAbsoluteDate(FieldAbsoluteDate<T>, double, TimeScale) - Constructor for class org.orekit.time.FieldAbsoluteDate
Build an instance from an apparent clock offset with respect to another instant in the perspective of a specific time scale.
FieldAbstractAnalyticalPropagator<T extends RealFieldElement<T>> - Class in org.orekit.propagation.analytical
Common handling of FieldPropagator methods for analytical propagators.
FieldAbstractAnalyticalPropagator(Field<T>, AttitudeProvider) - Constructor for class org.orekit.propagation.analytical.FieldAbstractAnalyticalPropagator
Build a new instance.
FieldAbstractDetector<D extends FieldEventDetector<T>,T extends RealFieldElement<T>> - Class in org.orekit.propagation.events
Common parts shared by several orbital events finders.
FieldAbstractDetector(T, T, int, FieldEventHandler<? super D, T>) - Constructor for class org.orekit.propagation.events.FieldAbstractDetector
Build a new instance.
FieldAbstractIntegratedPropagator<T extends RealFieldElement<T>> - Class in org.orekit.propagation.integration
Common handling of FieldPropagator methods for both numerical and semi-analytical propagators.
FieldAbstractIntegratedPropagator(Field<T>, FieldODEIntegrator<T>, boolean) - Constructor for class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator
Build a new instance.
FieldAbstractIntegratedPropagator.MainStateEquations<T extends RealFieldElement<T>> - Interface in org.orekit.propagation.integration
Differential equations for the main state (orbit, attitude and mass).
FieldAbstractPropagator<T extends RealFieldElement<T>> - Class in org.orekit.propagation
Common handling of Propagator methods for analytical propagators.
FieldAbstractPropagator(Field<T>) - Constructor for class org.orekit.propagation.FieldAbstractPropagator
Build a new instance.
FieldAdditionalEquations<T extends RealFieldElement<T>> - Interface in org.orekit.propagation.integration
This interface allows users to add their own differential equations to a numerical propagator.
FieldAdditionalStateProvider<T extends RealFieldElement<T>> - Interface in org.orekit.propagation
This interface represents providers for additional state data beyond SpacecraftState.
FieldAltitudeDetector<T extends RealFieldElement<T>> - Class in org.orekit.propagation.events
Finder for satellite altitude crossing events.
FieldAltitudeDetector(T, BodyShape) - Constructor for class org.orekit.propagation.events.FieldAltitudeDetector
Build a new altitude detector.
FieldAltitudeDetector(T, T, BodyShape) - Constructor for class org.orekit.propagation.events.FieldAltitudeDetector
Build a new altitude detector.
FieldAltitudeDetector(T, T, T, BodyShape) - Constructor for class org.orekit.propagation.events.FieldAltitudeDetector
Build a new altitude detector.
FieldAngularCoordinates<T extends RealFieldElement<T>> - Class in org.orekit.utils
Simple container for rotation / rotation 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 rotation / rotation rate / rotation acceleration triplet.
FieldAngularCoordinates(FieldPVCoordinates<T>, FieldPVCoordinates<T>, FieldPVCoordinates<T>, FieldPVCoordinates<T>, double) - Constructor for class org.orekit.utils.FieldAngularCoordinates
Build the rotation that transforms a pair of pv coordinates into another one.
FieldAngularCoordinates(Field<T>, AngularCoordinates) - Constructor for class org.orekit.utils.FieldAngularCoordinates
Builds a FieldAngularCoordinates from a field and a regular AngularCoordinates.
FieldApsideDetector<T extends RealFieldElement<T>> - Class in org.orekit.propagation.events
Finder for apside crossing events.
FieldApsideDetector(FieldOrbit<T>) - Constructor for class org.orekit.propagation.events.FieldApsideDetector
Build a new instance.
FieldApsideDetector(T, FieldOrbit<T>) - Constructor for class org.orekit.propagation.events.FieldApsideDetector
Build a new instance.
FieldAttitude<T extends RealFieldElement<T>> - Class in org.orekit.attitudes
This class handles attitude definition at a given date.
FieldAttitude(Frame, TimeStampedFieldAngularCoordinates<T>) - Constructor for class org.orekit.attitudes.FieldAttitude
Creates a new instance.
FieldAttitude(FieldAbsoluteDate<T>, Frame, FieldAngularCoordinates<T>) - Constructor for class org.orekit.attitudes.FieldAttitude
Creates a new instance.
FieldAttitude(FieldAbsoluteDate<T>, Frame, FieldRotation<T>, FieldVector3D<T>, FieldVector3D<T>) - Constructor for class org.orekit.attitudes.FieldAttitude
Creates a new instance.
FieldAttitude(FieldAbsoluteDate<T>, Frame, Rotation, Vector3D, Vector3D, Field<T>) - Constructor for class org.orekit.attitudes.FieldAttitude
Creates a new instance.
FieldAttitude(Field<T>, Attitude) - Constructor for class org.orekit.attitudes.FieldAttitude
Builds an instance for a regular Attitude.
FieldBodiesElements<T extends RealFieldElement<T>> - Class in org.orekit.data
Elements of the bodies having an effect on nutation.
FieldBodiesElements(FieldAbsoluteDate<T>, T, T, T, T, T, T, T, T, T, T, T, T, T, T, T, 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.
FieldBoundedPropagator<T extends RealFieldElement<T>> - Interface in org.orekit.propagation
This interface is intended for ephemerides valid only during a time range.
FieldCartesianOrbit<T extends RealFieldElement<T>> - Class in org.orekit.orbits
This class holds Cartesian orbital parameters.
FieldCartesianOrbit(TimeStampedFieldPVCoordinates<T>, Frame, double) - Constructor for class org.orekit.orbits.FieldCartesianOrbit
Constructor from Cartesian parameters.
FieldCartesianOrbit(FieldPVCoordinates<T>, Frame, FieldAbsoluteDate<T>, double) - Constructor for class org.orekit.orbits.FieldCartesianOrbit
Constructor from Cartesian parameters.
FieldCartesianOrbit(FieldOrbit<T>) - Constructor for class org.orekit.orbits.FieldCartesianOrbit
Constructor from any kind of orbital parameters.
FieldCircularOrbit<T extends RealFieldElement<T>> - Class in org.orekit.orbits
This class handles circular orbital parameters.
FieldCircularOrbit(T, T, T, T, T, T, PositionAngle, Frame, FieldAbsoluteDate<T>, double) - Constructor for class org.orekit.orbits.FieldCircularOrbit
Creates a new instance.
FieldCircularOrbit(T, T, T, T, T, T, T, T, T, T, T, T, PositionAngle, Frame, FieldAbsoluteDate<T>, double) - Constructor for class org.orekit.orbits.FieldCircularOrbit
Creates a new instance.
FieldCircularOrbit(TimeStampedFieldPVCoordinates<T>, Frame, double) - Constructor for class org.orekit.orbits.FieldCircularOrbit
Constructor from Cartesian parameters.
FieldCircularOrbit(FieldPVCoordinates<T>, Frame, FieldAbsoluteDate<T>, double) - Constructor for class org.orekit.orbits.FieldCircularOrbit
Constructor from Cartesian parameters.
FieldCircularOrbit(FieldOrbit<T>) - Constructor for class org.orekit.orbits.FieldCircularOrbit
Constructor from any kind of orbital parameters.
FieldContinueOnEvent<KK extends FieldEventDetector<T>,T extends RealFieldElement<T>> - Class in org.orekit.propagation.events.handlers
Event handler which will always return continue as a state.
FieldContinueOnEvent() - Constructor for class org.orekit.propagation.events.handlers.FieldContinueOnEvent
 
FieldDateDetector<T extends RealFieldElement<T>> - Class in org.orekit.propagation.events
Finder for date events.
FieldDateDetector(T, T, FieldTimeStamped<T>...) - Constructor for class org.orekit.propagation.events.FieldDateDetector
Build a new instance.
FieldDateDetector(FieldAbsoluteDate<T>) - Constructor for class org.orekit.propagation.events.FieldDateDetector
Build a new instance.
FieldDelaunayArguments<T extends RealFieldElement<T>> - Class in org.orekit.data
Delaunay arguments used for nutation or tides.
FieldDelaunayArguments(FieldAbsoluteDate<T>, T, T, T, T, T, T, T, T, T, T, T, T, T) - Constructor for class org.orekit.data.FieldDelaunayArguments
Simple constructor.
FieldEcksteinHechlerPropagator<T extends RealFieldElement<T>> - Class in org.orekit.propagation.analytical
This class propagates a FieldSpacecraftState using the analytical Eckstein-Hechler model.
FieldEcksteinHechlerPropagator(FieldOrbit<T>, UnnormalizedSphericalHarmonicsProvider) - Constructor for class org.orekit.propagation.analytical.FieldEcksteinHechlerPropagator
Build a propagator from FieldOrbit and potential provider.
FieldEcksteinHechlerPropagator(FieldOrbit<T>, AttitudeProvider, T, UnnormalizedSphericalHarmonicsProvider, UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics) - Constructor for class org.orekit.propagation.analytical.FieldEcksteinHechlerPropagator
Private helper constructor.
FieldEcksteinHechlerPropagator(FieldOrbit<T>, double, double, double, double, double, double, double) - Constructor for class org.orekit.propagation.analytical.FieldEcksteinHechlerPropagator
Build a propagator from FieldOrbit and potential.
FieldEcksteinHechlerPropagator(FieldOrbit<T>, T, UnnormalizedSphericalHarmonicsProvider) - Constructor for class org.orekit.propagation.analytical.FieldEcksteinHechlerPropagator
Build a propagator from FieldOrbit, mass and potential provider.
FieldEcksteinHechlerPropagator(FieldOrbit<T>, T, double, double, double, double, double, double, double) - Constructor for class org.orekit.propagation.analytical.FieldEcksteinHechlerPropagator
Build a propagator from FieldOrbit, mass and potential.
FieldEcksteinHechlerPropagator(FieldOrbit<T>, AttitudeProvider, UnnormalizedSphericalHarmonicsProvider) - Constructor for class org.orekit.propagation.analytical.FieldEcksteinHechlerPropagator
Build a propagator from FieldOrbit, attitude provider and potential provider.
FieldEcksteinHechlerPropagator(FieldOrbit<T>, AttitudeProvider, double, double, double, double, double, double, double) - Constructor for class org.orekit.propagation.analytical.FieldEcksteinHechlerPropagator
Build a propagator from FieldOrbit, attitude provider and potential.
FieldEcksteinHechlerPropagator(FieldOrbit<T>, AttitudeProvider, T, UnnormalizedSphericalHarmonicsProvider) - Constructor for class org.orekit.propagation.analytical.FieldEcksteinHechlerPropagator
Build a propagator from FieldOrbit, attitude provider, mass and potential provider.
FieldEcksteinHechlerPropagator(FieldOrbit<T>, AttitudeProvider, T, double, double, double, double, double, double, double) - Constructor for class org.orekit.propagation.analytical.FieldEcksteinHechlerPropagator
Build a propagator from FieldOrbit, attitude provider, mass and potential.
FieldEclipseDetector<T extends RealFieldElement<T>> - Class in org.orekit.propagation.events
Finder for satellite eclipse related events.
FieldEclipseDetector(PVCoordinatesProvider, double, PVCoordinatesProvider, double, Field<T>) - Constructor for class org.orekit.propagation.events.FieldEclipseDetector
Build a new eclipse detector.
FieldEclipseDetector(T, PVCoordinatesProvider, double, PVCoordinatesProvider, double) - Constructor for class org.orekit.propagation.events.FieldEclipseDetector
Build a new eclipse detector.
FieldEclipseDetector(T, T, PVCoordinatesProvider, double, PVCoordinatesProvider, double) - Constructor for class org.orekit.propagation.events.FieldEclipseDetector
Build a new eclipse detector.
FieldElevationDetector<T extends RealFieldElement<T>> - 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.
FieldElevationDetector(Field<T>, TopocentricFrame) - Constructor for class org.orekit.propagation.events.FieldElevationDetector
Creates an instance of Elevation detector based on passed in topocentric frame and the minimum elevation angle.
FieldElevationDetector(T, T, TopocentricFrame) - Constructor for class org.orekit.propagation.events.FieldElevationDetector
Creates an instance of Elevation detector based on passed in topocentric frame and overrides of default maximal checking interval and convergence threshold values.
FieldEquinoctialOrbit<T extends RealFieldElement<T>> - Class in org.orekit.orbits
This class handles equinoctial orbital parameters, which can support both circular and equatorial orbits.
FieldEquinoctialOrbit(T, T, T, T, T, T, PositionAngle, Frame, FieldAbsoluteDate<T>, double) - Constructor for class org.orekit.orbits.FieldEquinoctialOrbit
Creates a new instance.
FieldEquinoctialOrbit(T, T, T, T, T, T, T, T, T, T, T, T, PositionAngle, Frame, FieldAbsoluteDate<T>, double) - Constructor for class org.orekit.orbits.FieldEquinoctialOrbit
Creates a new instance.
FieldEquinoctialOrbit(TimeStampedFieldPVCoordinates<T>, Frame, double) - Constructor for class org.orekit.orbits.FieldEquinoctialOrbit
Constructor from Cartesian parameters.
FieldEquinoctialOrbit(FieldPVCoordinates<T>, Frame, FieldAbsoluteDate<T>, double) - Constructor for class org.orekit.orbits.FieldEquinoctialOrbit
Constructor from Cartesian parameters.
FieldEquinoctialOrbit(FieldOrbit<T>) - Constructor for class org.orekit.orbits.FieldEquinoctialOrbit
Constructor from any kind of orbital parameters.
FieldEventDetector<T extends RealFieldElement<T>> - Interface in org.orekit.propagation.events
This interface represents space-dynamics aware events detectors.
FieldEventHandler<KK extends FieldEventDetector<T>,T extends RealFieldElement<T>> - 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.
FieldEventHandler.Action - Enum in org.orekit.propagation.events.handlers
Enumerate for actions to be performed when an event occurs.
FieldEventsLogger<T extends RealFieldElement<T>> - Class in org.orekit.propagation.events
This class logs events detectors events during propagation.
FieldEventsLogger() - Constructor for class org.orekit.propagation.events.FieldEventsLogger
Simple constructor.
FieldEventsLogger.FieldLoggedEvent<T extends RealFieldElement<T>> - Class in org.orekit.propagation.events
Class for logged events entries.
FieldEventState<D extends FieldEventDetector<T>,T extends RealFieldElement<T>> - Class in org.orekit.propagation.events
This class handles the state for one event detector during integration steps.
FieldEventState(D) - Constructor for class org.orekit.propagation.events.FieldEventState
Simple constructor.
FieldEventState.EventOccurrence<T extends RealFieldElement<T>> - Class in org.orekit.propagation.events
Class to hold the data related to an event occurrence that is needed to decide how to modify integration.
FieldGeodeticPoint<T extends RealFieldElement<T>> - Class in org.orekit.bodies
Point location relative to a 2D body surface, using RealFieldElement.
FieldGeodeticPoint(T, T, T) - Constructor for class org.orekit.bodies.FieldGeodeticPoint
Build a new instance.
FieldIntegratedEphemeris<T extends RealFieldElement<T>> - Class in org.orekit.propagation.integration
This class stores sequentially generated orbital parameters for later retrieval.
FieldIntegratedEphemeris(FieldAbsoluteDate<T>, FieldAbsoluteDate<T>, FieldAbsoluteDate<T>, FieldStateMapper<T>, boolean, FieldDenseOutputModel<T>, Map<String, T[]>, List<FieldAdditionalStateProvider<T>>, String[]) - Constructor for class org.orekit.propagation.integration.FieldIntegratedEphemeris
Creates a new instance of IntegratedEphemeris.
FieldKeplerianOrbit<T extends RealFieldElement<T>> - Class in org.orekit.orbits
This class handles traditional Keplerian orbital parameters.
FieldKeplerianOrbit(T, T, T, T, T, T, PositionAngle, Frame, FieldAbsoluteDate<T>, double) - Constructor for class org.orekit.orbits.FieldKeplerianOrbit
Creates a new instance.
FieldKeplerianOrbit(T, T, T, T, T, T, T, T, T, T, T, T, PositionAngle, Frame, FieldAbsoluteDate<T>, double) - Constructor for class org.orekit.orbits.FieldKeplerianOrbit
Creates a new instance.
FieldKeplerianOrbit(TimeStampedFieldPVCoordinates<T>, Frame, double) - Constructor for class org.orekit.orbits.FieldKeplerianOrbit
Constructor from Cartesian parameters.
FieldKeplerianOrbit(FieldPVCoordinates<T>, Frame, FieldAbsoluteDate<T>, double) - Constructor for class org.orekit.orbits.FieldKeplerianOrbit
Constructor from Cartesian parameters.
FieldKeplerianOrbit(FieldOrbit<T>) - Constructor for class org.orekit.orbits.FieldKeplerianOrbit
Constructor from any kind of orbital parameters.
FieldKeplerianPropagator<T extends RealFieldElement<T>> - Class in org.orekit.propagation.analytical
Simple Keplerian orbit propagator.
FieldKeplerianPropagator(FieldOrbit<T>) - Constructor for class org.orekit.propagation.analytical.FieldKeplerianPropagator
Build a propagator from orbit only.
FieldKeplerianPropagator(FieldOrbit<T>, double) - Constructor for class org.orekit.propagation.analytical.FieldKeplerianPropagator
Build a propagator from orbit and central attraction coefficient μ.
FieldKeplerianPropagator(FieldOrbit<T>, AttitudeProvider) - Constructor for class org.orekit.propagation.analytical.FieldKeplerianPropagator
Build a propagator from orbit and attitude provider.
FieldKeplerianPropagator(FieldOrbit<T>, AttitudeProvider, double) - Constructor for class org.orekit.propagation.analytical.FieldKeplerianPropagator
Build a propagator from orbit, attitude provider and central attraction coefficient μ.
FieldKeplerianPropagator(FieldOrbit<T>, AttitudeProvider, double, T) - Constructor for class org.orekit.propagation.analytical.FieldKeplerianPropagator
Build propagator from orbit, attitude provider, central attraction coefficient μ and mass.
FieldModeHandler<T extends RealFieldElement<T>> - Interface in org.orekit.propagation.integration
Common interface for all propagator mode handlers initialization.
FieldNodeDetector<T extends RealFieldElement<T>> - Class in org.orekit.propagation.events
Finder for node crossing events.
FieldNodeDetector(FieldOrbit<T>, Frame) - Constructor for class org.orekit.propagation.events.FieldNodeDetector
Build a new instance.
FieldNodeDetector(T, FieldOrbit<T>, Frame) - Constructor for class org.orekit.propagation.events.FieldNodeDetector
Build a new instance.
FieldNumericalPropagator<T extends RealFieldElement<T>> - Class in org.orekit.propagation.numerical
This class propagates orbits using numerical integration.
FieldNumericalPropagator(Field<T>, FieldODEIntegrator<T>) - Constructor for class org.orekit.propagation.numerical.FieldNumericalPropagator
Create a new instance of NumericalPropagator, based on orbit definition mu.
FieldOfView - Class in org.orekit.propagation.events
Class representing a spacecraft sensor Field Of View.
FieldOfView(SphericalPolygonsSet, double) - Constructor for class org.orekit.propagation.events.FieldOfView
Build a new instance.
FieldOfView(Vector3D, Vector3D, double, Vector3D, double, double) - Constructor for class org.orekit.propagation.events.FieldOfView
Build a Field Of View with dihedral shape (i.e.
FieldOfView(Vector3D, Vector3D, double, int, double) - Constructor for class org.orekit.propagation.events.FieldOfView
Build Field Of View with a regular polygon shape.
FieldOfViewDetector - Class in org.orekit.propagation.events
Finder for target entry/exit events with respect to a satellite sensor Field Of View.
FieldOfViewDetector(PVCoordinatesProvider, FieldOfView) - Constructor for class org.orekit.propagation.events.FieldOfViewDetector
Build a new instance.
FieldOrbit<T extends RealFieldElement<T>> - Class in org.orekit.orbits
This class handles orbital parameters.
FieldOrbit(Frame, FieldAbsoluteDate<T>, double) - Constructor for class org.orekit.orbits.FieldOrbit
Default constructor.
FieldOrbit(TimeStampedFieldPVCoordinates<T>, Frame, double) - Constructor for class org.orekit.orbits.FieldOrbit
Set the orbit from Cartesian parameters.
FieldOrekitFixedStepHandler<T extends RealFieldElement<T>> - Interface in org.orekit.propagation.sampling
This interface is a space-dynamics aware fixed size step handler.
FieldOrekitStepHandler<T extends RealFieldElement<T>> - Interface in org.orekit.propagation.sampling
This interface is a space-dynamics aware step handler.
FieldOrekitStepHandlerMultiplexer<T extends RealFieldElement<T>> - Class in org.orekit.propagation.sampling
This class gathers several OrekitStepHandler instances into one.
FieldOrekitStepHandlerMultiplexer() - Constructor for class org.orekit.propagation.sampling.FieldOrekitStepHandlerMultiplexer
Simple constructor.
FieldOrekitStepInterpolator<T extends RealFieldElement<T>> - Interface in org.orekit.propagation.sampling
This interface is a space-dynamics aware step interpolator.
FieldOrekitStepNormalizer<T extends RealFieldElement<T>> - Class in org.orekit.propagation.sampling
This class wraps an object implementing OrekitFixedStepHandler into a OrekitStepHandler.
FieldOrekitStepNormalizer(T, FieldOrekitFixedStepHandler<T>) - Constructor for class org.orekit.propagation.sampling.FieldOrekitStepNormalizer
Simple constructor.
FieldPoleCorrection<T extends RealFieldElement<T>> - Class in org.orekit.frames
Simple container class for pole correction parameters.
FieldPoleCorrection(T, T) - Constructor for class org.orekit.frames.FieldPoleCorrection
Simple constructor.
FieldPropagator<T extends RealFieldElement<T>> - Interface in org.orekit.propagation
This interface provides a way to propagate an orbit at any time.
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 FieldPVCoordinates triplet with zero acceleration.
FieldPVCoordinates(FieldVector3D<T>, FieldVector3D<T>, FieldVector3D<T>) - Constructor for class org.orekit.utils.FieldPVCoordinates
Builds a FieldPVCoordinates triplet.
FieldPVCoordinates(Field<T>, PVCoordinates) - Constructor for class org.orekit.utils.FieldPVCoordinates
Builds a FieldPVCoordinates from a field and a regular PVCoordinates.
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.
FieldPVCoordinatesProvider<T extends RealFieldElement<T>> - Interface in org.orekit.utils
Interface for PV coordinates providers.
FieldSpacecraftState<T extends RealFieldElement<T>> - Class in org.orekit.propagation
This class is the representation of a complete state holding orbit, attitude and mass information at a given date.
FieldSpacecraftState(FieldOrbit<T>) - Constructor for class org.orekit.propagation.FieldSpacecraftState
Build a spacecraft state from orbit only.
FieldSpacecraftState(FieldOrbit<T>, FieldAttitude<T>) - Constructor for class org.orekit.propagation.FieldSpacecraftState
Build a spacecraft state from orbit and attitude provider.
FieldSpacecraftState(FieldOrbit<T>, T) - Constructor for class org.orekit.propagation.FieldSpacecraftState
Create a new instance from orbit and mass.
FieldSpacecraftState(FieldOrbit<T>, FieldAttitude<T>, T) - Constructor for class org.orekit.propagation.FieldSpacecraftState
Build a spacecraft state from orbit, attitude provider and mass.
FieldSpacecraftState(FieldOrbit<T>, Map<String, T[]>) - Constructor for class org.orekit.propagation.FieldSpacecraftState
Build a spacecraft state from orbit only.
FieldSpacecraftState(FieldOrbit<T>, FieldAttitude<T>, Map<String, T[]>) - Constructor for class org.orekit.propagation.FieldSpacecraftState
Build a spacecraft state from orbit and attitude provider.
FieldSpacecraftState(FieldOrbit<T>, T, Map<String, T[]>) - Constructor for class org.orekit.propagation.FieldSpacecraftState
Create a new instance from orbit and mass.
FieldSpacecraftState(FieldOrbit<T>, FieldAttitude<T>, T, Map<String, T[]>) - Constructor for class org.orekit.propagation.FieldSpacecraftState
Build a spacecraft state from orbit, attitude provider and mass.
FieldSpacecraftState(Field<T>, SpacecraftState) - Constructor for class org.orekit.propagation.FieldSpacecraftState
Convert a SpacecraftState.
FieldStateMapper<T extends RealFieldElement<T>> - Class in org.orekit.propagation.integration
This class maps between raw double elements and FieldSpacecraftState instances.
FieldStateMapper(FieldAbsoluteDate<T>, double, OrbitType, PositionAngle, AttitudeProvider, Frame) - Constructor for class org.orekit.propagation.integration.FieldStateMapper
Simple constructor.
FieldStopOnDecreasing<KK extends FieldEventDetector<T>,T extends RealFieldElement<T>> - Class in org.orekit.propagation.events.handlers
Handle a detection event and choose what to do next.
FieldStopOnDecreasing() - Constructor for class org.orekit.propagation.events.handlers.FieldStopOnDecreasing
 
FieldStopOnEvent<KK extends FieldEventDetector<T>,T extends RealFieldElement<T>> - Class in org.orekit.propagation.events.handlers
Event handler which will always return continue as a state.
FieldStopOnEvent() - Constructor for class org.orekit.propagation.events.handlers.FieldStopOnEvent
 
FieldStopOnIncreasing<KK extends FieldEventDetector<T>,T extends RealFieldElement<T>> - Class in org.orekit.propagation.events.handlers
Handle a detection event and choose what to do next.
FieldStopOnIncreasing() - Constructor for class org.orekit.propagation.events.handlers.FieldStopOnIncreasing
 
FieldTimeDerivativesEquations<T extends RealFieldElement<T>> - Interface in org.orekit.propagation.numerical
Interface summing up the contribution of several forces into orbit and mass derivatives.
FieldTimeInterpolable<T extends FieldTimeInterpolable<T,KK>,KK extends RealFieldElement<KK>> - Interface in org.orekit.time
This interface represents objects that can be interpolated in time.
FieldTimeShiftable<T extends FieldTimeInterpolable<T,KK>,KK extends RealFieldElement<KK>> - Interface in org.orekit.time
This interface represents objects that can be shifted in time.
FieldTimeSpanMap<T,D extends RealFieldElement<D>> - Class in org.orekit.utils
Container for objects that apply to spans of time.
FieldTimeSpanMap(T, Field<D>) - Constructor for class org.orekit.utils.FieldTimeSpanMap
Create a map containing a single object, initially valid throughout the timeline.
FieldTimeSpanMap.Transition<S,D extends RealFieldElement<D>> - Class in org.orekit.utils
Local class holding transition times.
FieldTimeStamped<T extends RealFieldElement<T>> - Interface in org.orekit.time
This interface represents objects that have a AbsoluteDate date attached to them.
FieldTransform<T extends RealFieldElement<T>> - Class in org.orekit.frames
Transformation class in three dimensional space.
FieldTransform(Field<T>, Transform) - Constructor for class org.orekit.frames.FieldTransform
Build a transform from a regular transform.
FieldTransform(FieldAbsoluteDate<T>, FieldVector3D<T>) - Constructor for class org.orekit.frames.FieldTransform
Build a translation transform.
FieldTransform(FieldAbsoluteDate<T>, FieldRotation<T>) - Constructor for class org.orekit.frames.FieldTransform
Build a rotation transform.
FieldTransform(FieldAbsoluteDate<T>, FieldVector3D<T>, FieldVector3D<T>) - Constructor for class org.orekit.frames.FieldTransform
Build a translation transform, with its first time derivative.
FieldTransform(FieldAbsoluteDate<T>, FieldVector3D<T>, FieldVector3D<T>, FieldVector3D<T>) - Constructor for class org.orekit.frames.FieldTransform
Build a translation transform, with its first and second time derivatives.
FieldTransform(FieldAbsoluteDate<T>, FieldPVCoordinates<T>) - Constructor for class org.orekit.frames.FieldTransform
Build a translation transform, with its first time derivative.
FieldTransform(FieldAbsoluteDate<T>, FieldRotation<T>, FieldVector3D<T>) - Constructor for class org.orekit.frames.FieldTransform
Build a rotation transform.
FieldTransform(FieldAbsoluteDate<T>, FieldRotation<T>, FieldVector3D<T>, FieldVector3D<T>) - Constructor for class org.orekit.frames.FieldTransform
Build a rotation transform.
FieldTransform(FieldAbsoluteDate<T>, FieldAngularCoordinates<T>) - Constructor for class org.orekit.frames.FieldTransform
Build a rotation transform.
FieldTransform(FieldAbsoluteDate<T>, FieldTransform<T>, FieldTransform<T>) - Constructor for class org.orekit.frames.FieldTransform
Build a transform by combining two existing ones.
FieldTransformGenerator<T extends RealFieldElement<T>> - Class in org.orekit.frames
Generator to use field transforms in GenericTimeStampedCache.
FieldTransformGenerator(Field<T>, int, TransformProvider, double) - Constructor for class org.orekit.frames.FieldTransformGenerator
simple 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(T, FieldVector3D<T>, T[], int) - Method in class org.orekit.orbits.FieldOrbit
Fill a Jacobian half row with a single vector.
fillHalfRow(T, FieldVector3D<T>, T, FieldVector3D<T>, T[], int) - Method in class org.orekit.orbits.FieldOrbit
Fill a Jacobian half row with a linear combination of vectors.
fillHalfRow(T, FieldVector3D<T>, T, FieldVector3D<T>, T, FieldVector3D<T>, T[], int) - Method in class org.orekit.orbits.FieldOrbit
Fill a Jacobian half row with a linear combination of vectors.
fillHalfRow(T, FieldVector3D<T>, T, FieldVector3D<T>, T, FieldVector3D<T>, T, FieldVector3D<T>, T[], int) - Method in class org.orekit.orbits.FieldOrbit
Fill a Jacobian half row with a linear combination of vectors.
fillHalfRow(T, FieldVector3D<T>, T, FieldVector3D<T>, T, FieldVector3D<T>, T, FieldVector3D<T>, T, FieldVector3D<T>, T[], int) - Method in class org.orekit.orbits.FieldOrbit
Fill a Jacobian half row with a linear combination of vectors.
fillHalfRow(T, FieldVector3D<T>, T, FieldVector3D<T>, T, FieldVector3D<T>, T, FieldVector3D<T>, T, FieldVector3D<T>, T, FieldVector3D<T>, T[], int) - Method in class org.orekit.orbits.FieldOrbit
Fill a Jacobian half row with a linear combination of vectors.
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.
filter(boolean) - Method in class org.orekit.utils.ParameterDriversList
Filter parameters to keep only one type of selection status.
FilterType - Enum in org.orekit.propagation.events
Enumerate for filtering events.
findEOP(Frame) - Static method in class org.orekit.frames.FramesFactory
Retrieve EOP from a frame hierarchy.
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.
fit() - Method in class org.orekit.utils.SecularAndHarmonic
Fit parameters.
FixedNumberInterpolationGrid - Class in org.orekit.propagation.semianalytical.dsst.utilities
Interpolation grid where a fixed number of points are evenly spaced between the start and the end of the integration step.
FixedNumberInterpolationGrid(int) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.FixedNumberInterpolationGrid
Constructor.
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.
FLOW_RATE - Static variable in class org.orekit.forces.maneuvers.ConstantThrustManeuver
Parameter name for flow rate.
FootprintOverlapDetector - Class in org.orekit.propagation.events
Detector triggered by geographical region entering/leaving a spacecraft sensor Field Of View.
FootprintOverlapDetector(FieldOfView, OneAxisEllipsoid, SphericalPolygonsSet, double) - Constructor for class org.orekit.propagation.events.FootprintOverlapDetector
Build a new instance.
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.FieldTransform
Get a frozen transform.
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.AngularSeparationDetector
Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.ApsideDetector
Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.BooleanDetector
 
g(SpacecraftState) - Method in class org.orekit.propagation.events.CircularFieldOfViewDetector
Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.DateDetector
Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.EclipseDetector
Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.ElevationDetector
Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.ElevationExtremumDetector
Compute the value of the detection function.
g(SpacecraftState) - Method in interface org.orekit.propagation.events.EventDetector
Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.EventEnablingPredicateFilter
Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.EventShifter
Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.EventSlopeFilter
Compute the value of the switching function.
g(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.events.FieldAbstractDetector
Compute the value of the switching function.
g(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.events.FieldAltitudeDetector
Compute the value of the switching function.
g(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.events.FieldApsideDetector
Compute the value of the switching function.
g(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.events.FieldDateDetector
Compute the value of the switching function.
g(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.events.FieldEclipseDetector
Compute the value of the switching function.
g(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.events.FieldElevationDetector
Compute the value of the switching function.
g(FieldSpacecraftState<T>) - Method in interface org.orekit.propagation.events.FieldEventDetector
Compute the value of the switching function.
g(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.events.FieldNodeDetector
Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.FieldOfViewDetector
Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.FootprintOverlapDetector
Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.GeographicZoneDetector
Compute the value of the detection function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.GroundFieldOfViewDetector
Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.LatitudeCrossingDetector
Compute the value of the detection function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.LatitudeExtremumDetector
Compute the value of the detection function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.LongitudeCrossingDetector
Compute the value of the detection function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.LongitudeExtremumDetector
Compute the value of the detection function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.NegateDetector
 
g(SpacecraftState) - Method in class org.orekit.propagation.events.NodeDetector
Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.PositionAngleDetector
Compute the value of the detection function.
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 Γmn,s(γ) function from equation 2.7.1-(13).
GammaMnsFunction(int, double, int) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.GammaMnsFunction
Simple constructor.
generate(AbsoluteDate, AbsoluteDate) - Method in class org.orekit.frames.FieldTransformGenerator
Generate a chronologically sorted list of entries to be cached.
generate(AbsoluteDate, AbsoluteDate) - Method in class org.orekit.frames.TransformGenerator
Generate a chronologically sorted list of entries to be cached.
generate(AbsoluteDate, AbsoluteDate) - Method in interface org.orekit.utils.TimeStampedGenerator
Generate a chronologically sorted list of entries to be cached.
generateCartesianOrbit() - Method in class org.orekit.files.ccsds.OMMFile
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>) - Constructor for class org.orekit.utils.GenericTimeStampedCache
Simple constructor.
GeodeticPoint - Class in org.orekit.bodies
Point location relative to a 2D body surface.
GeodeticPoint(double, double, double) - Constructor for class org.orekit.bodies.GeodeticPoint
Build a new instance.
GeographicZoneDetector - Class in org.orekit.propagation.events
Detector for entry/exit of a zone defined by geographic boundaries.
GeographicZoneDetector(BodyShape, SphericalPolygonsSet, double) - Constructor for class org.orekit.propagation.events.GeographicZoneDetector
Build a new detector.
GeographicZoneDetector(double, double, BodyShape, SphericalPolygonsSet, double) - Constructor for class org.orekit.propagation.events.GeographicZoneDetector
Build a detector.
Geoid - Class in org.orekit.models.earth
A geoid is a level surface of the gravity potential of a body.
Geoid(NormalizedSphericalHarmonicsProvider, ReferenceEllipsoid) - Constructor for class org.orekit.models.earth.Geoid
Creates a geoid from the given geopotential, reference ellipsoid and the assumptions in the comment for Geoid.
GeoMagneticElements - Class in org.orekit.models.earth
Contains the elements to represent a magnetic field at a single point.
GeoMagneticElements(Vector3D) - Constructor for class org.orekit.models.earth.GeoMagneticElements
Construct a new element with the given field vector.
GeoMagneticField - Class in org.orekit.models.earth
Used to calculate the geomagnetic field at a given geodetic point on earth.
GeoMagneticField(String, double, int, int, double, double) - Constructor for class org.orekit.models.earth.GeoMagneticField
Create a new geomagnetic field model with the given parameters.
GeoMagneticFieldFactory - Class in org.orekit.models.earth
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
 
get(FieldAbsoluteDate<D>) - Method in class org.orekit.utils.FieldTimeSpanMap
Get the entry valid at a specified date.
get(AbsoluteDate) - Method in class org.orekit.utils.TimeSpanMap
Get the entry valid at a specified date.
get24HoursKp(AbsoluteDate) - Method in class org.orekit.forces.drag.atmosphere.data.MarshallSolarActivityFutureEstimation
The Kp index is derived from the Ap index.
get24HoursKp(AbsoluteDate) - Method in interface org.orekit.forces.drag.atmosphere.DTM2000InputParameters
Get the last 24H mean geomagnetic index.
getA() - Method in class org.orekit.bodies.Ellipse
Get the semi major axis.
getA() - Method in class org.orekit.bodies.Ellipsoid
Get the length of the first semi-axis.
getA() - Method in class org.orekit.files.ccsds.OGMFile
Get the orbit semi-major axis.
getA() - Method in class org.orekit.orbits.CartesianOrbit
Get the semi-major axis.
getA() - Method in class org.orekit.orbits.CircularOrbit
Get the semi-major axis.
getA() - Method in class org.orekit.orbits.EquinoctialOrbit
Get the semi-major axis.
getA() - Method in class org.orekit.orbits.FieldCartesianOrbit
Get the semi-major axis.
getA() - Method in class org.orekit.orbits.FieldCircularOrbit
Get the semi-major axis.
getA() - Method in class org.orekit.orbits.FieldEquinoctialOrbit
Get the semi-major axis.
getA() - Method in class org.orekit.orbits.FieldKeplerianOrbit
Get the semi-major axis.
getA() - Method in class org.orekit.orbits.FieldOrbit
Get the semi-major axis.
getA() - Method in class org.orekit.orbits.KeplerianOrbit
Get the semi-major axis.
getA() - Method in class org.orekit.orbits.Orbit
Get the semi-major axis.
getA() - Method in class org.orekit.propagation.FieldSpacecraftState
Get the semi-major axis.
getA() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
Get A = sqrt(μ * a).
getA() - Method in class org.orekit.propagation.SpacecraftState
Get the semi-major axis.
getAbscissaGrid() - Method in class org.orekit.utils.InterpolationTableLoader
Returns a copy of the abscissa grid for the interpolation function.
getAbsoluteDate() - Method in class org.orekit.utils.FieldTimeSpanMap.Transition
Get the transition field absolute date.
getAcceleration() - Method in class org.orekit.frames.FieldTransform
Get the second time derivative of the translation.
getAcceleration() - Method in class org.orekit.frames.Transform
Get the second time derivative of the translation.
getAcceleration() - Method in class org.orekit.utils.FieldPVCoordinates
Gets the acceleration.
getAcceleration() - Method in class org.orekit.utils.PVCoordinates
Gets the acceleration.
getAccuracy() - Method in class org.orekit.files.sp3.SP3File.SP3Ephemeris
Get the formal accuracy for this satellite.
getAction() - Method in class org.orekit.propagation.events.EventState.EventOccurrence
Get the user requested action.
getAction() - Method in class org.orekit.propagation.events.FieldEventState.EventOccurrence
Get the user requested action.
getAdaptedPropagator() - Method in class org.orekit.propagation.conversion.AbstractPropagatorConverter
Get the adapted propagator.
getAdditionalState(SpacecraftState) - Method in interface org.orekit.propagation.AdditionalStateProvider
Get the additional state.
getAdditionalState(FieldSpacecraftState<T>) - Method in interface org.orekit.propagation.FieldAdditionalStateProvider
Get the additional state.
getAdditionalState(String) - Method in class org.orekit.propagation.FieldSpacecraftState
Get an additional state.
getAdditionalState(String) - Method in class org.orekit.propagation.SpacecraftState
Get an additional state.
getAdditionalStateDimension() - Method in class org.orekit.propagation.numerical.JacobiansMapper
Compute the length of the one-dimensional additional state array needed.
getAdditionalStateProviders() - Method in class org.orekit.propagation.AbstractPropagator
Get an unmodifiable list of providers for additional state.
getAdditionalStateProviders() - Method in class org.orekit.propagation.FieldAbstractPropagator
Get an unmodifiable list of providers for additional state.
getAdditionalStateProviders() - Method in interface org.orekit.propagation.FieldPropagator
Get an unmodifiable list of providers for additional state.
getAdditionalStateProviders() - Method in interface org.orekit.propagation.Propagator
Get an unmodifiable list of providers for additional state.
getAdditionalStates() - Method in class org.orekit.propagation.FieldSpacecraftState
Get an unmodifiable map of additional states.
getAdditionalStates() - Method in class org.orekit.propagation.SpacecraftState
Get an unmodifiable map of additional states.
getADot() - Method in class org.orekit.orbits.CartesianOrbit
Get the semi-major axis derivative.
getADot() - Method in class org.orekit.orbits.CircularOrbit
Get the semi-major axis derivative.
getADot() - Method in class org.orekit.orbits.EquinoctialOrbit
Get the semi-major axis derivative.
getADot() - Method in class org.orekit.orbits.FieldCartesianOrbit
Get the semi-major axis derivative.
getADot() - Method in class org.orekit.orbits.FieldCircularOrbit
Get the semi-major axis derivative.
getADot() - Method in class org.orekit.orbits.FieldEquinoctialOrbit
Get the semi-major axis derivative.
getADot() - Method in class org.orekit.orbits.FieldKeplerianOrbit
Get the semi-major axis derivative.
getADot() - Method in class org.orekit.orbits.FieldOrbit
Get the semi-major axis derivative.
getADot() - Method in class org.orekit.orbits.KeplerianOrbit
Get the semi-major axis derivative.
getADot() - Method in class org.orekit.orbits.Orbit
Get the semi-major axis derivative.
getAe() - Method in class org.orekit.forces.gravity.potential.CachedNormalizedSphericalHarmonicsProvider
Get the value of the central body reference radius.
getAe() - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
Get the central body reference radius.
getAe() - Method in interface org.orekit.forces.gravity.potential.SphericalHarmonicsProvider
Get the value of the central body reference radius.
getAf0() - Method in class org.orekit.gnss.GPSAlmanac
Gets the Zeroth Order Clock Correction.
getAf1() - Method in class org.orekit.gnss.GPSAlmanac
Gets the First Order Clock Correction.
getAfter() - Method in class org.orekit.utils.FieldTimeSpanMap.Transition
Get the entry valid after transition.
getAfter() - Method in class org.orekit.utils.TimeSpanMap.Transition
Get the entry valid after transition.
getAgency() - Method in class org.orekit.files.sp3.SP3File
Returns the agency that prepared this SP3 file.
getAlignAngle() - Method in class org.orekit.propagation.events.AlignmentDetector
Get the alignment angle (rad).
getAll() - Method in class org.orekit.utils.ImmutableTimeStampedCache
Get all of the data in this cache.
getAllForceModels() - Method in class org.orekit.propagation.numerical.FieldNumericalPropagator
Get all the force models, perturbing forces and Newtonian attraction included.
getAllForceModels() - Method in class org.orekit.propagation.numerical.NumericalPropagator
Get all the force models, perturbing forces and Newtonian attraction included.
getAlmanacs() - Method in class org.orekit.gnss.SEMParser
Gets all the GPS almanacs read from the file.
getAlmanacs() - Method in class org.orekit.gnss.YUMAParser
Gets all the GPS almanacs read from the file.
getAlpha() - Method in class org.orekit.models.earth.KlobucharIonoCoefficientsLoader
Returns the alpha coefficients array.
getAlpha(PositionAngle) - Method in class org.orekit.orbits.CircularOrbit
Get the latitude argument.
getAlpha(PositionAngle) - Method in class org.orekit.orbits.FieldCircularOrbit
Get the latitude argument.
getAlpha() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
Get direction cosine α for central body.
getAlphaDot(PositionAngle) - Method in class org.orekit.orbits.CircularOrbit
Get the latitude argument derivative.
getAlphaDot(PositionAngle) - Method in class org.orekit.orbits.FieldCircularOrbit
Get the latitude argument derivative.
getAlphaE() - Method in class org.orekit.orbits.CircularOrbit
Get the eccentric latitude argument.
getAlphaE() - Method in class org.orekit.orbits.FieldCircularOrbit
Get the eccentric latitude argument.
getAlphaEDot() - Method in class org.orekit.orbits.CircularOrbit
Get the eccentric latitude argument derivative.
getAlphaEDot() - Method in class org.orekit.orbits.FieldCircularOrbit
Get the eccentric latitude argument derivative.
getAlphaM() - Method in class org.orekit.orbits.CircularOrbit
Get the mean latitude argument.
getAlphaM() - Method in class org.orekit.orbits.FieldCircularOrbit
Get the mean latitude argument.
getAlphaMDot() - Method in class org.orekit.orbits.CircularOrbit
Get the mean latitude argument derivative.
getAlphaMDot() - Method in class org.orekit.orbits.FieldCircularOrbit
Get the mean latitude argument derivative.
getAlphaV() - Method in class org.orekit.orbits.CircularOrbit
Get the true latitude argument.
getAlphaV() - Method in class org.orekit.orbits.FieldCircularOrbit
Get the true latitude argument.
getAlphaVDot() - Method in class org.orekit.orbits.CircularOrbit
Get the true latitude argument derivative.
getAlphaVDot() - Method in class org.orekit.orbits.FieldCircularOrbit
Get the true latitude argument derivative.
getAltitude() - Method in class org.orekit.bodies.FieldGeodeticPoint
Get the altitude.
getAltitude() - Method in class org.orekit.bodies.GeodeticPoint
Get the altitude.
getAltitude() - Method in class org.orekit.propagation.events.AltitudeDetector
Get the threshold altitude value.
getAltitude() - Method in class org.orekit.propagation.events.FieldAltitudeDetector
Get the threshold altitude value.
getAncestor(int) - Method in class org.orekit.frames.Frame
Get the nth ancestor of the frame.
getAngle() - Method in class org.orekit.propagation.events.PositionAngleDetector
Get the fixed angle to be crossed (radians).
getAngleType() - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData
Getter for angleType.
getAngular() - Method in class org.orekit.frames.FieldTransform
Get the underlying elementary angular part.
getAngular() - Method in class org.orekit.frames.Transform
Get the underlying elementary angular part.
getAngularVelocity() - Method in class org.orekit.utils.FieldPVCoordinates
Get the angular velocity (spin) of this point as seen from the origin.
getAngularVelocity() - Method in class org.orekit.utils.PVCoordinates
Get the angular velocity (spin) of this point as seen from the origin.
getAnomaly() - Method in class org.orekit.files.ccsds.OGMFile
Get the orbit anomaly.
getAnomaly(PositionAngle) - Method in class org.orekit.orbits.FieldKeplerianOrbit
Get the anomaly.
getAnomaly(PositionAngle) - Method in class org.orekit.orbits.KeplerianOrbit
Get the anomaly.
getAnomalyDot(PositionAngle) - Method in class org.orekit.orbits.FieldKeplerianOrbit
Get the anomaly derivative.
getAnomalyDot(PositionAngle) - Method in class org.orekit.orbits.KeplerianOrbit
Get the anomaly derivative.
getAnomalyType() - Method in class org.orekit.files.ccsds.OGMFile
Get the type of anomaly (true or mean).
getAp(AbsoluteDate) - Method in interface org.orekit.forces.drag.atmosphere.NRLMSISE00InputParameters
Get the Ap geomagnetic indices.
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(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in interface org.orekit.attitudes.AttitudeProvider
Compute the attitude corresponding to an orbital state.
getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.AttitudesSequence
Compute the attitude corresponding to an orbital state.
getAttitude(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.AttitudesSequence
Compute the attitude corresponding to an orbital state.
getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.CelestialBodyPointed
Compute the attitude corresponding to an orbital state.
getAttitude(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.CelestialBodyPointed
Compute the attitude corresponding to an orbital state.
getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.FixedRate
Compute the attitude corresponding to an orbital state.
getAttitude(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.FixedRate
Compute the attitude corresponding to an orbital state.
getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.GroundPointing
Compute the attitude corresponding to an orbital state.
getAttitude(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.GroundPointing
Compute the attitude corresponding to an orbital state.
getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.InertialProvider
Compute the attitude corresponding to an orbital state.
getAttitude(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.InertialProvider
Compute the attitude corresponding to an orbital state.
getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.LofOffset
Compute the attitude corresponding to an orbital state.
getAttitude(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.LofOffset
Compute the attitude corresponding to an orbital state.
getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.LofOffsetPointing
Compute the attitude corresponding to an orbital state.
getAttitude(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.LofOffsetPointing
Compute the attitude corresponding to an orbital state.
getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.SpinStabilized
Compute the attitude corresponding to an orbital state.
getAttitude(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.SpinStabilized
Compute the attitude corresponding to an orbital state.
getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.TabulatedLofOffset
Compute the attitude corresponding to an orbital state.
getAttitude(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.TabulatedLofOffset
Compute the attitude corresponding to an orbital state.
getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.TabulatedProvider
Compute the attitude corresponding to an orbital state.
getAttitude(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.TabulatedProvider
Compute the attitude corresponding to an orbital state.
getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.YawCompensation
Compute the attitude corresponding to an orbital state.
getAttitude(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.YawCompensation
Compute the attitude corresponding to an orbital state.
getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.YawSteering
Compute the attitude corresponding to an orbital state.
getAttitude(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.YawSteering
Compute the attitude corresponding to an orbital state.
getAttitude() - Method in class org.orekit.propagation.FieldSpacecraftState
Get the attitude.
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.FieldAbstractPropagator
Get attitude provider.
getAttitudeProvider() - Method in interface org.orekit.propagation.FieldPropagator
Get attitude provider.
getAttitudeProvider() - Method in class org.orekit.propagation.integration.FieldStateMapper
Get the attitude provider.
getAttitudeProvider() - Method in class org.orekit.propagation.integration.StateMapper
Get the attitude provider.
getAttitudeProvider() - Method in interface org.orekit.propagation.Propagator
Get attitude provider.
getAvailableDerivatives() - Method in class org.orekit.files.ccsds.OEMFile.EphemeridesBlock
 
getAvailableDerivatives() - Method in interface org.orekit.files.general.EphemerisFile.EphemerisSegment
Get which derivatives of position are available in this ephemeris segment.
getAvailableDerivatives() - Method in class org.orekit.files.general.OrekitEphemerisFile.OrekitEphemerisSegment
 
getAvailableDerivatives() - Method in class org.orekit.files.sp3.SP3File.SP3Ephemeris
 
getAvailableSatelliteNumbers() - Method in class org.orekit.propagation.analytical.tle.TLESeries
Deprecated.
Get the available satellite numbers.
getAverageFlux(AbsoluteDate) - Method in interface org.orekit.forces.drag.atmosphere.NRLMSISE00InputParameters
Get the value of the 81 day average of F10.7 solar flux centered on current day.
getAzimuth(Vector3D, Frame, AbsoluteDate) - Method in class org.orekit.frames.TopocentricFrame
Get the azimuth of a point with regards to the topocentric frame center point.
getB() - Method in class org.orekit.bodies.Ellipse
Get the semi minor axis.
getB() - Method in class org.orekit.bodies.Ellipsoid
Get the length of the second semi-axis.
getB() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
Get B = sqrt(1 - e²).
getBaseFrame() - Method in class org.orekit.estimation.measurements.GroundStation
Get the base frame associated with the station.
getBaseState(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.YawCompensation
Compute the base system state at given date, without compensation.
getBaseState(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.YawCompensation
Compute the base system state at given date, without compensation.
getBaseState(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.YawSteering
Compute the base system state at given date, without compensation.
getBaseState(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.YawSteering
Compute the base system state at given date, without compensation.
getBaseWeight() - Method in class org.orekit.estimation.measurements.AbstractMeasurement
Get the base weight associated with the measurement
getBaseWeight() - Method in interface org.orekit.estimation.measurements.ObservedMeasurement
Get the base weight associated with the measurement
getBasicDimension() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
Get state vector dimension without additional parameters.
getBasicDimension() - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator
Get state vector dimension without additional parameters.
getBeacon() - Method in class org.orekit.propagation.events.AngularSeparationDetector
Get the beacon at the center of the proximity zone.
getBefore() - Method in class org.orekit.utils.FieldTimeSpanMap.Transition
Get the entry valid before transition.
getBefore() - Method in class org.orekit.utils.TimeSpanMap.Transition
Get the entry valid before transition.
getBeta() - Method in class org.orekit.models.earth.KlobucharIonoCoefficientsLoader
Returns the beta coefficients array.
getBeta() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
Get direction cosine β for central body.
getBody(String) - Static method in class org.orekit.bodies.CelestialBodyFactory
Get a celestial body.
getBody() - Method in class org.orekit.propagation.events.FootprintOverlapDetector
Get the body on which the geographic zone is defined.
getBody() - Method in class org.orekit.propagation.events.GeographicZoneDetector
Get the body on which the geographic zone is defined.
getBody() - Method in class org.orekit.propagation.events.LatitudeCrossingDetector
Get the body on which the geographic zone is defined.
getBody() - Method in class org.orekit.propagation.events.LatitudeExtremumDetector
Get the body on which the geographic zone is defined.
getBody() - Method in class org.orekit.propagation.events.LongitudeCrossingDetector
Get the body on which the geographic zone is defined.
getBody() - Method in class org.orekit.propagation.events.LongitudeExtremumDetector
Get the body on which the geographic zone is defined.
getBody() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBody
Get third body.
getBodyFrame() - Method in class org.orekit.attitudes.GroundPointing
Get the body frame.
getBodyFrame() - Method in interface org.orekit.bodies.BodyShape
Get body frame related to body shape.
getBodyFrame() - Method in class org.orekit.bodies.OneAxisEllipsoid
Get body frame related to body shape.
getBodyFrame() - Method in class org.orekit.models.earth.Geoid
 
getBodyOrientedFrame() - Method in interface org.orekit.bodies.CelestialBody
Get a body oriented, body centered frame.
getBodyShape() - Method in class org.orekit.propagation.events.AltitudeDetector
Get the body shape.
getBodyShape() - Method in class org.orekit.propagation.events.FieldAltitudeDetector
Get the body shape.
getBStar() - Method in class org.orekit.files.ccsds.OMMFile
Get the SGP/SGP4 drag-like coefficient.
getBStar() - Method in class org.orekit.propagation.analytical.tle.TLE
Get the ballistic coefficient.
getC() - Method in class org.orekit.bodies.Ellipsoid
Get the length of the third semi-axis.
getC() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
Get C = 1 + p² + q².
getC2n0(int) - Method in class org.orekit.models.earth.ReferenceEllipsoid
Get the fully normalized coefficient C2n,0 for the normal gravity potential.
getCacheSlotsNumber() - Static method in class org.orekit.utils.OrekitConfiguration
Get the number of slots to use in caches.
getCalendarWeek() - Method in class org.orekit.time.DateComponents
Get the calendar week number.
getCalls() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
Get the number of calls to the differential equations computation method.
getCalls() - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator
Get the number of calls to the differential equations computation method.
getCapitalizedAbbreviation() - Method in enum org.orekit.time.Month
Get the capitalized three letters abbreviation.
getCapitalizedName() - Method in enum org.orekit.time.Month
Get the capitalized full name.
getCartesian() - Method in class org.orekit.frames.FieldTransform
Get the underlying elementary Cartesian part.
getCartesian() - Method in class org.orekit.frames.Transform
Get the underlying elementary Cartesian part.
getCCSDSEpoch(Field<T>) - Static method in class org.orekit.time.FieldAbsoluteDate
Reference epoch for CCSDS Time Code Format (CCSDS 301.0-B-4): 1958-01-01T00:00:00 International Atomic Time (not UTC).
getCelestialBody() - Method in enum org.orekit.files.ccsds.CenterName
Get the celestial body corresponding to the CCSDS constant.
getCenter() - Method in class org.orekit.bodies.Ellipse
Get the center of the 2D ellipse.
getCenter() - Method in class org.orekit.models.earth.tessellation.Tile
Get the center point.
getCenter() - Method in class org.orekit.propagation.events.CircularFieldOfViewDetector
Get the direction of FOV center.
getCenterBody() - Method in class org.orekit.files.ccsds.ODMMetaData
Get the CelestialBody corresponding to the center name.
getCenterName() - Method in class org.orekit.files.ccsds.CcsdsModifiedFrame
Get the CCSDS center name.
getCenterName() - Method in class org.orekit.files.ccsds.ODMMetaData
Get the origin of reference frame.
getCenterOfCurvature(Vector2D) - Method in class org.orekit.bodies.Ellipse
Find the center of curvature (point on the evolute) at the nadir of a point.
getChildren() - Method in class org.orekit.frames.OrphanFrame
Get all children of the instance.
getCic() - Method in class org.orekit.gnss.GPSAlmanac
 
getCic() - Method in interface org.orekit.propagation.analytical.gnss.GPSOrbitalElements
Gets the Amplitude of the Cosine Harmonic Correction Term to the Angle of Inclination.
getCircularEx() - Method in class org.orekit.orbits.CircularOrbit
Get the first component of the circular eccentricity vector.
getCircularEx() - Method in class org.orekit.orbits.FieldCircularOrbit
Get the first component of the circular eccentricity vector.
getCircularExDot() - Method in class org.orekit.orbits.CircularOrbit
Get the first component of the circular eccentricity vector derivative.
getCircularExDot() - Method in class org.orekit.orbits.FieldCircularOrbit
Get the first component of the circular eccentricity vector derivative.
getCircularEy() - Method in class org.orekit.orbits.CircularOrbit
Get the second component of the circular eccentricity vector.
getCircularEy() - Method in class org.orekit.orbits.FieldCircularOrbit
Get the second component of the circular eccentricity vector.
getCircularEyDot() - Method in class org.orekit.orbits.CircularOrbit
Get the second component of the circular eccentricity vector derivative.
getCircularEyDot() - Method in class org.orekit.orbits.FieldCircularOrbit
Get the second component of the circular eccentricity vector derivative.
getCIRF(IERSConventions, boolean) - Static method in class org.orekit.frames.FramesFactory
Get the CIRF2000 reference frame.
getCis() - Method in class org.orekit.gnss.GPSAlmanac
 
getCis() - Method in interface org.orekit.propagation.analytical.gnss.GPSOrbitalElements
Gets the Amplitude of the Sine Harmonic Correction Term to the Angle of Inclination.
getCj(int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.CjSjCoefficient
Get the Cj coefficient.
getClassification() - Method in class org.orekit.propagation.analytical.tle.TLE
Get the classification.
getClassificationType() - Method in class org.orekit.files.ccsds.OMMFile
Get the classification type.
getClockCorrection() - Method in class org.orekit.files.sp3.SP3File.SP3Coordinate
Returns the clock correction value.
getClockRateChange() - Method in class org.orekit.files.sp3.SP3File.SP3Coordinate
Returns the clock rate.
getClosestTLE(AbsoluteDate) - Method in class org.orekit.propagation.analytical.tle.TLESeries
Deprecated.
Get the closest TLE to the selected date.
getCoefficients() - Method in enum org.orekit.forces.gravity.potential.OceanLoadDeformationCoefficients
Get the load deformation coefficients for ocean tides.
getCoefficients(String) - Method in class org.orekit.models.earth.displacement.OceanLoadingCoefficientsBLQFactory
Get the coefficients for a given site.
getCoefficients(AbsoluteDate, Set<String>) - Method in interface org.orekit.propagation.semianalytical.dsst.forces.ShortPeriodTerms
Computes the coefficients involved in the contributions.
getCoefficientsKeyPrefix() - Method in interface org.orekit.propagation.semianalytical.dsst.forces.ShortPeriodTerms
Get the prefix for short period coefficients keys.
getComment() - Method in class org.orekit.files.ccsds.ODMMetaData
Get the meta-data comment.
getComment() - Method in class org.orekit.files.ccsds.OPMFile.Maneuver
Get the maneuvers data comment, each string in the list corresponds to one line of comment.
getComment() - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData
Get the meta-data comment.
getComponents(TimeScale) - Method in class org.orekit.time.AbsoluteDate
Split the instance into date/time components.
getComponents(int) - Method in class org.orekit.time.AbsoluteDate
Split the instance into date/time components for a local time.
getComponents(TimeZone) - Method in class org.orekit.time.AbsoluteDate
Split the instance into date/time components for a time zone.
getComponents(TimeScale) - Method in class org.orekit.time.FieldAbsoluteDate
Split the instance into date/time components.
getComponents(int) - Method in class org.orekit.time.FieldAbsoluteDate
Split the instance into date/time components for a local time.
getComponents(TimeZone) - Method in class org.orekit.time.FieldAbsoluteDate
Split the instance into date/time components for a time zone.
getConstantNormalizedProvider(int, int) - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory
Get the constant gravity field coefficients provider from the first supported file.
getConstantProvider(boolean, int, int) - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
Get a time-independent provider for read spherical harmonics coefficients.
getConstantUnnormalizedProvider(int, int) - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory
Get the constant gravity field coefficients provider from the first supported file.
getConventions() - Method in class org.orekit.files.ccsds.ODMFile
Get IERS conventions.
getConventions() - Method in class org.orekit.files.ccsds.ODMParser
Get IERS conventions.
getConventions() - Method in class org.orekit.files.ccsds.TDMParser
Get IERS conventions.
getConventions() - Method in class org.orekit.frames.EOPHistory
Get the IERS conventions to which these EOP apply.
getCoordinates(SpacecraftState, int, DSFactory) - Static method in class org.orekit.estimation.measurements.AbstractMeasurement
Get Cartesian coordinates as derivatives.
getCoordinates() - Method in class org.orekit.files.ccsds.OEMFile.EphemeridesBlock
 
getCoordinates() - Method in interface org.orekit.files.general.EphemerisFile.EphemerisSegment
Get the coordinates for this ephemeris segment.
getCoordinates() - Method in class org.orekit.files.general.OrekitEphemerisFile.OrekitEphemerisSegment
 
getCoordinates() - Method in class org.orekit.files.sp3.SP3File.SP3Ephemeris
 
getCoordinateSystem() - Method in class org.orekit.files.sp3.SP3File
Returns the coordinate system of the entries in this orbit file.
getCorrectionAngle1() - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData
Getter for the correctionAngle1.
getCorrectionAngle2() - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData
Getter for the correctionAngle2.
getCorrectionDoppler() - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData
Getter for the correctionDoppler.
getCorrectionRange() - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData
Getter for the correctionRange.
getCorrectionReceive() - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData
Getter for the correctionReceive.
getCorrectionsApplied() - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData
Getter for the correctionApplied.
getCorrectionTransmit() - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData
Getter for the correctionTransmit.
getCount() - Method in class org.orekit.estimation.measurements.EstimatedMeasurement
Get the evaluations counter.
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.
getCrc() - Method in class org.orekit.gnss.GPSAlmanac
 
getCrc() - Method in interface org.orekit.propagation.analytical.gnss.GPSOrbitalElements
Gets the Amplitude of the Cosine Harmonic Correction Term to the Orbit Radius.
getCreationDate() - Method in class org.orekit.files.ccsds.ODMFile
Get the file creation date and time in UTC.
getCreationDate() - Method in class org.orekit.files.ccsds.TDMFile
Get the file creation date and time in UTC.
getCrs() - Method in class org.orekit.gnss.GPSAlmanac
 
getCrs() - Method in interface org.orekit.propagation.analytical.gnss.GPSOrbitalElements
Gets the Amplitude of the Sine Harmonic Correction Term to the Orbit Radius.
getCuc() - Method in class org.orekit.gnss.GPSAlmanac
 
getCuc() - Method in interface org.orekit.propagation.analytical.gnss.GPSOrbitalElements
Gets the Amplitude of the Cosine Harmonic Correction Term to the Argument of Latitude.
getCurrentState() - Method in interface org.orekit.propagation.sampling.FieldOrekitStepInterpolator
Get the state at previous grid point date.
getCurrentState() - Method in interface org.orekit.propagation.sampling.OrekitStepInterpolator
Get the state at current grid point date.
getCurrentWeight() - Method in class org.orekit.estimation.measurements.EstimatedMeasurement
Get the current weight.
getCus() - Method in class org.orekit.gnss.GPSAlmanac
 
getCus() - Method in interface org.orekit.propagation.analytical.gnss.GPSOrbitalElements
Gets the Amplitude of the Sine Harmonic Correction Term to the Argument of Latitude.
getD() - Method in class org.orekit.data.DelaunayArguments
Get the mean elongation of the Moon from the Sun.
getD() - Method in class org.orekit.data.FieldDelaunayArguments
Get the mean elongation of the Moon from the Sun.
getDailyFlux(AbsoluteDate) - Method in interface org.orekit.forces.drag.atmosphere.NRLMSISE00InputParameters
Get the value of the daily F10.7 solar flux for previous day.
getDataQuality() - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData
Getter for the dataQuality.
getDataUsed() - Method in class org.orekit.files.sp3.SP3File
Returns the data used indicator from the SP3 file.
getDate() - Method in class org.orekit.attitudes.Attitude
Get the date of attitude parameters.
getDate() - Method in class org.orekit.attitudes.FieldAttitude
Get the date of attitude parameters.
getDate() - Method in class org.orekit.data.DelaunayArguments
Get the date.
getDate() - Method in class org.orekit.data.FieldDelaunayArguments
Get the date.
getDate() - Method in class org.orekit.estimation.measurements.AbstractMeasurement
Get the date.
getDate() - Method in class org.orekit.estimation.measurements.EstimatedMeasurement
Get the date.
getDate() - Method in class org.orekit.forces.maneuvers.SmallManeuverAnalyticalModel
Get the date of the maneuver.
getDate() - Method in class org.orekit.frames.EOPEntry
Get the date.
getDate() - Method in class org.orekit.frames.FieldTransform
Get the date.
getDate() - Method in class org.orekit.frames.Transform
Get the date.
getDate() - Method in class org.orekit.gnss.DOP
Gets the calculation date of the DOP.
getDate() - Method in class org.orekit.gnss.GPSAlmanac
 
getDate() - Method in class org.orekit.orbits.FieldOrbit
Get the date of orbital parameters.
getDate() - Method in class org.orekit.orbits.Orbit
Get the date of orbital parameters.
getDate() - Method in class org.orekit.propagation.analytical.tle.TLE
Get the TLE current date.
getDate() - Method in class org.orekit.propagation.events.DateDetector
Get the current event date according to the propagator.
getDate() - Method in class org.orekit.propagation.events.FieldDateDetector
Get the current event date according to the propagator.
getDate() - Method in class org.orekit.propagation.FieldSpacecraftState
Get the date.
getDate() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
Get the date of the orbit.
getDate() - Method in class org.orekit.propagation.SpacecraftState
Get the date.
getDate() - Method in class org.orekit.time.AbsoluteDate
Get the date.
getDate() - Method in class org.orekit.time.DateTimeComponents
Get the date component.
getDate() - Method in class org.orekit.time.FieldAbsoluteDate
Get the date.
getDate() - Method in interface org.orekit.time.FieldTimeStamped
Get the date.
getDate() - Method in interface org.orekit.time.TimeStamped
Get the date.
getDate() - Method in class org.orekit.utils.FieldTimeSpanMap.Transition
Get the transition absolute date.
getDate() - Method in class org.orekit.utils.TimeSpanMap.Transition
Get the transition date.
getDate() - Method in class org.orekit.utils.TimeStampedAngularCoordinates
Get the date.
getDate() - Method in class org.orekit.utils.TimeStampedFieldAngularCoordinates
Get the date.
getDate() - Method in class org.orekit.utils.TimeStampedFieldPVCoordinates
Get the date.
getDate() - Method in class org.orekit.utils.TimeStampedPVCoordinates
Get the date.
getDay() - Method in class org.orekit.time.DateComponents
Get the day.
getDayFraction() - Method in class org.orekit.files.sp3.SP3File
Returns the day fraction for this SP3 file.
getDayOfWeek() - Method in class org.orekit.time.DateComponents
Get the day of week.
getDayOfYear() - Method in class org.orekit.time.DateComponents
Get the day number in year.
getDcjDh(int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.CjSjCoefficient
Get the dCj / dh coefficient.
getDcjDk(int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.CjSjCoefficient
Get the dCj / dk coefficient.
getDdEps() - Method in class org.orekit.frames.EOPEntry
Get the correction for nutation in obliquity δΔε.
getDDot() - Method in class org.orekit.data.DelaunayArguments
Get the mean elongation of the Moon from the Sun time derivative.
getDDot() - Method in class org.orekit.data.FieldDelaunayArguments
Get the mean elongation of the Moon from the Sun time derivative.
getDdPsi() - Method in class org.orekit.frames.EOPEntry
Get the correction for nutation in longitude δΔΨ.
getDecimalYear(int, int, int) - Static method in class org.orekit.models.earth.GeoMagneticField
Utility function to get a decimal year for a given day.
getDeclination() - Method in class org.orekit.models.earth.GeoMagneticElements
Returns the declination of the magnetic field in degrees.
getDecreasingTimeShift() - Method in class org.orekit.propagation.events.EventShifter
Get the decreasing events time shift.
getDefaultModel() - Static method in class org.orekit.models.earth.FixedTroposphericDelay
Returns the default model, loading delay values from the file "tropospheric-delay.txt".
getDelaunayMultipliers() - Method in class org.orekit.models.earth.displacement.Tide
Get the multipliers for Delaunay arguments (l, l', F, D, Ω).
getDeltaMass() - Method in class org.orekit.files.ccsds.OPMFile.Maneuver
Get mass change during maneuver (value is < 0).
getDeltaVSat() - Method in class org.orekit.forces.maneuvers.ImpulseManeuver
Get the velocity increment in satellite frame.
getDensity(AbsoluteDate, Vector3D, Frame) - Method in interface org.orekit.forces.drag.atmosphere.Atmosphere
Get the local density.
getDensity(FieldAbsoluteDate<T>, FieldVector3D<T>, Frame) - Method in interface org.orekit.forces.drag.atmosphere.Atmosphere
Get the local density.
getDensity(int, double, double, double, double, double, double, double, double) - Method in class org.orekit.forces.drag.atmosphere.DTM2000
Get the local density with initial entries.
getDensity(int, T, T, T, T, double, double, double, double) - Method in class org.orekit.forces.drag.atmosphere.DTM2000
Get the local density with initial entries.
getDensity(AbsoluteDate, Vector3D, Frame) - Method in class org.orekit.forces.drag.atmosphere.DTM2000
Get the local density.
getDensity(FieldAbsoluteDate<T>, FieldVector3D<T>, Frame) - Method in class org.orekit.forces.drag.atmosphere.DTM2000
Get the local density.
getDensity(Vector3D, Vector3D) - Method in class org.orekit.forces.drag.atmosphere.HarrisPriester
Get the local density.
getDensity(Vector3D, FieldVector3D<T>) - Method in class org.orekit.forces.drag.atmosphere.HarrisPriester
Get the local density.
getDensity(AbsoluteDate, Vector3D, Frame) - Method in class org.orekit.forces.drag.atmosphere.HarrisPriester
Get the local density at some position.
getDensity(FieldAbsoluteDate<T>, FieldVector3D<T>, Frame) - Method in class org.orekit.forces.drag.atmosphere.HarrisPriester
Get the local density at some position.
getDensity(double, double, double, double, double, double, double, double, double, double, double, double, double, double, double) - Method in class org.orekit.forces.drag.atmosphere.JB2008
Get the local density with initial entries.
getDensity(T, T, T, T, T, T, double, double, double, double, double, double, double, double, double) - Method in class org.orekit.forces.drag.atmosphere.JB2008
Get the local density with initial entries.
getDensity(AbsoluteDate, Vector3D, Frame) - Method in class org.orekit.forces.drag.atmosphere.JB2008
Get the local density.
getDensity(FieldAbsoluteDate<T>, FieldVector3D<T>, Frame) - Method in class org.orekit.forces.drag.atmosphere.JB2008
Get the local density.
getDensity(int) - Method in class org.orekit.forces.drag.atmosphere.NRLMSISE00.FieldOutput
Get one of the stored densities.
getDensity(AbsoluteDate, Vector3D, Frame) - Method in class org.orekit.forces.drag.atmosphere.NRLMSISE00
Get the local density.
getDensity(FieldAbsoluteDate<T>, FieldVector3D<T>, Frame) - Method in class org.orekit.forces.drag.atmosphere.NRLMSISE00
Get the local density.
getDensity(AbsoluteDate, Vector3D, Frame) - Method in class org.orekit.forces.drag.atmosphere.SimpleExponentialAtmosphere
Get the local density.
getDensity(FieldAbsoluteDate<T>, FieldVector3D<T>, Frame) - Method in class org.orekit.forces.drag.atmosphere.SimpleExponentialAtmosphere
 
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 dKj-n-1, s / de².
getDerivative(int, double) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenThirdBodyLinear
Compute the value of the Hansen coefficient dK₀n, s / dΧ.
getDerivative(int, double) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenZonalLinear
Get the dK₀-n-1,s / dΧ coefficient derivative.
getDerivativesDrivers() - Method in class org.orekit.estimation.measurements.EstimatedMeasurement
Get all the drivers with set derivatives.
getDetector() - Method in class org.orekit.propagation.events.handlers.RecordAndContinue.Event
Get the detector.
getdGjsdAlpha(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
Get the dGjs / dα coefficient.
getdGjsdBeta(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
Get the dGjs / dβ coefficient.
getdGjsdh(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
Get the dGjs / dh coefficient.
getdGjsdk(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
Get the dGjs / dk coefficient.
getdGmsdAlpha(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHmsjPolynomials
Get the dGmsj / dα coefficient.
getdGmsdBeta(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHmsjPolynomials
Get the dGmsj / dβ coefficient.
getdGmsdh(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHmsjPolynomials
Get the dGmsj / dh coefficient.
getdGmsdk(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHmsjPolynomials
Get the dGmsj / dk coefficient.
getdHjsdAlpha(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
Get the dHjs / dα coefficient.
getdHjsdBeta(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
Get the dHjs / dβ coefficient.
getdHjsdh(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
Get the dHjs / dh coefficient.
getdHjsdk(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
Get the dHjs / dk coefficient.
getdHmsdAlpha(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHmsjPolynomials
Get the dHmsj / dα coefficient.
getdHmsdBeta(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHmsjPolynomials
Get the dHmsj / dβ coefficient.
getdHmsdh(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHmsjPolynomials
Get the dHmsj / dh coefficient.
getdHmsdk(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHmsjPolynomials
Get the dHmsj / dk coefficient.
getdIjsdAlpha(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
Get the dIjs / dα coefficient.
getdIjsdBeta(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
Get the dIjs / dβ coefficient.
getdIjsdh(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
Get the dIjs / dh coefficient.
getdIjsdk(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
Get the dIjs / dk coefficient.
getDimension() - Method in class org.orekit.estimation.measurements.AbstractMeasurement
Get the dimension of the measurement.
getDimension() - Method in interface org.orekit.estimation.measurements.ObservedMeasurement
Get the dimension of the measurement.
getDisplacements() - Method in class org.orekit.estimation.measurements.GroundStation
Get the displacement models.
getdJjsdAlpha(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
Get the dJjs / dα coefficient.
getdJjsdBeta(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
Get the dJjs / dβ coefficient.
getdJjsdh(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
Get the dJjs / dh coefficient.
getdJjsdk(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
Get the dJjs / dk coefficient.
getdLnsdGamma(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.LnsCoefficients
Get the value of dLns / dγ (γ).
getDnl(double, double, int, int) - Static method in class org.orekit.propagation.semianalytical.dsst.utilities.UpperBounds
Get the upper bound value Dnl(Χ).
getDoodson() - Method in class org.orekit.forces.gravity.potential.OceanTidesWave
Get the Doodson number for the wave.
getDoodsonMultipliers() - Method in class org.orekit.models.earth.displacement.Tide
Get the multipliers for Doodson arguments (τ, s, h, p, N', ps).
getDoodsonNumber() - Method in class org.orekit.models.earth.displacement.Tide
Get the Doodson number.
getDragArea() - Method in class org.orekit.files.ccsds.OGMFile
Get the drag area.
getDragCoeff() - Method in class org.orekit.files.ccsds.OGMFile
Get the drag coefficient.
getDragParametersDrivers() - Method in class org.orekit.forces.BoxAndSolarArraySpacecraft
Get the drivers for supported parameters.
getDragParametersDrivers() - Method in interface org.orekit.forces.drag.DragSensitive
Get the drivers for supported parameters.
getDragParametersDrivers() - Method in class org.orekit.forces.drag.IsotropicDrag
Get the drivers for supported parameters.
getDrivers(double, Orbit, PositionAngle) - Method in enum org.orekit.orbits.OrbitType
Get parameters drivers initialized from a reference orbit.
getDrivers() - Method in class org.orekit.utils.ParameterDriversList
Get delegating drivers for all parameters.
getDsjDh(int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.CjSjCoefficient
Get the dSj / dh coefficient.
getDsjDk(int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.CjSjCoefficient
Get the dSj / dk coefficient.
getDSTDTC(AbsoluteDate) - Method in interface org.orekit.forces.drag.atmosphere.JB2008InputParameters
Get the temperature change computed from Dst index.
getDuration() - Method in class org.orekit.files.ccsds.OPMFile.Maneuver
Get duration (value is 0 for impulsive maneuver).
getDV() - Method in class org.orekit.files.ccsds.OPMFile.Maneuver
Get velocity increment.
getDx() - Method in class org.orekit.frames.EOPEntry
Get the correction for Celestial Intermediate Pole (CIP) coordinates.
getDy() - Method in class org.orekit.frames.EOPEntry
Get the correction for Celestial Intermediate Pole (CIP) coordinates.
getE() - Method in class org.orekit.files.ccsds.OGMFile
Get the orbit eccentricity.
getE() - Method in class org.orekit.gnss.GPSAlmanac
 
getE() - Method in class org.orekit.orbits.CartesianOrbit
Get the eccentricity.
getE() - Method in class org.orekit.orbits.CircularOrbit
Get the eccentricity.
getE() - Method in class org.orekit.orbits.EquinoctialOrbit
Get the eccentricity.
getE() - Method in class org.orekit.orbits.FieldCartesianOrbit
Get the eccentricity.
getE() - Method in class org.orekit.orbits.FieldCircularOrbit
Get the eccentricity.
getE() - Method in class org.orekit.orbits.FieldEquinoctialOrbit
Get the eccentricity.
getE() - Method in class org.orekit.orbits.FieldKeplerianOrbit
Get the eccentricity.
getE() - Method in class org.orekit.orbits.FieldOrbit
Get the eccentricity.
getE() - Method in class org.orekit.orbits.KeplerianOrbit
Get the eccentricity.
getE() - Method in class org.orekit.orbits.Orbit
Get the eccentricity.
getE() - Method in interface org.orekit.propagation.analytical.gnss.GPSOrbitalElements
Gets the Eccentricity.
getE() - Method in class org.orekit.propagation.analytical.tle.TLE
Get the eccentricity.
getE() - Method in class org.orekit.propagation.FieldSpacecraftState
Get the eccentricity.
getE() - Method in class org.orekit.propagation.SpacecraftState
Get the eccentricity.
getEarliest() - Method in class org.orekit.utils.GenericTimeStampedCache
Get the earliest cached entry.
getEarliest() - Method in class org.orekit.utils.ImmutableTimeStampedCache
 
getEarliest() - Method in interface org.orekit.utils.TimeStampedCache
Get the earliest entry in this cache.
getEarth() - Static method in class org.orekit.bodies.CelestialBodyFactory
Get the Earth singleton body.
getEarthMoonBarycenter() - Static method in class org.orekit.bodies.CelestialBodyFactory
Get the Earth-Moon barycenter singleton bodies pair.
getEarthOrientationAngleFunction(TimeScale) - Method in enum org.orekit.utils.IERSConventions
Get the function computing the raw Earth Orientation Angle.
getEast() - Method in class org.orekit.bodies.FieldGeodeticPoint
Get the direction to the east of point, expressed in parent shape frame.
getEast() - Method in class org.orekit.bodies.GeodeticPoint
Get the direction to the east of point, expressed in parent shape frame.
getEast() - Method in class org.orekit.frames.TopocentricFrame
Get the east direction of topocentric frame, expressed in parent shape frame.
getEastOffsetDriver() - Method in class org.orekit.estimation.measurements.GroundStation
Get a driver allowing to change station position along East axis.
getEcc() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
Get the eccentricity.
getEccentricAnomaly() - Method in class org.orekit.orbits.FieldKeplerianOrbit
Get the eccentric anomaly.
getEccentricAnomaly() - Method in class org.orekit.orbits.KeplerianOrbit
Get the eccentric anomaly.
getEccentricAnomalyDot() - Method in class org.orekit.orbits.FieldKeplerianOrbit
Get the eccentric anomaly derivative.
getEccentricAnomalyDot() - Method in class org.orekit.orbits.KeplerianOrbit
Get the eccentric anomaly derivative.
getECEF() - Method in class org.orekit.propagation.analytical.gnss.GPSPropagator
Gets the Earth Centered Earth Fixed frame used to propagate GPS orbits according to the GPS Interface Specification.
getECI() - Method in class org.orekit.propagation.analytical.gnss.GPSPropagator
Gets the Earth Centered Inertial frame used to propagate the orbit.
getEcliptic(IERSConventions) - Static method in class org.orekit.frames.FramesFactory
Get the ecliptic frame.
getEDot() - Method in class org.orekit.orbits.CartesianOrbit
Get the eccentricity derivative.
getEDot() - Method in class org.orekit.orbits.CircularOrbit
Get the eccentricity derivative.
getEDot() - Method in class org.orekit.orbits.EquinoctialOrbit
Get the eccentricity derivative.
getEDot() - Method in class org.orekit.orbits.FieldCartesianOrbit
Get the eccentricity derivative.
getEDot() - Method in class org.orekit.orbits.FieldCircularOrbit
Get the eccentricity derivative.
getEDot() - Method in class org.orekit.orbits.FieldEquinoctialOrbit
Get the eccentricity derivative.
getEDot() - Method in class org.orekit.orbits.FieldKeplerianOrbit
Get the eccentricity derivative.
getEDot() - Method in class org.orekit.orbits.FieldOrbit
Get the eccentricity derivative.
getEDot() - Method in class org.orekit.orbits.KeplerianOrbit
Get the eccentricity derivative.
getEDot() - Method in class org.orekit.orbits.Orbit
Get the eccentricity derivative.
getEffects() - Method in class org.orekit.propagation.analytical.AdapterPropagator
Get the differential effects.
getElem(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.PolynomialFunctionMatrix
Get the value of an element.
getElementNumber() - Method in class org.orekit.propagation.analytical.tle.TLE
Get the element number.
getElementSetNumber() - Method in class org.orekit.files.ccsds.OMMFile
Get the element set number for this satellite.
getElevation(Vector3D, Frame, AbsoluteDate) - Method in class org.orekit.frames.TopocentricFrame
Get the elevation of a point with regards to the local point.
getElevation(SpacecraftState) - Method in class org.orekit.propagation.events.ElevationExtremumDetector
Get the elevation value.
getElevation(double) - Method in class org.orekit.utils.ElevationMask
Get the interpolated elevation for a given azimuth according to the mask.
getElevationMask() - Method in class org.orekit.gnss.DOPComputer
Get the elevation mask.
getElevationMask() - Method in class org.orekit.propagation.events.ElevationDetector
Returns the currently configured elevation mask.
getElevationMask() - Method in class org.orekit.propagation.events.FieldElevationDetector
Returns the currently configured elevation mask.
getEllipsoid() - Method in interface org.orekit.models.earth.EarthShape
Get the underlying ellipsoid model that defines latitude and longitude.
getEllipsoid() - Method in class org.orekit.models.earth.Geoid
 
getEllipsoid() - Method in class org.orekit.models.earth.ReferenceEllipsoid
 
getEME2000() - Static method in class org.orekit.frames.FramesFactory
Get the unique EME2000 frame.
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() - Method in interface org.orekit.frames.EOPBasedTransformProvider
Get the EOP history.
getEOPHistory(IERSConventions, boolean) - Static method in class org.orekit.frames.FramesFactory
Get Earth Orientation Parameters history.
getEOPHistory() - Method in class org.orekit.frames.GTODProvider
Get the EOP history.
getEOPHistory() - 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.
getEphemeridesDataLinesComment() - Method in class org.orekit.files.ccsds.OEMFile.EphemeridesBlock
Get the ephemerides data lines comment.
getEphemerisType() - Method in class org.orekit.files.ccsds.OMMFile
Get the ephemeris type.
getEphemerisType() - Method in class org.orekit.propagation.analytical.tle.TLE
Get the type of ephemeris.
getEpoch() - Method in class org.orekit.files.ccsds.OEMFile.CovarianceMatrix
Get the epoch relative to the covariance matrix.
getEpoch() - Method in class org.orekit.files.ccsds.OGMFile
Get epoch of state vector, Keplerian elements and covariance matrix data.
getEpoch() - Method in class org.orekit.files.ccsds.TDMFile.Observation
Getter for the epoch.
getEpoch() - Method in class org.orekit.files.sp3.SP3File
Returns the start epoch of the orbit file.
getEpoch() - Method in class org.orekit.frames.HelmertTransformation
Get the reference epoch of the transform.
getEpoch() - Method in class org.orekit.models.earth.GeoMagneticField
Returns the epoch for this magnetic field model.
getEpochComment() - Method in class org.orekit.files.ccsds.OGMFile
Get the comment for epoch.
getEpochIgnition() - Method in class org.orekit.files.ccsds.OPMFile.Maneuver
Get epoch ignition.
getEpochInterval() - Method in class org.orekit.files.sp3.SP3File
Returns the time interval between epochs (in seconds).
getEquatorialRadius() - Method in class org.orekit.bodies.OneAxisEllipsoid
Get the equatorial radius of the body.
getEquatorialRadius() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTSolarRadiationPressure
Get the central body equatorial radius.
getEquinoctialEx() - Method in class org.orekit.orbits.CartesianOrbit
Get the first component of the equinoctial eccentricity vector derivative.
getEquinoctialEx() - Method in class org.orekit.orbits.CircularOrbit
Get the first component of the equinoctial eccentricity vector derivative.
getEquinoctialEx() - Method in class org.orekit.orbits.EquinoctialOrbit
Get the first component of the equinoctial eccentricity vector derivative.
getEquinoctialEx() - Method in class org.orekit.orbits.FieldCartesianOrbit
Get the first component of the equinoctial eccentricity vector.
getEquinoctialEx() - Method in class org.orekit.orbits.FieldCircularOrbit
Get the first component of the equinoctial eccentricity vector.
getEquinoctialEx() - Method in class org.orekit.orbits.FieldEquinoctialOrbit
Get the first component of the equinoctial eccentricity vector.
getEquinoctialEx() - Method in class org.orekit.orbits.FieldKeplerianOrbit
Get the first component of the equinoctial eccentricity vector.
getEquinoctialEx() - Method in class org.orekit.orbits.FieldOrbit
Get the first component of the equinoctial eccentricity vector.
getEquinoctialEx() - Method in class org.orekit.orbits.KeplerianOrbit
Get the first component of the equinoctial eccentricity vector derivative.
getEquinoctialEx() - Method in class org.orekit.orbits.Orbit
Get the first component of the equinoctial eccentricity vector derivative.
getEquinoctialEx() - Method in class org.orekit.propagation.FieldSpacecraftState
Get the first component of the eccentricity vector (as per equinoctial parameters).
getEquinoctialEx() - Method in class org.orekit.propagation.SpacecraftState
Get the first component of the eccentricity vector (as per equinoctial parameters).
getEquinoctialExDot() - Method in class org.orekit.orbits.CartesianOrbit
Get the first component of the equinoctial eccentricity vector.
getEquinoctialExDot() - Method in class org.orekit.orbits.CircularOrbit
Get the first component of the equinoctial eccentricity vector.
getEquinoctialExDot() - Method in class org.orekit.orbits.EquinoctialOrbit
Get the first component of the equinoctial eccentricity vector.
getEquinoctialExDot() - Method in class org.orekit.orbits.FieldCartesianOrbit
Get the first component of the equinoctial eccentricity vector.
getEquinoctialExDot() - Method in class org.orekit.orbits.FieldCircularOrbit
Get the first component of the equinoctial eccentricity vector.
getEquinoctialExDot() - Method in class org.orekit.orbits.FieldEquinoctialOrbit
Get the first component of the equinoctial eccentricity vector.
getEquinoctialExDot() - Method in class org.orekit.orbits.FieldKeplerianOrbit
Get the first component of the equinoctial eccentricity vector.
getEquinoctialExDot() - Method in class org.orekit.orbits.FieldOrbit
Get the first component of the equinoctial eccentricity vector.
getEquinoctialExDot() - Method in class org.orekit.orbits.KeplerianOrbit
Get the first component of the equinoctial eccentricity vector.
getEquinoctialExDot() - Method in class org.orekit.orbits.Orbit
Get the first component of the equinoctial eccentricity vector.
getEquinoctialEy() - Method in class org.orekit.orbits.CartesianOrbit
Get the second component of the equinoctial eccentricity vector derivative.
getEquinoctialEy() - Method in class org.orekit.orbits.CircularOrbit
Get the second component of the equinoctial eccentricity vector derivative.
getEquinoctialEy() - Method in class org.orekit.orbits.EquinoctialOrbit
Get the second component of the equinoctial eccentricity vector derivative.
getEquinoctialEy() - Method in class org.orekit.orbits.FieldCartesianOrbit
Get the second component of the equinoctial eccentricity vector.
getEquinoctialEy() - Method in class org.orekit.orbits.FieldCircularOrbit
Get the second component of the equinoctial eccentricity vector.
getEquinoctialEy() - Method in class org.orekit.orbits.FieldEquinoctialOrbit
Get the second component of the equinoctial eccentricity vector.
getEquinoctialEy() - Method in class org.orekit.orbits.FieldKeplerianOrbit
Get the second component of the equinoctial eccentricity vector.
getEquinoctialEy() - Method in class org.orekit.orbits.FieldOrbit
Get the second component of the equinoctial eccentricity vector.
getEquinoctialEy() - Method in class org.orekit.orbits.KeplerianOrbit
Get the second component of the equinoctial eccentricity vector derivative.
getEquinoctialEy() - Method in class org.orekit.orbits.Orbit
Get the second component of the equinoctial eccentricity vector derivative.
getEquinoctialEy() - Method in class org.orekit.propagation.FieldSpacecraftState
Get the second component of the eccentricity vector (as per equinoctial parameters).
getEquinoctialEy() - Method in class org.orekit.propagation.SpacecraftState
Get the second component of the eccentricity vector (as per equinoctial parameters).
getEquinoctialEyDot() - Method in class org.orekit.orbits.CartesianOrbit
Get the second component of the equinoctial eccentricity vector.
getEquinoctialEyDot() - Method in class org.orekit.orbits.CircularOrbit
Get the second component of the equinoctial eccentricity vector.
getEquinoctialEyDot() - Method in class org.orekit.orbits.EquinoctialOrbit
Get the second component of the equinoctial eccentricity vector.
getEquinoctialEyDot() - Method in class org.orekit.orbits.FieldCartesianOrbit
Get the second component of the equinoctial eccentricity vector.
getEquinoctialEyDot() - Method in class org.orekit.orbits.FieldCircularOrbit
Get the second component of the equinoctial eccentricity vector.
getEquinoctialEyDot() - Method in class org.orekit.orbits.FieldEquinoctialOrbit
Get the second component of the equinoctial eccentricity vector.
getEquinoctialEyDot() - Method in class org.orekit.orbits.FieldKeplerianOrbit
Get the second component of the equinoctial eccentricity vector.
getEquinoctialEyDot() - Method in class org.orekit.orbits.FieldOrbit
Get the second component of the equinoctial eccentricity vector.
getEquinoctialEyDot() - Method in class org.orekit.orbits.KeplerianOrbit
Get the second component of the equinoctial eccentricity vector.
getEquinoctialEyDot() - Method in class org.orekit.orbits.Orbit
Get the second component of the equinoctial eccentricity vector.
getEquinoxNutationCorrection(AbsoluteDate) - Method in class org.orekit.frames.EOPHistory
Get the correction to the nutation parameters for equinox-based paradigm.
getEquinoxNutationCorrection(FieldAbsoluteDate<T>) - Method in class org.orekit.frames.EOPHistory
Get the correction to the nutation parameters for equinox-based paradigm.
getEstimatedEarthFrame() - Method in class org.orekit.estimation.measurements.GroundStation
Get the estimated Earth frame, including the estimated linear models for pole and prime meridian.
getEstimatedMeasurement(int) - Method in interface org.orekit.estimation.measurements.EstimationsProvider
Get one estimated measurement.
getEstimatedUT1() - Method in class org.orekit.estimation.measurements.EstimatedEarthFrameProvider
Get the estimated UT1 time scale.
getEstimatedUT1() - Method in class org.orekit.estimation.measurements.GroundStation
Get the estimated UT1 scale, including the estimated linear models for prime meridian.
getEstimatedValue() - Method in class org.orekit.estimation.measurements.EstimatedMeasurement
Get the estimated value.
getEvaluations() - Method in class org.orekit.propagation.conversion.AbstractPropagatorConverter
Get the number of objective function evaluations.
getEvaluationsCount() - Method in class org.orekit.estimation.leastsquares.BatchLSEstimator
Get the number of evaluations used for last estimation.
getEventDate() - Method in class org.orekit.propagation.events.EventState
Get the occurrence time of the event triggered in the current step.
getEventDate() - Method in class org.orekit.propagation.events.FieldEventState
Get the occurrence time of the event triggered in the current step.
getEventDetector() - Method in class org.orekit.propagation.events.EventsLogger.LoggedEvent
Get the event detector triggered.
getEventDetector() - Method in class org.orekit.propagation.events.EventState
Get the underlying event detector.
getEventDetector() - Method in class org.orekit.propagation.events.FieldEventsLogger.FieldLoggedEvent
Get the event detector triggered.
getEventDetector() - Method in class org.orekit.propagation.events.FieldEventState
Get the underlying event detector.
getEvents() - Method in class org.orekit.propagation.events.handlers.RecordAndContinue
Get the events passed to this handler.
getEventsDetectors() - Method in class org.orekit.forces.AbstractParametricAcceleration
Get the discrete events related to the model.
getEventsDetectors() - Method in class org.orekit.forces.drag.DragForce
Get the discrete events related to the model.
getEventsDetectors() - Method in interface org.orekit.forces.ForceModel
Get the discrete events related to the model.
getEventsDetectors() - Method in class org.orekit.forces.gravity.HolmesFeatherstoneAttractionModel
Get the discrete events related to the model.
getEventsDetectors() - Method in class org.orekit.forces.gravity.NewtonianAttraction
Get the discrete events related to the model.
getEventsDetectors() - Method in class org.orekit.forces.gravity.OceanTides
Get the discrete events related to the model.
getEventsDetectors() - Method in class org.orekit.forces.gravity.Relativity
Get the discrete events related to the model.
getEventsDetectors() - Method in class org.orekit.forces.gravity.SolidTides
Get the discrete events related to the model.
getEventsDetectors() - Method in class org.orekit.forces.gravity.ThirdBodyAttraction
Get the discrete events related to the model.
getEventsDetectors() - Method in class org.orekit.forces.maneuvers.ConstantThrustManeuver
Get the discrete events related to the model.
getEventsDetectors() - Method in class org.orekit.forces.radiation.SolarRadiationPressure
Get the discrete events related to the model.
getEventsDetectors() - Method in class org.orekit.propagation.AbstractPropagator
Get all the events detectors that have been added.
getEventsDetectors() - Method in class org.orekit.propagation.analytical.AbstractAnalyticalPropagator
Get all the events detectors that have been added.
getEventsDetectors() - Method in class org.orekit.propagation.analytical.FieldAbstractAnalyticalPropagator
Get all the events detectors that have been added.
getEventsDetectors() - Method in class org.orekit.propagation.FieldAbstractPropagator
Get all the events detectors that have been added.
getEventsDetectors() - Method in interface org.orekit.propagation.FieldPropagator
Get all the events detectors that have been added.
getEventsDetectors() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
Get all the events detectors that have been added.
getEventsDetectors() - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator
Get all the events detectors that have been added.
getEventsDetectors() - Method in interface org.orekit.propagation.Propagator
Get all the events detectors that have been added.
getEventsDetectors() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTAtmosphericDrag
Get the discrete events related to the model.
getEventsDetectors() - Method in interface org.orekit.propagation.semianalytical.dsst.forces.DSSTForceModel
Get the discrete events related to the model.
getEventsDetectors() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTSolarRadiationPressure
Get the discrete events related to the model.
getEventsDetectors() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseral
Get the discrete events related to the model.
getEventsDetectors() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBody
Get the discrete events related to the model.
getEventsDetectors() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonal
Get the discrete events related to the model.
getException() - Method in exception org.orekit.errors.OrekitExceptionWrapper
Get the wrapped exception.
getExtrapolationThreshold() - Method in class org.orekit.propagation.analytical.Ephemeris
Get the maximum timespan outside of the stored ephemeris that is allowed for extrapolation.
getF() - Method in class org.orekit.data.DelaunayArguments
Get L - Ω where L is the mean longitude of the Moon.
getF() - Method in class org.orekit.data.FieldDelaunayArguments
Get L - Ω where L is the mean longitude of the Moon.
getF10(AbsoluteDate) - Method in interface org.orekit.forces.drag.atmosphere.JB2008InputParameters
Get the value of the instantaneous solar flux index (1e-22*Watt/(m²*Hertz)).
getF10B(AbsoluteDate) - Method in interface org.orekit.forces.drag.atmosphere.JB2008InputParameters
Get the value of the mean solar flux.
getFactoryKey() - Method in class org.orekit.frames.FactoryManagedFrame
Get the key of the frame within the factory.
getFDot() - Method in class org.orekit.data.DelaunayArguments
Get L - Ω where L is the mean longitude of the Moon time derivative.
getFDot() - Method in class org.orekit.data.FieldDelaunayArguments
Get L - Ω where L is the mean longitude of the Moon time derivative.
getField(GeoMagneticFieldFactory.FieldModel, double) - Static method in class org.orekit.models.earth.GeoMagneticFieldFactory
Get the GeoMagneticField for the given model type and year.
getField() - Method in class org.orekit.propagation.FieldAbstractPropagator
Field getter.
getField() - Method in class org.orekit.time.FieldAbsoluteDate
Get the field.
getFieldDate() - Method in class org.orekit.frames.FieldTransform
Get the date.
getFieldEventsDetectors(Field<T>) - Method in class org.orekit.forces.AbstractParametricAcceleration
Get the discrete events related to the model.
getFieldEventsDetectors(Field<T>) - Method in class org.orekit.forces.drag.DragForce
Get the discrete events related to the model.
getFieldEventsDetectors(Field<T>) - Method in interface org.orekit.forces.ForceModel
Get the discrete events related to the model.
getFieldEventsDetectors(Field<T>) - Method in class org.orekit.forces.gravity.HolmesFeatherstoneAttractionModel
 
getFieldEventsDetectors(Field<T>) - Method in class org.orekit.forces.gravity.NewtonianAttraction
Get the discrete events related to the model.
getFieldEventsDetectors(Field<T>) - Method in class org.orekit.forces.gravity.OceanTides
Get the discrete events related to the model.
getFieldEventsDetectors(Field<T>) - Method in class org.orekit.forces.gravity.Relativity
Get the discrete events related to the model.
getFieldEventsDetectors(Field<T>) - Method in class org.orekit.forces.gravity.SolidTides
Get the discrete events related to the model.
getFieldEventsDetectors(Field<T>) - Method in class org.orekit.forces.gravity.ThirdBodyAttraction
Get the discrete events related to the model.
getFieldEventsDetectors(Field<T>) - Method in class org.orekit.forces.maneuvers.ConstantThrustManeuver
Get the discrete events related to the model.
getFieldEventsDetectors(Field<T>) - Method in class org.orekit.forces.radiation.SolarRadiationPressure
Get the discrete events related to the model.
getFieldOfView() - Method in class org.orekit.propagation.events.FieldOfViewDetector
Get the Field Of View.
getFieldOfView() - Method in class org.orekit.propagation.events.FootprintOverlapDetector
Get the Field Of View.
getFieldOfView() - Method in class org.orekit.propagation.events.GroundFieldOfViewDetector
Get the Field Of View.
getFieldVector() - Method in class org.orekit.models.earth.GeoMagneticElements
Returns the magnetic field vector in nTesla.
getFiftiesEpoch(Field<T>) - Static method in class org.orekit.time.FieldAbsoluteDate
Reference epoch for 1950 dates: 1950-01-01T00:00:00 Terrestrial Time.
getFileDate(AbsoluteDate) - Method in class org.orekit.forces.drag.atmosphere.data.MarshallSolarActivityFutureEstimation
Get the date of the file from which data at the specified date comes from.
getFileFormat() - Method in class org.orekit.files.ccsds.TDMParser
Get file format.
getFilter(int) - Static method in enum org.orekit.utils.AngularDerivativesFilter
Get the filter corresponding to a maximum derivation order.
getFilter(int) - Static method in enum org.orekit.utils.CartesianDerivativesFilter
Get the filter corresponding to a maximum derivation order.
getFirst() - Method in class org.orekit.propagation.analytical.tle.TLESeries
Deprecated.
Get the first TLE.
getFirstDate() - Method in class org.orekit.propagation.analytical.tle.TLESeries
Deprecated.
Get the start date of the series.
getFirstKnownLeapSecond() - Method in class org.orekit.time.UTCScale
Get the date of the first known leap second.
getFittedParameters() - Method in class org.orekit.utils.SecularAndHarmonic
Get a copy of the last fitted parameters.
getFixedStepSize() - Method in class org.orekit.propagation.AbstractPropagator
Get the fixed step size.
getFixedStepSize() - Method in class org.orekit.propagation.FieldAbstractPropagator
Get the fixed step size.
getFlattening() - Method in class org.orekit.bodies.OneAxisEllipsoid
Get the flattening of the body: f = (a-b)/a.
getFlowRate() - Method in class org.orekit.forces.maneuvers.ConstantThrustManeuver
Get the flow rate.
getForceModels() - Method in class org.orekit.propagation.numerical.FieldNumericalPropagator
Deprecated.
as of 9.1, this method is deprecated, the perturbing force models are retrieved together with the Newtonian attraction by calling FieldNumericalPropagator.getAllForceModels()
getFormatVersion() - Method in class org.orekit.files.ccsds.ODMFile
Get the CCSDS ODM (OPM, OMM or OEM) format version.
getFormatVersion() - Method in class org.orekit.files.ccsds.TDMFile
Get the CCSDS TDM format version.
getFrame() - Method in class org.orekit.bodies.Ellipse
Get the defining frame.
getFrame() - Method in class org.orekit.bodies.Ellipsoid
Get the ellipsoid central frame.
getFrame(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 class org.orekit.files.ccsds.OEMFile.EphemeridesBlock
 
getFrame() - Method in interface org.orekit.files.general.EphemerisFile.EphemerisSegment
Get the reference frame for this ephemeris segment.
getFrame() - Method in class org.orekit.files.general.OrekitEphemerisFile.OrekitEphemerisSegment
 
getFrame() - Method in class org.orekit.files.sp3.SP3File.SP3Ephemeris
 
getFrame() - Method in interface org.orekit.forces.drag.atmosphere.Atmosphere
Get the frame of the central body.
getFrame() - Method in class org.orekit.forces.drag.atmosphere.DTM2000
Get the frame of the central body.
getFrame() - Method in class org.orekit.forces.drag.atmosphere.HarrisPriester
Get the frame of the central body.
getFrame() - Method in class org.orekit.forces.drag.atmosphere.JB2008
Get the frame of the central body.
getFrame() - Method in class org.orekit.forces.drag.atmosphere.NRLMSISE00
Get the frame of the central body.
getFrame() - Method in class org.orekit.forces.drag.atmosphere.SimpleExponentialAtmosphere
Get the frame of the central body.
getFrame(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.FieldOrbit
Get the frame in which the orbital parameters are defined.
getFrame() - Method in class org.orekit.orbits.Orbit
Get the frame in which the orbital parameters are defined.
getFrame() - Method in class org.orekit.propagation.AbstractPropagator
Get the frame in which the orbit is propagated.
getFrame() - Method in class org.orekit.propagation.analytical.Ephemeris
 
getFrame() - Method in class org.orekit.propagation.analytical.gnss.GPSPropagator
Get the frame in which the orbit is propagated.
getFrame() - Method in class org.orekit.propagation.analytical.tle.TLEPropagator
Get the frame in which the orbit is propagated.
getFrame() - Method in class org.orekit.propagation.conversion.AbstractPropagatorBuilder
Get the frame in which the orbit is propagated.
getFrame() - Method in class org.orekit.propagation.conversion.AbstractPropagatorConverter
Get the frame of the initial state.
getFrame() - Method in interface org.orekit.propagation.conversion.PropagatorBuilder
Get the frame in which the orbit is propagated.
getFrame() - Method in class org.orekit.propagation.events.FieldNodeDetector
Get the frame in which the equator is defined.
getFrame() - Method in class org.orekit.propagation.events.GroundFieldOfViewDetector
Get the sensor reference frame.
getFrame() - Method in class org.orekit.propagation.events.NodeDetector
Get the frame in which the equator is defined.
getFrame() - Method in class org.orekit.propagation.FieldAbstractPropagator
Get the frame in which the orbit is propagated.
getFrame() - Method in interface org.orekit.propagation.FieldPropagator
Get the frame in which the orbit is propagated.
getFrame() - Method in class org.orekit.propagation.FieldSpacecraftState
Get the inertial frame.
getFrame() - Method in class org.orekit.propagation.integration.FieldIntegratedEphemeris
 
getFrame() - Method in class org.orekit.propagation.integration.FieldStateMapper
Get the inertial frame.
getFrame() - Method in class org.orekit.propagation.integration.IntegratedEphemeris
 
getFrame() - Method in class org.orekit.propagation.integration.StateMapper
Get the inertial frame.
getFrame() - Method in interface org.orekit.propagation.Propagator
Get the frame in which the orbit is propagated.
getFrame() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
Get the definition frame of the orbit.
getFrame() - Method in class org.orekit.propagation.SpacecraftState
Get the inertial frame.
getFrameCenterString() - Method in class org.orekit.files.ccsds.OEMFile.EphemeridesBlock
 
getFrameCenterString() - Method in interface org.orekit.files.general.EphemerisFile.EphemerisSegment
Get the name of the center of the coordinate system the ephemeris is provided in.
getFrameCenterString() - Method in class org.orekit.files.general.OrekitEphemerisFile.OrekitEphemerisSegment
 
getFrameCenterString() - Method in class org.orekit.files.sp3.SP3File.SP3Ephemeris
 
getFrameEpoch() - Method in class org.orekit.files.ccsds.ODMMetaData
Get epoch of reference frame, if not intrinsic to the definition of the reference frame.
getFrameEpochString() - Method in class org.orekit.files.ccsds.ODMMetaData
Get epoch of reference frame, if not intrinsic to the definition of the reference frame.
getFrameString() - Method in class org.orekit.files.ccsds.ODMMetaData
Get the reference frame specifier as it appeared in the file.
getFrameString() - Method in class org.orekit.files.ccsds.OEMFile.EphemeridesBlock
 
getFrameString() - Method in interface org.orekit.files.general.EphemerisFile.EphemerisSegment
Get the defining frame for this ephemeris segment.
getFrameString() - Method in class org.orekit.files.general.OrekitEphemerisFile.OrekitEphemerisSegment
 
getFrameString() - Method in class org.orekit.files.sp3.SP3File.SP3Ephemeris
 
getFreqOffset() - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData
Getter for the freqOffset.
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.
getFutureInfinity(Field<T>) - Static method in class org.orekit.time.FieldAbsoluteDate
Dummy date at infinity in the future direction.
getGalileoEpoch(Field<T>) - Static method in class org.orekit.time.FieldAbsoluteDate
Reference epoch for Galileo System Time: 1999-08-22T00:00:00 UTC.
getGamma() - Method in class org.orekit.data.DelaunayArguments
Get the tide parameter γ = GMST + π.
getGamma() - Method in class org.orekit.data.FieldDelaunayArguments
Get the tide parameter γ = GMST + π.
getGamma() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
Get direction cosine γ for central body.
getGammaDot() - Method in class org.orekit.data.DelaunayArguments
Get the tide parameter γ = GMST + π time derivative.
getGammaDot() - Method in class org.orekit.data.FieldDelaunayArguments
Get the tide parameter γ = GMST + π time derivative.
getGASTFunction(TimeScale, EOPHistory) - Method in enum org.orekit.utils.IERSConventions
Get the function computing Greenwich apparent sidereal time, in radians.
getGCRF() - Static method in class org.orekit.frames.FramesFactory
Get the unique GCRF frame.
getGdop() - Method in class org.orekit.gnss.DOP
Gets the geometric dilution of precision.
getGenerateCalls() - Method in class org.orekit.utils.GenericTimeStampedCache
Get the number of calls to the generate method.
getGeneratedEphemeris() - Method in class org.orekit.propagation.AbstractPropagator
Get the ephemeris generated during propagation.
getGeneratedEphemeris() - Method in class org.orekit.propagation.analytical.AbstractAnalyticalPropagator
Get the ephemeris generated during propagation.
getGeneratedEphemeris() - Method in class org.orekit.propagation.analytical.FieldAbstractAnalyticalPropagator
Get the ephemeris generated during propagation.
getGeneratedEphemeris() - Method in class org.orekit.propagation.FieldAbstractPropagator
Get the ephemeris generated during propagation.
getGeneratedEphemeris() - Method in interface org.orekit.propagation.FieldPropagator
Get the ephemeris generated during propagation.
getGeneratedEphemeris() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
Get the ephemeris generated during propagation.
getGeneratedEphemeris() - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator
Get the ephemeris generated during propagation.
getGeneratedEphemeris() - Method in interface org.orekit.propagation.Propagator
Get the ephemeris generated during propagation.
getGenerator() - Method in class org.orekit.utils.GenericTimeStampedCache
Get the generator.
getGetNeighborsCalls() - Method in class org.orekit.utils.GenericTimeStampedCache
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 Gjs coefficient.
getGLONASS() - Static method in class org.orekit.time.TimeScalesFactory
Get the GLObal NAvigation Satellite System time scale.
getGM() - Method in interface org.orekit.bodies.CelestialBody
Get the attraction coefficient of the body.
getGM() - Method in class org.orekit.models.earth.ReferenceEllipsoid
Gets the gravitational parameter that is part of the definition of the reference ellipsoid.
getGmsj(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHmsjPolynomials
Get the Gmsj coefficient.
getGMST(IERSConventions, boolean) - Static method in class org.orekit.time.TimeScalesFactory
Get the Greenwich Mean Sidereal Time scale.
getGMSTFunction(TimeScale) - Method in enum org.orekit.utils.IERSConventions
Get the function computing Greenwich mean sidereal time, in radians.
getGMSTRateFunction(TimeScale) - Method in enum org.orekit.utils.IERSConventions
Get the function computing Greenwich mean sidereal time rate, in radians per second.
getGnssNb() - Method in class org.orekit.gnss.DOP
Gets the number of GNSS satellites taken into account for DOP computation.
getGPS() - Static method in class org.orekit.time.TimeScalesFactory
Get the Global Positioning System scale.
getGPSEpoch(Field<T>) - Static method in class org.orekit.time.FieldAbsoluteDate
Reference epoch for GPS weeks: 1980-01-06T00:00:00 GPS time.
getGPSOrbitalElements() - Method in class org.orekit.propagation.analytical.gnss.GPSPropagator
Gets the underlying GPS orbital elements.
getGpsWeek() - Method in class org.orekit.files.sp3.SP3File
Returns the GPS week as contained in the SP3 file.
getGridPoints() - Method in class org.orekit.frames.InterpolatingTransformProvider
Get the number of interpolation grid points.
getGridPoints() - Method in class org.orekit.frames.ShiftingTransformProvider
Get the number of interpolation grid points.
getGridPoints(double, double) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FixedNumberInterpolationGrid
Get grid points that are within the current step.
getGridPoints(double, double) - Method in interface org.orekit.propagation.semianalytical.dsst.utilities.InterpolationGrid
Get grid points that are within the current step.
getGridPoints(double, double) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.MaxGapInterpolationGrid
Get grid points that are within the current step.
getGrs80(Frame) - Static method in class org.orekit.models.earth.ReferenceEllipsoid
Get the GRS80 ellipsoid, attached to the given body frame.
getGST() - Static method in class org.orekit.time.TimeScalesFactory
Get the Galileo System Time scale.
getGTOD(boolean) - Static method in class org.orekit.frames.FramesFactory
Get the GTOD reference frame.
getGTOD(IERSConventions, boolean) - Static method in class org.orekit.frames.FramesFactory
Get the GTOD reference frame.
getH() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
Get the y component of eccentricity vector.
getHalfAperture() - Method in class org.orekit.propagation.events.CircularFieldOfViewDetector
Get FOV half aperture angle.
getHandler() - Method in class org.orekit.propagation.events.AbstractDetector
Get the handler.
getHandler() - Method in class org.orekit.propagation.events.FieldAbstractDetector
Get the handler.
getHarmonicAmplitude() - Method in class org.orekit.utils.SecularAndHarmonic
Get an upper bound of the fitted harmonic amplitude.
getHasCreatableBody() - Method in class org.orekit.files.ccsds.ODMMetaData
Get boolean testing whether the body corresponding to the centerName attribute can be created through the CelestialBodyFactory.
getHasManeuver() - Method in class org.orekit.files.ccsds.OPMFile
Get boolean testing whether the OPM contains at least one maneuver.
getHasRefFrameEpoch() - Method in class org.orekit.files.ccsds.OEMFile.EphemeridesBlock
Get boolean testing whether the reference frame has an epoch associated to it.
getHdop() - Method in class org.orekit.gnss.DOP
Gets the horizontal dilution of precision.
getHeaderComment() - Method in class org.orekit.files.ccsds.ODMFile
Get the header comment.
getHeaderComment() - Method in class org.orekit.files.ccsds.TDMFile
Get the header comment.
getHealth() - Method in class org.orekit.gnss.GPSAlmanac
Gets the Health status.
getHjs(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
Get the Hjs coefficient.
getHmsj(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHmsjPolynomials
Get the Hmsj coefficient.
getHorizontalIntensity() - Method in class org.orekit.models.earth.GeoMagneticElements
Returns the horizontal intensity of the magnetic field (= norm of the vector in the plane spanned by the x/y components of the field vector).
getHour() - Method in class org.orekit.time.TimeComponents
Get the hour number.
getHx() - Method in class org.orekit.orbits.CartesianOrbit
Get the first component of the inclination vector.
getHx() - Method in class org.orekit.orbits.CircularOrbit
Get the first component of the inclination vector.
getHx() - Method in class org.orekit.orbits.EquinoctialOrbit
Get the first component of the inclination vector.
getHx() - Method in class org.orekit.orbits.FieldCartesianOrbit
Get the first component of the inclination vector.
getHx() - Method in class org.orekit.orbits.FieldCircularOrbit
Get the first component of the inclination vector.
getHx() - Method in class org.orekit.orbits.FieldEquinoctialOrbit
Get the first component of the inclination vector.
getHx() - Method in class org.orekit.orbits.FieldKeplerianOrbit
Get the first component of the inclination vector.
getHx() - Method in class org.orekit.orbits.FieldOrbit
Get the first component of the inclination vector.
getHx() - Method in class org.orekit.orbits.KeplerianOrbit
Get the first component of the inclination vector.
getHx() - Method in class org.orekit.orbits.Orbit
Get the first component of the inclination vector.
getHx() - Method in class org.orekit.propagation.FieldSpacecraftState
Get the first component of the inclination vector (as per equinoctial parameters).
getHx() - Method in class org.orekit.propagation.SpacecraftState
Get the first component of the inclination vector (as per equinoctial parameters).
getHxDot() - Method in class org.orekit.orbits.CartesianOrbit
Get the first component of the inclination vector derivative.
getHxDot() - Method in class org.orekit.orbits.CircularOrbit
Get the first component of the inclination vector derivative.
getHxDot() - Method in class org.orekit.orbits.EquinoctialOrbit
Get the first component of the inclination vector derivative.
getHxDot() - Method in class org.orekit.orbits.FieldCartesianOrbit
Get the first component of the inclination vector derivative.
getHxDot() - Method in class org.orekit.orbits.FieldCircularOrbit
Get the first component of the inclination vector derivative.
getHxDot() - Method in class org.orekit.orbits.FieldEquinoctialOrbit
Get the first component of the inclination vector derivative.
getHxDot() - Method in class org.orekit.orbits.FieldKeplerianOrbit
Get the first component of the inclination vector derivative.
getHxDot() - Method in class org.orekit.orbits.FieldOrbit
Get the first component of the inclination vector derivative.
getHxDot() - Method in class org.orekit.orbits.KeplerianOrbit
Get the first component of the inclination vector derivative.
getHxDot() - Method in class org.orekit.orbits.Orbit
Get the first component of the inclination vector derivative.
getHy() - Method in class org.orekit.orbits.CartesianOrbit
Get the second component of the inclination vector.
getHy() - Method in class org.orekit.orbits.CircularOrbit
Get the second component of the inclination vector.
getHy() - Method in class org.orekit.orbits.EquinoctialOrbit
Get the second component of the inclination vector.
getHy() - Method in class org.orekit.orbits.FieldCartesianOrbit
Get the second component of the inclination vector.
getHy() - Method in class org.orekit.orbits.FieldCircularOrbit
Get the second component of the inclination vector.
getHy() - Method in class org.orekit.orbits.FieldEquinoctialOrbit
Get the second component of the inclination vector.
getHy() - Method in class org.orekit.orbits.FieldKeplerianOrbit
Get the second component of the inclination vector.
getHy() - Method in class org.orekit.orbits.FieldOrbit
Get the second component of the inclination vector.
getHy() - Method in class org.orekit.orbits.KeplerianOrbit
Get the second component of the inclination vector.
getHy() - Method in class org.orekit.orbits.Orbit
Get the second component of the inclination vector.
getHy() - Method in class org.orekit.propagation.FieldSpacecraftState
Get the second component of the inclination vector (as per equinoctial parameters).
getHy() - Method in class org.orekit.propagation.SpacecraftState
Get the second component of the inclination vector (as per equinoctial parameters).
getHyDot() - Method in class org.orekit.orbits.CartesianOrbit
Get the second component of the inclination vector derivative.
getHyDot() - Method in class org.orekit.orbits.CircularOrbit
Get the second component of the inclination vector derivative.
getHyDot() - Method in class org.orekit.orbits.EquinoctialOrbit
Get the second component of the inclination vector derivative.
getHyDot() - Method in class org.orekit.orbits.FieldCartesianOrbit
Get the second component of the inclination vector derivative.
getHyDot() - Method in class org.orekit.orbits.FieldCircularOrbit
Get the second component of the inclination vector derivative.
getHyDot() - Method in class org.orekit.orbits.FieldEquinoctialOrbit
Get the second component of the inclination vector derivative.
getHyDot() - Method in class org.orekit.orbits.FieldKeplerianOrbit
Get the second component of the inclination vector derivative.
getHyDot() - Method in class org.orekit.orbits.FieldOrbit
Get the second component of the inclination vector derivative.
getHyDot() - Method in class org.orekit.orbits.KeplerianOrbit
Get the second component of the inclination vector derivative.
getHyDot() - Method in class org.orekit.orbits.Orbit
Get the second component of the inclination vector derivative.
getI() - Method in class org.orekit.files.ccsds.OGMFile
Get the orbit inclination.
getI() - Method in class org.orekit.orbits.CartesianOrbit
Get the inclination.
getI() - Method in class org.orekit.orbits.CircularOrbit
Get the inclination.
getI() - Method in class org.orekit.orbits.EquinoctialOrbit
Get the inclination.
getI() - Method in class org.orekit.orbits.FieldCartesianOrbit
Get the inclination.
getI() - Method in class org.orekit.orbits.FieldCircularOrbit
Get the inclination.
getI() - Method in class org.orekit.orbits.FieldEquinoctialOrbit
Get the inclination.
getI() - Method in class org.orekit.orbits.FieldKeplerianOrbit
Get the inclination.
getI() - Method in class org.orekit.orbits.FieldOrbit
Get the inclination.
getI() - Method in class org.orekit.orbits.KeplerianOrbit
Get the inclination.
getI() - Method in class org.orekit.orbits.Orbit
Get the inclination.
getI() - Method in class org.orekit.propagation.analytical.tle.TLE
Get the inclination.
getI() - Method in class org.orekit.propagation.FieldSpacecraftState
Get the inclination.
getI() - Method in class org.orekit.propagation.SpacecraftState
Get the inclination.
getI0() - Method in class org.orekit.gnss.GPSAlmanac
 
getI0() - Method in interface org.orekit.propagation.analytical.gnss.GPSOrbitalElements
Gets the Inclination Angle at Reference Time.
getICRF() - Static method in class org.orekit.frames.FramesFactory
Get the unique ICRF frame.
getId() - Method in class org.orekit.files.ccsds.OEMFile.OemSatelliteEphemeris
 
getId() - Method in interface org.orekit.files.general.EphemerisFile.SatelliteEphemeris
Get the satellite ID.
getId() - Method in class org.orekit.files.general.OrekitEphemerisFile.OrekitSatelliteEphemeris
 
getId() - Method in class org.orekit.files.sp3.SP3File.SP3Ephemeris
 
getIdentity(Field<T>) - Static method in class org.orekit.frames.FieldTransform
Get the identity transform.
getIdentity(Field<T>) - Static method in class org.orekit.utils.FieldAngularCoordinates
Fixed orientation parallel with reference frame (identity rotation, zero rotation rate and acceleration).
getIDot() - Method in class org.orekit.gnss.GPSAlmanac
 
getIDot() - Method in class org.orekit.orbits.CartesianOrbit
Get the inclination derivative.
getIDot() - Method in class org.orekit.orbits.CircularOrbit
Get the inclination derivative.
getIDot() - Method in class org.orekit.orbits.EquinoctialOrbit
Get the inclination derivative.
getIDot() - Method in class org.orekit.orbits.FieldCartesianOrbit
Get the inclination derivative.
getIDot() - Method in class org.orekit.orbits.FieldCircularOrbit
Get the inclination derivative.
getIDot() - Method in class org.orekit.orbits.FieldEquinoctialOrbit
Get the inclination derivative.
getIDot() - Method in class org.orekit.orbits.FieldKeplerianOrbit
Get the inclination derivative.
getIDot() - Method in class org.orekit.orbits.FieldOrbit
Get the inclination derivative.
getIDot() - Method in class org.orekit.orbits.KeplerianOrbit
Get the inclination derivative.
getIDot() - Method in class org.orekit.orbits.Orbit
Get the inclination derivative.
getIDot() - Method in interface org.orekit.propagation.analytical.gnss.GPSOrbitalElements
Gets the Rate of Inclination Angle.
getIGRF(double) - Static method in class org.orekit.models.earth.GeoMagneticFieldFactory
Get the IGRF model for the given year.
getIjs(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
Get the Ijs coefficient.
getImaginary(int, int) - Method in class org.orekit.utils.LoveNumbers
Get the imaginary part of a nominal Love numbers.
getInclination() - Method in class org.orekit.models.earth.GeoMagneticElements
Returns the inclination of the magnetic field in degrees.
getIncreasingTimeShift() - Method in class org.orekit.propagation.events.EventShifter
Get the increasing events time shift.
getInertialDV() - Method in class org.orekit.forces.maneuvers.SmallManeuverAnalyticalModel
Get the inertial velocity increment of the maneuver.
getInertialFrame() - Method in class org.orekit.forces.maneuvers.SmallManeuverAnalyticalModel
Get the inertial frame in which the velocity increment is defined.
getInertiallyOrientedFrame() - Method in interface org.orekit.bodies.CelestialBody
Get an inertially oriented, body centered frame.
getInitialIntegrationState() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
Get the initial state for integration.
getInitialIntegrationState() - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator
Get the initial state for integration.
getInitialIntegrationState() - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator
Get the initial state for integration.
getInitialOrbitDate() - Method in class org.orekit.propagation.conversion.AbstractPropagatorBuilder
Get the date of the initial orbit.
getInitialOrbitDate() - Method in interface org.orekit.propagation.conversion.PropagatorBuilder
Get the date of the initial orbit.
getInitialState() - Method in class org.orekit.propagation.AbstractPropagator
Get the propagator initial state.
getInitialState() - Method in class org.orekit.propagation.analytical.AdapterPropagator
Get the propagator initial state.
getInitialState() - Method in class org.orekit.propagation.analytical.AggregateBoundedPropagator
 
getInitialState() - Method in class org.orekit.propagation.analytical.Ephemeris
Get the propagator initial state.
getInitialState() - Method in class org.orekit.propagation.FieldAbstractPropagator
Get the propagator initial state.
getInitialState() - Method in interface org.orekit.propagation.FieldPropagator
Get the propagator initial state.
getInitialState() - Method in class org.orekit.propagation.integration.FieldIntegratedEphemeris
Get the propagator initial state.
getInitialState() - Method in class org.orekit.propagation.integration.IntegratedEphemeris
Get the propagator initial state.
getInitialState() - Method in interface org.orekit.propagation.Propagator
Get the propagator initial state.
getInstance() - Static method in class org.orekit.data.DataProvidersManager
Get the unique instance.
getInstantFlux(AbsoluteDate) - Method in class org.orekit.forces.drag.atmosphere.data.MarshallSolarActivityFutureEstimation
Get the value of the instantaneous solar flux.
getInstantFlux(AbsoluteDate) - Method in interface org.orekit.forces.drag.atmosphere.DTM2000InputParameters
Get the value of the instantaneous solar flux.
getIntegrationInterval() - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData
Getter for the integrationInterval.
getIntegrationRef() - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData
Getter for the integrationRef.
getIntegrator() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
Get the integrator used by the propagator.
getIntegrator() - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator
Get the integrator used by the propagator.
getInterpolatedPoint(double, double) - Method in class org.orekit.models.earth.tessellation.Tile
Get an interpolated point inside the tile.
getInterpolatedState(FieldAbsoluteDate<T>) - Method in interface org.orekit.propagation.sampling.FieldOrekitStepInterpolator
Get the state at interpolated date.
getInterpolatedState(AbsoluteDate) - Method in interface org.orekit.propagation.sampling.OrekitStepInterpolator
Get the state at interpolated date.
getInterpolationDegree() - Method in class org.orekit.files.ccsds.OEMFile.EphemeridesBlock
Get the interpolation degree.
getInterpolationMethod() - Method in class org.orekit.files.ccsds.OEMFile.EphemeridesBlock
Get the interpolation method to be used.
getInterpolationSamples() - Method in class org.orekit.files.ccsds.OEMFile.EphemeridesBlock
 
getInterpolationSamples() - Method in interface org.orekit.files.general.EphemerisFile.EphemerisSegment
Get the number of samples to use in interpolation.
getInterpolationSamples() - Method in class org.orekit.files.general.OrekitEphemerisFile.OrekitEphemerisSegment
 
getInterpolationSamples() - Method in class org.orekit.files.sp3.SP3File.SP3Ephemeris
 
getIntersectionPoint(Line, Vector3D, Frame, AbsoluteDate) - Method in interface org.orekit.bodies.BodyShape
Get the intersection point of a line with the surface of the body.
getIntersectionPoint(FieldLine<T>, FieldVector3D<T>, Frame, FieldAbsoluteDate<T>) - Method in interface org.orekit.bodies.BodyShape
Get the intersection point of a line with the surface of the body.
getIntersectionPoint(Line, Vector3D, Frame, AbsoluteDate) - Method in class org.orekit.bodies.OneAxisEllipsoid
Get the intersection point of a line with the surface of the body.
getIntersectionPoint(FieldLine<T>, FieldVector3D<T>, Frame, FieldAbsoluteDate<T>) - Method in class org.orekit.bodies.OneAxisEllipsoid
Get the intersection point of a line with the surface of the body.
getIntersectionPoint(Line, Vector3D, Frame, AbsoluteDate) - Method in class org.orekit.models.earth.Geoid
Get the intersection point of a line with the surface of the body.
getIntersectionPoint(FieldLine<T>, FieldVector3D<T>, Frame, FieldAbsoluteDate<T>) - Method in class org.orekit.models.earth.Geoid
Get the intersection point of a line with the surface of the body.
getInverse() - Method in class org.orekit.frames.FieldTransform
Get the inverse transform of the instance.
getInverse() - Method in class org.orekit.frames.Transform
Get the inverse transform of the instance.
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.
getIteration() - Method in class org.orekit.estimation.measurements.EstimatedMeasurement
Get the iteration number.
getIterationsCount() - Method in class org.orekit.estimation.leastsquares.BatchLSEstimator
Get the number of iterations used for last estimation.
getITRF(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.
getJ2000Epoch(Field<T>) - Static method in class org.orekit.time.FieldAbsoluteDate
J2000.0 Reference epoch: 2000-01-01T12:00:00 Terrestrial Time (not UTC).
getJacobian(Orbit, PositionAngle, double[][]) - Method in class org.orekit.forces.maneuvers.SmallManeuverAnalyticalModel
Compute the Jacobian of the orbit with respect to maneuver parameters.
getJacobian(CartesianDerivativesFilter, T[][]) - Method in class org.orekit.frames.FieldTransform
Compute the Jacobian of the FieldTransform.transformPVCoordinates(FieldPVCoordinates) method of the transform.
getJacobian(CartesianDerivativesFilter, double[][]) - Method in class org.orekit.frames.Transform
Compute the Jacobian of the Transform.transformPVCoordinates(PVCoordinates) method of the transform.
getJacobianWrtCartesian(PositionAngle, T[][]) - Method in class org.orekit.orbits.FieldOrbit
Compute the Jacobian of the orbital parameters with respect to the Cartesian parameters.
getJacobianWrtCartesian(PositionAngle, double[][]) - Method in class org.orekit.orbits.Orbit
Compute the Jacobian of the orbital parameters with respect to the Cartesian parameters.
getJacobianWrtParameters(PositionAngle, T[][]) - Method in class org.orekit.orbits.FieldOrbit
Compute the Jacobian of the Cartesian parameters with respect to the orbital parameters.
getJacobianWrtParameters(PositionAngle, double[][]) - Method in class org.orekit.orbits.Orbit
Compute the Jacobian of the Cartesian parameters with respect to the orbital parameters.
getJavaEpoch(Field<T>) - Static method in class org.orekit.time.FieldAbsoluteDate
Java Reference epoch: 1970-01-01T00:00:00 Universal Time Coordinate.
getJjs(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
Get the Jjs coefficient.
getJulianDay() - Method in class org.orekit.files.sp3.SP3File
Returns the julian day for this SP3 file.
getJulianEpoch(Field<T>) - Static method in class org.orekit.time.FieldAbsoluteDate
Reference epoch for julian dates: -4712-01-01T12:00:00 Terrestrial Time.
getJupiter() - Static method in class org.orekit.bodies.CelestialBodyFactory
Get the Jupiter singleton body.
getK() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
Get the x component of eccentricity vector.
getKeplerianElementsComment() - Method in class org.orekit.files.ccsds.OGMFile
Get the comment for Keplerian elements.
getKeplerianMeanMotion() - Method in class org.orekit.orbits.FieldOrbit
Get the Keplerian mean motion.
getKeplerianMeanMotion() - Method in class org.orekit.orbits.Orbit
Get the Keplerian mean motion.
getKeplerianMeanMotion() - Method in class org.orekit.propagation.FieldSpacecraftState
Get the Keplerian mean motion.
getKeplerianMeanMotion() - Method in class org.orekit.propagation.SpacecraftState
Get the Keplerian mean motion.
getKeplerianPeriod() - Method in class org.orekit.orbits.FieldOrbit
Get the Keplerian period.
getKeplerianPeriod() - Method in class org.orekit.orbits.Orbit
Get the Keplerian period.
getKeplerianPeriod() - Method in class org.orekit.propagation.FieldSpacecraftState
Get the Keplerian period.
getKeplerianPeriod() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
Get the Keplerian period.
getKeplerianPeriod() - Method in class org.orekit.propagation.SpacecraftState
Get the Keplerian period.
getKeyword() - Method in class org.orekit.files.ccsds.TDMFile.Observation
Getter for the keyword.
getL() - Method in class org.orekit.data.DelaunayArguments
Get the mean anomaly of the Moon.
getL() - Method in class org.orekit.data.FieldDelaunayArguments
Get the mean anomaly of the Moon.
getL(PositionAngle) - Method in class org.orekit.orbits.EquinoctialOrbit
Get the longitude argument.
getL(PositionAngle) - Method in class org.orekit.orbits.FieldEquinoctialOrbit
Get the longitude argument.
getLast() - Method in class org.orekit.propagation.analytical.tle.TLESeries
Deprecated.
Get the last TLE.
getLastDate() - Method in class org.orekit.propagation.analytical.tle.TLESeries
Deprecated.
Get the last date of the series.
getLastEstimations() - Method in class org.orekit.estimation.leastsquares.BatchLSEstimator
Get the last estimations performed.
getLastKnownLeapSecond() - Method in class org.orekit.time.UTCScale
Get the date of the last known leap second.
getLatest() - Method in class org.orekit.utils.GenericTimeStampedCache
Get the latest cached entry.
getLatest() - Method in class org.orekit.utils.ImmutableTimeStampedCache
 
getLatest() - Method in interface org.orekit.utils.TimeStampedCache
Get the latest entry in this cache.
getLatitude() - Method in class org.orekit.bodies.FieldGeodeticPoint
Get the latitude.
getLatitude() - Method in class org.orekit.bodies.GeodeticPoint
Get the latitude.
getLatitude() - Method in class org.orekit.propagation.events.LatitudeCrossingDetector
Get the fixed latitude to be crossed (radians).
getLaunchNumber() - Method in class org.orekit.files.ccsds.ODMMetaData
Get the launch number.
getLaunchNumber() - Method in class org.orekit.files.ccsds.ODMParser
Get the launch number.
getLaunchNumber() - Method in class org.orekit.propagation.analytical.tle.TLE
Get the launch number.
getLaunchPiece() - Method in class org.orekit.files.ccsds.ODMMetaData
Get the piece of launch.
getLaunchPiece() - Method in class org.orekit.files.ccsds.ODMParser
Get the piece of launch.
getLaunchPiece() - Method in class org.orekit.propagation.analytical.tle.TLE
Get the launch piece.
getLaunchYear() - Method in class org.orekit.files.ccsds.ODMMetaData
Get the launch year.
getLaunchYear() - Method in class org.orekit.files.ccsds.ODMParser
Get the launch year.
getLaunchYear() - Method in class org.orekit.propagation.analytical.tle.TLE
Get the launch year.
getLDot() - Method in class org.orekit.data.DelaunayArguments
Get the mean anomaly of the Moon time derivative.
getLDot() - Method in class org.orekit.data.FieldDelaunayArguments
Get the mean anomaly of the Moon time derivative.
getLDot(PositionAngle) - Method in class org.orekit.orbits.EquinoctialOrbit
Get the longitude argument derivative.
getLDot(PositionAngle) - Method in class org.orekit.orbits.FieldEquinoctialOrbit
Get the longitude argument derivative.
getLE() - Method in class org.orekit.data.BodiesElements
Get the mean Earth longitude.
getLE() - Method in class org.orekit.data.FieldBodiesElements
Get the mean Earth longitude.
getLE() - Method in class org.orekit.orbits.CartesianOrbit
Get the eccentric longitude argument.
getLE() - Method in class org.orekit.orbits.CircularOrbit
Get the eccentric longitude argument.
getLE() - Method in class org.orekit.orbits.EquinoctialOrbit
Get the eccentric longitude argument.
getLE() - Method in class org.orekit.orbits.FieldCartesianOrbit
Get the eccentric longitude argument.
getLE() - Method in class org.orekit.orbits.FieldCircularOrbit
Get the eccentric longitude argument.
getLE() - Method in class org.orekit.orbits.FieldEquinoctialOrbit
Get the eccentric longitude argument.
getLE() - Method in class org.orekit.orbits.FieldKeplerianOrbit
Get the eccentric longitude argument.
getLE() - Method in class org.orekit.orbits.FieldOrbit
Get the eccentric longitude argument.
getLE() - Method in class org.orekit.orbits.KeplerianOrbit
Get the eccentric longitude argument.
getLE() - Method in class org.orekit.orbits.Orbit
Get the eccentric longitude argument.
getLE() - Method in class org.orekit.propagation.FieldSpacecraftState
Get the eccentric latitude argument (as per equinoctial parameters).
getLE() - Method in class org.orekit.propagation.SpacecraftState
Get the eccentric latitude argument (as per equinoctial parameters).
getLeap(AbsoluteDate) - Method in class org.orekit.time.GLONASSScale
Get the value of the previous leap.
getLeap(FieldAbsoluteDate<T>) - Method in class org.orekit.time.GLONASSScale
Get the value of the previous leap.
getLeap(AbsoluteDate) - Method in interface org.orekit.time.TimeScale
Get the value of the previous leap.
getLeap(FieldAbsoluteDate<T>) - Method in interface org.orekit.time.TimeScale
Get the value of the previous leap.
getLeap(AbsoluteDate) - Method in class org.orekit.time.UTCScale
Get the value of the previous leap.
getLeap(FieldAbsoluteDate<T>) - Method in class org.orekit.time.UTCScale
Get the value of the previous leap.
getLEDot() - Method in class org.orekit.data.BodiesElements
Get the mean Earth longitude time derivative.
getLEDot() - Method in class org.orekit.data.FieldBodiesElements
Get the mean Earth longitude time derivative.
getLEDot() - Method in class org.orekit.orbits.CartesianOrbit
Get the eccentric longitude argument derivative.
getLEDot() - Method in class org.orekit.orbits.CircularOrbit
Get the eccentric longitude argument derivative.
getLEDot() - Method in class org.orekit.orbits.EquinoctialOrbit
Get the eccentric longitude argument derivative.
getLEDot() - Method in class org.orekit.orbits.FieldCartesianOrbit
Get the eccentric longitude argument derivative.
getLEDot() - Method in class org.orekit.orbits.FieldCircularOrbit
Get the eccentric longitude argument derivative.
getLEDot() - Method in class org.orekit.orbits.FieldEquinoctialOrbit
Get the eccentric longitude argument derivative.
getLEDot() - Method in class org.orekit.orbits.FieldKeplerianOrbit
Get the eccentric longitude argument derivative.
getLEDot() - Method in class org.orekit.orbits.FieldOrbit
Get the eccentric longitude argument derivative.
getLEDot() - Method in class org.orekit.orbits.KeplerianOrbit
Get the eccentric longitude argument derivative.
getLEDot() - Method in class org.orekit.orbits.Orbit
Get the eccentric longitude argument derivative.
getLf() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
Get the eccentric longitude.
getLightingRatio(Vector3D, Frame, AbsoluteDate) - Method in class org.orekit.forces.radiation.SolarRadiationPressure
Get the lighting ratio ([0-1]).
getLightingRatio(FieldVector3D<T>, Frame, FieldAbsoluteDate<T>) - Method in class org.orekit.forces.radiation.SolarRadiationPressure
Get the lighting ratio ([0-1]).
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.
getLJuDot() - Method in class org.orekit.data.BodiesElements
Get the mean Jupiter longitude time derivative.
getLJuDot() - Method in class org.orekit.data.FieldBodiesElements
Get the mean Jupiter longitude time derivative.
getLLimits(SpacecraftState) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution
Compute the limits in L, the true longitude, for integration.
getLLimits(SpacecraftState) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTAtmosphericDrag
Compute the limits in L, the true longitude, for integration.
getLLimits(SpacecraftState) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTSolarRadiationPressure
Compute the limits in L, the true longitude, for integration.
getLM() - Method in class org.orekit.orbits.CartesianOrbit
Get the mean longitude argument.
getLM() - Method in class org.orekit.orbits.CircularOrbit
Get the mean longitude argument.
getLM() - Method in class org.orekit.orbits.EquinoctialOrbit
Get the mean longitude argument.
getLM() - Method in class org.orekit.orbits.FieldCartesianOrbit
Get the mean longitude argument.
getLM() - Method in class org.orekit.orbits.FieldCircularOrbit
Get the mean longitude argument.
getLM() - Method in class org.orekit.orbits.FieldEquinoctialOrbit
Get the mean longitude argument.
getLM() - Method in class org.orekit.orbits.FieldKeplerianOrbit
Get the mean longitude argument.
getLM() - Method in class org.orekit.orbits.FieldOrbit
Get the mean longitude argument.
getLM() - Method in class org.orekit.orbits.KeplerianOrbit
Get the mean longitude argument.
getLM() - Method in class org.orekit.orbits.Orbit
Get the mean longitude argument.
getLM() - Method in class org.orekit.propagation.FieldSpacecraftState
Get the mean latitude argument (as per equinoctial parameters).
getLM() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
Get the mean longitude.
getLM() - Method in class org.orekit.propagation.SpacecraftState
Get the mean 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.
getLMaDot() - Method in class org.orekit.data.BodiesElements
Get the mean Mars longitude time derivative.
getLMaDot() - Method in class org.orekit.data.FieldBodiesElements
Get the mean Mars longitude time derivative.
getLMDot() - Method in class org.orekit.orbits.CartesianOrbit
Get the mean longitude argument derivative.
getLMDot() - Method in class org.orekit.orbits.CircularOrbit
Get the mean longitude argument derivative.
getLMDot() - Method in class org.orekit.orbits.EquinoctialOrbit
Get the mean longitude argument derivative.
getLMDot() - Method in class org.orekit.orbits.FieldCartesianOrbit
Get the mean longitude argument derivative.
getLMDot() - Method in class org.orekit.orbits.FieldCircularOrbit
Get the mean longitude argument derivative.
getLMDot() - Method in class org.orekit.orbits.FieldEquinoctialOrbit
Get the mean longitude argument derivative.
getLMDot() - Method in class org.orekit.orbits.FieldKeplerianOrbit
Get the mean longitude argument derivative.
getLMDot() - Method in class org.orekit.orbits.FieldOrbit
Get the mean longitude argument derivative.
getLMDot() - Method in class org.orekit.orbits.KeplerianOrbit
Get the mean longitude argument derivative.
getLMDot() - Method in class org.orekit.orbits.Orbit
Get the mean longitude argument derivative.
getLMe() - Method in class org.orekit.data.BodiesElements
Get the mean Mercury longitude.
getLMe() - Method in class org.orekit.data.FieldBodiesElements
Get the mean Mercury longitude.
getLMeDot() - Method in class org.orekit.data.BodiesElements
Get the mean Mercury longitude time derivative.
getLMeDot() - Method in class org.orekit.data.FieldBodiesElements
Get the mean Mercury longitude time derivative.
getLNe() - Method in class org.orekit.data.BodiesElements
Get the mean Neptune longitude.
getLNe() - Method in class org.orekit.data.FieldBodiesElements
Get the mean Neptune longitude.
getLNeDot() - Method in class org.orekit.data.BodiesElements
Get the mean Neptune longitude time derivative.
getLNeDot() - Method in class org.orekit.data.FieldBodiesElements
Get the mean Neptune longitude time derivative.
getLns(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.LnsCoefficients
Get the value of Lns(γ).
getLoadedAstronomicalUnit() - Method in class org.orekit.bodies.JPLEphemeridesLoader
Get astronomical unit.
getLoadedConstant(String...) - Method in class org.orekit.bodies.JPLEphemeridesLoader
Get a constant defined in the ephemerides headers.
getLoadedDataNames() - Method in class org.orekit.data.DataProvidersManager
Get an unmodifiable view of the set of data file names that have been loaded.
getLoadedEarthMoonMassRatio() - Method in class org.orekit.bodies.JPLEphemeridesLoader
Get Earth/Moon mass ratio.
getLoadedGravitationalCoefficient(JPLEphemeridesLoader.EphemerisType) - Method in class org.orekit.bodies.JPLEphemeridesLoader
Get the gravitational coefficient of a body.
getLocalizedMessage() - Method in exception org.orekit.errors.OrekitException
getLocalizedMessage() - Method in exception org.orekit.errors.OrekitIllegalArgumentException
getLocalizedMessage() - Method in exception org.orekit.errors.OrekitIllegalStateException
getLocalizedMessage() - Method in exception org.orekit.errors.OrekitInternalError
getLocalizedMessage() - Method in exception org.orekit.errors.OrekitParseException
getLocalizedString(Locale) - Method in enum org.orekit.errors.OrekitMessages
getLocation() - Method in class org.orekit.gnss.DOP
Gets the location with respect to the Earth where DOP was calculated.
getLOD() - Method in class org.orekit.frames.EOPEntry
Get the LoD (Length of Day) value.
getLOD(AbsoluteDate) - Method in class org.orekit.frames.EOPHistory
Get the LoD (Length of Day) value.
getLOD(FieldAbsoluteDate<T>) - Method in class org.orekit.frames.EOPHistory
Get the LoD (Length of Day) value.
getLofType() - Method in enum org.orekit.files.ccsds.CCSDSFrame
Get the type of Local Orbital frame.
getLofType() - Method in class org.orekit.files.ccsds.OEMFile.CovarianceMatrix
Get coordinate system for covariance matrix, for Local Orbital Frames.
getLoggedEvents() - Method in class org.orekit.propagation.events.EventsLogger
Get an immutable copy of the logged events.
getLoggedEvents() - Method in class org.orekit.propagation.events.FieldEventsLogger
Get an immutable copy of the logged events.
getLongitude() - Method in class org.orekit.bodies.FieldGeodeticPoint
Get the longitude.
getLongitude() - Method in class org.orekit.bodies.GeodeticPoint
Get the longitude.
getLongitude() - Method in class org.orekit.propagation.events.LongitudeCrossingDetector
Get the fixed longitude to be crossed (radians).
getLoveNumbers() - Method in enum org.orekit.utils.IERSConventions
Get the Love numbers.
getLowerCaseAbbreviation() - Method in enum org.orekit.time.Month
Get the lower case three letters abbreviation.
getLowerCaseName() - Method in enum org.orekit.time.Month
Get the lower case full name.
getLPrime() - Method in class org.orekit.data.DelaunayArguments
Get the mean anomaly of the Sun.
getLPrime() - Method in class org.orekit.data.FieldDelaunayArguments
Get the mean anomaly of the Sun.
getLPrimeDot() - Method in class org.orekit.data.DelaunayArguments
Get the mean anomaly of the Sun time derivative.
getLPrimeDot() - Method in class org.orekit.data.FieldDelaunayArguments
Get the mean anomaly of the Sun time derivative.
getLSa() - Method in class org.orekit.data.BodiesElements
Get the mean Saturn longitude.
getLSa() - Method in class org.orekit.data.FieldBodiesElements
Get the mean Saturn longitude.
getLSaDot() - Method in class org.orekit.data.BodiesElements
Get the mean Saturn longitude time derivative.
getLSaDot() - Method in class org.orekit.data.FieldBodiesElements
Get the mean Saturn longitude time derivative.
getLUr() - Method in class org.orekit.data.BodiesElements
Get the mean Uranus longitude.
getLUr() - Method in class org.orekit.data.FieldBodiesElements
Get the mean Uranus longitude.
getLUrDot() - Method in class org.orekit.data.BodiesElements
Get the mean Uranus longitude time derivative.
getLUrDot() - Method in class org.orekit.data.FieldBodiesElements
Get the mean Uranus longitude time derivative.
getLv() - Method in class org.orekit.orbits.CartesianOrbit
Get the true longitude argument.
getLv() - Method in class org.orekit.orbits.CircularOrbit
Get the true longitude argument.
getLv() - Method in class org.orekit.orbits.EquinoctialOrbit
Get the true longitude argument.
getLv() - Method in class org.orekit.orbits.FieldCartesianOrbit
Get the true longitude argument.
getLv() - Method in class org.orekit.orbits.FieldCircularOrbit
Get the true longitude argument.
getLv() - Method in class org.orekit.orbits.FieldEquinoctialOrbit
Get the true longitude argument.
getLv() - Method in class org.orekit.orbits.FieldKeplerianOrbit
Get the true longitude argument.
getLv() - Method in class org.orekit.orbits.FieldOrbit
Get the true longitude argument.
getLv() - Method in class org.orekit.orbits.KeplerianOrbit
Get the true longitude argument.
getLv() - Method in class org.orekit.orbits.Orbit
Get the true longitude argument.
getLv() - Method in class org.orekit.propagation.FieldSpacecraftState
Get the true latitude argument (as per equinoctial parameters).
getLv() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
Get the true longitude.
getLv() - Method in class org.orekit.propagation.SpacecraftState
Get the true latitude argument (as per equinoctial parameters).
getLvDot() - Method in class org.orekit.orbits.CartesianOrbit
Get the true longitude argument derivative.
getLvDot() - Method in class org.orekit.orbits.CircularOrbit
Get the true longitude argument derivative.
getLvDot() - Method in class org.orekit.orbits.EquinoctialOrbit
Get the true longitude argument derivative.
getLvDot() - Method in class org.orekit.orbits.FieldCartesianOrbit
Get the true longitude argument derivative.
getLvDot() - Method in class org.orekit.orbits.FieldCircularOrbit
Get the true longitude argument derivative.
getLvDot() - Method in class org.orekit.orbits.FieldEquinoctialOrbit
Get the true longitude argument derivative.
getLvDot() - Method in class org.orekit.orbits.FieldKeplerianOrbit
Get the true longitude argument derivative.
getLvDot() - Method in class org.orekit.orbits.FieldOrbit
Get the true longitude argument derivative.
getLvDot() - Method in class org.orekit.orbits.KeplerianOrbit
Get the true longitude argument derivative.
getLvDot() - Method in class org.orekit.orbits.Orbit
Get the true longitude argument derivative.
getLVe() - Method in class org.orekit.data.BodiesElements
Get the mean Venus longitude.
getLVe() - Method in class org.orekit.data.FieldBodiesElements
Get the mean Venus longitude.
getLVeDot() - Method in class org.orekit.data.BodiesElements
Get the mean Venus longitude time derivative.
getLVeDot() - Method in class org.orekit.data.FieldBodiesElements
Get the mean Venus longitude time derivative.
getM0() - Method in class org.orekit.gnss.GPSAlmanac
 
getM0() - Method in interface org.orekit.propagation.analytical.gnss.GPSOrbitalElements
Gets the Mean Anomaly at Reference Time.
getMainStateEquations(ODEIntegrator) - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
Get the differential equations to integrate (for main state only).
getMainStateEquations(FieldODEIntegrator<T>) - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator
Get the differential equations to integrate (for main state only).
getMainStateEquations(FieldODEIntegrator<T>) - Method in class org.orekit.propagation.numerical.FieldNumericalPropagator
Get the differential equations to integrate (for main state only).
getMainStateEquations(ODEIntegrator) - Method in class org.orekit.propagation.numerical.NumericalPropagator
Get the differential equations to integrate (for main state only).
getMainStateEquations(ODEIntegrator) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator
Get the differential equations to integrate (for main state only).
getManagedAdditionalStates() - Method in class org.orekit.propagation.AbstractPropagator
Get all the names of all managed states.
getManagedAdditionalStates() - Method in class org.orekit.propagation.analytical.Ephemeris
Get all the names of all managed states.
getManagedAdditionalStates() - Method in class org.orekit.propagation.FieldAbstractPropagator
Get all the names of all managed states.
getManagedAdditionalStates() - Method in interface org.orekit.propagation.FieldPropagator
Get all the names of all managed states.
getManagedAdditionalStates() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
Get all the names of all managed states.
getManagedAdditionalStates() - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator
Get all the names of all managed states.
getManagedAdditionalStates() - Method in interface org.orekit.propagation.Propagator
Get all the names of all managed states.
getManeuver(int) - Method in class org.orekit.files.ccsds.OPMFile
Get a maneuver.
getManeuvers() - Method in class org.orekit.files.ccsds.OPMFile
Get a list of all maneuvers.
getMapper() - Method in class org.orekit.propagation.numerical.PartialDerivativesEquations
Get a mapper between two-dimensional Jacobians and one-dimensional additional state.
getMargin() - Method in class org.orekit.propagation.events.FieldOfView
Get the angular margin to apply (radians).
getMargin() - Method in class org.orekit.propagation.events.GeographicZoneDetector
Get the angular margin to apply (radians).
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.AggregateBoundedPropagator
 
getMass(AbsoluteDate) - Method in class org.orekit.propagation.analytical.EcksteinHechlerPropagator
Get the mass.
getMass(AbsoluteDate) - Method in class org.orekit.propagation.analytical.Ephemeris
Get the mass.
getMass(FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.analytical.FieldAbstractAnalyticalPropagator
Get the mass.
getMass(FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.analytical.FieldEcksteinHechlerPropagator
Get the mass.
getMass(FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.analytical.FieldKeplerianPropagator
Get the mass.
getMass(AbsoluteDate) - Method in class org.orekit.propagation.analytical.gnss.GPSPropagator
Get the mass.
getMass(AbsoluteDate) - Method in class org.orekit.propagation.analytical.KeplerianPropagator
Get the mass.
getMass(AbsoluteDate) - Method in class org.orekit.propagation.analytical.tle.TLEPropagator
Get the mass.
getMass() - Method in class org.orekit.propagation.FieldSpacecraftState
Gets the current mass.
getMass(FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.integration.FieldIntegratedEphemeris
Get the mass.
getMass(AbsoluteDate) - Method in class org.orekit.propagation.integration.IntegratedEphemeris
Get the mass.
getMass() - Method in class org.orekit.propagation.SpacecraftState
Gets the current mass.
getMasterStation() - Method in class org.orekit.estimation.measurements.TurnAroundRange
Get the master ground station from which measurement is performed.
getMatrix() - Method in class org.orekit.files.ccsds.OEMFile.CovarianceMatrix
Get the covariance matrix.
getMatrixLine(int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.PolynomialFunctionMatrix
Get a line of the matrix.
getMaxAlt() - Method in class org.orekit.forces.drag.atmosphere.HarrisPriester
Get the maximal altitude for the model.
getMaxAvailableDegree() - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
Get the maximal degree available in the last file parsed.
getMaxAvailableOrder() - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
Get the maximal order available in the last file parsed.
getMaxCheckInterval() - Method in class org.orekit.propagation.events.AbstractDetector
Get maximal time interval between switching function checks.
getMaxCheckInterval() - Method in interface org.orekit.propagation.events.EventDetector
Get maximal time interval between switching function checks.
getMaxCheckInterval() - Method in class org.orekit.propagation.events.FieldAbstractDetector
Get maximal time interval between switching function checks.
getMaxCheckInterval() - Method in interface org.orekit.propagation.events.FieldEventDetector
Get maximal time interval between switching function checks.
getMaxChunksDuration() - Method in class org.orekit.bodies.JPLEphemeridesLoader
Get the maximal chunks duration.
getMaxDate() - Method in class org.orekit.forces.drag.atmosphere.data.MarshallSolarActivityFutureEstimation
Gets the available data range maximum date.
getMaxDate() - Method in interface org.orekit.forces.drag.atmosphere.DTM2000InputParameters
Gets the available data range maximum date.
getMaxDate() - Method in interface org.orekit.forces.drag.atmosphere.JB2008InputParameters
Gets the available data range maximum date.
getMaxDate() - Method in interface org.orekit.forces.drag.atmosphere.NRLMSISE00InputParameters
Gets the available data range maximum date.
getMaxDate() - Method in class org.orekit.propagation.analytical.AggregateBoundedPropagator
 
getMaxDate() - Method in class org.orekit.propagation.analytical.Ephemeris
Get the last date of the range.
getMaxDate() - Method in interface org.orekit.propagation.BoundedPropagator
Get the last date of the range.
getMaxDate() - Method in interface org.orekit.propagation.FieldBoundedPropagator
Get the last date of the range.
getMaxDate() - Method in class org.orekit.propagation.integration.FieldIntegratedEphemeris
Get the last date of the range.
getMaxDate() - Method in class org.orekit.propagation.integration.IntegratedEphemeris
Get the last date of the range.
getMaxDegree() - Method in class org.orekit.forces.gravity.potential.CachedNormalizedSphericalHarmonicsProvider
Get the maximal supported degree.
getMaxDegree() - Method in class org.orekit.forces.gravity.potential.OceanTidesWave
Get the maximum supported degree.
getMaxDegree() - Method in interface org.orekit.forces.gravity.potential.SphericalHarmonicsProvider
Get the maximal supported degree.
getMaxIterationCount() - Method in class org.orekit.propagation.events.AbstractDetector
Get maximal number of iterations in the event time search.
getMaxIterationCount() - Method in interface org.orekit.propagation.events.EventDetector
Get maximal number of iterations in the event time search.
getMaxIterationCount() - Method in class org.orekit.propagation.events.FieldAbstractDetector
Get maximal number of iterations in the event time search.
getMaxIterationCount() - Method in interface org.orekit.propagation.events.FieldEventDetector
Get maximal number of iterations in the event time search.
getMaxOrder() - Method in class org.orekit.forces.gravity.potential.CachedNormalizedSphericalHarmonicsProvider
Get the maximal supported order.
getMaxOrder() - Method in class org.orekit.forces.gravity.potential.OceanTidesWave
Get the maximum supported order.
getMaxOrder() - Method in interface org.orekit.forces.gravity.potential.SphericalHarmonicsProvider
Get the maximal supported order.
getMaxOrder() - Method in enum org.orekit.utils.AngularDerivativesFilter
Get the maximum derivation order.
getMaxOrder() - Method in enum org.orekit.utils.CartesianDerivativesFilter
Get the maximum derivation order.
getMaxParseDegree() - Method in class org.orekit.forces.gravity.potential.OceanTidesReader
Get the degree limit for the next file parsing.
getMaxParseDegree() - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
Get the degree limit for the next file parsing.
getMaxParseOrder() - Method in class org.orekit.forces.gravity.potential.OceanTidesReader
Get the order limit for the next file parsing.
getMaxParseOrder() - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
Get the order limit for the next file parsing.
getMaxSlots() - Method in class org.orekit.utils.GenericTimeStampedCache
Get the maximum number of independent cached time slots.
getMaxSpan() - Method in class org.orekit.utils.GenericTimeStampedCache
Get the maximum duration span in seconds of one slot.
getMaxValue() - Method in class org.orekit.utils.ParameterDriver
Get maximum parameter value.
getMeanAnomaly() - Method in class org.orekit.orbits.FieldKeplerianOrbit
Get the mean anomaly.
getMeanAnomaly() - Method in class org.orekit.orbits.KeplerianOrbit
Get the mean anomaly.
getMeanAnomaly() - Method in class org.orekit.propagation.analytical.tle.TLE
Get the mean anomaly.
getMeanAnomalyDot() - Method in class org.orekit.orbits.FieldKeplerianOrbit
Get the mean anomaly derivative.
getMeanAnomalyDot() - Method in class org.orekit.orbits.KeplerianOrbit
Get the mean anomaly derivative.
getMeanElementRate(SpacecraftState) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution
Computes the mean equinoctial elements rates dai / dt.
getMeanElementRate(SpacecraftState) - Method in interface org.orekit.propagation.semianalytical.dsst.forces.DSSTForceModel
Computes the mean equinoctial elements rates dai / dt.
getMeanElementRate(SpacecraftState) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseral
Computes the mean equinoctial elements rates dai / dt.
getMeanElementRate(SpacecraftState) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBody
Computes the mean equinoctial elements rates dai / dt.
getMeanElementRate(SpacecraftState) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonal
Computes the mean equinoctial elements rates dai / dt.
getMeanElementTheory() - Method in class org.orekit.files.ccsds.OMMFile.OMMMetaData
Get the description of the Mean Element Theory.
getMeanFlux(AbsoluteDate) - Method in class org.orekit.forces.drag.atmosphere.data.MarshallSolarActivityFutureEstimation
Get the value of the mean solar flux.
getMeanFlux(AbsoluteDate) - Method in interface org.orekit.forces.drag.atmosphere.DTM2000InputParameters
Get the value of the mean solar flux.
getMeanMotion() - Method in class org.orekit.files.ccsds.OMMFile
Get the orbit mean motion.
getMeanMotion() - Method in class org.orekit.gnss.GPSAlmanac
 
getMeanMotion() - Method in interface org.orekit.propagation.analytical.gnss.GPSOrbitalElements
Gets the Mean Motion.
getMeanMotion() - Method in class org.orekit.propagation.analytical.tle.TLE
Get the mean motion.
getMeanMotion() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
Get the Keplerian mean motion.
getMeanMotionDot() - Method in class org.orekit.files.ccsds.OMMFile
Get the first time derivative of the mean motion.
getMeanMotionDotDot() - Method in class org.orekit.files.ccsds.OMMFile
Get the second time derivative of the mean motion.
getMeanMotionFirstDerivative() - Method in class org.orekit.propagation.analytical.tle.TLE
Get the mean motion first derivative.
getMeanMotionSecondDerivative() - Method in class org.orekit.propagation.analytical.tle.TLE
Get the mean motion second derivative.
getMeanObliquityFunction() - Method in enum org.orekit.utils.IERSConventions
Get the function computing mean obliquity of the ecliptic.
getMeasurement() - Method in class org.orekit.files.ccsds.TDMFile.Observation
Getter for the measurement.
getMeasurementsParametersDrivers(boolean) - Method in class org.orekit.estimation.leastsquares.BatchLSEstimator
Get the measurements parameters supported by this estimator (including measurements and modifiers).
getMercury() - Static method in class org.orekit.bodies.CelestialBodyFactory
Get the Mercury singleton body.
getMessage(Locale) - Method in interface org.orekit.errors.LocalizedException
Gets the message in a specified locale.
getMessage(Locale) - Method in exception org.orekit.errors.OrekitException
Gets the message in a specified locale.
getMessage() - Method in exception org.orekit.errors.OrekitException
getMessage(Locale) - Method in exception org.orekit.errors.OrekitIllegalArgumentException
Gets the message in a specified locale.
getMessage() - Method in exception org.orekit.errors.OrekitIllegalArgumentException
getMessage(Locale) - Method in exception org.orekit.errors.OrekitIllegalStateException
Gets the message in a specified locale.
getMessage() - Method in exception org.orekit.errors.OrekitIllegalStateException
getMessage(Locale) - Method in exception org.orekit.errors.OrekitInternalError
Gets the message in a specified locale.
getMessage() - Method in exception org.orekit.errors.OrekitInternalError
getMessage(Locale) - Method in exception org.orekit.errors.OrekitParseException
Gets the message in a specified locale.
getMessage() - Method in exception org.orekit.errors.OrekitParseException
getMetaData() - Method in class org.orekit.files.ccsds.OEMFile.EphemeridesBlock
Get the meta-data for the block.
getMetaData() - Method in class org.orekit.files.ccsds.OGMFile
Get the meta data.
getMetaData() - Method in class org.orekit.files.ccsds.OMMFile
Get the meta data.
getMetaData() - Method in class org.orekit.files.ccsds.OPMFile
Get the meta data.
getMetaData() - Method in class org.orekit.files.ccsds.TDMFile.ObservationsBlock
Get the meta-data for the block.
getMetaDataComment() - Method in class org.orekit.files.ccsds.OPMFile
Get the comment for meta-data.
getMinAlt() - Method in class org.orekit.forces.drag.atmosphere.HarrisPriester
Get the minimal altitude for the model.
getMinDate() - Method in class org.orekit.forces.drag.atmosphere.data.MarshallSolarActivityFutureEstimation
Gets the available data range minimum date.
getMinDate() - Method in interface org.orekit.forces.drag.atmosphere.DTM2000InputParameters
Gets the available data range minimum date.
getMinDate() - Method in interface org.orekit.forces.drag.atmosphere.JB2008InputParameters
Gets the available data range minimum date.
getMinDate() - Method in interface org.orekit.forces.drag.atmosphere.NRLMSISE00InputParameters
Gets the available data range minimum date.
getMinDate() - Method in class org.orekit.propagation.analytical.AggregateBoundedPropagator
 
getMinDate() - Method in class org.orekit.propagation.analytical.Ephemeris
Get the first date of the range.
getMinDate() - Method in interface org.orekit.propagation.