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

A

a - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator
final semi major axis.
a - Variable in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution
a.
A - Variable in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution
A = sqrt(μ * a).
a0dp - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator
original recovered semi major axis.
AbsoluteDate - Class in org.orekit.time
This class represents a specific instant in time.
AbsoluteDate() - Constructor for class org.orekit.time.AbsoluteDate
Create an instance with a default value (AbsoluteDate.J2000_EPOCH).
AbsoluteDate(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, int, int, 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(int, Month, int, TimeScale) - Constructor for class org.orekit.time.AbsoluteDate
Build an instance from a location in a time scale.
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(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.
AbsoluteDate(DateComponents, TimeComponents, 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(DateTimeComponents, TimeScale) - Constructor for class org.orekit.time.AbsoluteDate
Build an instance from a location in a 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.
AbstractCovarianceMatrixProvider - Class in org.orekit.estimation.sequential
Abstract provider handling a predefined initial covariance matrix.
AbstractCovarianceMatrixProvider(RealMatrix) - Constructor for class org.orekit.estimation.sequential.AbstractCovarianceMatrixProvider
Simple constructor.
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.
AbstractGNSSAttitudeProvider - Class in org.orekit.gnss.attitude
Base class for attitude providers for navigation satellites.
AbstractGNSSAttitudeProvider(AbsoluteDate, AbsoluteDate, ExtendedPVCoordinatesProvider, Frame) - Constructor for class org.orekit.gnss.attitude.AbstractGNSSAttitudeProvider
Simple constructor.
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
AbstractMeasurement(AbsoluteDate, double[], double[], double[], List<ObservableSatellite>) - Constructor for class org.orekit.estimation.measurements.AbstractMeasurement
Simple constructor, for multi-dimensional measurements.
AbstractMeasurement(AbsoluteDate, double, double, double, List<Integer>, ParameterDriver...) - Constructor for class org.orekit.estimation.measurements.AbstractMeasurement
AbstractMeasurement(AbsoluteDate, double, double, double, List<ObservableSatellite>) - Constructor for class org.orekit.estimation.measurements.AbstractMeasurement
Simple constructor for mono-dimensional measurements.
AbstractMeasurementBuilder<T extends ObservedMeasurement<T>> - Class in org.orekit.estimation.measurements.generation
Base class for measurements builders.
AbstractMeasurementBuilder(CorrelatedRandomVectorGenerator, double[], double[], ObservableSatellite...) - Constructor for class org.orekit.estimation.measurements.generation.AbstractMeasurementBuilder
Simple constructor.
AbstractMeasurementBuilder(CorrelatedRandomVectorGenerator, double, double, ObservableSatellite...) - Constructor for class org.orekit.estimation.measurements.generation.AbstractMeasurementBuilder
Simple constructor.
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.
AbstractScheduler<T extends ObservedMeasurement<T>> - Class in org.orekit.estimation.measurements.generation
Base implementation of Scheduler managing dates selection.
AbstractScheduler(MeasurementBuilder<T>, DatesSelector) - Constructor for class org.orekit.estimation.measurements.generation.AbstractScheduler
Simple constructor.
acceleration(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.AbstractParametricAcceleration
Compute acceleration.
acceleration(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.drag.DragForce
Compute acceleration.
acceleration(FieldSpacecraftState<T>, T[]) - Method in interface org.orekit.forces.ForceModel
Compute acceleration.
acceleration(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.gravity.HolmesFeatherstoneAttractionModel
Compute acceleration.
acceleration(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.gravity.NewtonianAttraction
Compute acceleration.
acceleration(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.gravity.OceanTides
Compute acceleration.
acceleration(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.gravity.Relativity
Compute acceleration.
acceleration(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.gravity.SolidTides
Compute acceleration.
acceleration(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.gravity.ThirdBodyAttraction
Compute acceleration.
acceleration(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.maneuvers.ConstantThrustManeuver
Compute acceleration.
acceleration(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.radiation.SolarRadiationPressure
Compute acceleration.
acceleration(SpacecraftState, double[]) - Method in class org.orekit.forces.AbstractParametricAcceleration
Compute acceleration.
acceleration(SpacecraftState, double[]) - Method in class org.orekit.forces.drag.DragForce
Compute acceleration.
acceleration(SpacecraftState, double[]) - Method in interface org.orekit.forces.ForceModel
Compute acceleration.
acceleration(SpacecraftState, double[]) - Method in class org.orekit.forces.gravity.HolmesFeatherstoneAttractionModel
Compute acceleration.
acceleration(SpacecraftState, double[]) - Method in class org.orekit.forces.gravity.NewtonianAttraction
Compute acceleration.
acceleration(SpacecraftState, double[]) - Method in class org.orekit.forces.gravity.OceanTides
Compute acceleration.
acceleration(SpacecraftState, double[]) - Method in class org.orekit.forces.gravity.Relativity
Compute acceleration.
acceleration(SpacecraftState, double[]) - Method in class org.orekit.forces.gravity.SolidTides
Compute acceleration.
acceleration(SpacecraftState, double[]) - Method in class org.orekit.forces.gravity.ThirdBodyAttraction
Compute acceleration.
acceleration(SpacecraftState, double[]) - Method in class org.orekit.forces.maneuvers.ConstantThrustManeuver
Compute acceleration.
acceleration(SpacecraftState, double[]) - Method in class org.orekit.forces.radiation.SolarRadiationPressure
Compute acceleration.
acceptStep(FieldAbstractAnalyticalPropagator.FieldBasicStepInterpolator, FieldAbsoluteDate<T>, double) - Method in class org.orekit.propagation.analytical.FieldAbstractAnalyticalPropagator
Accept a step, triggering events and step handlers.
acceptStep(OrekitStepInterpolator, AbsoluteDate, double) - Method in class org.orekit.propagation.analytical.AbstractAnalyticalPropagator
Accept a step, triggering events and step handlers.
AdamsBashforthIntegratorBuilder - Class in org.orekit.propagation.conversion
Builder for AdamsBashforthIntegrator.
AdamsBashforthIntegratorBuilder(int, double, double, double) - Constructor for class org.orekit.propagation.conversion.AdamsBashforthIntegratorBuilder
Build a new instance.
AdamsMoultonIntegratorBuilder - Class in org.orekit.propagation.conversion
Builder for AdamsMoultonIntegrator.
AdamsMoultonIntegratorBuilder(int, double, double, double) - Constructor for class org.orekit.propagation.conversion.AdamsMoultonIntegratorBuilder
Build a new instance.
AdapterDetector - Class in org.orekit.propagation.events
Base class for adapting an existing detector.
AdapterDetector(EventDetector) - Constructor for class org.orekit.propagation.events.AdapterDetector
Build an adaptor wrapping an existing detector.
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, double...) - Method in class org.orekit.propagation.SpacecraftState
Add an additional state.
addAdditionalState(String, T...) - Method in class org.orekit.propagation.FieldSpacecraftState
Add an additional state.
addAdditionalStateProvider(AdditionalStateProvider) - Method in class org.orekit.propagation.AbstractPropagator
Add a set of user-specified state parameters to be computed along with the orbit propagation.
addAdditionalStateProvider(AdditionalStateProvider) - Method in interface org.orekit.propagation.Propagator
Add a set of user-specified state parameters to be computed along with the orbit propagation.
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.
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(BodiesElements, double[][], double[][]) - Method in class org.orekit.forces.gravity.potential.OceanTidesWave
Add the contribution of the wave to Stokes coefficients.
addContribution(FieldSpacecraftState<T>, FieldTimeDerivativesEquations<T>) - 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 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.maneuvers.ConstantThrustManeuver
Compute the contribution of the force model to the perturbing acceleration.
addContribution(SpacecraftState, TimeDerivativesEquations) - Method in interface org.orekit.forces.ForceModel
Compute the contribution of the force model to the perturbing acceleration.
addContribution(SpacecraftState, TimeDerivativesEquations) - Method in class org.orekit.forces.gravity.NewtonianAttraction
Compute the contribution of the force model to the perturbing acceleration.
addContribution(SpacecraftState, TimeDerivativesEquations) - Method in class org.orekit.forces.maneuvers.ConstantThrustManeuver
Compute the contribution of the force model to the perturbing acceleration.
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(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(D) - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator
Add an event detector.
addEventDetector(EventDetector) - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
Add an event detector.
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(T) - Method in interface org.orekit.propagation.Propagator
Add an event detector.
addFilter(DataFilter) - Method in class org.orekit.data.DataProvidersManager
Add a data filter.
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.
ADDITIONAL_STATE_NAME_ALREADY_IN_USE - org.orekit.errors.OrekitMessages
 
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(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.
addKeplerContribution(PositionAngle, double, double[]) - Method in class org.orekit.orbits.CartesianOrbit
Add the contribution of the Keplerian motion to parameters derivatives
addKeplerContribution(PositionAngle, double, double[]) - Method in class org.orekit.orbits.CircularOrbit
Add the contribution of the Keplerian motion to parameters derivatives
addKeplerContribution(PositionAngle, double, double[]) - Method in class org.orekit.orbits.EquinoctialOrbit
Add the contribution of the Keplerian motion to parameters derivatives
addKeplerContribution(PositionAngle, double, double[]) - Method in class org.orekit.orbits.KeplerianOrbit
Add the contribution of the Keplerian motion to parameters derivatives
addKeplerContribution(PositionAngle, double, double[]) - Method in class org.orekit.orbits.Orbit
Add the contribution of the Keplerian motion to parameters derivatives
addKeplerContribution(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
addMassDerivative(double) - Method in interface org.orekit.propagation.numerical.TimeDerivativesEquations
Add the contribution of the flow rate (dm/dt).
addMassDerivative(T) - Method in interface org.orekit.propagation.numerical.FieldTimeDerivativesEquations
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 class org.orekit.estimation.measurements.generation.AbstractMeasurementBuilder
Add a modifier.
addModifier(EstimationModifier<T>) - Method in interface org.orekit.estimation.measurements.generation.MeasurementBuilder
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(String, AbsoluteDate, double) - Method in class org.orekit.files.ccsds.TDMFile.ObservationsBlock
Adds an observation data line.
addObservation(TDMFile.Observation) - 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(AngularCoordinates) - Method in class org.orekit.utils.TimeStampedAngularCoordinates
Add an offset from the instance.
addOffset(FieldAngularCoordinates<T>) - Method in class org.orekit.utils.FieldAngularCoordinates
Add an offset from the instance.
addOffset(FieldAngularCoordinates<T>) - Method in class org.orekit.utils.TimeStampedFieldAngularCoordinates
Add an offset from the instance.
addParameterDriver(ParameterDriver) - Method in class org.orekit.estimation.measurements.AbstractMeasurement
Add a parameter driver.
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.
addPropagationConfiguration(NumericalPropagatorBuilder, CovarianceMatrixProvider) - Method in class org.orekit.estimation.sequential.KalmanEstimatorBuilder
Add a propagation configuration.
addPropagator(Propagator) - Method in class org.orekit.estimation.measurements.generation.Generator
Add a propagator.
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.
addScheduler(Scheduler<T>) - Method in class org.orekit.estimation.measurements.generation.Generator
Add a sequences generator for a specific measurement type.
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, AbsoluteDate) - Method in class org.orekit.utils.TimeSpanMap
Add an entry valid after a limit date.
addValidAfter(T, FieldAbsoluteDate<D>) - Method in class org.orekit.utils.FieldTimeSpanMap
Add an entry valid after a limit date.
addValidBefore(T, AbsoluteDate) - Method in class org.orekit.utils.TimeSpanMap
Add an entry valid before a limit date.
addValidBefore(T, FieldAbsoluteDate<D>) - Method in class org.orekit.utils.FieldTimeSpanMap
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(double, double, 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.
AlignmentDetector(Orbit, PVCoordinatesProvider, double) - Constructor for class org.orekit.propagation.events.AlignmentDetector
Build a new alignment detector.
ALMOST_CRITICALLY_INCLINED_ORBIT - org.orekit.errors.OrekitMessages
 
ALMOST_EQUATORIAL_ORBIT - org.orekit.errors.OrekitMessages
 
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.
ALTITUDE_BELOW_ALLOWED_THRESHOLD - org.orekit.errors.OrekitMessages
 
AltitudeDetector - Class in org.orekit.propagation.events
Finder for satellite altitude crossing events.
AltitudeDetector(double, double, 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, BodyShape) - Constructor for class org.orekit.propagation.events.AltitudeDetector
Build a new altitude detector.
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.
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.
ANGLE_1 - org.orekit.files.ccsds.Keyword
Data: ANGLE_1 in degrees and in [-180, +360[ [deg].
ANGLE_2 - org.orekit.files.ccsds.Keyword
Data: ANGLE_2 in degrees and in [-180, +360[ [deg].
ANGLE_TYPE - org.orekit.files.ccsds.Keyword
Meta-data: The ANGLE_TYPE keyword shall indicate the type of antenna geometry represented in the angle data (ANGLE_1 and ANGLE_2 keywords).
ANGLE_TYPE_NOT_SUPPORTED - org.orekit.errors.OrekitMessages
 
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
AngularAzEl(GroundStation, AbsoluteDate, double[], double[], double[], int) - Constructor for class org.orekit.estimation.measurements.AngularAzEl
AngularAzEl(GroundStation, AbsoluteDate, double[], double[], double[], ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.AngularAzEl
Simple constructor.
AngularAzElBuilder - Class in org.orekit.estimation.measurements.generation
Builder for AngularAzEl measurements.
AngularAzElBuilder(CorrelatedRandomVectorGenerator, GroundStation, double[], double[], ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.generation.AngularAzElBuilder
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(FieldRotation<DerivativeStructure>) - Constructor for class org.orekit.utils.AngularCoordinates
Builds a AngularCoordinates from a FieldRotation<DerivativeStructure>.
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) - Constructor for class org.orekit.utils.AngularCoordinates
Build one of the rotations that transform one pv coordinates into another one.
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.
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
AngularRaDec(GroundStation, Frame, AbsoluteDate, double[], double[], double[], int) - Constructor for class org.orekit.estimation.measurements.AngularRaDec
AngularRaDec(GroundStation, Frame, AbsoluteDate, double[], double[], double[], ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.AngularRaDec
Simple constructor.
AngularRaDecBuilder - Class in org.orekit.estimation.measurements.generation
Builder for AngularRaDec measurements.
AngularRaDecBuilder(CorrelatedRandomVectorGenerator, GroundStation, Frame, double[], double[], ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.generation.AngularRaDecBuilder
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(DiscreteTroposphericModel) - Constructor for class org.orekit.estimation.measurements.modifiers.AngularTroposphericDelayModifier
Constructor.
Antenna - Class in org.orekit.gnss.antenna
GNSS antenna model.
Antenna(String, String, Map<Frequency, FrequencyPattern>) - Constructor for class org.orekit.gnss.antenna.Antenna
Simple constructor.
AntexLoader - Class in org.orekit.gnss.antenna
Factory for GNSS antennas (both receiver and satellite).
AntexLoader(String) - Constructor for class org.orekit.gnss.antenna.AntexLoader
Simple constructor.
apply(Orbit) - Method in class org.orekit.forces.maneuvers.SmallManeuverAnalyticalModel
Compute the effect of the maneuver on an orbit.
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.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(SpacecraftState) - Method in class org.orekit.propagation.analytical.J2DifferentialEffect
Apply the effect to a spacecraft state.
apply(SpacecraftState) - Method in interface org.orekit.propagation.events.FunctionalDetector.GFunction
Deprecated.
Use ToDoubleFunction.applyAsDouble(Object) instead. Will be removed in next major release.
applyAllFilters(NamedData) - Method in class org.orekit.data.DataProvidersManager
Apply all the relevant data filters, taking care of layers.
applyTo(FieldPVCoordinates<T>) - Method in class org.orekit.utils.AngularCoordinates
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(PVCoordinates) - 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(TimeStampedFieldPVCoordinates<T>) - Method in class org.orekit.utils.AngularCoordinates
Apply the rotation to a pv coordinates.
applyTo(TimeStampedFieldPVCoordinates<T>) - Method in class org.orekit.utils.FieldAngularCoordinates
Apply the rotation to a pv coordinates.
applyTo(TimeStampedPVCoordinates) - Method in class org.orekit.utils.AngularCoordinates
Apply the rotation to a pv coordinates.
applyTo(TimeStampedPVCoordinates) - 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.
APRIL - org.orekit.time.Month
April.
ApsideDetector - Class in org.orekit.propagation.events
Finder for apside crossing events.
ApsideDetector(double, Orbit) - Constructor for class org.orekit.propagation.events.ApsideDetector
Build a new instance.
ApsideDetector(Orbit) - Constructor for class org.orekit.propagation.events.ApsideDetector
Build a new instance.
ARC_SECONDS - org.orekit.data.PolynomialParser.Unit
Arc-seconds angles.
ARC_SECONDS_TO_RADIANS - Static variable in interface org.orekit.utils.Constants
Conversion factor from arc seconds to radians: 2*PI/(360*60*60).
ARG_OF_PERICENTER - org.orekit.files.ccsds.Keyword
Orbit argument of pericenter.
ASTRONOMICAL_DAWN_DUSK_ELEVATION - Static variable in class org.orekit.propagation.events.GroundAtNightDetector
Sun elevation at astronomical dawn/dusk (18° below horizon).
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, Rotation, Vector3D, Vector3D) - 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_POINTING_LAW_DOES_NOT_POINT_TO_GROUND - org.orekit.errors.OrekitMessages
 
attitudeProvider(AttitudeProvider) - Method in class org.orekit.propagation.analytical.gnss.GPSPropagator.Builder
Sets the attitude provider.
AttitudeProvider - Interface in org.orekit.attitudes
This interface represents an attitude provider model set.
AttitudeProviderModifier - Interface in org.orekit.attitudes
This interface represents an attitude provider that modifies/wraps another underlying provider.
AttitudesSequence - Class in org.orekit.attitudes
This classes manages a sequence of different attitude providers that are activated in turn according to switching events.
AttitudesSequence() - Constructor for class org.orekit.attitudes.AttitudesSequence
Constructor for an initially empty sequence.
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.
AUGUST - org.orekit.time.Month
August.
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.
AVERAGE - org.orekit.forces.drag.atmosphere.data.MarshallSolarActivityFutureEstimation.StrengthLevel
Average level of activity.

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.
B01 - org.orekit.gnss.Frequency
Beidou B1 (1561.098 MHz).
B02 - org.orekit.gnss.Frequency
Beidou B2 (1207.14 MHz).
B03 - org.orekit.gnss.Frequency
Beidou B3 (1268.52 MHz).
basicPropagate(AbsoluteDate) - Method in class org.orekit.propagation.analytical.AbstractAnalyticalPropagator
Propagate an orbit without any fancy features.
basicPropagate(AbsoluteDate) - Method in class org.orekit.propagation.analytical.AdapterPropagator
Propagate an orbit without any fancy features.
basicPropagate(AbsoluteDate) - Method in class org.orekit.propagation.analytical.Ephemeris
 
basicPropagate(AbsoluteDate) - Method in class org.orekit.propagation.integration.IntegratedEphemeris
Propagate an orbit without any fancy features.
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.
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.
BCT - org.orekit.files.sp3.SP3File.SP3OrbitType
broadcast.
BDTScale - Class in org.orekit.time
Beidou system time scale.
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.integration.AbstractIntegratedPropagator
Method called just before integration.
beforeIntegration(SpacecraftState, AbsoluteDate) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator
Method called just before integration.
BEIDOU - org.orekit.gnss.SatelliteSystem
Beidou system.
BEIDOU_2G - org.orekit.gnss.antenna.SatelliteAntennaCode
Deprecated.
BeiDou-2 GEO.
BEIDOU_2G - org.orekit.gnss.antenna.SatelliteType
BeiDou-2 GEO.
BEIDOU_2I - org.orekit.gnss.antenna.SatelliteAntennaCode
Deprecated.
BeiDou-2 IGSO.
BEIDOU_2I - org.orekit.gnss.antenna.SatelliteType
BeiDou-2 IGSO.
BEIDOU_2M - org.orekit.gnss.antenna.SatelliteAntennaCode
Deprecated.
BeiDou-2 MEO.
BEIDOU_2M - org.orekit.gnss.antenna.SatelliteType
BeiDou-2 MEO.
BEIDOU_3I - org.orekit.gnss.antenna.SatelliteAntennaCode
Deprecated.
BeiDou-3 IGSO.
BEIDOU_3I - org.orekit.gnss.antenna.SatelliteType
BeiDou-3 IGSO.
BeidouGeo - Class in org.orekit.gnss.attitude
Attitude providers for Beidou geostationary orbit navigation satellites.
BeidouGeo(AbsoluteDate, AbsoluteDate, ExtendedPVCoordinatesProvider, Frame) - Constructor for class org.orekit.gnss.attitude.BeidouGeo
Simple constructor.
BeidouIGSO - Class in org.orekit.gnss.attitude
Attitude providers for Beidou inclined geosynchronous orbit navigation satellites.
BeidouIGSO(AbsoluteDate, AbsoluteDate, ExtendedPVCoordinatesProvider, Frame) - Constructor for class org.orekit.gnss.attitude.BeidouIGSO
Simple constructor.
BeidouMeo - Class in org.orekit.gnss.attitude
Attitude providers for Beidou Medium Earth Orbit navigation satellites.
BeidouMeo(AbsoluteDate, AbsoluteDate, ExtendedPVCoordinatesProvider, Frame) - Constructor for class org.orekit.gnss.attitude.BeidouMeo
Simple constructor.
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.
BLOCK_I - org.orekit.gnss.antenna.SatelliteAntennaCode
Deprecated.
GPS Block I : SVN 01-11.
BLOCK_I - org.orekit.gnss.antenna.SatelliteType
GPS Block I : SVN 01-11.
BLOCK_II - org.orekit.gnss.antenna.SatelliteAntennaCode
Deprecated.
GPS Block II : SVN 13-21.
BLOCK_II - org.orekit.gnss.antenna.SatelliteType
GPS Block II : SVN 13-21.
BLOCK_IIA - org.orekit.gnss.antenna.SatelliteAntennaCode
Deprecated.
GPS Block IIA : SVN 22-40.
BLOCK_IIA - org.orekit.gnss.antenna.SatelliteType
GPS Block IIA : SVN 22-40.
BLOCK_IIF - org.orekit.gnss.antenna.SatelliteAntennaCode
Deprecated.
GPS Block IIF : SVN 62-73.
BLOCK_IIF - org.orekit.gnss.antenna.SatelliteType
GPS Block IIF : SVN 62-73.
BLOCK_IIIA - org.orekit.gnss.antenna.SatelliteAntennaCode
Deprecated.
GPS Block IIIA : SVN 74-81.
BLOCK_IIIA - org.orekit.gnss.antenna.SatelliteType
GPS Block IIIA : SVN 74-81.
BLOCK_IIR_A - org.orekit.gnss.antenna.SatelliteAntennaCode
Deprecated.
GPS Block IIR : SVN 41, 43-46, 51, 54, 56.
BLOCK_IIR_A - org.orekit.gnss.antenna.SatelliteType
GPS Block IIR : SVN 41, 43-46, 51, 54, 56.
BLOCK_IIR_B - org.orekit.gnss.antenna.SatelliteAntennaCode
Deprecated.
GPS Block IIR : SVN 47, 59-61.
BLOCK_IIR_B - org.orekit.gnss.antenna.SatelliteType
GPS Block IIR : SVN 47, 59-61.
BLOCK_IIR_M - org.orekit.gnss.antenna.SatelliteAntennaCode
Deprecated.
GPS Block IIR-M : SVN 48-50, 52-53, 55, 57-58.
BLOCK_IIR_M - org.orekit.gnss.antenna.SatelliteType
GPS Block IIR-M : SVN 48-50, 52-53, 55, 57-58.
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.
body - org.orekit.files.ccsds.Keyword
Body keyword.
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(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, 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(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.
BSTAR - org.orekit.files.ccsds.Keyword
SGP/SGP4 drag-like coefficient.
build() - Method in class org.orekit.estimation.sequential.KalmanEstimatorBuilder
Construct a KalmanEstimator from the data in this builder.
build() - Method in class org.orekit.propagation.analytical.gnss.GPSPropagator.Builder
Finalizes the build.
build(SpacecraftState[]) - Method in class org.orekit.estimation.measurements.generation.AngularAzElBuilder
Generate a single measurement.
build(SpacecraftState[]) - Method in class org.orekit.estimation.measurements.generation.AngularRaDecBuilder
Generate a single measurement.
build(SpacecraftState[]) - Method in class org.orekit.estimation.measurements.generation.InterSatellitesRangeBuilder
Generate a single measurement.
build(SpacecraftState[]) - Method in interface org.orekit.estimation.measurements.generation.MeasurementBuilder
Generate a single measurement.
build(SpacecraftState[]) - Method in class org.orekit.estimation.measurements.generation.PositionBuilder
Generate a single measurement.
build(SpacecraftState[]) - Method in class org.orekit.estimation.measurements.generation.PVBuilder
Generate a single measurement.
build(SpacecraftState[]) - Method in class org.orekit.estimation.measurements.generation.RangeBuilder
Generate a single measurement.
build(SpacecraftState[]) - Method in class org.orekit.estimation.measurements.generation.RangeRateBuilder
Generate a single measurement.
build(SpacecraftState[]) - Method in class org.orekit.estimation.measurements.generation.TurnAroundRangeBuilder
Generate a single measurement.
buildAttitudeProvider(AbsoluteDate, AbsoluteDate, ExtendedPVCoordinatesProvider, Frame, int) - Method in enum org.orekit.gnss.antenna.SatelliteType
Build an attitude provider suitable for this satellite type.
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).
BurstSelector - Class in org.orekit.time
Selector generating high rate bursts of dates separated by some rest period.
BurstSelector(int, double, double, TimeScale) - Constructor for class org.orekit.time.BurstSelector
Simple constructor.

C

C - Variable in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution
C = 1 + p² + q².
C01 - org.orekit.gnss.Frequency
In the ANTEX files, both C01 and C02 refer to Beidou B1 signal (1561.098 MHz).
C02 - org.orekit.gnss.Frequency
In the ANTEX files, both C01 and C02 refer to Beidou B1 signal (1561.098 MHz).
C06 - org.orekit.gnss.Frequency
In the ANTEX files, C06 appears without much reference, we assume it is B2 (1207.14 MHz).
C07 - org.orekit.gnss.Frequency
In the ANTEX files, C07 seems to refer to a signal close to E06, probably B3...
c1 - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator
C1 from SPTRCK #3.
C1 - org.orekit.gnss.ObservationType
Pseudorange GPS L1 / GLONASS G1 / Galileo E2-L1-E1 / SBAS L1 for Rinex2.
C1A - org.orekit.gnss.ObservationType
Pseudorange Galileo E1 A for Rinex3.
C1B - org.orekit.gnss.ObservationType
Pseudorange Galileo E1 I/NAV OS/CS/SoL for Rinex3.
C1C - org.orekit.gnss.ObservationType
Pseudorange GPS L1 C/A / GLONASS G1 C/A / Galileo E1 C / SBAS L1 C/A / QZSS L1 C/A for Rinex3.
C1I - org.orekit.gnss.ObservationType
Pseudorange Beidou B1 I for Rinex3.02.
C1L - org.orekit.gnss.ObservationType
Pseudorange GPS L1 L1C(P) / QZSS L1 L1C(P) for Rinex3.
C1M - org.orekit.gnss.ObservationType
Pseudorange GPS L1 M for Rinex3.
C1P - org.orekit.gnss.ObservationType
Pseudorange GPS L1 P(AS off) / GLONASS G1 P for Rinex3.
C1Q - org.orekit.gnss.ObservationType
Pseudorange Beidou B1 Q for Rinex3.02.
C1S - org.orekit.gnss.ObservationType
Pseudorange GPS L1 L1C(D) / QZSS L1 L1C(D) for Rinex3.
C1W - org.orekit.gnss.ObservationType
Pseudorange GPS L1 Z-tracking and similar (AS on) for Rinex3.
C1X - org.orekit.gnss.ObservationType
Pseudorange GPS L1 L1C (D+P) / Galileo E1 B+C / QZSS L1 L1C(D+P) for Rinex3.
C1Y - org.orekit.gnss.ObservationType
Pseudorange GPS L1 Y for Rinex3.
C1Z - org.orekit.gnss.ObservationType
Pseudorange Galileo E1 C1Z A+B+C / QZSS L1 L1-SAIF for Rinex3.
c2 - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator
C2 from SPTRCK #3.
C2 - org.orekit.gnss.ObservationType
Pseudorange GPS L2 / GLONASS G2 / Beidou B02 for Rinex2.
C2C - org.orekit.gnss.ObservationType
Pseudorange GPS L2 C/A / GLONASS G2 C/A for Rinex3.
C2D - org.orekit.gnss.ObservationType
Pseudorange GPS L1(C/A)+(P2-P1) (semi-codeless) for Rinex3.
C2I - org.orekit.gnss.ObservationType
Pseudorange Beidou B1 I for Rinex3.03.
C2L - org.orekit.gnss.ObservationType
Pseudorange GPS L2 L2C(L) / QZSS L2 L2C(2) for Rinex3.
C2M - org.orekit.gnss.ObservationType
Pseudorange GPS L2 M for Rinex3.
C2P - org.orekit.gnss.ObservationType
Pseudorange GPS L2 P(AS off) / GLONASS G2 P for Rinex3.
C2Q - org.orekit.gnss.ObservationType
Pseudorange Beidou B1 Q for Rinex3.03.
C2S - org.orekit.gnss.ObservationType
Pseudorange GPS L2 L2C(M) / QZSS L2 L2C(M) for Rinex3.
C2W - org.orekit.gnss.ObservationType
Pseudorange GPS L2 Z-tracking and similar (AS on) for Rinex3.
C2X - org.orekit.gnss.ObservationType
Pseudorange GPS L2 L2C (M+L) / QZSS L2 L2C(M+L) for Rinex3.
C2Y - org.orekit.gnss.ObservationType
Pseudorange GPS L2 Y for Rinex3.
C3I - org.orekit.gnss.ObservationType
Pseudorange GLONASS G3 I for Rinex3.
C3Q - org.orekit.gnss.ObservationType
Pseudorange GLONASS G3 Q for Rinex3.
C3X - org.orekit.gnss.ObservationType
Pseudorange GLONASS G3 I+Q for Rinex3.
c4 - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator
C4 from SPTRCK #3.
C5 - org.orekit.gnss.ObservationType
Pseudorange GPS L5 / Galileo E5a / SBAS L5 for Rinex2.
C5A - org.orekit.gnss.ObservationType
Pseudorange IRNSS L5 A for Rinex3.
C5B - org.orekit.gnss.ObservationType
Pseudorange IRNSS L5 B for Rinex3.
C5C - org.orekit.gnss.ObservationType
Pseudorange IRNSS L5 C for Rinex3.
C5I - org.orekit.gnss.ObservationType
Pseudorange GPS L5 I/ Galileo E5a F/NAV OS / SBAS L5 I / QZSS L5 I for Rinex3.
C5Q - org.orekit.gnss.ObservationType
Pseudorange GPS L5 Q/ Galileo E5a Q / SBAS L5 Q / QZSS L5 Q for Rinex3.
C5X - org.orekit.gnss.ObservationType
Pseudorange GPS L5 I+Q/ Galileo E5a I+Q / SBAS L5 I+Q / QZSS L5 I+Q / IRNSS L5 B+C for Rinex3.
C6 - org.orekit.gnss.ObservationType
Pseudorange Galileo E6 / Beidou B03 for Rinex2.
C6A - org.orekit.gnss.ObservationType
Pseudorange Galileo E6 A PRS for Rinex3.
C6B - org.orekit.gnss.ObservationType
Pseudorange Galileo E6 B C/NAV CS for Rinex3.
C6C - org.orekit.gnss.ObservationType
Pseudorange Galileo E6 C no data for Rinex3.
C6I - org.orekit.gnss.ObservationType
Pseudorange Beidou B3 I for Rinex3.
C6L - org.orekit.gnss.ObservationType
Pseudorange QZSS LEX(6) L for Rinex3.
C6Q - org.orekit.gnss.ObservationType
Pseudorange Beidou B3 Q for Rinex3.
C6S - org.orekit.gnss.ObservationType
Pseudorange QZSS LEX(6) S for Rinex3.
C6X - org.orekit.gnss.ObservationType
Pseudorange Galileo E6 B+C / QZSS LEX(6) S+L / Beidou B3 I+Q for Rinex3.
C6Z - org.orekit.gnss.ObservationType
Pseudorange Galileo E6 A+B+C for Rinex3.
C7 - org.orekit.gnss.ObservationType
Pseudorange Galileo E5b / Beidou B02 for Rinex2.
C7I - org.orekit.gnss.ObservationType
Pseudorange Galileo E5b I I/NAV OS/CS/SoL / Beidou B2 I for Rinex3.
C7Q - org.orekit.gnss.ObservationType
Pseudorange Galileo Q no data / Beidou B2 Q for Rinex3.
C7X - org.orekit.gnss.ObservationType
Pseudorange Galileo E5b I+Q / Beidou B2 I+Q for Rinex3.
C8 - org.orekit.gnss.ObservationType
Pseudorange Galileo E5a+b for Rinex2.
C8I - org.orekit.gnss.ObservationType
Pseudorange Galileo E5(E5a+E5b) I for Rinex3.
C8Q - org.orekit.gnss.ObservationType
Pseudorange Galileo E5(E5a+E5b) Q for Rinex3.
C8X - org.orekit.gnss.ObservationType
Pseudorange Galileo E5(E5a+E5b) I+Q for Rinex3.
C9A - org.orekit.gnss.ObservationType
Pseudorange IRNSS S A for Rinex3.
C9B - org.orekit.gnss.ObservationType
Pseudorange IRNSS S B for Rinex3.
C9C - org.orekit.gnss.ObservationType
Pseudorange IRNSS S C for Rinex3.
C9X - org.orekit.gnss.ObservationType
Pseudorange IRNSS S B+C for Rinex3.
CA - org.orekit.gnss.ObservationType
Pseudorange GPS L1 C/A / GLONASS G1 C/A for Rinex2.
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.
CANNOT_FIND_SATELLITE_IN_SYSTEM - org.orekit.errors.OrekitMessages
 
CANNOT_PARSE_BOTH_TAU_AND_GAMMA - org.orekit.errors.OrekitMessages
 
CARRIER_PHASE - org.orekit.gnss.MeasurementType
Carrier-phase measurement.
CARRIER_POWER - org.orekit.files.ccsds.Keyword
Data: Carrier power [dBW].
CARTESIAN - org.orekit.orbits.OrbitType
Type for propagation in Cartesian parameters.
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(Orbit) - Constructor for class org.orekit.orbits.CartesianOrbit
Constructor from any kind of orbital parameters.
CartesianOrbit(PVCoordinates, Frame, AbsoluteDate, double) - Constructor for class org.orekit.orbits.CartesianOrbit
Constructor from Cartesian parameters.
CartesianOrbit(TimeStampedPVCoordinates, Frame, double) - Constructor for class org.orekit.orbits.CartesianOrbit
Constructor from Cartesian parameters.
CB - org.orekit.gnss.ObservationType
Pseudorange GPS L1C for Rinex2.
CC - org.orekit.gnss.ObservationType
Pseudorange GPS L2C for Rinex2.
CCSDS_DATE_INVALID_LENGTH_TIME_FIELD - org.orekit.errors.OrekitMessages
 
CCSDS_DATE_INVALID_PREAMBLE_FIELD - org.orekit.errors.OrekitMessages
 
CCSDS_DATE_MISSING_AGENCY_EPOCH - org.orekit.errors.OrekitMessages
 
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_INVALID_FRAME - org.orekit.errors.OrekitMessages
 
CCSDS_NO_CORRESPONDING_TIME_SCALE - org.orekit.errors.OrekitMessages
 
CCSDS_OEM_INCONSISTENT_TIME_SYSTEMS - org.orekit.errors.OrekitMessages
 
CCSDS_OEM_VERS - org.orekit.files.ccsds.Keyword
File creation date in UTC.
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.
CCSDS_OMM_VERS - org.orekit.files.ccsds.Keyword
CCSDS OMM format version.
CCSDS_OPM_VERS - org.orekit.files.ccsds.Keyword
CCSDS OPM format version.
CCSDS_TDM_INCONSISTENT_DATA_LINE - org.orekit.errors.OrekitMessages
 
CCSDS_TDM_INCONSISTENT_TIME_SYSTEMS - org.orekit.errors.OrekitMessages
 
CCSDS_TDM_KEYWORD_NOT_FOUND - org.orekit.errors.OrekitMessages
 
CCSDS_TDM_UNKNOWN_FORMAT - org.orekit.errors.OrekitMessages
 
CCSDS_TDM_VERS - org.orekit.files.ccsds.Keyword
Header: TDM format version in the form of ‘x.y’, where ‘y’ shall be incremented for corrections and minor changes, and ‘x’ shall be incremented for major changes.
CCSDS_TDM_XML_INCONSISTENT_DATA_BLOCK - org.orekit.errors.OrekitMessages
 
CCSDS_TIME_SYSTEM_NOT_IMPLEMENTED - org.orekit.errors.OrekitMessages
 
CCSDS_TIME_SYSTEM_NOT_READ_YET - org.orekit.errors.OrekitMessages
 
CCSDS_UNEXPECTED_KEYWORD - org.orekit.errors.OrekitMessages
 
CCSDS_UNKNOWN_CONVENTIONS - org.orekit.errors.OrekitMessages
 
CCSDS_UNKNOWN_GM - org.orekit.errors.OrekitMessages
 
CCSDS_UNKNOWN_SPACECRAFT_MASS - org.orekit.errors.OrekitMessages
 
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.
CD - org.orekit.gnss.ObservationType
Pseudorange GLONASS G2 for Rinex2.
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.
CENTER_NAME - org.orekit.files.ccsds.Keyword
Origin of reference frame.
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.
CIRCULAR - org.orekit.orbits.OrbitType
Type for propagation in circular parameters.
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, double, double, double, double, double, double, PositionAngle, Frame, AbsoluteDate, double) - Constructor for class org.orekit.orbits.CircularOrbit
Creates a new instance.
CircularOrbit(double, double, double, double, double, double, PositionAngle, Frame, AbsoluteDate, double) - Constructor for class org.orekit.orbits.CircularOrbit
Creates a new instance.
CircularOrbit(Orbit) - Constructor for class org.orekit.orbits.CircularOrbit
Constructor from any kind of orbital parameters.
CircularOrbit(PVCoordinates, Frame, AbsoluteDate, double) - Constructor for class org.orekit.orbits.CircularOrbit
Constructor from Cartesian parameters.
CircularOrbit(TimeStampedPVCoordinates, Frame, double) - Constructor for class org.orekit.orbits.CircularOrbit
Constructor from Cartesian parameters.
circularToPosition(T, T, T, T, T, T, double) - Static method in class org.orekit.orbits.FieldCircularOrbit
CIRF_CONVENTIONS_1996_ACCURATE_EOP - org.orekit.frames.Predefined
CIRF frame, IERS 1996 conventions, with accurate EOP interpolation.
CIRF_CONVENTIONS_1996_SIMPLE_EOP - org.orekit.frames.Predefined
CIRF frame, IERS 1996 conventions, with simple EOP interpolation.
CIRF_CONVENTIONS_2003_ACCURATE_EOP - org.orekit.frames.Predefined
CIRF frame, IERS 2003 conventions, with accurate EOP interpolation.
CIRF_CONVENTIONS_2003_SIMPLE_EOP - org.orekit.frames.Predefined
CIRF frame, IERS 2003 conventions, with simple EOP interpolation.
CIRF_CONVENTIONS_2010_ACCURATE_EOP - org.orekit.frames.Predefined
CIRF frame, IERS 2010 conventions, with accurate EOP interpolation.
CIRF_CONVENTIONS_2010_SIMPLE_EOP - org.orekit.frames.Predefined
CIRF frame, IERS 2010 conventions, with simple EOP interpolation.
CIVIL_DAWN_DUSK_ELEVATION - Static variable in class org.orekit.propagation.events.GroundAtNightDetector
Sun elevation at civil dawn/dusk (6° below horizon).
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.
CLASSIFICATION_TYPE - org.orekit.files.ccsds.Keyword
Classification type.
ClasspathCrawler - Class in org.orekit.data
Provider for data files stored as resources in the classpath.
ClasspathCrawler(ClassLoader, String...) - Constructor for class org.orekit.data.ClasspathCrawler
Build a data classpath crawler.
ClasspathCrawler(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() - Static method in class org.orekit.bodies.CelestialBodyFactory
Clear all loaded celestial bodies.
clearCelestialBodyCache(String) - Static method in class org.orekit.bodies.CelestialBodyFactory
Clear the specified celestial body from the internal cache.
clearCelestialBodyLoaders() - Static method in class org.orekit.bodies.CelestialBodyFactory
Clear loaders for all celestial bodies.
clearCelestialBodyLoaders(String) - Static method in class org.orekit.bodies.CelestialBodyFactory
Clear loaders for one celestial body.
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.
clearFilters() - Method in class org.orekit.data.DataProvidersManager
Remove all data filters, except the predefined ones.
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.
CLOCK_BIAS - org.orekit.files.ccsds.Keyword
Data: Clock bias [s].
CLOCK_CORRECTIONS - Static variable in class org.orekit.propagation.analytical.gnss.ClockCorrectionsProvider
Name of the additional state for satellite clock corrections.
CLOCK_DRIFT - org.orekit.files.ccsds.Keyword
Data: Clock drift [s/s].
CLOCK_OFFSET_PREFIX - Static variable in class org.orekit.estimation.measurements.ObservableSatellite
Prefix for clock offset parameter driver, the propagator index will be appended to it.
ClockCorrectionsProvider - Class in org.orekit.propagation.analytical.gnss
Provider for clock corrections as additional states.
ClockCorrectionsProvider(GPSOrbitalElements) - Constructor for class org.orekit.propagation.analytical.gnss.ClockCorrectionsProvider
Simple constructor.
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.
COMMENT - org.orekit.files.ccsds.Keyword
Comments specific to a ODM file.
ComparableMeasurement - Interface in org.orekit.estimation.measurements
Base interface for comparing measurements regardless of their type.
compare(TimeStamped, TimeStamped) - Method in class org.orekit.time.ChronologicalComparator
Compare two time-stamped instances.
compareTo(ComparableMeasurement) - Method in interface org.orekit.estimation.measurements.ComparableMeasurement
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
COMPASS - org.orekit.files.sp3.SP3File.SP3FileType
COMPASS only file.
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(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) - Method in interface org.orekit.propagation.integration.AbstractIntegratedPropagator.MainStateEquations
Compute differential equations for main state.
computeDerivatives(SpacecraftState, double[]) - Method in interface org.orekit.propagation.integration.AdditionalEquations
Compute the derivatives related to the additional state parameters.
computeDerivatives(SpacecraftState, double[]) - Method in class org.orekit.propagation.numerical.PartialDerivativesEquations
Compute the derivatives related to the additional state parameters.
computeGsHs(double, double, double, double, int) - Static method in class org.orekit.propagation.semianalytical.dsst.utilities.CoefficientsFactory
Compute recursively Gs and Hs polynomials from equation 3.1-(5).
computeInitValues(double) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenZonalLinear
Compute the roots for the Hansen coefficients and their derivatives.
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)
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).
computeZenithDelay(double, double[], AbsoluteDate) - Method in interface org.orekit.models.earth.DiscreteTroposphericModel
This method allows the computation of the zenith hydrostatic and zenith wet delay.
computeZenithDelay(double, double[], AbsoluteDate) - Method in class org.orekit.models.earth.EstimatedTroposphericModel
This method allows the computation of the zenith hydrostatic and zenith total delays.
computeZenithDelay(double, double[], AbsoluteDate) - Method in class org.orekit.models.earth.MendesPavlisModel
This method allows the computation of the zenith hydrostatic and zenith wet delay.
computeZenithDelay(double, double[], AbsoluteDate) - Method in interface org.orekit.models.earth.TroposphericModel
This method allows the computation of the zenith hydrostatic and zenith wet delay.
computeZenithDelay(double, double[], AbsoluteDate) - Method in class org.orekit.models.earth.ViennaOneModel
This method allows the computation of the zenith hydrostatic and zenith wet delay.
computeZenithDelay(double, double[], AbsoluteDate) - Method in class org.orekit.models.earth.ViennaThreeModel
This method allows the computation of the zenith hydrostatic and zenith wet delay.
computeZenithDelay(T, T[], FieldAbsoluteDate<T>) - Method in interface org.orekit.models.earth.DiscreteTroposphericModel
This method allows the computation of the zenith hydrostatic and zenith wet delay.
computeZenithDelay(T, T[], FieldAbsoluteDate<T>) - Method in class org.orekit.models.earth.EstimatedTroposphericModel
This method allows the computation of the zenith hydrostatic and zenith total delays.
computeZenithDelay(T, T[], FieldAbsoluteDate<T>) - Method in class org.orekit.models.earth.MendesPavlisModel
This method allows the computation of the zenith hydrostatic and zenith wet delay.
computeZenithDelay(T, T[], FieldAbsoluteDate<T>) - Method in interface org.orekit.models.earth.TroposphericModel
This method allows the computation of the zenith hydrostatic and zenith wet delay.
computeZenithDelay(T, T[], FieldAbsoluteDate<T>) - Method in class org.orekit.models.earth.ViennaOneModel
This method allows the computation of the zenith hydrostatic and zenith wet delay.
computeZenithDelay(T, T[], FieldAbsoluteDate<T>) - Method in class org.orekit.models.earth.ViennaThreeModel
This method allows the computation of the zenith hydrostatic and zenith wet delay.
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.
ConstantProcessNoise - Class in org.orekit.estimation.sequential
Provider for constant process noise matrices.
ConstantProcessNoise(RealMatrix) - Constructor for class org.orekit.estimation.sequential.ConstantProcessNoise
Simple constructor.
ConstantProcessNoise(RealMatrix, RealMatrix) - Constructor for class org.orekit.estimation.sequential.ConstantProcessNoise
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.
ConstantThrustManeuver(AbsoluteDate, double, double, double, AttitudeProvider, Vector3D) - Constructor for class org.orekit.forces.maneuvers.ConstantThrustManeuver
Simple constructor for a constant direction and constant thrust.
ConstantThrustManeuver(AbsoluteDate, double, double, double, AttitudeProvider, 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.
CONTINUE - org.orekit.propagation.events.handlers.EventHandler.Action
Continue indicator.
CONTINUE - org.orekit.propagation.events.handlers.FieldEventHandler.Action
Continue indicator.
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
 
ContinuousScheduler<T extends ObservedMeasurement<T>> - Class in org.orekit.estimation.measurements.generation
Scheduler generating measurements sequences continuously.
ContinuousScheduler(MeasurementBuilder<T>, DatesSelector) - Constructor for class org.orekit.estimation.measurements.generation.ContinuousScheduler
Simple constructor.
convert() - Method in class org.orekit.propagation.conversion.OsculatingToMeanElementsConverter
Convert an osculating orbit into a mean orbit, in DSST sense.
convert(double[]) - Method in interface org.orekit.data.SimpleTimeStampedTableParser.RowConverter
Convert a row.
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(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.
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, 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(Propagator, double, int, String...) - Method in class org.orekit.propagation.conversion.AbstractPropagatorConverter
Convert a propagator to another.
convert(Propagator, double, int, String...) - Method in interface org.orekit.propagation.conversion.PropagatorConverter
Convert a propagator into another one.
convert(Propagator, double, int, List<String>) - Method in class org.orekit.propagation.conversion.AbstractPropagatorConverter
Convert a propagator to another.
convert(Propagator, double, int, List<String>) - Method in interface org.orekit.propagation.conversion.PropagatorConverter
Convert a propagator into another one.
convertType(FieldOrbit<T>) - Method in enum org.orekit.orbits.OrbitType
Convert an orbit to the instance type.
convertType(Orbit) - Method in enum org.orekit.orbits.OrbitType
Convert an orbit to the instance type.
copy() - Method in class org.orekit.propagation.conversion.NumericalPropagatorBuilder
Create a copy of a NumericalPropagatorBuilder object.
correctedYaw(GNSSAttitudeContext) - Method in class org.orekit.gnss.attitude.AbstractGNSSAttitudeProvider
Select the /** Compute GNSS attitude with midnight/noon yaw turn correction.
correctedYaw(GNSSAttitudeContext) - Method in class org.orekit.gnss.attitude.BeidouGeo
Select the /** Compute GNSS attitude with midnight/noon yaw turn correction.
correctedYaw(GNSSAttitudeContext) - Method in class org.orekit.gnss.attitude.BeidouMeo
Select the /** Compute GNSS attitude with midnight/noon yaw turn correction.
correctedYaw(GNSSAttitudeContext) - Method in class org.orekit.gnss.attitude.Galileo
Select the /** Compute GNSS attitude with midnight/noon yaw turn correction.
correctedYaw(GNSSAttitudeContext) - Method in class org.orekit.gnss.attitude.GenericGNSS
Select the /** Compute GNSS attitude with midnight/noon yaw turn correction.
correctedYaw(GNSSAttitudeContext) - Method in class org.orekit.gnss.attitude.Glonass
Select the /** Compute GNSS attitude with midnight/noon yaw turn correction.
correctedYaw(GNSSAttitudeContext) - Method in class org.orekit.gnss.attitude.GPSBlockIIA
Select the /** Compute GNSS attitude with midnight/noon yaw turn correction.
correctedYaw(GNSSAttitudeContext) - Method in class org.orekit.gnss.attitude.GPSBlockIIF
Select the /** Compute GNSS attitude with midnight/noon yaw turn correction.
correctedYaw(GNSSAttitudeContext) - Method in class org.orekit.gnss.attitude.GPSBlockIIR
Select the /** Compute GNSS attitude with midnight/noon yaw turn correction.
correctedYaw(GNSSFieldAttitudeContext<T>) - Method in class org.orekit.gnss.attitude.AbstractGNSSAttitudeProvider
Compute GNSS attitude with midnight/noon yaw turn correction.
correctedYaw(GNSSFieldAttitudeContext<T>) - Method in class org.orekit.gnss.attitude.BeidouGeo
Compute GNSS attitude with midnight/noon yaw turn correction.
correctedYaw(GNSSFieldAttitudeContext<T>) - Method in class org.orekit.gnss.attitude.BeidouMeo
Compute GNSS attitude with midnight/noon yaw turn correction.
correctedYaw(GNSSFieldAttitudeContext<T>) - Method in class org.orekit.gnss.attitude.Galileo
Compute GNSS attitude with midnight/noon yaw turn correction.
correctedYaw(GNSSFieldAttitudeContext<T>) - Method in class org.orekit.gnss.attitude.GenericGNSS
Compute GNSS attitude with midnight/noon yaw turn correction.
correctedYaw(GNSSFieldAttitudeContext<T>) - Method in class org.orekit.gnss.attitude.Glonass
Compute GNSS attitude with midnight/noon yaw turn correction.
correctedYaw(GNSSFieldAttitudeContext<T>) - Method in class org.orekit.gnss.attitude.GPSBlockIIA
Compute GNSS attitude with midnight/noon yaw turn correction.
correctedYaw(GNSSFieldAttitudeContext<T>) - Method in class org.orekit.gnss.attitude.GPSBlockIIF
Compute GNSS attitude with midnight/noon yaw turn correction.
correctedYaw(GNSSFieldAttitudeContext<T>) - Method in class org.orekit.gnss.attitude.GPSBlockIIR
Compute GNSS attitude with midnight/noon yaw turn correction.
CORRECTION_ANGLE_1 - org.orekit.files.ccsds.Keyword
Meta-data: Correction angle 1.
CORRECTION_ANGLE_2 - org.orekit.files.ccsds.Keyword
Meta-data: Correction angle 2.
CORRECTION_DOPPLER - org.orekit.files.ccsds.Keyword
Meta-data: Correction Doppler.
CORRECTION_RANGE - org.orekit.files.ccsds.Keyword
Meta-data: Correction Range.
CORRECTION_RECEIVE - org.orekit.files.ccsds.Keyword
Meta-data: Correction receive.
CORRECTION_TRANSMIT - org.orekit.files.ccsds.Keyword
Meta-data: Correction transmit.
CORRECTIONS_APPLIED - org.orekit.files.ccsds.Keyword
Meta-data: Correction applied ? YES/NO
CORRUPTED_FILE - org.orekit.errors.OrekitMessages
 
cosi0 - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator
cosinus original inclination.
COV_REF_FRAME - org.orekit.files.ccsds.Keyword
Coordinate system for covariance matrix.
COVARIANCE_START - org.orekit.files.ccsds.Keyword
This keyword must appear before the first line of the covariance matrix data.
COVARIANCE_STOP - org.orekit.files.ccsds.Keyword
This keyword must appear after the last line of the covariance matrix data.
CovarianceMatrixProvider - Interface in org.orekit.estimation.sequential
Provider for process noise matrices.
create(double, double, int, EventHandler<? super ImpulseManeuver<T>>) - Method in class org.orekit.forces.maneuvers.ImpulseManeuver
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(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 FunctionalDetector>) - Method in class org.orekit.propagation.events.FunctionalDetector
 
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 GroundAtNightDetector>) - Method in class org.orekit.propagation.events.GroundAtNightDetector
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 InterSatDirectViewDetector>) - Method in class org.orekit.propagation.events.InterSatDirectViewDetector
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.
create(double, double, int, EventHandler<? super T>) - Method in class org.orekit.propagation.events.AbstractDetector
Build a new instance.
create(OneAxisEllipsoid, GeodeticPoint) - Static method in class org.orekit.gnss.DOPComputer
Creates a DOP computer for one location.
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.
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
Deprecated.
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(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.
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.
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.
CREATION_DATE - org.orekit.files.ccsds.Keyword
CCSDS OEM format version.
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.
CX_DOT_X - org.orekit.files.ccsds.Keyword
Covariance matrix [4, 1] element.
CX_DOT_X_DOT - org.orekit.files.ccsds.Keyword
Covariance matrix [4, 4] element.
CX_DOT_Y - org.orekit.files.ccsds.Keyword
Covariance matrix [4, 2] element.
CX_DOT_Z - org.orekit.files.ccsds.Keyword
Covariance matrix [4, 3] element.
CX_X - org.orekit.files.ccsds.Keyword
Covariance matrix [1, 1] element.
CY_DOT_X - org.orekit.files.ccsds.Keyword
Covariance matrix [5, 1] element.
CY_DOT_X_DOT - org.orekit.files.ccsds.Keyword
Covariance matrix [5, 4] element.
CY_DOT_Y - org.orekit.files.ccsds.Keyword
Covariance matrix [5, 2] element.
CY_DOT_Y_DOT - org.orekit.files.ccsds.Keyword
Covariance matrix [5, 5] element.
CY_DOT_Z - org.orekit.files.ccsds.Keyword
Covariance matrix [5, 3] element.
CY_X - org.orekit.files.ccsds.Keyword
Covariance matrix [2, 1] element.
CY_Y - org.orekit.files.ccsds.Keyword
Covariance matrix [2, 2] element.
CZ_DOT_X - org.orekit.files.ccsds.Keyword
Covariance matrix [6, 1] element.
CZ_DOT_X_DOT - org.orekit.files.ccsds.Keyword
Covariance matrix [6, 4] element.
CZ_DOT_Y - org.orekit.files.ccsds.Keyword
Covariance matrix [6, 2] element.
CZ_DOT_Y_DOT - org.orekit.files.ccsds.Keyword
Covariance matrix [6, 5] element.
CZ_DOT_Z - org.orekit.files.ccsds.Keyword
Covariance matrix [6, 3] element.
CZ_DOT_Z_DOT - org.orekit.files.ccsds.Keyword
Covariance matrix [6, 6] element.
CZ_X - org.orekit.files.ccsds.Keyword
Covariance matrix [3, 1] element.
CZ_Y - org.orekit.files.ccsds.Keyword
Covariance matrix [3, 2] element.
CZ_Z - org.orekit.files.ccsds.Keyword
Covariance matrix [3, 3] element.

D

D1 - org.orekit.gnss.ObservationType
Doppler GPS L1 / GLONASS G1 / Galileo E2-L1-E1 / SBAS L1 for Rinex2.
D1A - org.orekit.gnss.ObservationType
Doppler Galileo E1 A for Rinex3.
D1B - org.orekit.gnss.ObservationType
Doppler Galileo E1 I/NAV OS/CS/SoL for Rinex3.
D1C - org.orekit.gnss.ObservationType
Doppler GPS L1 C/A / GLONASS G1 C/A / Galileo E1 C / SBAS L1 C/A / QZSS L1 C/A for Rinex3.
D1I - org.orekit.gnss.ObservationType
Doppler Beidou B1 I for Rinex3.
D1L - org.orekit.gnss.ObservationType
Doppler GPS L1 L1C(P) / QZSS L1 L1C(P) for Rinex3.
D1M - org.orekit.gnss.ObservationType
Doppler GPS L2 M for Rinex3.
D1N - org.orekit.gnss.ObservationType
Doppler GPS L1 codeless for Rinex3.
D1P - org.orekit.gnss.ObservationType
Doppler GPS L2 P(AS off) / GLONASS G2 P for Rinex3.
D1S - org.orekit.gnss.ObservationType
Doppler GPS L1 L1C(D) / QZSS L1 L1C(D) for Rinex3.
D1W - org.orekit.gnss.ObservationType
Doppler GPS L1 Z-tracking and similar (AS on) for Rinex3.
D1X - org.orekit.gnss.ObservationType
Doppler GPS L1 L1C (D+P) / Galileo E1 B+C / QZSS L1 L1C(D+P) for Rinex3.
D1Y - org.orekit.gnss.ObservationType
Doppler GPS L1 Y for Rinex3.
D1Z - org.orekit.gnss.ObservationType
Doppler Galileo E1 C1Z A+B+C / QZSS L1 L1-SAIF for Rinex3.
D2 - org.orekit.gnss.ObservationType
Doppler GPS L2 / GLONASS G2 / Beidou BO2 for Rinex2.
D2C - org.orekit.gnss.ObservationType
Doppler GPS L2 C/A / GLONASS G2 C/A for Rinex3.
D2D - org.orekit.gnss.ObservationType
Doppler GPS L1(C/A)+(P2-P1) (semi-codeless) for Rinex3.
D2I - org.orekit.gnss.ObservationType
Doppler Beidou B1 I for Rinex3.03.
D2L - org.orekit.gnss.ObservationType
Doppler GPS L2 L2C(L) / QZSS L2 L2C(2) for Rinex3.
D2M - org.orekit.gnss.ObservationType
Doppler GPS L2 M for Rinex3.
D2N - org.orekit.gnss.ObservationType
Doppler GPS L2 codeless for Rinex3.
D2P - org.orekit.gnss.ObservationType
Doppler GPS L2 P(AS off) / GLONASS G2 P for Rinex3.
D2Q - org.orekit.gnss.ObservationType
Doppler Beidou B1 Q for Rinex3.03.
D2S - org.orekit.gnss.ObservationType
Doppler GPS L2 L2C(M) / QZSS L2 L2C(M) for Rinex3.
D2W - org.orekit.gnss.ObservationType
Doppler GPS L2 Z-tracking and similar (AS on) for Rinex3.
D2X - org.orekit.gnss.ObservationType
Doppler GPS L2 L2C (M+L) / QZSS L2 L2C(M+L) for Rinex3.
D2Y - org.orekit.gnss.ObservationType
Doppler GPS L2 Y for Rinex3.
D3I - org.orekit.gnss.ObservationType
Doppler GLONASS G3 I for Rinex3.
D3Q - org.orekit.gnss.ObservationType
Doppler GLONASS G3 Q for Rinex3.
D3X - org.orekit.gnss.ObservationType
Doppler GLONASS G3 I+Q for Rinex3.
D5 - org.orekit.gnss.ObservationType
Doppler GPS L5 / Galileo E5a / SBAS L5 for Rinex2.
D5A - org.orekit.gnss.ObservationType
Doppler IRNSS L5 A for Rinex3.
D5B - org.orekit.gnss.ObservationType
Doppler IRNSS L5 B for Rinex3.
D5C - org.orekit.gnss.ObservationType
Doppler IRNSS L5 C for Rinex3.
D5I - org.orekit.gnss.ObservationType
Doppler GPS L5 I/ Galileo E5a F/NAV OS / SBAS L5 I / QZSS L5 I for Rinex3.
D5Q - org.orekit.gnss.ObservationType
Doppler GPS L5 Q/ Galileo E5a Q / SBAS L5 Q / QZSS L5 Q for Rinex3.
D5X - org.orekit.gnss.ObservationType
Doppler GPS L5 I+Q/ Galileo E5a I+Q / SBAS L5 I+Q / QZSS L5 I+Q / IRNSS L5 B+C for Rinex3.
D6 - org.orekit.gnss.ObservationType
Doppler Galileo E6 / Beidou B03 for Rinex2.
D6A - org.orekit.gnss.ObservationType
Doppler Galileo E6 A PRS for Rinex3.
D6B - org.orekit.gnss.ObservationType
Doppler Galileo E6 B C/NAV CS for Rinex3.
D6C - org.orekit.gnss.ObservationType
Doppler Galileo E6 C no data for Rinex3.
D6I - org.orekit.gnss.ObservationType
Doppler Beidou B3 I for Rinex3.
D6L - org.orekit.gnss.ObservationType
Doppler QZSS LEX(6) L for Rinex3.
D6Q - org.orekit.gnss.ObservationType
Doppler Beidou B3 Q for Rinex3.
D6S - org.orekit.gnss.ObservationType
Doppler QZSS LEX(6) S for Rinex3.
D6X - org.orekit.gnss.ObservationType
Doppler Galileo E6 B+C / QZSS LEX(6) S+L / Beidou B3 I+Q for Rinex3.
D6Z - org.orekit.gnss.ObservationType
Doppler Galileo E6 A+B+C for Rinex3.
D7 - org.orekit.gnss.ObservationType
Doppler Galileo E5b / Beidou B02 for Rinex2.
D7I - org.orekit.gnss.ObservationType
Doppler Galileo E5b I I/NAV OS/CS/SoL / Beidou B2 I for Rinex3.
D7Q - org.orekit.gnss.ObservationType
Doppler Galileo Q no data / Beidou B2 Q for Rinex3.
D7X - org.orekit.gnss.ObservationType
Doppler Galileo E5b I+Q / Beidou B2 I+Q for Rinex3.
D8 - org.orekit.gnss.ObservationType
Doppler Galileo E5a+b for Rinex2.
D8I - org.orekit.gnss.ObservationType
Doppler Galileo E5(E5a+E5b) I for Rinex3.
D8Q - org.orekit.gnss.ObservationType
Doppler Galileo E5(E5a+E5b) Q for Rinex3.
D8X - org.orekit.gnss.ObservationType
Doppler Galileo E5(E5a+E5b) I+Q for Rinex3.
D9A - org.orekit.gnss.ObservationType
Doppler IRNSS S A for Rinex3.
D9B - org.orekit.gnss.ObservationType
Doppler IRNSS S B for Rinex3.
D9C - org.orekit.gnss.ObservationType
Doppler IRNSS S C for Rinex3.
D9X - org.orekit.gnss.ObservationType
Doppler IRNSS S B+C for Rinex3.
DA - org.orekit.gnss.ObservationType
Doppler GPS L1 C/A / GLONASS G1 C/A for Rinex2.
data - org.orekit.files.ccsds.Keyword
Data keyword.
DATA_QUALITY - org.orekit.files.ccsds.Keyword
Meta-data: Data quality.
DATA_ROOT_DIRECTORY_DOES_NOT_EXIST - org.orekit.errors.OrekitMessages
 
DATA_START - org.orekit.files.ccsds.Keyword
Keyword used to delineate the start of a Data block in Keyvalue files.
DATA_STOP - org.orekit.files.ccsds.Keyword
Keyword used to delineate the end of a Data block in Keyvalue files..
DataFilter - Interface in org.orekit.data
Interface for filtering data (typically uncompressing it) in data providers before passing it to data loaders.
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) - Constructor for class org.orekit.time.DateComponents
Build a date from its offset with respect to a DateComponents.J2000_EPOCH.
DateComponents(int, int) - Constructor for class org.orekit.time.DateComponents
Build a date from a year and day number.
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(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.
DatesSelector - Interface in org.orekit.time
Interface for selecting dates within an interval.
DateTimeComponents - Class in org.orekit.time
Holder for date and time components.
DateTimeComponents(int, int, int) - Constructor for class org.orekit.time.DateTimeComponents
Build an instance from raw level 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) - 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(DateComponents, TimeComponents) - Constructor for class org.orekit.time.DateTimeComponents
Build a new instance from its components.
DateTimeComponents(DateTimeComponents, double) - Constructor for class org.orekit.time.DateTimeComponents
Build an instance from a seconds offset with respect to another one.
DB - org.orekit.gnss.ObservationType
Doppler GPS L1C for Rinex2.
DC - org.orekit.gnss.ObservationType
Doppler GPS L2C for Rinex2.
DD - org.orekit.gnss.ObservationType
Doppler GLONASS G2 for Rinex2.
DECEMBER - org.orekit.time.Month
December.
decomposer(MatrixDecomposer) - Method in class org.orekit.estimation.sequential.KalmanEstimatorBuilder
Configure the matrix decomposer.
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_ANTEX_SUPPORTED_NAMES - Static variable in class org.orekit.gnss.antenna.AntexLoader
Default supported files name pattern for antex files.
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_RINEX_2_SUPPORTED_NAMES - Static variable in class org.orekit.gnss.RinexLoader
Default supported files name pattern for rinex 2 observation files.
DEFAULT_RINEX_3_SUPPORTED_NAMES - Static variable in class org.orekit.gnss.RinexLoader
Default supported files name pattern for rinex 3 observation files.
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.GlobalPressureTemperature2Model
Default supported files name pattern.
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.models.earth.ViennaModelCoefficientsLoader
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).
DEFAULT_YAW_BIAS - Static variable in class org.orekit.gnss.attitude.GPSBlockIIA
Default yaw bias (rad).
DEFAULT_YAW_BIAS - Static variable in class org.orekit.gnss.attitude.GPSBlockIIF
Default yaw bias (rad).
DEFAULT_YAW_RATE - Static variable in class org.orekit.gnss.attitude.Galileo
Default yaw rates for all spacecrafts in radians per seconds.
DEFAULT_YAW_RATE - Static variable in class org.orekit.gnss.attitude.Glonass
Default yaw rates for all spacecrafts in radians per seconds.
DEFAULT_YAW_RATE - Static variable in class org.orekit.gnss.attitude.GPSBlockIIF
Default yaw rates for all spacecrafts in radians per seconds.
DEFAULT_YAW_RATE - Static variable in class org.orekit.gnss.attitude.GPSBlockIIR
Default yaw rates for all spacecrafts in radians per seconds.
DEFAULT_YAW_RATES - Static variable in class org.orekit.gnss.attitude.GPSBlockIIA
Default yaw rates for all spacecrafts in radians per seconds (indexed by prnNumber, hence entry 0 is unused).
DEGREES - org.orekit.data.PolynomialParser.Unit
Degrees angles.
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(double) - Method in class org.orekit.data.PolynomialNutation
Evaluate the time derivative of the polynomial.
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(T) - Method in class org.orekit.data.PolynomialNutation
Evaluate the time derivative of the polynomial.
differentiate(ParameterFunction, int, double) - Static method in class org.orekit.utils.Differentiation
Differentiate a scalar function using finite differences.
differentiate(ParameterFunction, ParameterDriver, int, double) - Static method in class org.orekit.utils.Differentiation
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.
DIMENSION_INCONSISTENT_WITH_PARAMETERS - org.orekit.errors.OrekitMessages
 
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.
DiscreteTroposphericModel - Interface in org.orekit.models.earth
Defines a tropospheric model, used to calculate the path delay imposed to electro-magnetic signals between an orbital satellite and a ground station.
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(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.events.FieldEventState
Notify the user's listener of the event.
doEvent(SpacecraftState) - Method in class org.orekit.propagation.events.EventState
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.
DOPPLER - org.orekit.gnss.MeasurementType
Doppler measurement.
DOPPLER_INSTANTANEOUS - org.orekit.files.ccsds.Keyword
Data: Doppler instantaneous [km/s].
DOPPLER_INTEGRATED - org.orekit.files.ccsds.Keyword
Data: Doppler integrated [km/s].
DOR - org.orekit.files.ccsds.Keyword
Data: DOR [s].
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_AREA - org.orekit.files.ccsds.Keyword
Drag area.
DRAG_COEFF - org.orekit.files.ccsds.Keyword
Drag coefficient.
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[]) - Method in interface org.orekit.forces.drag.DragSensitive
Compute the acceleration due to drag.
dragAcceleration(AbsoluteDate, Frame, Vector3D, Rotation, double, double, Vector3D, double[]) - 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.BoxAndSolarArraySpacecraft
Compute acceleration due to drag, with parameters derivatives.
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[], String) - Method in class org.orekit.forces.drag.IsotropicDrag
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(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(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.
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.
DSST_ECC_NO_NUMERICAL_AVERAGING_METHOD - org.orekit.errors.OrekitMessages
 
DSST_NEWCOMB_OPERATORS_COMPUTATION - org.orekit.errors.OrekitMessages
 
DSST_SPR_SHADOW_INCONSISTENT - org.orekit.errors.OrekitMessages
 
DSST_VMNS_COEFFICIENT_ERROR_MS - org.orekit.errors.OrekitMessages
 
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) - Constructor for class org.orekit.propagation.semianalytical.dsst.DSSTPropagator
Create a new instance of DSSTPropagator.
DSSTPropagator(ODEIntegrator, boolean) - 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, double, double, ExtendedPVCoordinatesProvider, double) - Constructor for class org.orekit.propagation.semianalytical.dsst.forces.DSSTSolarRadiationPressure
Constructor with customizable reference values but spherical spacecraft.
DSSTSolarRadiationPressure(double, double, double, double, PVCoordinatesProvider, double) - Constructor for class org.orekit.propagation.semianalytical.dsst.forces.DSSTSolarRadiationPressure
DSSTSolarRadiationPressure(double, double, ExtendedPVCoordinatesProvider, double) - Constructor for class org.orekit.propagation.semianalytical.dsst.forces.DSSTSolarRadiationPressure
Simple constructor with default reference values and spherical spacecraft.
DSSTSolarRadiationPressure(double, double, ExtendedPVCoordinatesProvider, double, RadiationSensitive) - Constructor for class org.orekit.propagation.semianalytical.dsst.forces.DSSTSolarRadiationPressure
Complete constructor.
DSSTSolarRadiationPressure(double, double, PVCoordinatesProvider, double) - Constructor for class org.orekit.propagation.semianalytical.dsst.forces.DSSTSolarRadiationPressure
DSSTSolarRadiationPressure(double, double, PVCoordinatesProvider, double, RadiationSensitive) - Constructor for class org.orekit.propagation.semianalytical.dsst.forces.DSSTSolarRadiationPressure
DSSTSolarRadiationPressure(ExtendedPVCoordinatesProvider, double, RadiationSensitive) - Constructor for class org.orekit.propagation.semianalytical.dsst.forces.DSSTSolarRadiationPressure
Simple constructor with default reference values, but custom spacecraft.
DSSTSolarRadiationPressure(PVCoordinatesProvider, double, RadiationSensitive) - Constructor for class org.orekit.propagation.semianalytical.dsst.forces.DSSTSolarRadiationPressure
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.
DUPLICATED_GRAVITY_FIELD_COEFFICIENT_IN_FILE - org.orekit.errors.OrekitMessages
 
durationFrom(AbsoluteDate) - Method in class org.orekit.time.AbsoluteDate
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.
durationFrom(FieldAbsoluteDate<T>) - Method in class org.orekit.time.FieldAbsoluteDate
Compute the physically elapsed duration between two instants.
DynamicOutlierFilter<T extends ObservedMeasurement<T>> - Class in org.orekit.estimation.measurements.modifiers
Modifier that sets estimated measurement weight to 0 if residual is too far from expected domain.
DynamicOutlierFilter(int, double) - Constructor for class org.orekit.estimation.measurements.modifiers.DynamicOutlierFilter
Simple constructor.

E

e - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator
final eccentricity.
E01 - org.orekit.gnss.Frequency
Galileo, "E1" (1575.42 MHz).
E05 - org.orekit.gnss.Frequency
Galileo E5a (1176.45 MHz).
E06 - org.orekit.gnss.Frequency
Galileo E6 (1278.75 MHz).
E07 - org.orekit.gnss.Frequency
Galileo E5b (1207.14 MHz).
E08 - org.orekit.gnss.Frequency
Galileo E5 (E5a + E5b) (1191.795MHz).
e0sq - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator
original eccentricity squared.
EARTH - org.orekit.bodies.JPLEphemeridesLoader.EphemerisType
Constant for the Earth.
EARTH - org.orekit.files.ccsds.CenterName
Earth body.
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 - org.orekit.bodies.JPLEphemeridesLoader.EphemerisType
Constant for the Earth-Moon barycenter.
EARTH_MOON - org.orekit.files.ccsds.CenterName
Earth-Moon barycenter bodies pair.
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.
ECCENTRIC - org.orekit.orbits.PositionAngle
Eccentric angle.
ECCENTRICITY - org.orekit.files.ccsds.Keyword
Orbit 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, 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, 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, double, UnnormalizedSphericalHarmonicsProvider) - Constructor for class org.orekit.propagation.analytical.EcksteinHechlerPropagator
Build a propagator from orbit, mass 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, 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.
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, UnnormalizedSphericalHarmonicsProvider, UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics) - Constructor for class org.orekit.propagation.analytical.EcksteinHechlerPropagator
Private helper constructor.
EcksteinHechlerPropagator(Orbit, AttitudeProvider, UnnormalizedSphericalHarmonicsProvider) - Constructor for class org.orekit.propagation.analytical.EcksteinHechlerPropagator
Build a propagator from orbit, attitude provider and potential provider.
EcksteinHechlerPropagator(Orbit, UnnormalizedSphericalHarmonicsProvider) - Constructor for class org.orekit.propagation.analytical.EcksteinHechlerPropagator
Build a propagator from orbit and potential provider.
EcksteinHechlerPropagatorBuilder - Class in org.orekit.propagation.conversion
Builder for Eckstein-Hechler propagator.
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.
EcksteinHechlerPropagatorBuilder(Orbit, UnnormalizedSphericalHarmonicsProvider, 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(double, double, 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(PVCoordinatesProvider, double, PVCoordinatesProvider, double) - Constructor for class org.orekit.propagation.events.EclipseDetector
Build a new eclipse detector.
ECLIPTIC_CONVENTIONS_1996 - org.orekit.frames.Predefined
Ecliptic framen IERS 1996 conventions.
ECLIPTIC_CONVENTIONS_2003 - org.orekit.frames.Predefined
Ecliptic framen IERS 2003 conventions.
ECLIPTIC_CONVENTIONS_2010 - org.orekit.frames.Predefined
Ecliptic framen IERS 2010 conventions.
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.
EGM_FILENAME - Static variable in class org.orekit.forces.gravity.potential.GravityFieldFactory
Default regular expression for EGM files.
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.
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.
ELEMENT_SET_NO - org.orekit.files.ccsds.Keyword
Element set number of the satellite.
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(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.
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.
ElevationExtremumDetector - Class in org.orekit.propagation.events
Detector for elevation extremum with respect to a ground point.
ElevationExtremumDetector(double, double, TopocentricFrame) - Constructor for class org.orekit.propagation.events.ElevationExtremumDetector
Build a detector.
ElevationExtremumDetector(TopocentricFrame) - Constructor for class org.orekit.propagation.events.ElevationExtremumDetector
Build a new 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(double, double) - Static method in class org.orekit.orbits.KeplerianOrbit
Computes the mean anomaly from the elliptic eccentric anomaly.
ellipticEccentricToMean(T, T) - Static method in class org.orekit.orbits.FieldKeplerianOrbit
Computes the mean 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.
ellipticEccentricToTrue(T, T) - Static method in class org.orekit.orbits.FieldKeplerianOrbit
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
EME2000 - org.orekit.files.ccsds.CCSDSFrame
Earth Mean Equator and Equinox of J2000.
EME2000 - org.orekit.frames.Predefined
EME2000 frame.
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
EOPEntry(int, double, double, double, double, double, double, double, double, ITRFVersion) - 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_FILE_NO_MULTI_SUPPORT - org.orekit.errors.OrekitMessages
 
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.
EPHEMERIS_TYPE - org.orekit.files.ccsds.Keyword
Ephemeris type.
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.
EPOCH - org.orekit.files.ccsds.Keyword
Epoch of state vector and optional Keplerian elements.
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.analytical.tle.TLE
Check if this tle equals the provided tle.
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
EQUINOCTIAL - org.orekit.orbits.OrbitType
Type for propagation in equinoctial parameters.
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, 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, PositionAngle, Frame, AbsoluteDate, double) - Constructor for class org.orekit.orbits.EquinoctialOrbit
Creates a new instance.
EquinoctialOrbit(Orbit) - Constructor for class org.orekit.orbits.EquinoctialOrbit
Constructor from any kind of orbital parameters.
EquinoctialOrbit(PVCoordinates, Frame, AbsoluteDate, double) - Constructor for class org.orekit.orbits.EquinoctialOrbit
Constructor from Cartesian parameters.
EquinoctialOrbit(TimeStampedPVCoordinates, Frame, double) - Constructor for class org.orekit.orbits.EquinoctialOrbit
Constructor from Cartesian parameters.
equinoctialToPosition(T, T, T, T, T, T, double) - Static method in class org.orekit.orbits.FieldEquinoctialOrbit
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.
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(Frame, Vector3D, AbsoluteDate, Vector3D, AbsoluteDate, Vector3D, AbsoluteDate) - Method in class org.orekit.estimation.iod.IodGibbs
Give an initial orbit estimation, assuming Keplerian motion.
estimate(Frame, PV, PV, PV) - Method in class org.orekit.estimation.iod.IodGibbs
Give an initial orbit estimation, assuming Keplerian motion.
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.
EstimatedMeasurement.Status - Enum in org.orekit.estimation.measurements
Enumerate for the status of the measurement.
estimatedMeasurementsParameters(ParameterDriversList) - Method in class org.orekit.estimation.sequential.KalmanEstimatorBuilder
Configure the estimated measurement parameters.
EstimatedTroposphericModel - Class in org.orekit.models.earth
An estimated tropospheric model.
EstimatedTroposphericModel(double, double, MappingFunction, double) - Constructor for class org.orekit.models.earth.EstimatedTroposphericModel
Build a new instance using the given environmental conditions.
EstimatedTroposphericModel(MappingFunction, double) - Constructor for class org.orekit.models.earth.EstimatedTroposphericModel
Build a new instance using a standard atmosphere model.
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.
estimateRate(Rotation, Rotation, double) - Static method in class org.orekit.utils.AngularCoordinates
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.
estimationStep(ObservedMeasurement<?>) - Method in class org.orekit.estimation.sequential.KalmanEstimator
Process a single measurement.
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(FieldOrekitStepInterpolator<T>) - Method in class org.orekit.propagation.events.FieldEventState
Evaluate the impact of the proposed step on the event detector.
evaluateStep(OrekitStepInterpolator) - Method in class org.orekit.propagation.events.EventState
Evaluate the impact of the proposed step on the event detector.
evaluateTC(AbsoluteDate) - Method in enum org.orekit.utils.IERSConventions
Evaluate the date offset between the current date and the reference date.
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.
evaluationPerformed(KalmanEstimation) - Method in interface org.orekit.estimation.sequential.KalmanObserver
Notification callback after each one of a Kalman filter estimation.
EVENT_DATE_TOO_CLOSE - org.orekit.errors.OrekitMessages
 
EventBasedScheduler<T extends ObservedMeasurement<T>> - Class in org.orekit.estimation.measurements.generation
Scheduler based on EventDetector for generating measurements sequences.
EventBasedScheduler(MeasurementBuilder<T>, DatesSelector, Propagator, EventDetector, SignSemantic) - Constructor for class org.orekit.estimation.measurements.generation.EventBasedScheduler
Simple constructor.
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<? super 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(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(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, boolean) - Method in class org.orekit.propagation.events.AbstractDetector
Handle the event.
eventOccurred(SpacecraftState, boolean) - Method in class org.orekit.propagation.events.AdapterDetector
Handle the event.
eventOccurred(SpacecraftState, boolean) - Method in interface org.orekit.propagation.events.EventDetector
Handle the event.
eventOccurred(SpacecraftState, T, boolean) - Method in class org.orekit.propagation.events.handlers.ContinueOnEvent
Specific implementation of the eventOccurred interface.
eventOccurred(SpacecraftState, T, boolean) - Method in interface org.orekit.propagation.events.handlers.EventHandler
eventOccurred method mirrors the same interface method as in EventDetector and its subclasses, but with an additional parameter that allows the calling method to pass in an object from the detector which would have potential additional data to allow the implementing class to determine the correct return state.
eventOccurred(SpacecraftState, T, boolean) - Method in class org.orekit.propagation.events.handlers.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.
EXT - org.orekit.files.sp3.SP3File.SP3OrbitType
extrapolated or predicted.
ExtendedPVCoordinatesProvider - Interface in org.orekit.utils
Interface for PV coordinates providers that also support fields.
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.
extractRange(AbsoluteDate, AbsoluteDate) - Method in class org.orekit.utils.TimeSpanMap
Extract a range of the map.

F

f - Variable in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution
Equinoctial frame f vector.
F0 - Static variable in enum org.orekit.gnss.Frequency
Common frequency F0 in MHz (10.23 MHz).
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.
FEASIBLE_MEASUREMENT_WHEN_NEGATIVE - org.orekit.estimation.measurements.generation.SignSemantic
Semantic for detectors that have negative g function when measurements are feasible.
FEASIBLE_MEASUREMENT_WHEN_POSITIVE - org.orekit.estimation.measurements.generation.SignSemantic
Semantic for detectors that have positive g function when measurements are feasible.
FEBRUARY - org.orekit.time.Month
February.
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.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(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 org.hipparchus.RealFieldElement<T>> - Class in org.orekit.time
This class represents a specific instant in time.
FieldAbsoluteDate(Field<T>) - Constructor for class org.orekit.time.FieldAbsoluteDate
Create an instance with a default value (FieldAbsoluteDate.getJ2000Epoch(Field)).
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, 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, 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, TimeScale) - Constructor for class org.orekit.time.FieldAbsoluteDate
Build an instance from a location in a time scale.
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>, Date, TimeScale) - Constructor for class org.orekit.time.FieldAbsoluteDate
Build an instance from a location in a time scale.
FieldAbsoluteDate(Field<T>, AbsoluteDate) - Constructor for class org.orekit.time.FieldAbsoluteDate
Build an instance from an AbsoluteDate.
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>, DateComponents, TimeScale) - Constructor for class org.orekit.time.FieldAbsoluteDate
Build an instance from a location 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(AbsoluteDate, T) - Constructor for class org.orekit.time.FieldAbsoluteDate
Build an instance from an elapsed duration since to another instant.
FieldAbsoluteDate(FieldAbsoluteDate<T>, double) - 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.
FieldAbsoluteDate(FieldAbsoluteDate<T>, T) - Constructor for class org.orekit.time.FieldAbsoluteDate
Build an instance from an elapsed duration since to another instant.
FieldAbstractAnalyticalPropagator<T extends org.hipparchus.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 org.hipparchus.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 org.hipparchus.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 org.hipparchus.RealFieldElement<T>> - Interface in org.orekit.propagation.integration
Differential equations for the main state (orbit, attitude and mass).
FieldAbstractPropagator<T extends org.hipparchus.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 org.hipparchus.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 org.hipparchus.RealFieldElement<T>> - Interface in org.orekit.propagation
This interface represents providers for additional state data beyond SpacecraftState.
FieldAltitudeDetector<T extends org.hipparchus.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 org.hipparchus.RealFieldElement<T>> - Class in org.orekit.utils
Simple container for rotation / rotation rate pairs, using RealFieldElement.
FieldAngularCoordinates(Field<T>, AngularCoordinates) - Constructor for class org.orekit.utils.FieldAngularCoordinates
Builds a FieldAngularCoordinates from a field and a regular AngularCoordinates.
FieldAngularCoordinates(FieldRotation<FieldDerivativeStructure<T>>) - Constructor for class org.orekit.utils.FieldAngularCoordinates
Builds a FieldAngularCoordinates from a FieldRotation<FieldDerivativeStructure>.
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.
FieldApsideDetector<T extends org.hipparchus.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 org.hipparchus.RealFieldElement<T>> - Class in org.orekit.attitudes
This class handles attitude definition at a given date.
FieldAttitude(Field<T>, Attitude) - Constructor for class org.orekit.attitudes.FieldAttitude
Builds an instance for a regular Attitude.
FieldAttitude(Frame, TimeStampedFieldAngularCoordinates<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(FieldAbsoluteDate<T>, Frame, FieldAngularCoordinates<T>) - Constructor for class org.orekit.attitudes.FieldAttitude
Creates a new instance.
FieldBodiesElements<T extends org.hipparchus.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 org.hipparchus.RealFieldElement<T>> - Interface in org.orekit.propagation
This interface is intended for ephemerides valid only during a time range.
FieldCartesianOrbit<T extends org.hipparchus.RealFieldElement<T>> - Class in org.orekit.orbits
This class holds Cartesian orbital parameters.
FieldCartesianOrbit(FieldOrbit<T>) - Constructor for class org.orekit.orbits.FieldCartesianOrbit
Constructor from any kind of orbital parameters.
FieldCartesianOrbit(FieldPVCoordinates<T>, Frame, FieldAbsoluteDate<T>, double) - Constructor for class org.orekit.orbits.FieldCartesianOrbit
Constructor from Cartesian parameters.
FieldCartesianOrbit(TimeStampedFieldPVCoordinates<T>, Frame, double) - Constructor for class org.orekit.orbits.FieldCartesianOrbit
Constructor from Cartesian parameters.
FieldCircularOrbit<T extends org.hipparchus.RealFieldElement<T>> - Class in org.orekit.orbits
This class handles circular orbital parameters.
FieldCircularOrbit(FieldOrbit<T>) - Constructor for class org.orekit.orbits.FieldCircularOrbit
Constructor from any kind of orbital parameters.
FieldCircularOrbit(FieldPVCoordinates<T>, Frame, FieldAbsoluteDate<T>, double) - Constructor for class org.orekit.orbits.FieldCircularOrbit
Constructor from Cartesian parameters.
FieldCircularOrbit(TimeStampedFieldPVCoordinates<T>, Frame, double) - Constructor for class org.orekit.orbits.FieldCircularOrbit
Constructor from Cartesian 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.
FieldContinueOnEvent<KK extends FieldEventDetector<T>,T extends org.hipparchus.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 org.hipparchus.RealFieldElement<T>> - Class in org.orekit.propagation.events
Finder for date events.
FieldDateDetector(FieldAbsoluteDate<T>) - Constructor for class org.orekit.propagation.events.FieldDateDetector
Build a new instance.
FieldDateDetector(T, T, FieldTimeStamped<T>...) - Constructor for class org.orekit.propagation.events.FieldDateDetector
Build a new instance.
FieldDelaunayArguments<T extends org.hipparchus.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 org.hipparchus.RealFieldElement<T>> - Class in org.orekit.propagation.analytical
This class propagates a FieldSpacecraftState using the analytical Eckstein-Hechler model.
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>, 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, UnnormalizedSphericalHarmonicsProvider) - Constructor for class org.orekit.propagation.analytical.FieldEcksteinHechlerPropagator
Build a propagator from FieldOrbit, attitude provider 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.
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, UnnormalizedSphericalHarmonicsProvider, UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics) - Constructor for class org.orekit.propagation.analytical.FieldEcksteinHechlerPropagator
Private helper constructor.
FieldEcksteinHechlerPropagator(FieldOrbit<T>, UnnormalizedSphericalHarmonicsProvider) - Constructor for class org.orekit.propagation.analytical.FieldEcksteinHechlerPropagator
Build a propagator from FieldOrbit 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>, T, UnnormalizedSphericalHarmonicsProvider) - Constructor for class org.orekit.propagation.analytical.FieldEcksteinHechlerPropagator
Build a propagator from FieldOrbit, mass and potential provider.
FieldEclipseDetector<T extends org.hipparchus.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 org.hipparchus.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 org.hipparchus.RealFieldElement<T>> - Class in org.orekit.orbits
This class handles equinoctial orbital parameters, which can support both circular and equatorial orbits.
FieldEquinoctialOrbit(FieldOrbit<T>) - Constructor for class org.orekit.orbits.FieldEquinoctialOrbit
Constructor from any kind of orbital parameters.
FieldEquinoctialOrbit(FieldPVCoordinates<T>, Frame, FieldAbsoluteDate<T>, double) - Constructor for class org.orekit.orbits.FieldEquinoctialOrbit
Constructor from Cartesian parameters.
FieldEquinoctialOrbit(TimeStampedFieldPVCoordinates<T>, Frame, double) - Constructor for class org.orekit.orbits.FieldEquinoctialOrbit
Constructor from Cartesian parameters.
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.
FieldEventDetector<T extends org.hipparchus.RealFieldElement<T>> - Interface in org.orekit.propagation.events
This interface represents space-dynamics aware events detectors.
FieldEventHandler<KK extends FieldEventDetector<T>,T extends org.hipparchus.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 org.hipparchus.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 org.hipparchus.RealFieldElement<T>> - Class in org.orekit.propagation.events
Class for logged events entries.
FieldEventState<D extends FieldEventDetector<T>,T extends org.hipparchus.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 org.hipparchus.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 org.hipparchus.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 org.hipparchus.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 org.hipparchus.RealFieldElement<T>> - Class in org.orekit.orbits
This class handles traditional Keplerian orbital parameters.
FieldKeplerianOrbit(FieldOrbit<T>) - Constructor for class org.orekit.orbits.FieldKeplerianOrbit
Constructor from any kind of orbital parameters.
FieldKeplerianOrbit(FieldPVCoordinates<T>, Frame, FieldAbsoluteDate<T>, double) - Constructor for class org.orekit.orbits.FieldKeplerianOrbit
Constructor from Cartesian parameters.
FieldKeplerianOrbit(TimeStampedFieldPVCoordinates<T>, Frame, double) - Constructor for class org.orekit.orbits.FieldKeplerianOrbit
Constructor from Cartesian 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.
FieldKeplerianPropagator<T extends org.hipparchus.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 org.hipparchus.RealFieldElement<T>> - Interface in org.orekit.propagation.integration
Common interface for all propagator mode handlers initialization.
FieldNodeDetector<T extends org.hipparchus.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 org.hipparchus.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(Vector3D, Vector3D, double, int, double) - Constructor for class org.orekit.propagation.events.FieldOfView
Build Field Of View with a regular polygon shape.
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(SphericalPolygonsSet, double) - Constructor for class org.orekit.propagation.events.FieldOfView
Build a new instance.
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 org.hipparchus.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 org.hipparchus.RealFieldElement<T>> - Interface in org.orekit.propagation.sampling
This interface is a space-dynamics aware fixed size step handler.
FieldOrekitStepHandler<T extends org.hipparchus.RealFieldElement<T>> - Interface in org.orekit.propagation.sampling
This interface is a space-dynamics aware step handler.
FieldOrekitStepHandlerMultiplexer<T extends org.hipparchus.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 org.hipparchus.RealFieldElement<T>> - Interface in org.orekit.propagation.sampling
This interface is a space-dynamics aware step interpolator.
FieldOrekitStepNormalizer<T extends org.hipparchus.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 org.hipparchus.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 org.hipparchus.RealFieldElement<T>> - Interface in org.orekit.propagation
This interface provides a way to propagate an orbit at any time.
FieldPVCoordinates<T extends org.hipparchus.RealFieldElement<T>> - Class in org.orekit.utils
Simple container for Position/Velocity pairs, using RealFieldElement.
FieldPVCoordinates(double, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.FieldPVCoordinates
Multiplicative constructor.
FieldPVCoordinates(double, FieldPVCoordinates<T>, double, FieldPVCoordinates<T>) - 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(double, FieldPVCoordinates<T>, double, FieldPVCoordinates<T>, double, FieldPVCoordinates<T>, double, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.FieldPVCoordinates
Linear constructor.
FieldPVCoordinates(Field<T>, PVCoordinates) - Constructor for class org.orekit.utils.FieldPVCoordinates
Builds a FieldPVCoordinates from a field and a regular PVCoordinates.
FieldPVCoordinates(FieldVector3D<FieldDerivativeStructure<T>>) - Constructor for class org.orekit.utils.FieldPVCoordinates
Builds a FieldPVCoordinates triplet from a FieldVector3D<FieldDerivativeStructure>.
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(FieldPVCoordinates<T>, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.FieldPVCoordinates
Subtractive constructor.
FieldPVCoordinates(T, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.FieldPVCoordinates
Multiplicative constructor.
FieldPVCoordinates(T, FieldPVCoordinates<T>, T, 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, FieldPVCoordinates<T>, T, FieldPVCoordinates<T>, T, FieldPVCoordinates<T>, T, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.FieldPVCoordinates
Linear constructor.
FieldPVCoordinates(T, PVCoordinates) - Constructor for class org.orekit.utils.FieldPVCoordinates
Multiplicative constructor.
FieldPVCoordinates(T, PVCoordinates, T, PVCoordinates) - 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(T, PVCoordinates, T, PVCoordinates, T, PVCoordinates, T, PVCoordinates) - Constructor for class org.orekit.utils.FieldPVCoordinates
Linear constructor.
FieldPVCoordinatesProvider<T extends org.hipparchus.RealFieldElement<T>> - Interface in org.orekit.utils
Interface for PV coordinates providers.
FieldSpacecraftState<T extends org.hipparchus.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(Field<T>, SpacecraftState) - Constructor for class org.orekit.propagation.FieldSpacecraftState
Convert a SpacecraftState.
FieldSpacecraftState(FieldOrbit<T>) - Constructor for class org.orekit.propagation.FieldSpacecraftState
Build a spacecraft state from orbit only.
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>) - Constructor for class org.orekit.propagation.FieldSpacecraftState
Build a spacecraft state from orbit and attitude provider.
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>, FieldAttitude<T>, T) - Constructor for class org.orekit.propagation.FieldSpacecraftState
Build a spacecraft state from orbit, attitude provider 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(FieldOrbit<T>, T) - Constructor for class org.orekit.propagation.FieldSpacecraftState
Create a new instance from orbit and mass.
FieldSpacecraftState(FieldOrbit<T>, T, Map<String, T[]>) - Constructor for class org.orekit.propagation.FieldSpacecraftState
Create a new instance from orbit and mass.
FieldStateMapper<T extends org.hipparchus.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 org.hipparchus.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 org.hipparchus.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 org.hipparchus.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 org.hipparchus.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 org.hipparchus.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 org.hipparchus.RealFieldElement<KK>> - Interface in org.orekit.time
This interface represents objects that can be shifted in time.
FieldTimeSpanMap<T,D extends org.hipparchus.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 org.hipparchus.RealFieldElement<D>> - Class in org.orekit.utils
Local class holding transition times.
FieldTimeStamped<T extends org.hipparchus.RealFieldElement<T>> - Interface in org.orekit.time
This interface represents objects that have a AbsoluteDate date attached to them.
FieldTransform<T extends org.hipparchus.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>, FieldRotation<T>) - Constructor for class org.orekit.frames.FieldTransform
Build a rotation transform.
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>, FieldVector3D<T>) - Constructor for class org.orekit.frames.FieldTransform
Build a translation 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>, FieldTransform<T>, FieldTransform<T>) - Constructor for class org.orekit.frames.FieldTransform
Build a transform by combining two existing ones.
FieldTransform(FieldAbsoluteDate<T>, FieldAngularCoordinates<T>) - Constructor for class org.orekit.frames.FieldTransform
Build a rotation transform.
FieldTransform(FieldAbsoluteDate<T>, FieldPVCoordinates<T>) - Constructor for class org.orekit.frames.FieldTransform
Build a translation transform, with its first time derivative.
FieldTransformGenerator<T extends org.hipparchus.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(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.
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.
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.
filter(NamedData) - Method in interface org.orekit.data.DataFilter
Filter the named data.
filter(NamedData) - Method in class org.orekit.data.GzipFilter
Filter the named data.
filter(NamedData) - Method in class org.orekit.data.UnixCompressFilter
Filter the named data.
FilterType - Enum in org.orekit.propagation.events
Enumerate for filtering events.
finalizeEstimation(ObservedMeasurement<?>, ProcessEstimate) - Method in class org.orekit.estimation.sequential.Model
Finalize estimation.
findByName(String) - Method in class org.orekit.utils.ParameterDriversList
Find a delegating driver by name.
findEOP(Frame) - Static method in class org.orekit.frames.FramesFactory
Retrieve EOP from a frame hierarchy.
findSatelliteAntenna(SatelliteSystem, int) - Method in class org.orekit.gnss.antenna.AntexLoader
Find the time map for a specific satellite antenna.
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.
FIT - org.orekit.files.sp3.SP3File.SP3OrbitType
fitted.
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.
FixedStepSelector - Class in org.orekit.time
Selector generating a continuous stream of dates separated by a constant step.
FixedStepSelector(double, TimeScale) - Constructor for class org.orekit.time.FixedStepSelector
Simple constructor.
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, TransformProvider, 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, boolean) - Constructor for class org.orekit.frames.Frame
Build a frame from its transform with respect to its parent.
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, Transform, String, boolean) - Constructor for class org.orekit.frames.Frame
Build a frame from its transform with respect to its parent.
FRAME_ALREADY_ATTACHED - org.orekit.errors.OrekitMessages
 
FRAME_ANCESTOR_OF_BOTH_FRAMES - org.orekit.errors.OrekitMessages
 
FRAME_ANCESTOR_OF_NEITHER_FRAME - org.orekit.errors.OrekitMessages
 
FRAME_NO_NTH_ANCESTOR - org.orekit.errors.OrekitMessages
 
FRAME_NOT_ATTACHED - org.orekit.errors.OrekitMessages
 
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.
FRAMES_MISMATCH - org.orekit.errors.OrekitMessages
 
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.
FREQ_OFFSET - org.orekit.files.ccsds.Keyword
Meta-data: Frequency offset.
Frequency - Enum in org.orekit.gnss
Enumerate for GNSS frequencies.
FrequencyPattern - Class in org.orekit.gnss.antenna
Pattern for GNSS antenna model on one frequency.
FrequencyPattern(Vector3D, PhaseCenterVariationFunction) - Constructor for class org.orekit.gnss.antenna.FrequencyPattern
Simple constructor.
FunctionalDetector - Class in org.orekit.propagation.events
A detector that implements the FunctionalDetector.g(SpacecraftState) function using a lambda that can be set using FunctionalDetector.withFunction(ToDoubleFunction).
FunctionalDetector() - Constructor for class org.orekit.propagation.events.FunctionalDetector
Create an event detector with the default values.
FunctionalDetector.GFunction - Interface in org.orekit.propagation.events
Deprecated.
Use ToDoubleFunction instead. Will be removed in next major release.
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 - Variable in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution
Equinoctial frame g vector.
g(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.events.FieldAbstractDetector
Compute the value of the switching function.
g(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.events.FieldAltitudeDetector
Compute the value of the switching function.
g(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.events.FieldApsideDetector
Compute the value of the switching function.
g(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.events.FieldDateDetector
Compute the value of the switching function.
g(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.events.FieldEclipseDetector
Compute the value of the switching function.
g(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.events.FieldElevationDetector
Compute the value of the switching function.
g(FieldSpacecraftState<T>) - Method in interface org.orekit.propagation.events.FieldEventDetector
Compute the value of the switching function.
g(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.events.FieldNodeDetector
Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.forces.maneuvers.ImpulseManeuver
Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.AbstractDetector
Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.AdapterDetector
Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.AlignmentDetector
Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.AltitudeDetector
Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.AngularSeparationDetector
Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.ApsideDetector
Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.BooleanDetector
 
g(SpacecraftState) - Method in class org.orekit.propagation.events.CircularFieldOfViewDetector
Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.DateDetector
Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.EclipseDetector
Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.ElevationDetector
Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.ElevationExtremumDetector
Compute the value of the detection function.
g(SpacecraftState) - Method in interface org.orekit.propagation.events.EventDetector
Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.EventEnablingPredicateFilter
Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.EventShifter
Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.EventSlopeFilter
Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.FieldOfViewDetector
Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.FootprintOverlapDetector
Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.FunctionalDetector
 
g(SpacecraftState) - Method in class org.orekit.propagation.events.GeographicZoneDetector
Compute the value of the detection function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.GroundAtNightDetector
Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.GroundFieldOfViewDetector
Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.InterSatDirectViewDetector
Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.LatitudeCrossingDetector
Compute the value of the detection function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.LatitudeExtremumDetector
Compute the value of the detection function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.LongitudeCrossingDetector
Compute the value of the detection function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.LongitudeExtremumDetector
Compute the value of the detection function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.NegateDetector
 
g(SpacecraftState) - Method in class org.orekit.propagation.events.NodeDetector
Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.PositionAngleDetector
Compute the value of the detection function.
G0_STANDARD_GRAVITY - Static variable in interface org.orekit.utils.Constants
Standard gravity constant, used in maneuvers definition: 9.80665 m/s².
G01 - org.orekit.gnss.Frequency
GPS L1 (1575.42 MHz).
G02 - org.orekit.gnss.Frequency
GPS L2 (1227.6 MHz).
G05 - org.orekit.gnss.Frequency
GPS L5 (1176.45 MHz).
GAL - org.orekit.files.sp3.SP3File.TimeSystem
GALILEO.
Galileo - Class in org.orekit.gnss.attitude
Attitude providers for Galileo navigation satellites.
Galileo(double, AbsoluteDate, AbsoluteDate, ExtendedPVCoordinatesProvider, Frame) - Constructor for class org.orekit.gnss.attitude.Galileo
Simple constructor.
GALILEO - org.orekit.files.sp3.SP3File.SP3FileType
Galileo only file.
GALILEO - org.orekit.gnss.SatelliteSystem
Galileo system.
GALILEO_0A - org.orekit.gnss.antenna.SatelliteAntennaCode
Deprecated.
Galileo In-Orbit Validation Element A (GIOVE-A).
GALILEO_0A - org.orekit.gnss.antenna.SatelliteType
Galileo In-Orbit Validation Element A (GIOVE-A).
GALILEO_0B - org.orekit.gnss.antenna.SatelliteAntennaCode
Deprecated.
Galileo In-Orbit Validation Element B (GIOVE-B).
GALILEO_0B - org.orekit.gnss.antenna.SatelliteType
Galileo In-Orbit Validation Element B (GIOVE-B).
GALILEO_1 - org.orekit.gnss.antenna.SatelliteAntennaCode
Deprecated.
Galileo IOV : GSAT 0101-0104.
GALILEO_1 - org.orekit.gnss.antenna.SatelliteType
Galileo IOV : GSAT 0101-0104.
GALILEO_2 - org.orekit.gnss.antenna.SatelliteAntennaCode
Deprecated.
Galileo FOC : GSAT 0201-0222.
GALILEO_2 - org.orekit.gnss.antenna.SatelliteType
Galileo FOC : GSAT 0201-0222.
GALILEO_EPOCH - Static variable in class org.orekit.time.AbsoluteDate
Reference epoch for Galileo System Time: 1999-08-22T00:00:00 UTC.
GALILEO_EPOCH - Static variable in class org.orekit.time.DateComponents
Reference epoch for Galileo System Time: 1999-08-22.
GalileoScale - Class in org.orekit.time
Galileo system time scale.
GammaMnsFunction - Class in org.orekit.propagation.semianalytical.dsst.utilities
Compute the Γmn,s(γ) function from equation 2.7.1-(13).
GammaMnsFunction(int, double, int) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.GammaMnsFunction
Simple constructor.
GCRF - org.orekit.files.ccsds.CCSDSFrame
Geocentric Celestial Reference Frame.
GCRF - org.orekit.frames.Predefined
GCRF frame.
GEGOUT - org.orekit.forces.gravity.potential.OceanLoadDeformationCoefficients
Coefficients computed by Pascal Gégout, CNRS / UMR5563 (GET).
generate(List<OrekitStepInterpolator>) - Method in class org.orekit.estimation.measurements.generation.ContinuousScheduler
Generate a sequence of measurements.
generate(List<OrekitStepInterpolator>) - Method in class org.orekit.estimation.measurements.generation.EventBasedScheduler
Generate a sequence of measurements.
generate(List<OrekitStepInterpolator>) - Method in interface org.orekit.estimation.measurements.generation.Scheduler
Generate a sequence of measurements.
generate(AbsoluteDate, AbsoluteDate) - Method in class org.orekit.estimation.measurements.generation.Generator
Generate measurements.
generate(AbsoluteDate, AbsoluteDate) - Method in class org.orekit.frames.FieldTransformGenerator
Generate a chronologically sorted list of entries to be cached.
generate(AbsoluteDate, AbsoluteDate) - Method in class org.orekit.frames.TransformGenerator
Generate a chronologically sorted list of entries to be cached.
generate(AbsoluteDate, AbsoluteDate) - Method in interface org.orekit.utils.TimeStampedGenerator
Generate a chronologically sorted list of entries to be cached.
generateCartesianOrbit() - Method in class org.orekit.files.ccsds.OMMFile
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.
Generator - Class in org.orekit.estimation.measurements.generation
Main generator for observed measurements.
Generator() - Constructor for class org.orekit.estimation.measurements.generation.Generator
Build a generator with no sequences generator.
GenericGNSS - Class in org.orekit.gnss.attitude
Attitude providers for navigation satellites for which no specialized model is known.
GenericGNSS(AbsoluteDate, AbsoluteDate, ExtendedPVCoordinatesProvider, Frame) - Constructor for class org.orekit.gnss.attitude.GenericGNSS
Simple constructor.
GenericTimeStampedCache<T extends TimeStamped> - Class in org.orekit.utils
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(double, double, BodyShape, SphericalPolygonsSet, double) - Constructor for class org.orekit.propagation.events.GeographicZoneDetector
Build a detector.
GeographicZoneDetector(BodyShape, SphericalPolygonsSet, double) - Constructor for class org.orekit.propagation.events.GeographicZoneDetector
Build a new detector.
Geoid - Class in org.orekit.models.earth
A geoid is a level surface of the gravity potential of a body.
Geoid(NormalizedSphericalHarmonicsProvider, ReferenceEllipsoid) - Constructor for class org.orekit.models.earth.Geoid
Creates a geoid from the given geopotential, reference ellipsoid and the assumptions in the comment for Geoid.
GeoMagneticElements - Class in org.orekit.models.earth
Contains the elements to represent a magnetic field at a single point.
GeoMagneticElements(Vector3D) - Constructor for class org.orekit.models.earth.GeoMagneticElements
Construct a new element with the given field vector.
GeoMagneticField - Class in org.orekit.models.earth
Used to calculate the geomagnetic field at a given geodetic point on earth.
GeoMagneticField(String, double, int, int, double, double) - Constructor for class org.orekit.models.earth.GeoMagneticField
Create a new geomagnetic field model with the given parameters.
GeoMagneticFieldFactory - Class in org.orekit.models.earth
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(AbsoluteDate) - Method in class org.orekit.utils.TimeSpanMap
Get the entry valid at a specified date.
get(FieldAbsoluteDate<D>) - Method in class org.orekit.utils.FieldTimeSpanMap
Get the entry valid at a specified date.
get24HoursKp(AbsoluteDate) - Method in class org.orekit.forces.drag.atmosphere.data.MarshallSolarActivityFutureEstimation
The Kp index is derived from the Ap index.
get24HoursKp(AbsoluteDate) - Method in interface org.orekit.forces.drag.atmosphere.DTM2000InputParameters
Get the last 24H mean geomagnetic index.
getA() - Method in class org.orekit.bodies.Ellipse
Get the semi major axis.
getA() - Method in class org.orekit.bodies.Ellipsoid
Get the length of the first semi-axis.
getA() - Method in class org.orekit.files.ccsds.OGMFile
Get the orbit semi-major axis.
getA() - Method in class org.orekit.models.earth.GlobalPressureTemperature2Model
Returns the a coefficients array.
getA() - Method in class org.orekit.models.earth.ViennaModelCoefficientsLoader
Returns the a coefficients array.
getA() - Method in class org.orekit.orbits.CartesianOrbit
Get the semi-major axis.
getA() - Method in class org.orekit.orbits.CircularOrbit
Get the semi-major axis.
getA() - Method in class org.orekit.orbits.EquinoctialOrbit
Get the semi-major axis.
getA() - Method in class org.orekit.orbits.FieldCartesianOrbit
Get the semi-major axis.
getA() - Method in class org.orekit.orbits.FieldCircularOrbit
Get the semi-major axis.
getA() - Method in class org.orekit.orbits.FieldEquinoctialOrbit
Get the semi-major axis.
getA() - Method in class org.orekit.orbits.FieldKeplerianOrbit
Get the semi-major axis.
getA() - Method in class org.orekit.orbits.FieldOrbit
Get the semi-major axis.
getA() - Method in class org.orekit.orbits.KeplerianOrbit
Get the semi-major axis.
getA() - Method in class org.orekit.orbits.Orbit
Get the semi-major axis.
getA() - Method in class org.orekit.propagation.FieldSpacecraftState
Get the semi-major axis.
getA() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
Get A = sqrt(μ * a).
getA() - Method in class org.orekit.propagation.SpacecraftState
Get the semi-major axis.
getAbscissaGrid() - Method in class org.orekit.utils.InterpolationTableLoader
Returns a copy of the abscissa grid for the interpolation function.
getAbsoluteDate() - Method in class org.orekit.utils.FieldTimeSpanMap.Transition
Get the transition field absolute date.
getAcceleration() - Method in class org.orekit.frames.FieldTransform
Get the second time derivative of the translation.
getAcceleration() - Method in class org.orekit.frames.Transform
Get the second time derivative of the translation.
getAcceleration() - Method in class org.orekit.utils.FieldPVCoordinates
Gets the acceleration.
getAcceleration() - Method in class org.orekit.utils.PVCoordinates
Gets the acceleration.
getAccuracy() - Method in class org.orekit.files.sp3.SP3File.SP3Ephemeris
Get the formal accuracy for this satellite.
getAction() - Method in class org.orekit.propagation.events.EventState.EventOccurrence
Get the user requested action.
getAction() - Method in class org.orekit.propagation.events.FieldEventState.EventOccurrence
Get the user requested action.
getAdaptedPropagator() - Method in class org.orekit.propagation.conversion.AbstractPropagatorConverter
Get the adapted propagator.
getAdditionalState(String) - Method in class org.orekit.propagation.FieldSpacecraftState
Get an additional state.
getAdditionalState(String) - Method in class org.orekit.propagation.SpacecraftState
Get an additional state.
getAdditionalState(FieldSpacecraftState<T>) - Method in interface org.orekit.propagation.FieldAdditionalStateProvider
Get the additional state.
getAdditionalState(SpacecraftState) - Method in interface org.orekit.propagation.AdditionalStateProvider
Get the additional state.
getAdditionalState(SpacecraftState) - Method in class org.orekit.propagation.analytical.gnss.ClockCorrectionsProvider
Get the additional state.
getAdditionalStateDimension() - Method in class org.orekit.propagation.numerical.JacobiansMapper
Compute the length of the one-dimensional additional state array needed.
getAdditionalStateProviders() - Method in class org.orekit.propagation.AbstractPropagator
Get an unmodifiable list of providers for additional state.
getAdditionalStateProviders() - Method in class org.orekit.propagation.FieldAbstractPropagator
Get an unmodifiable list of providers for additional state.
getAdditionalStateProviders() - Method in interface org.orekit.propagation.FieldPropagator
Get an unmodifiable list of providers for additional state.
getAdditionalStateProviders() - Method in interface org.orekit.propagation.Propagator
Get an unmodifiable list of providers for additional state.
getAdditionalStates() - Method in class org.orekit.propagation.FieldSpacecraftState
Get an unmodifiable map of additional states.
getAdditionalStates() - Method in class org.orekit.propagation.SpacecraftState
Get an unmodifiable map of additional states.
getADot() - Method in class org.orekit.orbits.CartesianOrbit
Get the semi-major axis derivative.
getADot() - Method in class org.orekit.orbits.CircularOrbit
Get the semi-major axis derivative.
getADot() - Method in class org.orekit.orbits.EquinoctialOrbit
Get the semi-major axis derivative.
getADot() - Method in class org.orekit.orbits.FieldCartesianOrbit
Get the semi-major axis derivative.
getADot() - Method in class org.orekit.orbits.FieldCircularOrbit
Get the semi-major axis derivative.
getADot() - Method in class org.orekit.orbits.FieldEquinoctialOrbit
Get the semi-major axis derivative.
getADot() - Method in class org.orekit.orbits.FieldKeplerianOrbit
Get the semi-major axis derivative.
getADot() - Method in class org.orekit.orbits.FieldOrbit
Get the semi-major axis derivative.
getADot() - Method in class org.orekit.orbits.KeplerianOrbit
Get the semi-major axis derivative.
getADot() - Method in class org.orekit.orbits.Orbit
Get the semi-major axis derivative.
getAe() - Method in class org.orekit.forces.gravity.potential.CachedNormalizedSphericalHarmonicsProvider
Get the value of the central body reference radius.
getAe() - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
Get the central body reference radius.
getAe() - Method in interface org.orekit.forces.gravity.potential.SphericalHarmonicsProvider
Get the value of the central body reference radius.
getAf0() - Method in class org.orekit.gnss.GPSAlmanac
 
getAf0() - Method in interface org.orekit.propagation.analytical.gnss.GPSOrbitalElements
Gets the Zeroth Order Clock Correction.
getAf1() - Method in class org.orekit.gnss.GPSAlmanac
 
getAf1() - Method in interface org.orekit.propagation.analytical.gnss.GPSOrbitalElements
Gets the First Order Clock Correction.
getAf2() - Method in interface org.orekit.propagation.analytical.gnss.GPSOrbitalElements
Gets the Second Order Clock Correction.
getAfter() - Method in class org.orekit.utils.FieldTimeSpanMap.Transition
Get the entry valid after transition.
getAfter() - Method in class org.orekit.utils.TimeSpanMap.Transition
Get the entry valid after transition.
getAgency() - Method in class org.orekit.files.sp3.SP3File
Returns the agency that prepared this SP3 file.
getAgencyName() - Method in class org.orekit.gnss.RinexHeader
Get name of the agency.
getAlignAngle() - Method in class org.orekit.propagation.events.AlignmentDetector
Get the alignment angle (rad).
getAll() - Method in class org.orekit.utils.ImmutableTimeStampedCache
Get all of the data in this cache.
getAllForceModels() - Method in class org.orekit.propagation.conversion.NumericalPropagatorBuilder
Get the list of all force models.
getAllForceModels() - Method in class org.orekit.propagation.numerical.FieldNumericalPropagator
Get all the force models, perturbing forces and Newtonian attraction included.
getAllForceModels() - Method in class org.orekit.propagation.numerical.NumericalPropagator
Get all the force models, perturbing forces and Newtonian attraction included.
getAlmanacs() - Method in class org.orekit.gnss.SEMParser
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() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
Get direction cosine α for central body.
getAlpha(PositionAngle) - Method in class org.orekit.orbits.CircularOrbit
Get the latitude argument.
getAlpha(PositionAngle) - Method in class org.orekit.orbits.FieldCircularOrbit
Get the latitude argument.
getAlphaDot(PositionAngle) - Method in class org.orekit.orbits.CircularOrbit
Get the latitude argument derivative.
getAlphaDot(PositionAngle) - Method in class org.orekit.orbits.FieldCircularOrbit
Get the latitude argument derivative.
getAlphaE() - Method in class org.orekit.orbits.CircularOrbit
Get the eccentric latitude argument.
getAlphaE() - Method in class org.orekit.orbits.FieldCircularOrbit
Get the eccentric latitude argument.
getAlphaEDot() - Method in class org.orekit.orbits.CircularOrbit
Get the eccentric latitude argument derivative.
getAlphaEDot() - Method in class org.orekit.orbits.FieldCircularOrbit
Get the eccentric latitude argument derivative.
getAlphaM() - Method in class org.orekit.orbits.CircularOrbit
Get the mean latitude argument.
getAlphaM() - Method in class org.orekit.orbits.FieldCircularOrbit
Get the mean latitude argument.
getAlphaMDot() - Method in class org.orekit.orbits.CircularOrbit
Get the mean latitude argument derivative.
getAlphaMDot() - Method in class org.orekit.orbits.FieldCircularOrbit
Get the mean latitude argument derivative.
getAlphaV() - Method in class org.orekit.orbits.CircularOrbit
Get the true latitude argument.
getAlphaV() - Method in class org.orekit.orbits.FieldCircularOrbit
Get the true latitude argument.
getAlphaVDot() - Method in class org.orekit.orbits.CircularOrbit
Get the true latitude argument derivative.
getAlphaVDot() - Method in class org.orekit.orbits.FieldCircularOrbit
Get the true latitude argument derivative.
getAltitude() - Method in class org.orekit.bodies.FieldGeodeticPoint
Get the altitude.
getAltitude() - Method in class org.orekit.bodies.GeodeticPoint
Get the altitude.
getAltitude() - Method in class org.orekit.propagation.events.AltitudeDetector
Get the threshold altitude value.
getAltitude() - Method in class org.orekit.propagation.events.FieldAltitudeDetector
Get the threshold altitude value.
getAncestor(int) - Method in class org.orekit.frames.Frame
Get the nth ancestor of the frame.
getAngle() - Method in class org.orekit.propagation.events.PositionAngleDetector
Get the fixed angle to be crossed (radians).
getAngleType() - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData
Getter for angleType.
getAngular() - Method in class org.orekit.frames.FieldTransform
Get the underlying elementary angular part.
getAngular() - Method in class org.orekit.frames.Transform
Get the underlying elementary angular part.
getAngularVelocity() - Method in class org.orekit.utils.FieldPVCoordinates
Get the angular velocity (spin) of this point as seen from the origin.
getAngularVelocity() - Method in class org.orekit.utils.PVCoordinates
Get the angular velocity (spin) of this point as seen from the origin.
getAnomaly() - Method in class org.orekit.files.ccsds.OGMFile
Get the orbit anomaly.
getAnomaly(PositionAngle) - Method in class org.orekit.orbits.FieldKeplerianOrbit
Get the anomaly.
getAnomaly(PositionAngle) - Method in class org.orekit.orbits.KeplerianOrbit
Get the anomaly.
getAnomalyDot(PositionAngle) - Method in class org.orekit.orbits.FieldKeplerianOrbit
Get the anomaly derivative.
getAnomalyDot(PositionAngle) - Method in class org.orekit.orbits.KeplerianOrbit
Get the anomaly derivative.
getAnomalyType() - Method in class org.orekit.files.ccsds.OGMFile
Get the type of anomaly (true or mean).
getAntennaAzimuth() - Method in class org.orekit.gnss.RinexHeader
Get the azimuth of the zero direction of a fixed antenna.
getAntennaBSight() - Method in class org.orekit.gnss.RinexHeader
Get the antenna B.Sight.
getAntennaHeight() - Method in class org.orekit.gnss.RinexHeader
Get the antenna height.
getAntennaNumber() - Method in class org.orekit.gnss.RinexHeader
Get the number of the antenna.
getAntennaPhaseCenter() - Method in class org.orekit.gnss.RinexHeader
Get the antenna phasecenter.
getAntennaReferencePoint() - Method in class org.orekit.gnss.RinexHeader
Get the position of antenna reference point for antenna on vehicle.
getAntennaType() - Method in class org.orekit.gnss.RinexHeader
Get the type of the antenna.
getAntennaZeroDirection() - Method in class org.orekit.gnss.RinexHeader
Get the zero direction of antenna.
getAp(AbsoluteDate) - Method in class org.orekit.forces.drag.atmosphere.data.MarshallSolarActivityFutureEstimation
Get the Ap geomagnetic indices.
getAp(AbsoluteDate) - Method in interface org.orekit.forces.drag.atmosphere.NRLMSISE00InputParameters
Get the Ap geomagnetic indices.
getApproxPos() - Method in class org.orekit.gnss.RinexHeader
Get the Approximate Marker Position.
getArea() - Method in class org.orekit.forces.BoxAndSolarArraySpacecraft.Facet
Get facet area.
getAstronomicalAmplitudesMap() - Method in class org.orekit.forces.gravity.potential.AstronomicalAmplitudeReader
Get astronomical amplitudes map.
getAtmosphere() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTAtmosphericDrag
Get the atmospheric model.
getAttitude() - Method in class org.orekit.propagation.FieldSpacecraftState
Get the attitude.
getAttitude() - Method in class org.orekit.propagation.SpacecraftState
Get the attitude.
getAttitude(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in interface org.orekit.attitudes.AttitudeProvider
Compute the attitude corresponding to an orbital state.
getAttitude(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.AttitudesSequence
Compute the attitude corresponding to an orbital state.
getAttitude(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.CelestialBodyPointed
Compute the attitude corresponding to an orbital state.
getAttitude(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.FixedRate
Compute the attitude corresponding to an orbital state.
getAttitude(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.GroundPointing
Compute the attitude corresponding to an orbital state.
getAttitude(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.InertialProvider
Compute the attitude corresponding to an orbital state.
getAttitude(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.LofOffset
Compute the attitude corresponding to an orbital state.
getAttitude(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.LofOffsetPointing
Compute the attitude corresponding to an orbital state.
getAttitude(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.SpinStabilized
Compute the attitude corresponding to an orbital state.
getAttitude(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.TabulatedLofOffset
Compute the attitude corresponding to an orbital state.
getAttitude(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.TabulatedProvider
Compute the attitude corresponding to an orbital state.
getAttitude(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.YawCompensation
Compute the attitude corresponding to an orbital state.
getAttitude(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.YawSteering
Compute the attitude corresponding to an orbital state.
getAttitude(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.gnss.attitude.AbstractGNSSAttitudeProvider
Compute the attitude corresponding to an orbital state.
getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in interface org.orekit.attitudes.AttitudeProvider
Compute the attitude corresponding to an orbital state.
getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.AttitudesSequence
Compute the attitude corresponding to an orbital state.
getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.CelestialBodyPointed
Compute the attitude corresponding to an orbital state.
getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.FixedRate
Compute the attitude corresponding to an orbital state.
getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.GroundPointing
Compute the attitude corresponding to an orbital state.
getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.InertialProvider
Compute the attitude corresponding to an orbital state.
getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.LofOffset
Compute the attitude corresponding to an orbital state.
getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.LofOffsetPointing
Compute the attitude corresponding to an orbital state.
getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.SpinStabilized
Compute the attitude corresponding to an orbital state.
getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.TabulatedLofOffset
Compute the attitude corresponding to an orbital state.
getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.TabulatedProvider
Compute the attitude corresponding to an orbital state.
getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.YawCompensation
Compute the attitude corresponding to an orbital state.
getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.YawSteering
Compute the attitude corresponding to an orbital state.
getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.gnss.attitude.AbstractGNSSAttitudeProvider
Compute the attitude corresponding to an orbital state.
getAttitudeOverride() - Method in class org.orekit.forces.maneuvers.ConstantThrustManeuver
Get the attitude override used for the maneuver.
getAttitudeOverride() - Method in class org.orekit.forces.maneuvers.ImpulseManeuver
Get the Attitude Provider to use during maneuver.
getAttitudeProvider() - Method in class org.orekit.propagation.AbstractPropagator
Get attitude provider.
getAttitudeProvider() - Method in class org.orekit.propagation.conversion.NumericalPropagatorBuilder
Get the attitudeProvider.
getAttitudeProvider() - Method in class org.orekit.propagation.FieldAbstractPropagator
Get attitude provider.
getAttitudeProvider() - Method in interface org.orekit.propagation.FieldPropagator
Get attitude provider.
getAttitudeProvider() - Method in class org.orekit.propagation.integration.FieldStateMapper
Get the attitude provider.
getAttitudeProvider() - Method in class org.orekit.propagation.integration.StateMapper
Get the attitude provider.
getAttitudeProvider() - Method in interface org.orekit.propagation.Propagator
Get attitude provider.
getAvailableDerivatives() - Method in class org.orekit.files.ccsds.OEMFile.EphemeridesBlock
 
getAvailableDerivatives() - Method in interface org.orekit.files.general.EphemerisFile.EphemerisSegment
Get which derivatives of position are available in this ephemeris segment.
getAvailableDerivatives() - Method in class org.orekit.files.general.OrekitEphemerisFile.OrekitEphemerisSegment
 
getAvailableDerivatives() - Method in class org.orekit.files.sp3.SP3File.SP3Ephemeris
 
getAvailableSatelliteNumbers() - Method in class org.orekit.propagation.analytical.tle.TLESeries
Deprecated.
Get the available satellite numbers.
getAverageFlux(AbsoluteDate) - Method in class org.orekit.forces.drag.atmosphere.data.MarshallSolarActivityFutureEstimation
Get the value of the 81 day average of F10.7 solar flux centered on current day.
getAverageFlux(AbsoluteDate) - Method in interface org.orekit.forces.drag.atmosphere.NRLMSISE00InputParameters
Get the value of the 81 day average of F10.7 solar flux centered on current day.
getAzimuth(FieldVector3D<T>, Frame, FieldAbsoluteDate<T>) - Method in class org.orekit.frames.TopocentricFrame
Get the azimuth of a point with regards to the topocentric frame center point.
getAzimuth(Vector3D, Frame, AbsoluteDate) - Method in class org.orekit.frames.TopocentricFrame
Get the azimuth of a point with regards to the topocentric frame center point.
getB() - Method in class org.orekit.bodies.Ellipse
Get the semi minor axis.
getB() - Method in class org.orekit.bodies.Ellipsoid
Get the length of the second semi-axis.
getB() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
Get B = sqrt(1 - e²).
getBaseFrame() - Method in class org.orekit.estimation.measurements.GroundStation
Get the base frame associated with the station.
getBaseState(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.YawCompensation
Compute the base system state at given date, without compensation.
getBaseState(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.YawSteering
Compute the base system state at given date, without compensation.
getBaseState(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.YawCompensation
Compute the base system state at given date, without compensation.
getBaseState(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.YawSteering
Compute the base system state at given date, without compensation.
getBaseWeight() - Method in class org.orekit.estimation.measurements.AbstractMeasurement
Get the base weight associated with the measurement
getBaseWeight() - Method in class org.orekit.estimation.measurements.generation.AbstractMeasurementBuilder
Get the base weight associated with the measurement
getBaseWeight() - Method in interface org.orekit.estimation.measurements.ObservedMeasurement
Get the base weight associated with the measurement
getBasicDimension() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
Get state vector dimension without additional parameters.
getBasicDimension() - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator
Get state vector dimension without additional parameters.
getBDT() - Static method in class org.orekit.time.TimeScalesFactory
Get the BeiDou Navigation Satellite System time scale.
getBeacon() - Method in class org.orekit.propagation.events.AngularSeparationDetector
Get the beacon at the center of the proximity zone.
getBefore() - Method in class org.orekit.utils.FieldTimeSpanMap.Transition
Get the entry valid before transition.
getBefore() - Method in class org.orekit.utils.TimeSpanMap.Transition
Get the entry valid before transition.
getBeta() - Method in class org.orekit.models.earth.KlobucharIonoCoefficientsLoader
Returns the beta coefficients array.
getBeta() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
Get direction cosine β for central body.
getBody() - Method in class org.orekit.propagation.events.FootprintOverlapDetector
Get the body on which the geographic zone is defined.
getBody() - Method in class org.orekit.propagation.events.GeographicZoneDetector
Get the body on which the geographic zone is defined.
getBody() - Method in class org.orekit.propagation.events.LatitudeCrossingDetector
Get the body on which the geographic zone is defined.
getBody() - Method in class org.orekit.propagation.events.LatitudeExtremumDetector
Get the body on which the geographic zone is defined.
getBody() - Method in class org.orekit.propagation.events.LongitudeCrossingDetector
Get the body on which the geographic zone is defined.
getBody() - Method in class org.orekit.propagation.events.LongitudeExtremumDetector
Get the body on which the geographic zone is defined.
getBody() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBody
Get third body.
getBody(String) - Static method in class org.orekit.bodies.CelestialBodyFactory
Get a celestial body.
getBodyFrame() - Method in class org.orekit.attitudes.GroundPointing
Get the body frame.
getBodyFrame() - Method in interface org.orekit.bodies.BodyShape
Get body frame related to body shape.
getBodyFrame() - Method in class org.orekit.bodies.OneAxisEllipsoid
Get body frame related to body shape.
getBodyFrame() - Method in class org.orekit.models.earth.Geoid
 
getBodyOrientedFrame() - Method in interface org.orekit.bodies.CelestialBody
Get a body oriented, body centered frame.
getBodyShape() - Method in class org.orekit.propagation.events.AltitudeDetector
Get the body shape.
getBodyShape() - Method in class org.orekit.propagation.events.FieldAltitudeDetector
Get the body shape.
getBStar() - Method in class org.orekit.files.ccsds.OMMFile
Get the SGP/SGP4 drag-like coefficient.
getBStar() - Method in class org.orekit.propagation.analytical.tle.TLE
Get the ballistic coefficient.
getBuilder() - Method in class org.orekit.estimation.measurements.generation.AbstractScheduler
Get the measurements builder.
getC() - Method in class org.orekit.bodies.Ellipsoid
Get the length of the third semi-axis.
getC() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
Get C = 1 + p² + q².
getC2n0(int) - Method in class org.orekit.models.earth.ReferenceEllipsoid
Get the fully normalized coefficient C2n,0 for the normal gravity potential.
getCacheSlotsNumber() - Static method in class org.orekit.utils.OrekitConfiguration
Get the number of slots to use in caches.
getCalendarWeek() - Method in class org.orekit.time.DateComponents
Get the calendar week number.
getCalls() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
Get the number of calls to the differential equations computation method.
getCalls() - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator
Get the number of calls to the differential equations computation method.
getCapitalizedAbbreviation() - Method in enum org.orekit.time.Month
Get the capitalized three letters abbreviation.
getCapitalizedName() - Method in enum org.orekit.time.Month
Get the capitalized full name.
getCartesian() - Method in class org.orekit.frames.FieldTransform
Get the underlying elementary Cartesian part.
getCartesian() - Method in class org.orekit.frames.Transform
Get the underlying elementary Cartesian part.
getCartesianIntersectionPoint(FieldLine<T>, FieldVector3D<T>, Frame, FieldAbsoluteDate<T>) - Method in class org.orekit.bodies.OneAxisEllipsoid
Get the intersection point of a line with the surface of the body.
getCartesianIntersectionPoint(Line, Vector3D, Frame, AbsoluteDate) - Method in class org.orekit.bodies.OneAxisEllipsoid
Get the intersection point of a line with the surface of the body.
getCCSDSEpoch(Field<T>) - Static method in class org.orekit.time.FieldAbsoluteDate
Reference epoch for CCSDS Time Code Format (CCSDS 301.0-B-4): 1958-01-01T00:00:00 International Atomic Time (not UTC).
getCelestialBody() - Method in enum org.orekit.files.ccsds.CenterName
Get the celestial body corresponding to the CCSDS constant.
getCenter() - Method in class org.orekit.bodies.Ellipse
Get the center of the 2D ellipse.
getCenter() - Method in class org.orekit.models.earth.tessellation.Tile
Get the center point.
getCenter() - Method in class org.orekit.propagation.events.CircularFieldOfViewDetector
Get the direction of FOV center.
getCenterBody() - Method in class org.orekit.files.ccsds.ODMMetaData
Get the CelestialBody corresponding to the center name.
getCenterMass() - Method in class org.orekit.gnss.RinexHeader
Get the current center of mass of vehicle in body fixed coordinate system.
getCenterName() - Method in class org.orekit.files.ccsds.CcsdsModifiedFrame
Get the CCSDS center name.
getCenterName() - Method in class org.orekit.files.ccsds.ODMMetaData
Get the origin of reference frame.
getCenterOfCurvature(Vector2D) - Method in class org.orekit.bodies.Ellipse
Find the center of curvature (point on the evolute) at the nadir of a point.
getCentralBody() - Method in class org.orekit.propagation.events.InterSatDirectViewDetector
Get the central body.
getChildren() - Method in class org.orekit.frames.OrphanFrame
Get all children of the instance.
getCic() - Method in class org.orekit.gnss.GPSAlmanac
 
getCic() - Method in interface org.orekit.propagation.analytical.gnss.GPSOrbitalElements
Gets the Amplitude of the Cosine Harmonic Correction Term to the Angle of Inclination.
getCircularEx() - Method in class org.orekit.orbits.CircularOrbit
Get the first component of the circular eccentricity vector.
getCircularEx() - Method in class org.orekit.orbits.FieldCircularOrbit
Get the first component of the circular eccentricity vector.
getCircularExDot() - Method in class org.orekit.orbits.CircularOrbit
Get the first component of the circular eccentricity vector derivative.
getCircularExDot() - Method in class org.orekit.orbits.FieldCircularOrbit
Get the first component of the circular eccentricity vector derivative.
getCircularEy() - Method in class org.orekit.orbits.CircularOrbit
Get the second component of the circular eccentricity vector.
getCircularEy() - Method in class org.orekit.orbits.FieldCircularOrbit
Get the second component of the circular eccentricity vector.
getCircularEyDot() - Method in class org.orekit.orbits.CircularOrbit
Get the second component of the circular eccentricity vector derivative.
getCircularEyDot() - Method in class org.orekit.orbits.FieldCircularOrbit
Get the second component of the circular eccentricity vector derivative.
getCIRF(IERSConventions, boolean) - Static method in class org.orekit.frames.FramesFactory
Get the CIRF2000 reference frame.
getCis() - Method in class org.orekit.gnss.GPSAlmanac
 
getCis() - Method in interface org.orekit.propagation.analytical.gnss.GPSOrbitalElements
Gets the Amplitude of the Sine Harmonic Correction Term to the Angle of Inclination.
getCj(int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.CjSjCoefficient
Get the Cj coefficient.
getClassification() - Method in class org.orekit.propagation.analytical.tle.TLE
Get the classification.
getClassificationType() - Method in class org.orekit.files.ccsds.OMMFile
Get the classification type.
getClkOffset() - Method in class org.orekit.gnss.RinexHeader
Get the realtime-derived receiver clock offset.
getClockCorrection() - Method in class org.orekit.files.sp3.SP3File.SP3Coordinate
Returns the clock correction value.
getClockOffsetDriver() - Method in class org.orekit.estimation.measurements.GroundStation
Get a driver allowing to change station clock (which is related to measurement date).
getClockOffsetDriver() - Method in class org.orekit.estimation.measurements.ObservableSatellite
Get the clock offset parameter driver.
getClockRateChange() - Method in class org.orekit.files.sp3.SP3File.SP3Coordinate
Returns the clock rate.
getClosestTLE(AbsoluteDate) - Method in class org.orekit.propagation.analytical.tle.TLESeries
Deprecated.
Get the closest TLE to the selected date.
getCoefficients() - Method in enum org.orekit.forces.gravity.potential.OceanLoadDeformationCoefficients
Get the load deformation coefficients for ocean tides.
getCoefficients(String) - Method in class org.orekit.models.earth.displacement.OceanLoadingCoefficientsBLQFactory
Get the coefficients for a given site.
getCoefficients(AbsoluteDate, Set<String>) - Method in interface org.orekit.propagation.semianalytical.dsst.forces.ShortPeriodTerms
Computes the coefficients involved in the contributions.
getCoefficientsKeyPrefix() - Method in interface org.orekit.propagation.semianalytical.dsst.forces.ShortPeriodTerms
Get the prefix for short period coefficients keys.
getCombinedProvider(TransformProvider, TransformProvider) - Static method in class org.orekit.frames.TransformProviderUtils
Combine two transform providers.
getComment() - Method in class org.orekit.files.ccsds.ODMMetaData
Get the meta-data comment.
getComment() - Method in class org.orekit.files.ccsds.OPMFile.Maneuver
Get the maneuvers data comment, each string in the list corresponds to one line of comment.
getComment() - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData
Get the meta-data comment.
getComponents(int) - Method in class org.orekit.time.AbsoluteDate
Split the instance into date/time components for a local time.
getComponents(int) - Method in class org.orekit.time.FieldAbsoluteDate
Split the instance into date/time components for a local time.
getComponents(TimeZone) - Method in class org.orekit.time.AbsoluteDate
Split the instance into date/time components for a time zone.
getComponents(TimeZone) - Method in class org.orekit.time.FieldAbsoluteDate
Split the instance into date/time components for a time zone.
getComponents(TimeScale) - Method in class org.orekit.time.AbsoluteDate
Split the instance into date/time components.
getComponents(TimeScale) - Method in class org.orekit.time.FieldAbsoluteDate
Split the instance into date/time components.
getConstantNormalizedProvider(int, int) - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory
Get the constant gravity field coefficients provider from the first supported file.
getConstantProvider(boolean, int, int) - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
Get a time-independent provider for read spherical harmonics coefficients.
getConstantUnnormalizedProvider(int, int) - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory
Get the constant gravity field coefficients provider from the first supported file.
getConventions() - Method in class org.orekit.files.ccsds.ODMFile
Get IERS conventions.
getConventions() - Method in class org.orekit.files.ccsds.ODMParser
Get IERS conventions.
getConventions() - Method in class org.orekit.files.ccsds.TDMParser
Get IERS conventions.
getConventions() - Method in class org.orekit.frames.EOPHistory
Get the IERS conventions to which these EOP apply.
getConverter(ITRFVersion, ITRFVersion) - Static method in enum org.orekit.frames.ITRFVersion
Find a converter between specified ITRF frames.
getCoordinates() - Method in class org.orekit.files.ccsds.OEMFile.EphemeridesBlock
 
getCoordinates() - Method in interface org.orekit.files.general.EphemerisFile.EphemerisSegment
Get the coordinates for this ephemeris segment.
getCoordinates() - Method in class org.orekit.files.general.OrekitEphemerisFile.OrekitEphemerisSegment
 
getCoordinates() - Method in class org.orekit.files.sp3.SP3File.SP3Ephemeris
 
getCoordinates(SpacecraftState, int, DSFactory) - Static method in class org.orekit.estimation.measurements.AbstractMeasurement
Get Cartesian coordinates as derivatives.
getCoordinateSystem() - Method in class org.orekit.files.sp3.SP3File
Returns the coordinate system of the entries in this orbit file.
getCorrectedMeasurement() - Method in interface org.orekit.estimation.sequential.KalmanEstimation
Get the estimated measurement.
getCorrectedMeasurement() - Method in class org.orekit.estimation.sequential.Model
Get the estimated measurement.
getCorrectedSpacecraftStates() - Method in interface org.orekit.estimation.sequential.KalmanEstimation
Get the corrected spacecraft states.
getCorrectedSpacecraftStates() - Method in class org.orekit.estimation.sequential.Model
Get the corrected spacecraft states.
getCorrection() - Method in class org.orekit.gnss.RinexLoader.Parser.PhaseShiftCorrection
Get the Phase Shift Corrections.
getCorrection() - Method in class org.orekit.gnss.RinexLoader.Parser.ScaleFactorCorrection
Get the Scale Factor.
getCorrectionAngle1() - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData
Getter for the correctionAngle1.
getCorrectionAngle2() - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData
Getter for the correctionAngle2.
getCorrectionDoppler() - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData
Getter for the correctionDoppler.
getCorrectionRange() - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData
Getter for the correctionRange.
getCorrectionReceive() - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData
Getter for the correctionReceive.
getCorrectionsApplied() - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData
Getter for the correctionApplied.
getCorrectionTransmit() - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData
Getter for the correctionTransmit.
getCorrelationCoefficientsMatrix() - Method in class org.orekit.estimation.measurements.Position
Get the correlation coefficients matrix.
getCorrelationCoefficientsMatrix() - Method in class org.orekit.estimation.measurements.PV
Get the correlation coefficients matrix.
getCosparID() - Method in class org.orekit.gnss.antenna.SatelliteAntenna
Get COSPAR ID.
getCount() - Method in class org.orekit.estimation.measurements.EstimatedMeasurement
Get the evaluations counter.
getCovariance() - Method in class org.orekit.estimation.sequential.MeasurementDecorator
getCovarianceComment() - Method in class org.orekit.files.ccsds.OGMFile
Get the comment for covariance.
getCovarianceMatrices() - Method in class org.orekit.files.ccsds.OEMFile.EphemeridesBlock
Get the list of Covariance Matrices.
getCovarianceMatrix() - Method in class org.orekit.estimation.measurements.Position
Get the covariance matrix.
getCovarianceMatrix() - Method in class org.orekit.estimation.measurements.PV
Get the covariance matrix.
getCovarianceMatrix() - Method in class org.orekit.files.ccsds.OGMFile
Get the Position/Velocity covariance matrix.
getCovRefFrame() - Method in class org.orekit.files.ccsds.OGMFile
Get coordinate system for covariance matrix, for absolute frames.
getCovRefLofType() - Method in class org.orekit.files.ccsds.OGMFile
Get coordinate system for covariance matrix, for Local Orbital Frames.
getCrc() - Method in class org.orekit.gnss.GPSAlmanac
 
getCrc() - Method in interface org.orekit.propagation.analytical.gnss.GPSOrbitalElements
Gets the Amplitude of the Cosine Harmonic Correction Term to the Orbit Radius.
getCreationDate() - Method in class org.orekit.files.ccsds.ODMFile
Get the file creation date and time in UTC.
getCreationDate() - Method in class org.orekit.files.ccsds.TDMFile
Get the file creation date and time in UTC.
getCrs() - Method in class org.orekit.gnss.GPSAlmanac
 
getCrs() - Method in interface org.orekit.propagation.analytical.gnss.GPSOrbitalElements
Gets the Amplitude of the Sine Harmonic Correction Term to the Orbit Radius.
getCuc() - Method in class org.orekit.gnss.GPSAlmanac
 
getCuc() - Method in interface org.orekit.propagation.analytical.gnss.GPSOrbitalElements
Gets the Amplitude of the Cosine Harmonic Correction Term to the Argument of Latitude.
getCurrentDate() - Method in interface org.orekit.estimation.sequential.KalmanEstimation
Get the current date.
getCurrentDate() - Method in class org.orekit.estimation.sequential.KalmanEstimator
Get the current date.
getCurrentDate() - Method in class org.orekit.estimation.sequential.Model
Get the current date.
getCurrentMeasurementNumber() - Method in interface org.orekit.estimation.sequential.KalmanEstimation
Get the current measurement number.
getCurrentMeasurementNumber() - Method in class org.orekit.estimation.sequential.KalmanEstimator
Get the current measurement number.
getCurrentMeasurementNumber() - Method in class org.orekit.estimation.sequential.Model
Get the current measurement number.
getCurrentState() - Method in interface org.orekit.propagation.sampling.FieldOrekitStepInterpolator
Get the state at previous grid point date.
getCurrentState() - Method in interface org.orekit.propagation.sampling.OrekitStepInterpolator
Get the state at current grid point date.
getCurrentWeight() - Method in class org.orekit.estimation.measurements.EstimatedMeasurement
Deprecated.
as of 9.2, weight should not be changed anymore, rejected measurements are identified by their status
getCus() - Method in class org.orekit.gnss.GPSAlmanac
 
getCus() - Method in interface org.orekit.propagation.analytical.gnss.GPSOrbitalElements
Gets the Amplitude of the Sine Harmonic Correction Term to the Argument of Latitude.
getD() - Method in class org.orekit.data.DelaunayArguments
Get the mean elongation of the Moon from the Sun.
getD() - Method in class org.orekit.data.FieldDelaunayArguments
Get the mean elongation of the Moon from the Sun.
getDailyFlux(AbsoluteDate) - Method in class org.orekit.forces.drag.atmosphere.data.MarshallSolarActivityFutureEstimation
Get the value of the daily F10.7 solar flux for previous day.
getDailyFlux(AbsoluteDate) - Method in interface org.orekit.forces.drag.atmosphere.NRLMSISE00InputParameters
Get the value of the daily F10.7 solar flux for previous day.
getData() - Method in class org.orekit.utils.TimeSpanMap.Span
Get the data valid during this time span.
getDataQuality() - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData
Getter for the dataQuality.
getDataUsed() - Method in class org.orekit.files.sp3.SP3File
Returns the data used indicator from the SP3 file.
getDate() - Method in class org.orekit.attitudes.Attitude
Get the date of attitude parameters.
getDate() - Method in class org.orekit.attitudes.FieldAttitude
Get the date of attitude parameters.
getDate() - Method in class org.orekit.data.DelaunayArguments
Get the date.
getDate() - Method in class org.orekit.data.FieldDelaunayArguments
Get the date.
getDate() - Method in class org.orekit.estimation.measurements.AbstractMeasurement
Get the date.
getDate() - Method in class org.orekit.estimation.measurements.EstimatedMeasurement
Get the date.
getDate() - Method in class org.orekit.forces.maneuvers.SmallManeuverAnalyticalModel
Get the date of the maneuver.
getDate() - Method in class org.orekit.frames.EOPEntry
Get the date.
getDate() - Method in class org.orekit.frames.FieldTransform
Get the date.
getDate() - Method in class org.orekit.frames.Transform
Get the date.
getDate() - Method in class org.orekit.gnss.DOP
Gets the calculation date of the DOP.
getDate() - Method in class org.orekit.gnss.GPSAlmanac
 
getDate() - Method in class org.orekit.gnss.ObservationDataSet
Get the date.
getDate() - Method in class org.orekit.orbits.FieldOrbit
Get the date of orbital parameters.
getDate() - Method in class org.orekit.orbits.Orbit
Get the date of orbital parameters.
getDate() - Method in class org.orekit.propagation.analytical.tle.TLE
Get the TLE current date.
getDate() - Method in class org.orekit.propagation.events.DateDetector
Get the current event date according to the propagator.
getDate() - Method in class org.orekit.propagation.events.FieldDateDetector
Get the current event date according to the propagator.
getDate() - Method in class org.orekit.propagation.FieldSpacecraftState
Get the date.
getDate() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
Get the date of the orbit.
getDate() - Method in class org.orekit.propagation.SpacecraftState
Get the date.
getDate() - Method in class org.orekit.time.AbsoluteDate
Get the date.
getDate() - Method in class org.orekit.time.DateTimeComponents
Get the date component.
getDate() - Method in class org.orekit.time.FieldAbsoluteDate
Get the date.
getDate() - Method in interface org.orekit.time.FieldTimeStamped
Get the date.
getDate() - Method in class org.orekit.time.GPSDate
Get the date.
getDate() - Method in interface org.orekit.time.TimeStamped
Get the date.
getDate() - Method in class org.orekit.utils.FieldTimeSpanMap.Transition
Get the transition absolute date.
getDate() - Method in class org.orekit.utils.TimeSpanMap.Transition
Get the transition date.
getDate() - Method in class org.orekit.utils.TimeStampedAngularCoordinates
Get the date.
getDate() - Method in class org.orekit.utils.TimeStampedFieldAngularCoordinates
Get the date.
getDate() - Method in class org.orekit.utils.TimeStampedFieldPVCoordinates
Get the date.
getDate() - Method in class org.orekit.utils.TimeStampedPVCoordinates
Get the date.
getDay() - Method in class org.orekit.time.DateComponents
Get the day.
getDayFraction() - Method in class org.orekit.files.sp3.SP3File
Returns the day fraction for this SP3 file.
getDayOfWeek() - Method in class org.orekit.time.DateComponents
Get the day of week.
getDayOfYear() - Method in class org.orekit.time.DateComponents
Get the day number in year.
getDcjDh(int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.CjSjCoefficient
Get the dCj / dh coefficient.
getDcjDk(int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.CjSjCoefficient
Get the dCj / dk coefficient.
getDdEps() - Method in class org.orekit.frames.EOPEntry
Get the correction for nutation in obliquity δΔε.
getDDot() - Method in class org.orekit.data.DelaunayArguments
Get the mean elongation of the Moon from the Sun time derivative.
getDDot() - Method in class org.orekit.data.FieldDelaunayArguments
Get the mean elongation of the Moon from the Sun time derivative.
getDdPsi() - Method in class org.orekit.frames.EOPEntry
Get the correction for nutation in longitude δΔΨ.
getDecimalYear(int, int, int) - Static method in class org.orekit.models.earth.GeoMagneticField
Utility function to get a decimal year for a given day.
getDeclination() - Method in class org.orekit.models.earth.GeoMagneticElements
Returns the declination of the magnetic field in degrees.
getDecreasingTimeShift() - Method in class org.orekit.propagation.events.EventShifter
Get the decreasing events time shift.
getDefaultModel() - Static method in class org.orekit.models.earth.FixedTroposphericDelay
Returns the default model, loading delay values from the file "tropospheric-delay.txt".
getDelaunayMultipliers() - Method in class org.orekit.models.earth.displacement.Tide
Get the multipliers for Delaunay arguments (l, l', F, D, Ω).
getDeltaMass() - Method in class org.orekit.files.ccsds.OPMFile.Maneuver
Get mass change during maneuver (value is < 0).
getDeltaVSat() - Method in class org.orekit.forces.maneuvers.ImpulseManeuver
Get the velocity increment in satellite frame.
getDensity(double, double, double, double, double, double, double, double, double, double, double, double, double, double, double) - Method in class org.orekit.forces.drag.atmosphere.JB2008
Get the local density with initial entries.
getDensity(int) - Method in class org.orekit.forces.drag.atmosphere.NRLMSISE00.FieldOutput
Get one of the stored densities.
getDensity(int, double, double, double, double, double, double, double, double) - Method in class org.orekit.forces.drag.atmosphere.DTM2000
Get the local density with initial entries.
getDensity(int, T, T, T, T, double, double, double, double) - Method in class org.orekit.forces.drag.atmosphere.DTM2000
Get the local density with initial entries.
getDensity(Vector3D, FieldVector3D<T>) - Method in class org.orekit.forces.drag.atmosphere.HarrisPriester
Get the local density.
getDensity(Vector3D, Vector3D) - Method in class org.orekit.forces.drag.atmosphere.HarrisPriester
Get the local density.
getDensity(AbsoluteDate, Vector3D, Frame) - Method in interface org.orekit.forces.drag.atmosphere.Atmosphere
Get the local density.
getDensity(AbsoluteDate, Vector3D, Frame) - Method in class org.orekit.forces.drag.atmosphere.DTM2000
Get the local density.
getDensity(AbsoluteDate, Vector3D, Frame) - Method in class org.orekit.forces.drag.atmosphere.HarrisPriester
Get the local density at some position.
getDensity(AbsoluteDate, Vector3D, Frame) - Method in class org.orekit.forces.drag.atmosphere.JB2008
Get the local density.
getDensity(AbsoluteDate, Vector3D, Frame) - Method in class org.orekit.forces.drag.atmosphere.NRLMSISE00
Get the local density.
getDensity(AbsoluteDate, Vector3D, Frame) - Method in class org.orekit.forces.drag.atmosphere.SimpleExponentialAtmosphere
Get the local density.
getDensity(FieldAbsoluteDate<T>, FieldVector3D<T>, Frame) - Method in interface org.orekit.forces.drag.atmosphere.Atmosphere
Get the local density.
getDensity(FieldAbsoluteDate<T>, FieldVector3D<T>, Frame) - Method in class org.orekit.forces.drag.atmosphere.DTM2000
Get the local density.
getDensity(FieldAbsoluteDate<T>, FieldVector3D<T>, Frame) - Method in class org.orekit.forces.drag.atmosphere.HarrisPriester
Get the local density at some position.
getDensity(FieldAbsoluteDate<T>, FieldVector3D<T>, Frame) - Method in class org.orekit.forces.drag.atmosphere.JB2008
Get the local density.
getDensity(FieldAbsoluteDate<T>, FieldVector3D<T>, Frame) - Method in class org.orekit.forces.drag.atmosphere.NRLMSISE00
Get the local density.
getDensity(FieldAbsoluteDate<T>, FieldVector3D<T>, Frame) - Method in class org.orekit.forces.drag.atmosphere.SimpleExponentialAtmosphere
 
getDensity(T, T, T, T, T, T, double, double, double, double, double, double, double, double, double) - Method in class org.orekit.forces.drag.atmosphere.JB2008
Get the local density with initial entries.
getDepth() - Method in class org.orekit.frames.Frame
Get the depth of the frame.
getDerivative(int, double) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenTesseralLinear
Compute the value of the derivative dKj-n-1, s / de².
getDerivative(int, double) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenThirdBodyLinear
Compute the value of the Hansen coefficient dK₀n, s / dΧ.
getDerivative(int, double) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenZonalLinear
Get the dK₀-n-1,s / dΧ coefficient derivative.
getDerivative(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GammaMnsFunction
Get Γ function derivative.
getDerivativesDrivers() - Method in class org.orekit.estimation.measurements.EstimatedMeasurement
Get all the drivers with set derivatives.
getDestination() - Method in enum org.orekit.frames.HelmertTransformation.Predefined
Get the destination ITRF.
getDestination() - Method in class org.orekit.frames.ITRFVersion.Converter
Get the destination ITRF.
getDetector() - Method in class org.orekit.propagation.events.AdapterDetector
Get the wrapped detector.
getDetector() - Method in class org.orekit.propagation.events.handlers.RecordAndContinue.Event
Get the detector.
getdGjsdAlpha(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
Get the dGjs / dα coefficient.
getdGjsdBeta(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
Get the dGjs / dβ coefficient.
getdGjsdh(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
Get the dGjs / dh coefficient.
getdGjsdk(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
Get the dGjs / dk coefficient.
getdGmsdAlpha(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHmsjPolynomials
Get the dGmsj / dα coefficient.
getdGmsdBeta(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHmsjPolynomials
Get the dGmsj / dβ coefficient.
getdGmsdh(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHmsjPolynomials
Get the dGmsj / dh coefficient.
getdGmsdk(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHmsjPolynomials
Get the dGmsj / dk coefficient.
getdHjsdAlpha(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
Get the dHjs / dα coefficient.
getdHjsdBeta(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
Get the dHjs / dβ coefficient.
getdHjsdh(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
Get the dHjs / dh coefficient.
getdHjsdk(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
Get the dHjs / dk coefficient.
getdHmsdAlpha(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHmsjPolynomials
Get the dHmsj / dα coefficient.
getdHmsdBeta(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHmsjPolynomials
Get the dHmsj / dβ coefficient.
getdHmsdh(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHmsjPolynomials
Get the dHmsj / dh coefficient.
getdHmsdk(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHmsjPolynomials
Get the dHmsj / dk coefficient.
getdIjsdAlpha(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
Get the dIjs / dα coefficient.
getdIjsdBeta(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
Get the dIjs / dβ coefficient.
getdIjsdh(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
Get the dIjs / dh coefficient.
getdIjsdk(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
Get the dIjs / dk coefficient.
getDimension() - Method in class org.orekit.estimation.measurements.AbstractMeasurement
Get the dimension of the measurement.
getDimension() - Method in interface org.orekit.estimation.measurements.ObservedMeasurement
Get the dimension of the measurement.
getDirection() - Method in class org.orekit.forces.maneuvers.ConstantThrustManeuver
Get the direction.
getDisplacements() - Method in class org.orekit.estimation.measurements.GroundStation
Get the displacement models.
getdJjsdAlpha(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
Get the dJjs / dα coefficient.
getdJjsdBeta(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
Get the dJjs / dβ coefficient.
getdJjsdh(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
Get the dJjs / dh coefficient.
getdJjsdk(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
Get the dJjs / dk coefficient.
getdLnsdGamma(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.LnsCoefficients
Get the value of dLns / dγ (γ).
getDnl(double, double, int, int) - Static method in class org.orekit.propagation.semianalytical.dsst.utilities.UpperBounds
Get the upper bound value Dnl(Χ).
getDoodson() - Method in class org.orekit.forces.gravity.potential.OceanTidesWave
Get the Doodson number for the wave.
getDoodsonMultipliers() - Method in class org.orekit.models.earth.displacement.Tide
Get the multipliers for Doodson arguments (τ, s, h, p, N', ps).
getDoodsonNumber() - Method in class org.orekit.models.earth.displacement.Tide
Get the Doodson number.
getDragArea() - Method in class org.orekit.files.ccsds.OGMFile
Get the drag area.
getDragCoeff() - Method in class org.orekit.files.ccsds.OGMFile
Get the drag coefficient.
getDragParametersDrivers() - Method in class org.orekit.forces.BoxAndSolarArraySpacecraft
Get the drivers for supported parameters.
getDragParametersDrivers() - Method in interface org.orekit.forces.drag.DragSensitive
Get the drivers for supported parameters.
getDragParametersDrivers() - Method in class org.orekit.forces.drag.IsotropicDrag
Get the drivers for supported parameters.
getDrivers() - Method in class org.orekit.utils.ParameterDriversList
Get delegating drivers for all parameters.
getDrivers(double, Orbit, PositionAngle) - Method in enum org.orekit.orbits.OrbitType
Get parameters drivers initialized from a reference orbit.
getDsjDh(int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.CjSjCoefficient
Get the dSj / dh coefficient.
getDsjDk(int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.CjSjCoefficient
Get the dSj / dk coefficient.
getDSTDTC(AbsoluteDate) - Method in interface org.orekit.forces.drag.atmosphere.JB2008InputParameters
Get the temperature change computed from Dst index.
getDuration() - Method in class org.orekit.files.ccsds.OPMFile.Maneuver
Get duration (value is 0 for impulsive maneuver).
getDuration() - Method in class org.orekit.forces.maneuvers.ConstantThrustManeuver
Get the duration of the maneuver (s).
getDV() - Method in class org.orekit.files.ccsds.OPMFile.Maneuver
Get velocity increment.
getDx() - Method in class org.orekit.frames.EOPEntry
Get the correction for Celestial Intermediate Pole (CIP) coordinates.
getDy() - Method in class org.orekit.frames.EOPEntry
Get the correction for Celestial Intermediate Pole (CIP) coordinates.
getE() - Method in class org.orekit.files.ccsds.OGMFile
Get the orbit eccentricity.
getE() - Method in class org.orekit.gnss.GPSAlmanac
 
getE() - Method in class org.orekit.orbits.CartesianOrbit
Get the eccentricity.
getE() - Method in class org.orekit.orbits.CircularOrbit
Get the eccentricity.
getE() - Method in class org.orekit.orbits.EquinoctialOrbit
Get the eccentricity.
getE() - Method in class org.orekit.orbits.FieldCartesianOrbit
Get the eccentricity.
getE() - Method in class org.orekit.orbits.FieldCircularOrbit
Get the eccentricity.
getE() - Method in class org.orekit.orbits.FieldEquinoctialOrbit
Get the eccentricity.
getE() - Method in class org.orekit.orbits.FieldKeplerianOrbit
Get the eccentricity.
getE() - Method in class org.orekit.orbits.FieldOrbit
Get the eccentricity.
getE() - Method in class org.orekit.orbits.KeplerianOrbit
Get the eccentricity.
getE() - Method in class org.orekit.orbits.Orbit
Get the eccentricity.
getE() - Method in interface org.orekit.propagation.analytical.gnss.GPSOrbitalElements
Gets the Eccentricity.
getE() - Method in class org.orekit.propagation.analytical.tle.TLE
Get the eccentricity.
getE() - Method in class org.orekit.propagation.FieldSpacecraftState
Get the eccentricity.
getE() - Method in class org.orekit.propagation.SpacecraftState
Get the eccentricity.
getEarliest() - Method in class org.orekit.utils.GenericTimeStampedCache
Get the earliest cached entry.
getEarliest() - Method in class org.orekit.utils.ImmutableTimeStampedCache
 
getEarliest() - Method in interface org.orekit.utils.TimeStampedCache
Get the earliest entry in this cache.
getEarth() - Static method in class org.orekit.bodies.CelestialBodyFactory
Get the Earth singleton body.
getEarthMoonBarycenter() - Static method in class org.orekit.bodies.CelestialBodyFactory
Get the Earth-Moon barycenter singleton bodies pair.
getEarthOrientationAngleFunction(TimeScale) - Method in enum org.orekit.utils.IERSConventions
Get the function computing the raw Earth Orientation Angle.
getEast() - Method in class org.orekit.bodies.FieldGeodeticPoint
Get the direction to the east of point, expressed in parent shape frame.
getEast() - Method in class org.orekit.bodies.GeodeticPoint
Get the direction to the east of point, expressed in parent shape frame.
getEast() - Method in class org.orekit.frames.TopocentricFrame
Get the east direction of topocentric frame, expressed in parent shape frame.
getEastOffsetDriver() - Method in class org.orekit.estimation.measurements.GroundStation
Get a driver allowing to change station position along East axis.
getEcc() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
Get the eccentricity.
getEccentricAnomaly() - Method in class org.orekit.orbits.FieldKeplerianOrbit
Get the eccentric anomaly.
getEccentricAnomaly() - Method in class org.orekit.orbits.KeplerianOrbit
Get the eccentric anomaly.
getEccentricAnomalyDot() - Method in class org.orekit.orbits.FieldKeplerianOrbit
Get the eccentric anomaly derivative.
getEccentricAnomalyDot() - Method in class org.orekit.orbits.KeplerianOrbit
Get the eccentric anomaly derivative.
getEccentricities() - Method in class org.orekit.gnss.antenna.FrequencyPattern
Get the phase center eccentricities.
getEccentricities() - Method in class org.orekit.gnss.RinexHeader
Get the eccentricities of antenna center.
getEccentricities(Frequency) - Method in class org.orekit.gnss.antenna.Antenna
Get the phase center eccentricities.
getECEF() - Method in class org.orekit.propagation.analytical.gnss.GPSPropagator
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(double) - Method in class org.orekit.utils.ElevationMask
Get the interpolated elevation for a given azimuth according to the mask.
getElevation(FieldVector3D<T>, Frame, FieldAbsoluteDate<T>) - Method in class org.orekit.frames.TopocentricFrame
Get the elevation of a point with regards to the local point.
getElevation(Vector3D, Frame, AbsoluteDate) - Method in class org.orekit.frames.TopocentricFrame
Get the elevation of a point with regards to the local point.
getElevation(SpacecraftState) - Method in class org.orekit.propagation.events.ElevationExtremumDetector
Get the elevation value.
getElevationMask() - Method in class org.orekit.gnss.DOPComputer
Get the elevation mask.
getElevationMask() - Method in class org.orekit.propagation.events.ElevationDetector
Returns the currently configured elevation mask.
getElevationMask() - Method in class org.orekit.propagation.events.FieldElevationDetector
Returns the currently configured elevation mask.
getEllipsoid() - Method in interface org.orekit.models.earth.EarthShape
Get the underlying ellipsoid model that defines latitude and longitude.
getEllipsoid() - Method in class org.orekit.models.earth.Geoid
 
getEllipsoid() - Method in class org.orekit.models.earth.ReferenceEllipsoid
 
getEME2000() - Static method in class org.orekit.frames.FramesFactory
Get the unique EME2000 frame.
getEnd() - Method in class org.orekit.estimation.measurements.generation.AbstractMeasurementBuilder
Get the end of the measurements time span.
getEnd() - Method in class org.orekit.utils.TimeSpanMap.Span
Get the end of this time span.
getEndDate() - Method in class org.orekit.forces.maneuvers.ConstantThrustManeuver
Get the end date.
getEndDate() - Method in class org.orekit.frames.EOPHistory
Get the date of the last available Earth Orientation Parameters.
getEntries() - Method in class org.orekit.frames.EOPHistory
Get a non-modifiable view of the EOP entries.
getEntries() - Method in class org.orekit.utils.GenericTimeStampedCache
Get the total number of entries cached.
getEOPHistory() - Method in interface org.orekit.frames.EOPBasedTransformProvider
Get the EOP history.
getEOPHistory() - Method in class org.orekit.frames.GTODProvider
Get the EOP history.
getEOPHistory() - Method in class org.orekit.time.UT1Scale
Get the EOP history.
getEOPHistory(IERSConventions, boolean) - Static method in class org.orekit.frames.FramesFactory
Get Earth Orientation Parameters history.
getEOPTidalCorrection() - Method in enum org.orekit.utils.IERSConventions
Get the function computing tidal corrections for Earth Orientation Parameters.
getEphemeridesBlocks() - Method in class org.orekit.files.ccsds.OEMFile
Get the list of ephemerides blocks as an unmodifiable list.
getEphemeridesDataLinesComment() - Method in class org.orekit.files.ccsds.OEMFile.EphemeridesBlock
Get the ephemerides data lines comment.
getEphemerisType() - Method in class org.orekit.files.ccsds.OMMFile
Get the ephemeris type.
getEphemerisType() - Method in class org.orekit.propagation.analytical.tle.TLE
Get the type of ephemeris.
getEpoch() - Method in class org.orekit.files.ccsds.OEMFile.CovarianceMatrix
Get the epoch relative to the covariance matrix.
getEpoch() - Method in class org.orekit.files.ccsds.OGMFile
Get epoch of state vector, Keplerian elements and covariance matrix data.
getEpoch() - Method in class org.orekit.files.ccsds.TDMFile.Observation
Getter for the epoch.
getEpoch() - Method in class org.orekit.files.sp3.SP3File
Returns the start epoch of the orbit file.
getEpoch() - Method in class org.orekit.frames.HelmertTransformation
Get the reference epoch of the transform.
getEpoch() - Method in class org.orekit.models.earth.GeoMagneticField
Returns the epoch for this magnetic field model.
getEpochComment() - Method in class org.orekit.files.ccsds.OGMFile
Get the comment for epoch.
getEpochIgnition() - Method in class org.orekit.files.ccsds.OPMFile.Maneuver
Get epoch ignition.
getEpochInterval() - Method in class org.orekit.files.sp3.SP3File
Returns the time interval between epochs (in seconds).
getEquatorialRadius() - Method in class org.orekit.bodies.OneAxisEllipsoid
Get the equatorial radius of the body.
getEquatorialRadius() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTSolarRadiationPressure
Get the central body equatorial radius.
getEquinoctialEx() - Method in class org.orekit.orbits.CartesianOrbit
Get the first component of the equinoctial eccentricity vector derivative.
getEquinoctialEx() - Method in class org.orekit.orbits.CircularOrbit
Get the first component of the equinoctial eccentricity vector derivative.
getEquinoctialEx() - Method in class org.orekit.orbits.EquinoctialOrbit
Get the first component of the equinoctial eccentricity vector derivative.
getEquinoctialEx() - Method in class org.orekit.orbits.FieldCartesianOrbit
Get the first component of the equinoctial eccentricity vector.
getEquinoctialEx() - Method in class org.orekit.orbits.FieldCircularOrbit
Get the first component of the equinoctial eccentricity vector.
getEquinoctialEx() - Method in class org.orekit.orbits.FieldEquinoctialOrbit
Get the first component of the equinoctial eccentricity vector.
getEquinoctialEx() - Method in class org.orekit.orbits.FieldKeplerianOrbit
Get the first component of the equinoctial eccentricity vector.
getEquinoctialEx() - Method in class org.orekit.orbits.FieldOrbit
Get the first component of the equinoctial eccentricity vector.
getEquinoctialEx() - Method in class org.orekit.orbits.KeplerianOrbit
Get the first component of the equinoctial eccentricity vector derivative.
getEquinoctialEx() - Method in class org.orekit.orbits.Orbit
Get the first component of the equinoctial eccentricity vector derivative.
getEquinoctialEx() - Method in class org.orekit.propagation.FieldSpacecraftState
Get the first component of the eccentricity vector (as per equinoctial parameters).
getEquinoctialEx() - Method in class org.orekit.propagation.SpacecraftState
Get the first component of the eccentricity vector (as per equinoctial parameters).
getEquinoctialExDot() - Method in class org.orekit.orbits.CartesianOrbit
Get the first component of the equinoctial eccentricity vector.
getEquinoctialExDot() - Method in class org.orekit.orbits.CircularOrbit
Get the first component of the equinoctial eccentricity vector.
getEquinoctialExDot() - Method in class org.orekit.orbits.EquinoctialOrbit
Get the first component of the equinoctial eccentricity vector.
getEquinoctialExDot() - Method in class org.orekit.orbits.FieldCartesianOrbit
Get the first component of the equinoctial eccentricity vector.
getEquinoctialExDot() - Method in class org.orekit.orbits.FieldCircularOrbit
Get the first component of the equinoctial eccentricity vector.
getEquinoctialExDot() - Method in class org.orekit.orbits.FieldEquinoctialOrbit
Get the first component of the equinoctial eccentricity vector.
getEquinoctialExDot() - Method in class org.orekit.orbits.FieldKeplerianOrbit
Get the first component of the equinoctial eccentricity vector.
getEquinoctialExDot() - Method in class org.orekit.orbits.FieldOrbit
Get the first component of the equinoctial eccentricity vector.
getEquinoctialExDot() - Method in class org.orekit.orbits.KeplerianOrbit
Get the first component of the equinoctial eccentricity vector.
getEquinoctialExDot() - Method in class org.orekit.orbits.Orbit
Get the first component of the equinoctial eccentricity vector.
getEquinoctialEy() - Method in class org.orekit.orbits.CartesianOrbit
Get the second component of the equinoctial eccentricity vector derivative.
getEquinoctialEy() - Method in class org.orekit.orbits.CircularOrbit
Get the second component of the equinoctial eccentricity vector derivative.
getEquinoctialEy() - Method in class org.orekit.orbits.EquinoctialOrbit
Get the second component of the equinoctial eccentricity vector derivative.
getEquinoctialEy() - Method in class org.orekit.orbits.FieldCartesianOrbit
Get the second component of the equinoctial eccentricity vector.
getEquinoctialEy() - Method in class org.orekit.orbits.FieldCircularOrbit
Get the second component of the equinoctial eccentricity vector.
getEquinoctialEy() - Method in class org.orekit.orbits.FieldEquinoctialOrbit
Get the second component of the equinoctial eccentricity vector.
getEquinoctialEy() - Method in class org.orekit.orbits.FieldKeplerianOrbit
Get the second component of the equinoctial eccentricity vector.
getEquinoctialEy() - Method in class org.orekit.orbits.FieldOrbit
Get the second component of the equinoctial eccentricity vector.
getEquinoctialEy() - Method in class org.orekit.orbits.KeplerianOrbit
Get the second component of the equinoctial eccentricity vector derivative.
getEquinoctialEy() - Method in class org.orekit.orbits.Orbit
Get the second component of the equinoctial eccentricity vector derivative.
getEquinoctialEy() - Method in class org.orekit.propagation.FieldSpacecraftState
Get the second component of the eccentricity vector (as per equinoctial parameters).
getEquinoctialEy() - Method in class org.orekit.propagation.SpacecraftState
Get the second component of the eccentricity vector (as per equinoctial parameters).
getEquinoctialEyDot() - Method in class org.orekit.orbits.CartesianOrbit
Get the second component of the equinoctial eccentricity vector.
getEquinoctialEyDot() - Method in class org.orekit.orbits.CircularOrbit
Get the second component of the equinoctial eccentricity vector.
getEquinoctialEyDot() - Method in class org.orekit.orbits.EquinoctialOrbit
Get the second component of the equinoctial eccentricity vector.
getEquinoctialEyDot() - Method in class org.orekit.orbits.FieldCartesianOrbit
Get the second component of the equinoctial eccentricity vector.
getEquinoctialEyDot() - Method in class org.orekit.orbits.FieldCircularOrbit
Get the second component of the equinoctial eccentricity vector.
getEquinoctialEyDot() - Method in class org.orekit.orbits.FieldEquinoctialOrbit
Get the second component of the equinoctial eccentricity vector.
getEquinoctialEyDot() - Method in class org.orekit.orbits.FieldKeplerianOrbit
Get the second component of the equinoctial eccentricity vector.
getEquinoctialEyDot() - Method in class org.orekit.orbits.FieldOrbit
Get the second component of the equinoctial eccentricity vector.
getEquinoctialEyDot() - Method in class org.orekit.orbits.KeplerianOrbit
Get the second component of the equinoctial eccentricity vector.
getEquinoctialEyDot() - Method in class org.orekit.orbits.Orbit
Get the second component of the equinoctial eccentricity vector.
getEquinoxNutationCorrection(AbsoluteDate) - Method in class org.orekit.frames.EOPHistory
Get the correction to the nutation parameters for equinox-based paradigm.
getEquinoxNutationCorrection(FieldAbsoluteDate<T>) - Method in class org.orekit.frames.EOPHistory
Get the correction to the nutation parameters for equinox-based paradigm.
getEstimate() - Method in class org.orekit.estimation.sequential.Model
Get the current corrected estimate.
getEstimatedEarthFrame() - Method in class org.orekit.estimation.measurements.GroundStation
Get the estimated Earth frame, including the estimated linear models for pole and prime meridian.
getEstimatedMeasurement(int) - Method in interface org.orekit.estimation.measurements.EstimationsProvider
Get one estimated measurement.
getEstimatedMeasurementsParameters() - Method in interface org.orekit.estimation.sequential.KalmanEstimation
Get the list of estimated measurements parameters.
getEstimatedMeasurementsParameters() - Method in class org.orekit.estimation.sequential.KalmanEstimator
Get the list of estimated measurements parameters.
getEstimatedMeasurementsParameters() - Method in class org.orekit.estimation.sequential.Model
Get the list of estimated measurements parameters.
getEstimatedOrbitalParameters() - Method in interface org.orekit.estimation.sequential.KalmanEstimation
Get the list of estimated orbital parameters.
getEstimatedOrbitalParameters() - Method in class org.orekit.estimation.sequential.Model
Get the list of estimated orbital parameters.
getEstimatedPropagationParameters() - Method in interface org.orekit.estimation.sequential.KalmanEstimation
Get the list of estimated propagation parameters.
getEstimatedPropagationParameters() - Method in class org.orekit.estimation.sequential.Model
Get the list of estimated propagation parameters.
getEstimatedPropagators() - Method in class org.orekit.estimation.sequential.Model
Get the propagators estimated with the values set in the propagators builders.
getEstimatedUT1() - Method in class org.orekit.estimation.measurements.EstimatedEarthFrameProvider
Get the estimated UT1 time scale.
getEstimatedUT1() - Method in class org.orekit.estimation.measurements.GroundStation
Get the estimated UT1 scale, including the estimated linear models for prime meridian.
getEstimatedValue() - Method in class org.orekit.estimation.measurements.EstimatedMeasurement
Get the estimated value.
getEvaluations() - Method in class org.orekit.propagation.conversion.AbstractPropagatorConverter
Get the number of objective function evaluations.
getEvaluationsCount() - Method in class org.orekit.estimation.leastsquares.BatchLSEstimator
Get the number of evaluations used for last estimation.
getEventDate() - Method in class org.orekit.propagation.events.EventState
Get the occurrence time of the event triggered in the current step.
getEventDate() - Method in class org.orekit.propagation.events.FieldEventState
Get the occurrence time of the event triggered in the current step.
getEventDetector() - Method in class org.orekit.propagation.events.EventsLogger.LoggedEvent
Get the event detector triggered.
getEventDetector() - Method in class org.orekit.propagation.events.EventState
Get the underlying event detector.
getEventDetector() - Method in class org.orekit.propagation.events.FieldEventsLogger.FieldLoggedEvent
Get the event detector triggered.
getEventDetector() - Method in class org.orekit.propagation.events.FieldEventState
Get the underlying event detector.
getEvents() - Method in class org.orekit.propagation.events.handlers.RecordAndContinue
Get the events passed to this handler.
getEventsDetectors() - Method in class org.orekit.forces.AbstractParametricAcceleration
Get the discrete events related to the model.
getEventsDetectors() - Method in class org.orekit.forces.drag.DragForce
Get the discrete events related to the model.
getEventsDetectors() - Method in interface org.orekit.forces.ForceModel
Get the discrete events related to the model.
getEventsDetectors() - Method in class org.orekit.forces.gravity.HolmesFeatherstoneAttractionModel
Get the discrete events related to the model.
getEventsDetectors() - Method in class org.orekit.forces.gravity.NewtonianAttraction
Get the discrete events related to the model.
getEventsDetectors() - Method in class org.orekit.forces.gravity.OceanTides
Get the discrete events related to the model.
getEventsDetectors() - Method in class org.orekit.forces.gravity.Relativity
Get the discrete events related to the model.
getEventsDetectors() - Method in class org.orekit.forces.gravity.SolidTides
Get the discrete events related to the model.
getEventsDetectors() - Method in class org.orekit.forces.gravity.ThirdBodyAttraction
Get the discrete events related to the model.
getEventsDetectors() - Method in class org.orekit.forces.maneuvers.ConstantThrustManeuver
Get the discrete events related to the model.
getEventsDetectors() - Method in class org.orekit.forces.radiation.SolarRadiationPressure
Get the discrete events related to the model.
getEventsDetectors() - Method in class org.orekit.propagation.AbstractPropagator
Get all the events detectors that have been added.
getEventsDetectors() - Method in class org.orekit.propagation.analytical.AbstractAnalyticalPropagator
Get all the events detectors that have been added.
getEventsDetectors() - Method in class org.orekit.propagation.analytical.FieldAbstractAnalyticalPropagator
Get all the events detectors that have been added.
getEventsDetectors() - Method in class org.orekit.propagation.FieldAbstractPropagator
Get all the events detectors that have been added.
getEventsDetectors() - Method in interface org.orekit.propagation.FieldPropagator
Get all the events detectors that have been added.
getEventsDetectors() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
Get all the events detectors that have been added.
getEventsDetectors() - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator
Get all the events detectors that have been added.
getEventsDetectors() - Method in interface org.orekit.propagation.Propagator
Get all the events detectors that have been added.
getEventsDetectors() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTAtmosphericDrag
Get the discrete events related to the model.
getEventsDetectors() - Method in interface org.orekit.propagation.semianalytical.dsst.forces.DSSTForceModel
Get the discrete events related to the model.
getEventsDetectors() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTSolarRadiationPressure
Get the discrete events related to the model.
getEventsDetectors() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseral
Get the discrete events related to the model.
getEventsDetectors() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBody
Get the discrete events related to the model.
getEventsDetectors() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonal
Get the discrete events related to the model.
getEvolution(double, RealVector, MeasurementDecorator) - Method in class org.orekit.estimation.sequential.Model
getException() - Method in exception org.orekit.errors.OrekitExceptionWrapper
Deprecated.
Get the wrapped exception.
getExtrapolationThreshold() - Method in class org.orekit.propagation.analytical.Ephemeris
Get the maximum timespan outside of the stored ephemeris that is allowed for extrapolation.
getF() - Method in class org.orekit.data.DelaunayArguments
Get L - Ω where L is the mean longitude of the Moon.
getF() - Method in class org.orekit.data.FieldDelaunayArguments
Get L - Ω where L is the mean longitude of the Moon.
getF10(AbsoluteDate) - Method in interface org.orekit.forces.drag.atmosphere.JB2008InputParameters
Get the value of the instantaneous solar flux index (1e-22*Watt/(m²*Hertz)).
getF10B(AbsoluteDate) - Method in interface org.orekit.forces.drag.atmosphere.JB2008InputParameters
Get the value of the mean solar flux.
getFactoryKey() - Method in class org.orekit.frames.FactoryManagedFrame
Get the key of the frame within the factory.
getFDot() - Method in class org.orekit.data.DelaunayArguments
Get L - Ω where L is the mean longitude of the Moon time derivative.
getFDot() - Method in class org.orekit.data.FieldDelaunayArguments
Get L - Ω where L is the mean longitude of the Moon time derivative.
getField() - Method in class org.orekit.propagation.FieldAbstractPropagator
Field getter.
getField() - Method in class org.orekit.time.FieldAbsoluteDate
Get the field.
getField(GeoMagneticFieldFactory.FieldModel, double) - Static method in class org.orekit.models.earth.GeoMagneticFieldFactory
Get the GeoMagneticField for the given model type and year.
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() - Method in class org.orekit.files.ccsds.ODMMetaData
Get the reference frame in which data are given: used for state vector and Keplerian elements data (and for the covariance reference frame if none is given).
getFrame() - Method in class org.orekit.files.ccsds.OEMFile.CovarianceMatrix
Get coordinate system for covariance matrix, for absolute frames.
getFrame() - Method in class org.orekit.files.ccsds.OEMFile.EphemeridesBlock
 
getFrame() - Method in interface org.orekit.files.general.EphemerisFile.EphemerisSegment
Get the reference frame for this ephemeris segment.
getFrame() - Method in class org.orekit.files.general.OrekitEphemerisFile.OrekitEphemerisSegment
 
getFrame() - Method in class org.orekit.files.sp3.SP3File.SP3Ephemeris
 
getFrame() - Method in interface org.orekit.forces.drag.atmosphere.Atmosphere
Get the frame of the central body.
getFrame() - Method in class org.orekit.forces.drag.atmosphere.DTM2000
Get the frame of the central body.
getFrame() - Method in class org.orekit.forces.drag.atmosphere.HarrisPriester
Get the frame of the central body.
getFrame() - Method in class org.orekit.forces.drag.atmosphere.JB2008
Get the frame of the central body.
getFrame() - Method in class org.orekit.forces.drag.atmosphere.NRLMSISE00
Get the frame of the central body.
getFrame() - Method in class org.orekit.forces.drag.atmosphere.SimpleExponentialAtmosphere
Get the frame of the central body.
getFrame() - Method in class org.orekit.frames.OrphanFrame
Get the associated frame.
getFrame() - Method in class org.orekit.orbits.FieldOrbit
Get the frame in which the orbital parameters are defined.
getFrame() - Method in class org.orekit.orbits.Orbit
Get the frame in which the orbital parameters are defined.
getFrame() - Method in class org.orekit.propagation.AbstractPropagator
Get the frame in which the orbit is propagated.
getFrame() - Method in class org.orekit.propagation.analytical.Ephemeris
 
getFrame() - Method in class org.orekit.propagation.analytical.gnss.GPSPropagator
Get the frame in which the orbit is propagated.
getFrame() - Method in class org.orekit.propagation.analytical.tle.TLEPropagator
Get the frame in which the orbit is propagated.
getFrame() - Method in class org.orekit.propagation.conversion.AbstractPropagatorBuilder
Get the frame in which the orbit is propagated.
getFrame() - Method in class org.orekit.propagation.conversion.AbstractPropagatorConverter
Get the frame of the initial state.
getFrame() - Method in interface org.orekit.propagation.conversion.PropagatorBuilder
Get the frame in which the orbit is propagated.
getFrame() - Method in class org.orekit.propagation.events.FieldNodeDetector
Get the frame in which the equator is defined.
getFrame() - Method in class org.orekit.propagation.events.GroundFieldOfViewDetector
Get the sensor reference frame.
getFrame() - Method in class org.orekit.propagation.events.NodeDetector
Get the frame in which the equator is defined.
getFrame() - Method in class org.orekit.propagation.FieldAbstractPropagator
Get the frame in which the orbit is propagated.
getFrame() - Method in interface org.orekit.propagation.FieldPropagator
Get the frame in which the orbit is propagated.
getFrame() - Method in class org.orekit.propagation.FieldSpacecraftState
Get the inertial frame.
getFrame() - Method in class org.orekit.propagation.integration.FieldIntegratedEphemeris
 
getFrame() - Method in class org.orekit.propagation.integration.FieldStateMapper
Get the inertial frame.
getFrame() - Method in class org.orekit.propagation.integration.IntegratedEphemeris
 
getFrame() - Method in class org.orekit.propagation.integration.StateMapper
Get the inertial frame.
getFrame() - Method in interface org.orekit.propagation.Propagator
Get the frame in which the orbit is propagated.
getFrame() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
Get the definition frame of the orbit.
getFrame() - Method in class org.orekit.propagation.SpacecraftState
Get the inertial frame.
getFrame(Predefined) - Static method in class org.orekit.frames.FramesFactory
Get one of the predefined frames.
getFrame(IERSConventions, boolean) - Method in enum org.orekit.files.ccsds.CCSDSFrame
Get the frame corresponding to the CCSDS constant.
getFrameCenterString() - Method in class org.orekit.files.ccsds.OEMFile.EphemeridesBlock
 
getFrameCenterString() - Method in interface org.orekit.files.general.EphemerisFile.EphemerisSegment
Get the name of the center of the coordinate system the ephemeris is provided in.
getFrameCenterString() - Method in class org.orekit.files.general.OrekitEphemerisFile.OrekitEphemerisSegment
 
getFrameCenterString() - Method in class org.orekit.files.sp3.SP3File.SP3Ephemeris
 
getFrameEpoch() - Method in class org.orekit.files.ccsds.ODMMetaData
Get epoch of reference frame, if not intrinsic to the definition of the reference frame.
getFrameEpochString() - Method in class org.orekit.files.ccsds.ODMMetaData
Get epoch of reference frame, if not intrinsic to the definition of the reference frame.
getFrameString() - Method in class org.orekit.files.ccsds.ODMMetaData
Get the reference frame specifier as it appeared in the file.
getFrameString() - Method in class org.orekit.files.ccsds.OEMFile.EphemeridesBlock
 
getFrameString() - Method in interface org.orekit.files.general.EphemerisFile.EphemerisSegment
Get the defining frame for this ephemeris segment.
getFrameString() - Method in class org.orekit.files.general.OrekitEphemerisFile.OrekitEphemerisSegment
 
getFrameString() - Method in class org.orekit.files.sp3.SP3File.SP3Ephemeris
 
getFreeStateParameters() - Method in class org.orekit.estimation.measurements.modifiers.TroposphericDSConverter
Get the number of free state parameters.
getFreqOffset() - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData
Getter for the freqOffset.
getFrequency(SatelliteSystem) - Method in enum org.orekit.gnss.ObservationType
Get the frequency for a specified satellite system.
getFrozenFrame(Frame, AbsoluteDate, String) - Method in class org.orekit.frames.Frame
Get a new version of the instance, frozen with respect to a reference frame.
getFunction() - Method in class org.orekit.propagation.events.FunctionalDetector
Get the switching function.
getFutureInfinity(Field<T>) - Static method in class org.orekit.time.FieldAbsoluteDate
Dummy date at infinity in the future direction.
getGalileoEpoch(Field<T>) - Static method in class org.orekit.time.FieldAbsoluteDate
Reference epoch for Galileo System Time: 1999-08-22T00:00:00 UTC.
getGamma() - Method in class org.orekit.data.DelaunayArguments
Get the tide parameter γ = GMST + π.
getGamma() - Method in class org.orekit.data.FieldDelaunayArguments
Get the tide parameter γ = GMST + π.
getGamma() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
Get direction cosine γ for central body.
getGammaDot() - Method in class org.orekit.data.DelaunayArguments
Get the tide parameter γ = GMST + π time derivative.
getGammaDot() - Method in class org.orekit.data.FieldDelaunayArguments
Get the tide parameter γ = GMST + π time derivative.
getGASTFunction(TimeScale, EOPHistory) - Method in enum org.orekit.utils.IERSConventions
Get the function computing Greenwich apparent sidereal time, in radians.
getGCRF() - Static method in class org.orekit.frames.FramesFactory
Get the unique GCRF frame.
getGdop() - Method in class org.orekit.gnss.DOP
Gets the geometric dilution of precision.
getGenerateCalls() - Method in class org.orekit.utils.GenericTimeStampedCache
Get the number of calls to the generate method.
getGeneratedEphemeris() - Method in class org.orekit.propagation.AbstractPropagator
Get the ephemeris generated during propagation.
getGeneratedEphemeris() - Method in class org.orekit.propagation.analytical.AbstractAnalyticalPropagator
Get the ephemeris generated during propagation.
getGeneratedEphemeris() - Method in class org.orekit.propagation.analytical.FieldAbstractAnalyticalPropagator
Get the ephemeris generated during propagation.
getGeneratedEphemeris() - Method in class org.orekit.propagation.FieldAbstractPropagator
Get the ephemeris generated during propagation.
getGeneratedEphemeris() - Method in interface org.orekit.propagation.FieldPropagator
Get the ephemeris generated during propagation.
getGeneratedEphemeris() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
Get the ephemeris generated during propagation.
getGeneratedEphemeris() - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator
Get the ephemeris generated during propagation.
getGeneratedEphemeris() - Method in interface org.orekit.propagation.Propagator
Get the ephemeris generated during propagation.
getGenerator() - Method in class org.orekit.utils.GenericTimeStampedCache
Get the generator.
getGetNeighborsCalls() - Method in class org.orekit.utils.GenericTimeStampedCache
Get the number of calls to the GenericTimeStampedCache.getNeighbors(AbsoluteDate) method.
getGFunction() - Method in class org.orekit.propagation.events.FunctionalDetector
Deprecated.
use FunctionalDetector.getFunction() instead. Will be removed in next major release.
getGjs(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
Get the Gjs coefficient.
getGLONASS() - Static method in class org.orekit.time.TimeScalesFactory
Get the GLObal NAvigation Satellite System time scale.
getGM() - Method in interface org.orekit.bodies.CelestialBody
Get the attraction coefficient of the body.
getGM() - Method in class org.orekit.models.earth.ReferenceEllipsoid
Gets the gravitational parameter that is part of the definition of the reference ellipsoid.
getGmsj(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHmsjPolynomials
Get the Gmsj coefficient.
getGMST(IERSConventions, boolean) - Static method in class org.orekit.time.TimeScalesFactory
Get the Greenwich Mean Sidereal Time scale.
getGMSTFunction(TimeScale) - Method in enum org.orekit.utils.IERSConventions
Get the function computing Greenwich mean sidereal time, in radians.
getGMSTRateFunction(TimeScale) - Method in enum org.orekit.utils.IERSConventions
Get the function computing Greenwich mean sidereal time rate, in radians per second.
getGnssNb() - Method in class org.orekit.gnss.DOP
Gets the number of GNSS satellites taken into account for DOP computation.
getGPS() - Static method in class org.orekit.time.TimeScalesFactory
Get the Global Positioning System scale.
getGPSEpoch(Field<T>) - Static method in class org.orekit.time.FieldAbsoluteDate
Reference epoch for GPS weeks: 1980-01-06T00:00:00 GPS time.
getGPSOrbitalElements() - Method in class org.orekit.propagation.analytical.gnss.GPSPropagator
Gets the underlying GPS orbital elements.
getGpsWeek() - Method in class org.orekit.files.sp3.SP3File
Returns the GPS week as contained in the SP3 file.
getGridPoints() - Method in class org.orekit.frames.InterpolatingTransformProvider
Get the number of interpolation grid points.
getGridPoints() - Method in class org.orekit.frames.ShiftingTransformProvider
Get the number of interpolation grid points.
getGridPoints(double, double) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FixedNumberInterpolationGrid
Get grid points that are within the current step.
getGridPoints(double, double) - Method in interface org.orekit.propagation.semianalytical.dsst.utilities.InterpolationGrid
Get grid points that are within the current step.
getGridPoints(double, double) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.MaxGapInterpolationGrid
Get grid points that are within the current step.
getGrs80(Frame) - Static method in class org.orekit.models.earth.ReferenceEllipsoid
Get the GRS80 ellipsoid, attached to the given body frame.
getGST() - Static method in class org.orekit.time.TimeScalesFactory
Get the Galileo System Time scale.
getGTOD(boolean) - Static method in class org.orekit.frames.FramesFactory
Get the GTOD reference frame.
getGTOD(IERSConventions, boolean) - Static method in class org.orekit.frames.FramesFactory
Get the GTOD reference frame.
getH() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
Get the y component of eccentricity vector.
getHalfAperture() - Method in class org.orekit.propagation.events.CircularFieldOfViewDetector
Get FOV half aperture angle.
getHandler() - Method in class org.orekit.propagation.events.AbstractDetector
Get the handler.
getHandler() - Method in class org.orekit.propagation.events.FieldAbstractDetector
Get the handler.
getHarmonicAmplitude() - Method in class org.orekit.utils.SecularAndHarmonic
Get an upper bound of the fitted harmonic amplitude.
getHasCreatableBody() - Method in class org.orekit.files.ccsds.ODMMetaData
Get boolean testing whether the body corresponding to the centerName attribute can be created through the CelestialBodyFactory.
getHasManeuver() - Method in class org.orekit.files.ccsds.OPMFile
Get boolean testing whether the OPM contains at least one maneuver.
getHasRefFrameEpoch() - Method in class org.orekit.files.ccsds.OEMFile.EphemeridesBlock
Get boolean testing whether the reference frame has an epoch associated to it.
getHdop() - Method in class org.orekit.gnss.DOP
Gets the horizontal dilution of precision.
getHeader() - Method in class org.orekit.gnss.ObservationDataSet
Get the Rinex header associated with this data set.
getHeaderComment() - Method in class org.orekit.files.ccsds.ODMFile
Get the header comment.
getHeaderComment() - Method in class org.orekit.files.ccsds.TDMFile
Get the header comment.
getHealth() - Method in class org.orekit.gnss.GPSAlmanac
Gets the Health status.
getHjs(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
Get the Hjs coefficient.
getHmsj(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHmsjPolynomials
Get the Hmsj coefficient.
getHorizontalIntensity() - Method in class org.orekit.models.earth.GeoMagneticElements
Returns the horizontal intensity of the magnetic field (= norm of the vector in the plane spanned by the x/y components of the field vector).
getHour() - Method in class org.orekit.time.TimeComponents
Get the hour number.
getHx() - Method in class org.orekit.orbits.CartesianOrbit
Get the first component of the inclination vector.
getHx() - Method in class org.orekit.orbits.CircularOrbit
Get the first component of the inclination vector.
getHx() - Method in class org.orekit.orbits.EquinoctialOrbit
Get the first component of the inclination vector.
getHx() - Method in class org.orekit.orbits.FieldCartesianOrbit
Get the first component of the inclination vector.
getHx() - Method in class org.orekit.orbits.FieldCircularOrbit
Get the first component of the inclination vector.
getHx() - Method in class org.orekit.orbits.FieldEquinoctialOrbit
Get the first component of the inclination vector.
getHx() - Method in class org.orekit.orbits.FieldKeplerianOrbit
Get the first component of the inclination vector.
getHx() - Method in class org.orekit.orbits.FieldOrbit
Get the first component of the inclination vector.
getHx() - Method in class org.orekit.orbits.KeplerianOrbit
Get the first component of the inclination vector.
getHx() - Method in class org.orekit.orbits.Orbit
Get the first component of the inclination vector.
getHx() - Method in class org.orekit.propagation.FieldSpacecraftState
Get the first component of the inclination vector (as per equinoctial parameters).
getHx() - Method in class org.orekit.propagation.SpacecraftState
Get the first component of the inclination vector (as per equinoctial parameters).
getHxDot() - Method in class org.orekit.orbits.CartesianOrbit
Get the first component of the inclination vector derivative.
getHxDot() - Method in class org.orekit.orbits.CircularOrbit
Get the first component of the inclination vector derivative.
getHxDot() - Method in class org.orekit.orbits.EquinoctialOrbit
Get the first component of the inclination vector derivative.
getHxDot() - Method in class org.orekit.orbits.FieldCartesianOrbit
Get the first component of the inclination vector derivative.
getHxDot() - Method in class org.orekit.orbits.FieldCircularOrbit
Get the first component of the inclination vector derivative.
getHxDot() - Method in class org.orekit.orbits.FieldEquinoctialOrbit
Get the first component of the inclination vector derivative.
getHxDot() - Method in class org.orekit.orbits.FieldKeplerianOrbit
Get the first component of the inclination vector derivative.
getHxDot() - Method in class org.orekit.orbits.FieldOrbit
Get the first component of the inclination vector derivative.
getHxDot() - Method in class org.orekit.orbits.KeplerianOrbit
Get the first component of the inclination vector derivative.
getHxDot() - Method in class org.orekit.orbits.Orbit
Get the first component of the inclination vector derivative.
getHy() - Method in class org.orekit.orbits.CartesianOrbit
Get the second component of the inclination vector.
getHy() - Method in class org.orekit.orbits.CircularOrbit
Get the second component of the inclination vector.
getHy() - Method in class org.orekit.orbits.EquinoctialOrbit
Get the second component of the inclination vector.
getHy() - Method in class org.orekit.orbits.FieldCartesianOrbit
Get the second component of the inclination vector.
getHy() - Method in class org.orekit.orbits.FieldCircularOrbit
Get the second component of the inclination vector.
getHy() - Method in class org.orekit.orbits.FieldEquinoctialOrbit
Get the second component of the inclination vector.
getHy() - Method in class org.orekit.orbits.FieldKeplerianOrbit
Get the second component of the inclination vector.
getHy() - Method in class org.orekit.orbits.FieldOrbit
Get the second component of the inclination vector.
getHy() - Method in class org.orekit.orbits.KeplerianOrbit
Get the second component of the inclination vector.
getHy() - Method in class org.orekit.orbits.Orbit
Get the second component of the inclination vector.
getHy() - Method in class org.orekit.propagation.FieldSpacecraftState
Get the second component of the inclination vector (as per equinoctial parameters).
getHy() - Method in class org.orekit.propagation.SpacecraftState
Get the second component of the inclination vector (as per equinoctial parameters).
getHyDot() - Method in class org.orekit.orbits.CartesianOrbit
Get the second component of the inclination vector derivative.
getHyDot() - Method in class org.orekit.orbits.CircularOrbit
Get the second component of the inclination vector derivative.
getHyDot() - Method in class org.orekit.orbits.EquinoctialOrbit
Get the second component of the inclination vector derivative.
getHyDot() - Method in class org.orekit.orbits.FieldCartesianOrbit
Get the second component of the inclination vector derivative.
getHyDot() - Method in class org.orekit.orbits.FieldCircularOrbit
Get the second component of the inclination vector derivative.
getHyDot() - Method in class org.orekit.orbits.FieldEquinoctialOrbit
Get the second component of the inclination vector derivative.
getHyDot() - Method in class org.orekit.orbits.FieldKeplerianOrbit
Get the second component of the inclination vector derivative.
getHyDot() - Method in class org.orekit.orbits.FieldOrbit
Get the second component of the inclination vector derivative.
getHyDot() - Method in class org.orekit.orbits.KeplerianOrbit
Get the second component of the inclination vector derivative.
getHyDot() - Method in class org.orekit.orbits.Orbit
Get the second component of the inclination vector derivative.
getI() - Method in class org.orekit.files.ccsds.OGMFile
Get the orbit inclination.
getI() - Method in class org.orekit.orbits.CartesianOrbit
Get the inclination.
getI() - Method in class org.orekit.orbits.CircularOrbit
Get the inclination.
getI() - Method in class org.orekit.orbits.EquinoctialOrbit
Get the inclination.
getI() - Method in class org.orekit.orbits.FieldCartesianOrbit
Get the inclination.
getI() - Method in class org.orekit.orbits.FieldCircularOrbit
Get the inclination.
getI() - Method in class org.orekit.orbits.FieldEquinoctialOrbit
Get the inclination.
getI() - Method in class org.orekit.orbits.FieldKeplerianOrbit
Get the inclination.
getI() - Method in class org.orekit.orbits.FieldOrbit
Get the inclination.
getI() - Method in class org.orekit.orbits.KeplerianOrbit
Get the inclination.
getI() - Method in class org.orekit.orbits.Orbit
Get the inclination.
getI() - Method in class org.orekit.propagation.analytical.tle.TLE
Get the inclination.
getI() - Method in class org.orekit.propagation.FieldSpacecraftState
Get the inclination.
getI() - Method in class org.orekit.propagation.SpacecraftState
Get the inclination.
getI0() - Method in class org.orekit.gnss.GPSAlmanac
 
getI0() - Method in interface org.orekit.propagation.analytical.gnss.GPSOrbitalElements
Gets the Inclination Angle at Reference Time.
getICRF() - Static method in class org.orekit.frames.FramesFactory
Get the unique ICRF frame.
getId() - Method in class org.orekit.files.ccsds.OEMFile.OemSatelliteEphemeris
 
getId() - Method in interface org.orekit.files.general.EphemerisFile.SatelliteEphemeris
Get the satellite ID.
getId() - Method in class org.orekit.files.general.OrekitEphemerisFile.OrekitSatelliteEphemeris
 
getId() - Method in class org.orekit.files.sp3.SP3File.SP3Ephemeris
 
getIdentity(Field<T>) - Static method in class org.orekit.frames.FieldTransform
Get the identity transform.
getIdentity(Field<T>) - Static method in class org.orekit.utils.FieldAngularCoordinates
Fixed orientation parallel with reference frame (identity rotation, zero rotation rate and acceleration).
getIDot() - Method in class org.orekit.gnss.GPSAlmanac
 
getIDot() - Method in class org.orekit.orbits.CartesianOrbit
Get the inclination derivative.
getIDot() - Method in class org.orekit.orbits.CircularOrbit
Get the inclination derivative.
getIDot() - Method in class org.orekit.orbits.EquinoctialOrbit
Get the inclination derivative.
getIDot() - Method in class org.orekit.orbits.FieldCartesianOrbit
Get the inclination derivative.
getIDot() - Method in class org.orekit.orbits.FieldCircularOrbit
Get the inclination derivative.
getIDot() - Method in class org.orekit.orbits.FieldEquinoctialOrbit
Get the inclination derivative.
getIDot() - Method in class org.orekit.orbits.FieldKeplerianOrbit
Get the inclination derivative.
getIDot() - Method in class org.orekit.orbits.FieldOrbit
Get the inclination derivative.
getIDot() - Method in class org.orekit.orbits.KeplerianOrbit
Get the inclination derivative.
getIDot() - Method in class org.orekit.orbits.Orbit
Get the inclination derivative.
getIDot() - Method in interface org.orekit.propagation.analytical.gnss.GPSOrbitalElements
Gets the Rate of Inclination Angle.
getIGRF(double) - Static method in class org.orekit.models.earth.GeoMagneticFieldFactory
Get the IGRF model for the given year.
getIjs(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
Get the Ijs coefficient.
getImaginary(int, int) - Method in class org.orekit.utils.LoveNumbers
Get the imaginary part of a nominal Love numbers.
getInclination() - Method in class org.orekit.models.earth.GeoMagneticElements
Returns the inclination of the magnetic field in degrees.
getIncreasingTimeShift() - Method in class org.orekit.propagation.events.EventShifter
Get the increasing events time shift.
getInertialDV() - Method in class org.orekit.forces.maneuvers.SmallManeuverAnalyticalModel
Get the inertial velocity increment of the maneuver.
getInertialFrame() - Method in class org.orekit.forces.maneuvers.SmallManeuverAnalyticalModel
Get the inertial frame in which the velocity increment is defined.
getInertiallyOrientedFrame() - Method in interface org.orekit.bodies.CelestialBody
Get an inertially oriented, body centered frame.
getInitialCovarianceMatrix(SpacecraftState) - Method in class org.orekit.estimation.sequential.AbstractCovarianceMatrixProvider
Get the initial covariance matrix.
getInitialCovarianceMatrix(SpacecraftState) - Method in interface org.orekit.estimation.sequential.CovarianceMatrixProvider
Get the initial covariance matrix.
getInitialIntegrationState() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
Get the initial state for integration.
getInitialIntegrationState() - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator
Get the initial state for integration.
getInitialIntegrationState() - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator
Get the initial state for integration.
getInitialOrbitDate() - Method in class org.orekit.propagation.conversion.AbstractPropagatorBuilder
Get the date of the initial orbit.
getInitialOrbitDate() - Method in interface org.orekit.propagation.conversion.PropagatorBuilder
Get the date of the initial orbit.
getInitialState() - Method in class org.orekit.propagation.AbstractPropagator
Get the propagator initial state.
getInitialState() - Method in class org.orekit.propagation.analytical.AdapterPropagator
Get the propagator initial state.
getInitialState() - Method in class org.orekit.propagation.analytical.AggregateBoundedPropagator
 
getInitialState() - Method in class org.orekit.propagation.analytical.Ephemeris
Get the propagator initial state.
getInitialState() - Method in class org.orekit.propagation.FieldAbstractPropagator
Get the propagator initial state.
getInitialState() - Method in interface org.orekit.propagation.FieldPropagator
Get the propagator initial state.
getInitialState() - Method in class org.orekit.propagation.integration.FieldIntegratedEphemeris
Get the propagator initial state.
getInitialState() - Method in class org.orekit.propagation.integration.IntegratedEphemeris
Get the propagator initial state.
getInitialState() - Method in interface org.orekit.propagation.Propagator
Get the propagator initial state.
getInnovation(MeasurementDecorator, NonLinearEvolution, RealMatrix) - Method in class org.orekit.estimation.sequential.Model
getInstance() - Static method in class org.orekit.data.DataProvidersManager
Get the unique instance.
getInstantFlux(AbsoluteDate) - Method in class org.orekit.forces.drag.atmosphere.data.MarshallSolarActivityFutureEstimation
Get the value of the instantaneous solar flux.
getInstantFlux(AbsoluteDate) - Method in interface org.orekit.forces.drag.atmosphere.DTM2000InputParameters
Get the value of the instantaneous solar flux.
getIntegrationInterval() - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData
Getter for the integrationInterval.
getIntegrationRef() - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData
Getter for the integrationRef.
getIntegrator() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
Get the integrator used by the propagator.
getIntegrator() - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator
Get the integrator used by the propagator.
getIntegratorBuilder() - Method in class org.orekit.propagation.conversion.NumericalPropagatorBuilder
Get the integrator builder.
getInterpolatedPoint(double, double) - Method in class org.orekit.models.earth.tessellation.Tile
Get an interpolated point inside the tile.
getInterpolatedState(AbsoluteDate) - Method in interface org.orekit.propagation.sampling.OrekitStepInterpolator
Get the state at interpolated date.
getInterpolatedState(FieldAbsoluteDate<T>) - Method in interface org.orekit.propagation.sampling.FieldOrekitStepInterpolator
Get the state at interpolated date.
getInterpolationDegree() - Method in class org.orekit.files.ccsds.OEMFile.EphemeridesBlock
Get the interpolation degree.
getInterpolationMethod() - Method in class org.orekit.files.ccsds.OEMFile.EphemeridesBlock
Get the interpolation method to be used.
getInterpolationSamples() - Method in class org.orekit.files.ccsds.OEMFile.EphemeridesBlock
 
getInterpolationSamples() - Method in interface org.orekit.files.general.EphemerisFile.EphemerisSegment
Get the number of samples to use in interpolation.
getInterpolationSamples() - Method in class org.orekit.files.general.OrekitEphemerisFile.OrekitEphemerisSegment
 
getInterpolationSamples() - Method in class org.orekit.files.sp3.SP3File.SP3Ephemeris
 
getIntersectionPoint(FieldLine<T>, FieldVector3D<T>, Frame, FieldAbsoluteDate<T>) - Method in interface org.orekit.bodies.BodyShape
Get the intersection point of a line with the surface of the body.
getIntersectionPoint(FieldLine<T>, FieldVector3D<T>, Frame, FieldAbsoluteDate<T>) - Method in class org.orekit.bodies.OneAxisEllipsoid
Get the intersection point of a line with the surface of the body.
getIntersectionPoint(FieldLine<T>, FieldVector3D<T>, Frame, FieldAbsoluteDate<T>) - Method in class org.orekit.models.earth.Geoid
Get the intersection point of a line with the surface of the body.
getIntersectionPoint(Line, Vector3D, Frame, AbsoluteDate) - Method in interface org.orekit.bodies.BodyShape
Get the intersection point of a line with the surface of the body.
getIntersectionPoint(Line, Vector3D, Frame, AbsoluteDate) - Method in class org.orekit.bodies.OneAxisEllipsoid
Get the intersection point of a line with the surface of the body.
getIntersectionPoint(Line, Vector3D, Frame, AbsoluteDate) - Method in class org.orekit.models.earth.Geoid
Get the intersection point of a line with the surface of the body.
getInterval() - Method in class org.orekit.gnss.RinexHeader
Get the observation interval in seconds.
getInverse() - Method in class org.orekit.frames.FieldTransform
Get the inverse transform of the instance.
getInverse() - Method in class org.orekit.frames.Transform
Get the inverse transform of the instance.
getIODC() - Method in interface org.orekit.propagation.analytical.gnss.GPSOrbitalElements
Gets the Issue Of Data Clock (IODC).
getIODE() - Method in interface org.orekit.propagation.analytical.gnss.GPSOrbitalElements
Gets the Issue Of Data Ephemeris (IODE).
getIRNSS() - Static method in class org.orekit.time.TimeScalesFactory
Get the Indian Regional Navigation Satellite System time scale.
getIsp() - Method in class org.orekit.forces.maneuvers.ImpulseManeuver
Get the specific impulse.
getISP() - Method in class org.orekit.forces.maneuvers.ConstantThrustManeuver
Get the specific impulse.
getIteration() - Method in class org.orekit.estimation.measurements.EstimatedMeasurement
Get the iteration number.
getIterationsCount() - Method in class org.orekit.estimation.leastsquares.BatchLSEstimator
Get the number of iterations used for last estimation.
getITRF(ITRFVersion, IERSConventions, boolean) - Static method in class org.orekit.frames.FramesFactory
Get an specific International Terrestrial Reference Frame.
getITRF(IERSConventions, boolean) - Static method in class org.orekit.frames.FramesFactory
Get an unspecified International Terrestrial Reference Frame.
getITRFEquinox(IERSConventions, boolean) - Static method in class org.orekit.frames.FramesFactory
Get the equinox-based ITRF reference frame.
getITRFType() - Method in class org.orekit.frames.EOPEntry
Get the ITRF version this entry defines.
getITRFVersion() - Method in class org.orekit.frames.VersionedITRF
Get the ITRF version.
getITRFVersion(int) - Static method in enum org.orekit.frames.ITRFVersion
Find an ITRF version from its reference year.
getITRFVersion(String) - Static method in enum org.orekit.frames.ITRFVersion
Find an ITRF version from its name.
getITRFVersion(AbsoluteDate) - Method in class org.orekit.frames.EOPHistory
Get the ITRF version.
getJ2000Day() - Method in class org.orekit.time.DateComponents
Get the day number with respect to J2000 epoch.
getJ2000Epoch(Field<T>) - Static method in class org.orekit.time.FieldAbsoluteDate
J2000.0 Reference epoch: 2000-01-01T12:00:00 Terrestrial Time (not UTC).
getJacobian(Orbit, PositionAngle, double[][]) - Method in class org.orekit.forces.maneuvers.SmallManeuverAnalyticalModel
Compute the Jacobian of the orbit with respect to maneuver parameters.
getJacobian(CartesianDerivativesFilter, double[][]) - Method in class org.orekit.frames.Transform
Compute the Jacobian of the Transform.transformPVCoordinates(PVCoordinates) method of the transform.
getJacobian(CartesianDerivativesFilter, T[][]) - Method in class org.orekit.frames.FieldTransform
Compute the Jacobian of the FieldTransform.transformPVCoordinates(FieldPVCoordinates) method of the transform.
getJacobianWrtCartesian(PositionAngle, double[][]) - Method in class org.orekit.orbits.Orbit
Compute the Jacobian of the orbital parameters with respect to the Cartesian parameters.
getJacobianWrtCartesian(PositionAngle, T[][]) - Method in class org.orekit.orbits.FieldOrbit
Compute the Jacobian of the orbital parameters with respect to the Cartesian parameters.
getJacobianWrtParameters(PositionAngle, double[][]) - Method in class org.orekit.orbits.Orbit
Compute the Jacobian of the Cartesian parameters with respect to the orbital parameters.
getJacobianWrtParameters(PositionAngle, T[][]) - Method in class org.orekit.orbits.FieldOrbit
Compute the Jacobian of the Cartesian parameters with respect to the orbital parameters.
getJavaEpoch(Field<T>) - Static method in class org.orekit.time.FieldAbsoluteDate
Java Reference epoch: 1970-01-01T00:00:00 Universal Time Coordinate.
getJjs(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
Get the Jjs coefficient.
getJulianDay() - Method in class org.orekit.files.sp3.SP3File
Returns the julian day for this SP3 file.
getJulianEpoch(Field<T>) - Static method in class org.orekit.time.FieldAbsoluteDate
Reference epoch for julian dates: -4712-01-01T12:00:00 Terrestrial Time.
getJupiter() - Static method in class org.orekit.bodies.CelestialBodyFactory
Get the Jupiter singleton body.
getK() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
Get the x component of eccentricity vector.
getKeplerianElementsComment() - Method in class org.orekit.files.ccsds.OGMFile
Get the comment for Keplerian elements.
getKeplerianMeanMotion() - Method in class org.orekit.orbits.FieldOrbit
Get the Keplerian mean motion.
getKeplerianMeanMotion() - Method in class org.orekit.orbits.Orbit
Get the Keplerian mean motion.
getKeplerianMeanMotion() - Method in class org.orekit.propagation.FieldSpacecraftState
Get the Keplerian mean motion.
getKeplerianMeanMotion() - Method in class org.orekit.propagation.SpacecraftState
Get the Keplerian mean motion.
getKeplerianPeriod() - Method in class org.orekit.orbits.FieldOrbit
Get the Keplerian period.
getKeplerianPeriod() - Method in class org.orekit.orbits.Orbit
Get the Keplerian period.
getKeplerianPeriod() - Method in class org.orekit.propagation.FieldSpacecraftState
Get the Keplerian period.
getKeplerianPeriod() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
Get the Keplerian period.
getKeplerianPeriod() - Method in class org.orekit.propagation.SpacecraftState
Get the Keplerian period.
getKey() - Method in enum org.orekit.gnss.SatelliteSystem
Get the key for the system.
getKeyword() - Method in class org.orekit.files.ccsds.TDMFile.Observation
Getter for the keyword.
getL() - Method in class org.orekit.data.DelaunayArguments
Get the mean anomaly of the Moon.
getL() - Method in class org.orekit.data.FieldDelaunayArguments
Get the mean anomaly of the Moon.
getL(PositionAngle) - Method in class org.orekit.orbits.EquinoctialOrbit
Get the longitude argument.
getL(PositionAngle) - Method in class org.orekit.orbits.FieldEquinoctialOrbit
Get the longitude argument.
getLast() - Method in class org.orekit.propagation.analytical.tle.TLESeries
Deprecated.
Get the last TLE.
getLastDate() - Method in class org.orekit.propagation.analytical.tle.TLESeries
Deprecated.
Get the last date of the series.
getLastEstimations() - Method in class org.orekit.estimation.leastsquares.BatchLSEstimator
Get the last estimations performed.
getLastKnownLeapSecond() - Method in class org.orekit.time.UTCScale
Get the date of the last known leap second.
getLatest() - Method in class org.orekit.utils.GenericTimeStampedCache
Get the latest cached entry.
getLatest() - Method in class org.orekit.utils.ImmutableTimeStampedCache
 
getLatest() - Method in interface org.orekit.utils.TimeStampedCache
Get the latest entry in this cache.
getLatitude() - Method in class org.orekit.bodies.FieldGeodeticPoint
Get the latitude.
getLatitude() - Method in class org.orekit.bodies.GeodeticPoint
Get the latitude.
getLatitude() - Method in class org.orekit.propagation.events.LatitudeCrossingDetector
Get the fixed latitude to be crossed (radians).
getLaunchNumber() - Method in class org.orekit.files.ccsds.ODMMetaData
Get the launch number.
getLaunchNumber() - Method in class org.orekit.files.ccsds.ODMParser
Get the launch number.
getLaunchNumber() - Method in class org.orekit.propagation.analytical.tle.TLE
Get the launch number.
getLaunchPiece() - Method in class org.orekit.files.ccsds.ODMMetaData
Get the piece of launch.
getLaunchPiece() - Method in class org.orekit.files.ccsds.ODMParser
Get the piece of launch.
getLaunchPiece() - Method in class org.orekit.propagation.analytical.tle.TLE
Get the launch piece.
getLaunchYear() - Method in class org.orekit.files.ccsds.ODMMetaData
Get the launch year.
getLaunchYear() - Method in class org.orekit.files.ccsds.ODMParser
Get the launch year.
getLaunchYear() - Method in class org.orekit.propagation.analytical.tle.TLE
Get the launch year.
getLDot() - Method in class org.orekit.data.DelaunayArguments
Get the mean anomaly of the Moon time derivative.
getLDot() - Method in class org.orekit.data.FieldDelaunayArguments
Get the mean anomaly of the Moon time derivative.
getLDot(PositionAngle) - Method in class org.orekit.orbits.EquinoctialOrbit
Get the longitude argument derivative.
getLDot(PositionAngle) - Method in class org.orekit.orbits.FieldEquinoctialOrbit
Get the longitude argument derivative.
getLE() - Method in class org.orekit.data.BodiesElements
Get the mean Earth longitude.
getLE() - Method in class org.orekit.data.FieldBodiesElements
Get the mean Earth longitude.
getLE() - Method in class org.orekit.orbits.CartesianOrbit
Get the eccentric longitude argument.
getLE() - Method in class org.orekit.orbits.CircularOrbit
Get the eccentric longitude argument.
getLE() - Method in class org.orekit.orbits.EquinoctialOrbit
Get the eccentric longitude argument.
getLE() - Method in class org.orekit.orbits.FieldCartesianOrbit
Get the eccentric longitude argument.
getLE() - Method in class org.orekit.orbits.FieldCircularOrbit
Get the eccentric longitude argument.
getLE() - Method in class org.orekit.orbits.FieldEquinoctialOrbit
Get the eccentric longitude argument.
getLE() - Method in class org.orekit.orbits.FieldKeplerianOrbit
Get the eccentric longitude argument.
getLE() - Method in class org.orekit.orbits.FieldOrbit
Get the eccentric longitude argument.
getLE() - Method in class org.orekit.orbits.KeplerianOrbit
Get the eccentric longitude argument.
getLE() - Method in class org.orekit.orbits.Orbit
Get the eccentric longitude argument.
getLE() - Method in class org.orekit.propagation.FieldSpacecraftState
Get the eccentric latitude argument (as per equinoctial parameters).
getLE() - Method in class org.orekit.propagation.SpacecraftState
Get the eccentric longitude argument (as per equinoctial parameters).
getLeap(AbsoluteDate) - Method in class org.orekit.time.GLONASSScale
Get the value of the previous leap.
getLeap(AbsoluteDate) - Method in interface org.orekit.time.TimeScale
Get the value of the previous leap.
getLeap(AbsoluteDate) - Method in class org.orekit.time.UTCScale
Get the value of the previous leap.
getLeap(FieldAbsoluteDate<T>) - Method in class org.orekit.time.GLONASSScale
Get the value of the previous leap.
getLeap(FieldAbsoluteDate<T>) - Method in interface org.orekit.time.TimeScale
Get the value of the previous leap.
getLeap(FieldAbsoluteDate<T>) - Method in class org.orekit.time.UTCScale
Get the value of the previous leap.
getLeapSeconds() - Method in class org.orekit.gnss.RinexHeader
Get the Number of leap seconds since 6-Jan-1980.
getLeapSecondsDayNum() - Method in class org.orekit.gnss.RinexHeader
Get the respective leap second day number.
getLeapSecondsFuture() - Method in class org.orekit.gnss.RinexHeader
Get the future or past leap seconds.
getLeapSecondsWeekNum() - Method in class org.orekit.gnss.RinexHeader
Get the respective leap second week number.
getLEDot() - Method in class org.orekit.data.BodiesElements
Get the mean Earth longitude time derivative.
getLEDot() - Method in class org.orekit.data.FieldBodiesElements
Get the mean Earth longitude time derivative.
getLEDot() - Method in class org.orekit.orbits.CartesianOrbit
Get the eccentric longitude argument derivative.
getLEDot() - Method in class org.orekit.orbits.CircularOrbit
Get the eccentric longitude argument derivative.
getLEDot() - Method in class org.orekit.orbits.EquinoctialOrbit
Get the eccentric longitude argument derivative.
getLEDot() - Method in class org.orekit.orbits.FieldCartesianOrbit
Get the eccentric longitude argument derivative.
getLEDot() - Method in class org.orekit.orbits.FieldCircularOrbit
Get the eccentric longitude argument derivative.
getLEDot() - Method in class org.orekit.orbits.FieldEquinoctialOrbit
Get the eccentric longitude argument derivative.
getLEDot() - Method in class org.orekit.orbits.FieldKeplerianOrbit
Get the eccentric longitude argument derivative.
getLEDot() - Method in class org.orekit.orbits.FieldOrbit
Get the eccentric longitude argument derivative.
getLEDot() - Method in class org.orekit.orbits.KeplerianOrbit
Get the eccentric longitude argument derivative.
getLEDot() - Method in class org.orekit.orbits.Orbit
Get the eccentric longitude argument derivative.
getLf() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
Get the eccentric longitude.
getLightingRatio(FieldVector3D<T>, Frame, FieldAbsoluteDate<T>) - Method in class org.orekit.forces.radiation.SolarRadiationPressure
Get the lighting ratio ([0-1]).
getLightingRatio(Vector3D, Frame, AbsoluteDate) - Method in class org.orekit.forces.radiation.SolarRadiationPressure
Get the lighting ratio ([0-1]).
getLine1() - Method in class org.orekit.propagation.analytical.tle.TLE
Get the first line.
getLine2() - Method in class org.orekit.propagation.analytical.tle.TLE
Get the second line.
getListAppliedDCBS() - Method in class org.orekit.gnss.RinexHeader
Get the list of applied differential code bias corrections.
getListAppliedPCVS() - Method in class org.orekit.gnss.RinexHeader
Get the list of antenna center variation corrections.
getLJu() - Method in class org.orekit.data.BodiesElements
Get the mean Jupiter longitude.
getLJu() - Method in class org.orekit.data.FieldBodiesElements
Get the mean Jupiter longitude.
getLJuDot() - Method in class org.orekit.data.BodiesElements
Get the mean Jupiter longitude time derivative.
getLJuDot() - Method in class org.orekit.data.FieldBodiesElements
Get the mean Jupiter longitude time derivative.
getLLimits(SpacecraftState) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution
Compute the limits in L, the true longitude, for integration.
getLLimits(SpacecraftState) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTAtmosphericDrag
Compute the limits in L, the true longitude, for integration.
getLLimits(SpacecraftState) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTSolarRadiationPressure
Compute the limits in L, the true longitude, for integration.
getLM() - Method in class org.orekit.orbits.CartesianOrbit
Get the mean longitude argument.
getLM() - Method in class org.orekit.orbits.CircularOrbit
Get the mean longitude argument.
getLM() - Method in class org.orekit.orbits.EquinoctialOrbit
Get the mean longitude argument.
getLM() - Method in class org.orekit.orbits.FieldCartesianOrbit
Get the mean longitude argument.
getLM() - Method in class org.orekit.orbits.FieldCircularOrbit
Get the mean longitude argument.
getLM() - Method in class org.orekit.orbits.FieldEquinoctialOrbit
Get the mean longitude argument.
getLM() - Method in class org.orekit.orbits.FieldKeplerianOrbit
Get the mean longitude argument.
getLM() - Method in class org.orekit.orbits.FieldOrbit
Get the mean longitude argument.
getLM() - Method in class org.orekit.orbits.KeplerianOrbit
Get the mean longitude argument.
getLM() - Method in class org.orekit.orbits.Orbit
Get the mean longitude argument.
getLM() - Method in class org.orekit.propagation.FieldSpacecraftState
Get the mean latitude argument (as per equinoctial parameters).
getLM() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
Get the mean longitude.
getLM() - Method in class org.orekit.propagation.SpacecraftState
Get the mean longitude argument (as per equinoctial parameters).
getLMa() - Method in class org.orekit.data.BodiesElements
Get the mean Mars longitude.
getLMa() - Method in class org.orekit.data.FieldBodiesElements
Get the mean Mars longitude.
getLMaDot() - Method in class org.orekit.data.BodiesElements
Get the mean Mars longitude time derivative.
getLMaDot() - Method in class org.orekit.data.FieldBodiesElements
Get the mean Mars longitude time derivative.
getLMDot() - Method in class org.orekit.orbits.CartesianOrbit
Get the mean longitude argument derivative.
getLMDot() - Method in class org.orekit.orbits.CircularOrbit
Get the mean longitude argument derivative.
getLMDot() - Method in class org.orekit.orbits.EquinoctialOrbit
Get the mean longitude argument derivative.
getLMDot() - Method in class org.orekit.orbits.FieldCartesianOrbit
Get the mean longitude argument derivative.
getLMDot() - Method in class org.orekit.orbits.FieldCircularOrbit
Get the mean longitude argument derivative.
getLMDot() - Method in class org.orekit.orbits.FieldEquinoctialOrbit
Get the mean longitude argument derivative.
getLMDot() - Method in class org.orekit.orbits.FieldKeplerianOrbit
Get the mean longitude argument derivative.
getLMDot() - Method in class org.orekit.orbits.FieldOrbit
Get the mean longitude argument derivative.
getLMDot() - Method in class org.orekit.orbits.KeplerianOrbit
Get the mean longitude argument derivative.
getLMDot() - Method in class org.orekit.orbits.Orbit
Get the mean longitude argument derivative.
getLMe() - Method in class org.orekit.data.BodiesElements
Get the mean Mercury longitude.
getLMe() - Method in class org.orekit.data.FieldBodiesElements
Get the mean Mercury longitude.
getLMeDot() - Method in class org.orekit.data.BodiesElements
Get the mean Mercury longitude time derivative.
getLMeDot() - Method in class org.orekit.data.FieldBodiesElements
Get the mean Mercury longitude time derivative.
getLNe() - Method in class org.orekit.data.BodiesElements
Get the mean Neptune longitude.
getLNe() - Method in class org.orekit.data.FieldBodiesElements
Get the mean Neptune longitude.
getLNeDot() - Method in class org.orekit.data.BodiesElements
Get the mean Neptune longitude time derivative.
getLNeDot() - Method in class org.orekit.data.FieldBodiesElements
Get the mean Neptune longitude time derivative.
getLns(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.LnsCoefficients
Get the value of Lns(γ).
getLoadedAstronomicalUnit() - Method in class org.orekit.bodies.JPLEphemeridesLoader
Get astronomical unit.
getLoadedConstant(String...) - Method in class org.orekit.bodies.JPLEphemeridesLoader
Get a constant defined in the ephemerides headers.
getLoadedDataNames() - Method in class org.orekit.data.DataProvidersManager
Get an unmodifiable view of the set of data file names that have been loaded.
getLoadedEarthMoonMassRatio() - Method in class org.orekit.bodies.JPLEphemeridesLoader
Get Earth/Moon mass ratio.
getLoadedGravitationalCoefficient(JPLEphemeridesLoader.EphemerisType) - Method in class org.orekit.bodies.JPLEphemeridesLoader
Get the gravitational coefficient of a body.
getLocalizedMessage() - Method in exception org.orekit.errors.OrekitException
getLocalizedMessage() - Method in exception org.orekit.errors.OrekitIllegalArgumentException
getLocalizedMessage() - Method in exception org.orekit.errors.OrekitIllegalStateException
getLocalizedMessage() - Method in exception org.orekit.errors.OrekitInternalError
getLocalizedMessage() - Method in exception org.orekit.errors.OrekitIOException
getLocalizedMessage() - Method in exception org.orekit.errors.OrekitParseException
getLocalizedString(Locale) - Method in enum org.orekit.errors.OrekitMessages
getLocation() - Method in class org.orekit.gnss.DOP
Gets the location with respect to the Earth where DOP was calculated.
getLOD() - Method in class org.orekit.frames.EOPEntry
Get the LoD (Length of Day) value.
getLOD(AbsoluteDate) - Method in class org.orekit.frames.EOPHistory
Get the LoD (Length of Day) value.
getLOD(FieldAbsoluteDate<T>) - Method in class org.orekit.frames.EOPHistory
Get the LoD (Length of Day) value.
getLofCartesianOrbitalParametersEvolution() - Method in class org.orekit.estimation.sequential.UnivariateProcessNoise
Getter for the lofCartesianOrbitalParametersEvolution.
getLofType() - Method in class org.orekit.estimation.sequential.UnivariateProcessNoise
Getter for the lofType.
getLofType() - Method in enum org.orekit.files.ccsds.CCSDSFrame
Get the type of Local Orbital frame.
getLofType() - Method in class org.orekit.files.ccsds.OEMFile.CovarianceMatrix
Get coordinate system for covariance matrix, for Local Orbital Frames.
getLoggedEvents() - Method in class org.orekit.propagation.events.EventsLogger
Get an immutable copy of the logged events.
getLoggedEvents() - Method in class org.orekit.propagation.events.FieldEventsLogger
Get an immutable copy of the logged events.
getLongitude() - Method in class org.orekit.bodies.FieldGeodeticPoint
Get the longitude.
getLongitude() - Method in class org.orekit.bodies.GeodeticPoint
Get the longitude.
getLongitude() - Method in class org.orekit.propagation.events.LongitudeCrossingDetector
Get the fixed longitude to be crossed (radians).
getLossOfLockIndicator() - Method in class org.orekit.gnss.ObservationData
Get the Loss of Lock Indicator.
getLoveNumbers() - Method in enum org.orekit.utils.IERSConventions
Get the Love numbers.
getLowerCaseAbbreviation() - Method in enum org.orekit.time.Month
Get the lower case three letters abbreviation.
getLowerCaseName() - Method in enum org.orekit.time.Month
Get the lower case full name.
getLPrime() - Method in class org.orekit.data.DelaunayArguments
Get the mean anomaly of the Sun.
getLPrime() - Method in class org.orekit.data.FieldDelaunayArguments
Get the mean anomaly of the Sun.
getLPrimeDot() - Method in class org.orekit.data.DelaunayArguments
Get the mean anomaly of the Sun time derivative.
getLPrimeDot() - Method in class org.orekit.data.FieldDelaunayArguments
Get the mean anomaly of the Sun time derivative.
getLSa() - Method in class org.orekit.data.BodiesElements
Get the mean Saturn longitude.
getLSa() - Method in class org.orekit.data.FieldBodiesElements
Get the mean Saturn longitude.
getLSaDot() - Method in class org.orekit.data.BodiesElements
Get the mean Saturn longitude time derivative.
getLSaDot() - Method in class org.orekit.data.FieldBodiesElements
Get the mean Saturn longitude time derivative.
getLUr() - Method in class org.orekit.data.BodiesElements
Get the mean Uranus longitude.
getLUr() - Method in class org.orekit.data.FieldBodiesElements
Get the mean Uranus longitude.
getLUrDot() - Method in class org.orekit.data.BodiesElements
Get the mean Uranus longitude time derivative.
getLUrDot() - Method in class org.orekit.data.FieldBodiesElements
Get the mean Uranus longitude time derivative.
getLv() - Method in class org.orekit.orbits.CartesianOrbit
Get the true longitude argument.
getLv() - Method in class org.orekit.orbits.CircularOrbit
Get the true longitude argument.
getLv() - Method in class org.orekit.orbits.EquinoctialOrbit
Get the true longitude argument.
getLv() - Method in class org.orekit.orbits.FieldCartesianOrbit
Get the true longitude argument.
getLv() - Method in class org.orekit.orbits.FieldCircularOrbit
Get the true longitude argument.
getLv() - Method in class org.orekit.orbits.FieldEquinoctialOrbit
Get the true longitude argument.
getLv() - Method in class org.orekit.orbits.FieldKeplerianOrbit
Get the true longitude argument.
getLv() - Method in class org.orekit.orbits.FieldOrbit
Get the true longitude argument.
getLv() - Method in class org.orekit.orbits.KeplerianOrbit
Get the true longitude argument.
getLv() - Method in class org.orekit.orbits.Orbit
Get the true longitude argument.
getLv() - Method in class org.orekit.propagation.FieldSpacecraftState
Get the true latitude argument (as per equinoctial parameters).
getLv() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
Get the true longitude.
getLv() - Method in class org.orekit.propagation.SpacecraftState
Get the true longitude argument (as per equinoctial parameters).
getLvDot() - Method in class org.orekit.orbits.CartesianOrbit
Get the true longitude argument derivative.
getLvDot() - Method in class org.orekit.orbits.CircularOrbit
Get the true longitude argument derivative.
getLvDot() - Method in class org.orekit.orbits.EquinoctialOrbit
Get the true longitude argument derivative.
getLvDot() - Method in class org.orekit.orbits.FieldCartesianOrbit
Get the true longitude argument derivative.
getLvDot() - Method in class org.orekit.orbits.FieldCircularOrbit
Get the true longitude argument derivative.
getLvDot() - Method in class org.orekit.orbits.FieldEquinoctialOrbit
Get the true longitude argument derivative.
getLvDot() - Method in class org.orekit.orbits.FieldKeplerianOrbit
Get the true longitude argument derivative.
getLvDot() - Method in class org.orekit.orbits.FieldOrbit
Get the true longitude argument derivative.
getLvDot() - Method in class org.orekit.orbits.KeplerianOrbit
Get the true longitude argument derivative.
getLvDot() - Method in class org.orekit.orbits.Orbit
Get the true longitude argument derivative.
getLVe() - Method in class org.orekit.data.BodiesElements
Get the mean Venus longitude.
getLVe() - Method in class org.orekit.data.FieldBodiesElements
Get the mean Venus longitude.
getLVeDot() - Method in class org.orekit.data.BodiesElements
Get the mean Venus longitude time derivative.
getLVeDot() - Method in class org.orekit.data.FieldBodiesElements
Get the mean Venus longitude time derivative.
getM0() - Method in class org.orekit.gnss.GPSAlmanac
 
getM0() - Method in interface org.orekit.propagation.analytical.gnss.GPSOrbitalElements
Gets the Mean Anomaly at Reference Time.
getMainStateEquations(FieldODEIntegrator<T>) - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator
Get the differential equations to integrate (for main state only).
getMainStateEquations(FieldODEIntegrator<T>) - Method in class org.orekit.propagation.numerical.FieldNumericalPropagator
Get the differential equations to integrate (for main state only).
getMainStateEquations(ODEIntegrator) - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
Get the differential equations to integrate (for main state only).
getMainStateEquations(ODEIntegrator) - Method in class org.orekit.propagation.numerical.NumericalPropagator
Get the differential equations to integrate (for main state only).
getMainStateEquations(ODEIntegrator) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator
Get the differential equations to integrate (for main state only).
getManagedAdditionalStates() - Method in class org.orekit.propagation.AbstractPropagator
Get all the names of all managed states.
getManagedAdditionalStates() - Method in class org.orekit.propagation.analytical.Ephemeris
Get all the names of all managed states.
getManagedAdditionalStates() - Method in class org.orekit.propagation.FieldAbstractPropagator
Get all the names of all managed states.
getManagedAdditionalStates() - Method in interface org.orekit.propagation.FieldPropagator
Get all the names of all managed states.
getManagedAdditionalStates() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
Get all the names of all managed states.
getManagedAdditionalStates() - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator
Get all the names of all managed states.
getManagedAdditionalStates() - Method in interface org.orekit.propagation.Propagator
Get all the names of all managed states.
getManeuver(int) - Method in class org.orekit.files.ccsds.OPMFile
Get a maneuver.
getManeuvers() - Method in class org.orekit.files.ccsds.OPMFile
Get a list of all maneuvers.
getMapper() - Method in class org.orekit.propagation.numerical.PartialDerivativesEquations
Get a mapper between two-dimensional Jacobians and one-dimensional additional state.
getMargin() - Method in class org.orekit.propagation.events.FieldOfView
Get the angular margin to apply (radians).
getMargin() - Method in class org.orekit.propagation.events.GeographicZoneDetector
Get the angular margin to apply (radians).
getMarkerName() - Method in class org.orekit.gnss.RinexHeader
Get name of the antenna marker.
getMarkerNumber() - Method in class org.orekit.gnss.RinexHeader
Get number of the antenna marker.
getMarkerType() - Method in class org.orekit.gnss.RinexHeader
Get type of the antenna marker.
getMars() - Static method in class org.orekit.bodies.CelestialBodyFactory
Get the Mars singleton body.
getMass() - Method in class org.orekit.files.ccsds.OGMFile
Get the spacecraft mass.
getMass() - Method in class org.orekit.propagation.conversion.NumericalPropagatorBuilder
Get the mass.
getMass() - Method in class org.orekit.propagation.FieldSpacecraftState
Gets the current mass.
getMass() - Method in class org.orekit.propagation.SpacecraftState
Gets the current mass.
getMass(AbsoluteDate) - Method in class org.orekit.propagation.analytical.AbstractAnalyticalPropagator
Get the mass.
getMass(AbsoluteDate) - Method in class org.orekit.propagation.analytical.AdapterPropagator
Get the mass.
getMass(AbsoluteDate) - Method in class org.orekit.propagation.analytical.AggregateBoundedPropagator
 
getMass(AbsoluteDate) - Method in class org.orekit.propagation.analytical.EcksteinHechlerPropagator
Get the mass.
getMass(AbsoluteDate) - Method in class org.orekit.propagation.analytical.Ephemeris
Get the mass.
getMass(AbsoluteDate) - Method in class org.orekit.propagation.analytical.gnss.GPSPropagator
Get the mass.
getMass(AbsoluteDate) - Method in class org.orekit.propagation.analytical.KeplerianPropagator
Get the mass.
getMass(AbsoluteDate) - Method in class org.orekit.propagation.analytical.tle.TLEPropagator
Get the mass.
getMass(AbsoluteDate) - Method in class org.orekit.propagation.integration.IntegratedEphemeris
Get the mass.
getMass(FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.analytical.FieldAbstractAnalyticalPropagator
Get the mass.
getMass(FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.analytical.FieldEcksteinHechlerPropagator
Get the mass.
getMass(FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.analytical.FieldKeplerianPropagator
Get the mass.
getMass(FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.integration.FieldIntegratedEphemeris
Get the mass.
getMasterStation() - Method in class org.orekit.estimation.measurements.TurnAroundRange
Get the master ground station from which measurement is performed.
getMatrix() - Method in class org.orekit.files.ccsds.OEMFile.CovarianceMatrix
Get the covariance matrix.
getMatrixLine(int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.PolynomialFunctionMatrix
Get a line of the matrix.
getMaxAlt() - Method in class org.orekit.forces.drag.atmosphere.HarrisPriester
Get the maximal altitude for the model.
getMaxAvailableDegree() - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
Get the maximal degree available in the last file parsed.
getMaxAvailableOrder() - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
Get the maximal order available in the last file parsed.
getMaxCheckInterval() - Method in class org.orekit.propagation.events.AbstractDetector
Get maximal time interval between switching function checks.
getMaxCheckInterval() - Method in class org.orekit.propagation.events.AdapterDetector
Get maximal time interval between switching function checks.
getMaxCheckInterval() - Method in interface org.orekit.propagation.events.EventDetector
Get maximal time interval between switching function checks.
getMaxCheckInterval() - Method in class org.orekit.propagation.events.FieldAbstractDetector
Get maximal time interval between switching function checks.
getMaxCheckInterval() - Method in interface org.orekit.propagation.events.FieldEventDetector
Get maximal time interval between switching function checks.
getMaxChunksDuration() - Method in class org.orekit.bodies.JPLEphemeridesLoader
Get the maximal chunks duration.
getMaxDate() - Method in class org.orekit.forces.drag.atmosphere.data.MarshallSolarActivityFutureEstimation
Gets the available data range maximum date.
getMaxDate() - Method in interface org.orekit.forces.drag.atmosphere.DTM2000InputParameters
Gets the available data range maximum date.
getMaxDate() - Method in interface org.orekit.forces.drag.atmosphere.JB2008InputParameters
Gets the available data range maximum date.
getMaxDate() - Method in interface org.orekit.forces.drag.atmosphere.NRLMSISE00InputParameters
Gets the available data range maximum date.
getMaxDate() - Method in class org.orekit.propagation.analytical.AggregateBoundedPropagator
 
getMaxDate() - Method in class org.orekit.propagation.analytical.Ephemeris
Get the last date of the range.
getMaxDate() - Method in interface org.orekit.propagation.BoundedPropagator
Get the last date of the range.
getMaxDate() - Method in interface org.orekit.propagation.FieldBoundedPropagator
Get the last date of the range.
getMaxDate() - Method in class org.orekit.propagation.integration.FieldIntegratedEphemeris
Get the last date of the range.
getMaxDate() - Method in class org.orekit.propagation.integration.IntegratedEphemeris
Get the last date of the range.
getMaxDegree() - Method in class org.orekit.forces.gravity.potential.CachedNormalizedSphericalHarmonicsProvider
Get the maximal supported degree.
getMaxDegree() - Method in class org.orekit.forces.gravity.potential.OceanTidesWave
Get the maximum supported degree.
getMaxDegree() - Method in interface org.orekit.forces.gravity.potential.SphericalHarmonicsProvider
Get the maximal supported degree.
getMaxIterationCount() - Method in class org.orekit.propagation.events.AbstractDetector
Get maximal number of iterations in the event time search.
getMaxIterationCount() - Method in class org.orekit.propagation.events.AdapterDetector
Get maximal number of iterations in the event time search.
getMaxIterationCount() - Method in interface org.orekit.propagation.events.EventDetector
Get maximal number of iterations in the event time search.
getMaxIterationCount() - Method in class org.orekit.propagation.events.FieldAbstractDetector
Get maximal number of iterations in the event time search.
getMaxIterationCount() - Method in interface org.orekit.propagation.events.FieldEventDetector
Get maximal number of iterations in the event time search.
getMaxOrder() - Method in class org.orekit.forces.gravity.potential.CachedNormalizedSphericalHarmonicsProvider
Get the maximal supported order.
getMaxOrder() - Method in class org.orekit.forces.gravity.potential.OceanTidesWave
Get the maximum supported order.
getMaxOrder() - Method in interface org.orekit.forces.gravity.potential.SphericalHarmonicsProvider
Get the maximal supported order.
getMaxOrder() - Method in enum org.orekit.utils.AngularDerivativesFilter
Get the maximum derivation order.
getMaxOrder() - Method in enum org.orekit.utils.CartesianDerivativesFilter
Get the maximum derivation order.
getMaxParseDegree() - Method in class org.orekit.forces.gravity.potential.OceanTidesReader
Get the degree limit for the next file parsing.
getMaxParseDegree() - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
Get the degree limit for the next file parsing.
getMaxParseOrder() - Method in class org.orekit.forces.gravity.potential.OceanTidesReader
Get the order limit for the next file parsing.
getMaxParseOrder() - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
Get the order limit for the next file parsing.
getMaxSigma() - Method in class org.orekit.estimation.measurements.modifiers.OutlierFilter
Get the value of the outlier detection limit.
getMaxSlots() - Method in class org.orekit.utils.GenericTimeStampedCache
Get the maximum number of independent cached time slots.
getMaxSpan() - Method in class org.orekit.utils.GenericTimeStampedCache
Get the maximum duration span in seconds of one slot.
getMaxValue() - Method in class org.orekit.utils.ParameterDriver
Get maximum parameter value.
getMeanAnomaly() - Method in class org.orekit.orbits.FieldKeplerianOrbit
Get the mean anomaly.
getMeanAnomaly() - Method in class org.orekit.orbits.KeplerianOrbit
Get the mean anomaly.
getMeanAnomaly() - Method in class org.orekit.propagation.analytical.tle.TLE
Get the mean anomaly.
getMeanAnomalyDot() - Method in class org.orekit.orbits.FieldKeplerianOrbit
Get the mean anomaly derivative.
getMeanAnomalyDot() - Method in class org.orekit.orbits.KeplerianOrbit
Get the mean anomaly derivative.
getMeanElementRate(SpacecraftState) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution
Computes the mean equinoctial elements rates dai / dt.
getMeanElementRate(SpacecraftState) - Method in interface org.orekit.propagation.semianalytical.dsst.forces.DSSTForceModel
Computes the mean equinoctial elements rates dai / dt.
getMeanElementRate(SpacecraftState) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseral
Computes the mean equinoctial elements rates dai / dt.
getMeanElementRate(SpacecraftState) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBody
Computes the mean equinoctial elements rates dai / dt.
getMeanElementRate(SpacecraftState) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonal
Computes the mean equinoctial elements rates dai / dt.
getMeanElementTheory() - Method in class org.orekit.files.ccsds.OMMFile.OMMMetaData
Get the description of the Mean Element Theory.
getMeanFlux(AbsoluteDate) - Method in class org.orekit.forces.drag.atmosphere.data.MarshallSolarActivityFutureEstimation
Get the value of the mean solar flux.
getMeanFlux(AbsoluteDate) - Method in interface org.orekit.forces.drag.atmosphere.DTM2000InputParameters
Get the value of the mean solar flux.
getMeanMotion() - Method in class org.orekit.files.ccsds.OMMFile
Get the orbit mean motion.
getMeanMotion() - Method in class org.orekit.gnss.GPSAlmanac
 
getMeanMotion() - Method in interface org.orekit.propagation.analytical.gnss.GPSOrbitalElements
Gets the Mean Motion.
getMeanMotion() - Method in class org.orekit.propagation.analytical.tle.TLE
Get the mean motion.
getMeanMotion() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
Get the Keplerian mean motion.
getMeanMotionDot() - Method in class org.orekit.files.ccsds.OMMFile
Get the first time derivative of the mean motion.
getMeanMotionDotDot() - Method in class org.orekit.files.ccsds.OMMFile
Get the second time derivative of the mean motion.
getMeanMotionFirstDerivative() - Method in class org.orekit.propagation.analytical.tle.TLE
Get the mean motion first derivative.
getMeanMotionSecondDerivative() - Method in class org.orekit.propagation.analytical.tle.TLE
Get the mean motion second derivative.
getMeanObliquityFunction() - Method in enum org.orekit.utils.IERSConventions
Get the function computing mean obliquity of the ecliptic.
getMeasurement() - Method in class org.orekit.files.ccsds.TDMFile.Observation
Getter for the measurement.
getMeasurementsParametersDrivers(boolean) - Method in class org.orekit.estimation.leastsquares.BatchLSEstimator
Get the measurements parameters supported by this estimator (including measurements and modifiers).
getMeasurementType() - Method in enum org.orekit.gnss.ObservationType
Get the measurement type.
getMercury() - Static method in class org.orekit.bodies.CelestialBodyFactory
Get the Mercury singleton body.
getMessage() - Method in exception org.orekit.errors.OrekitException
getMessage() - Method in exception org.orekit.errors.OrekitIllegalArgumentException
getMessage() - Method in exception org.orekit.errors.OrekitIllegalStateException
getMessage() - Method in exception org.orekit.errors.OrekitInternalError
getMessage() - Method in exception org.orekit.errors.OrekitIOException
getMessage() - Method in exception org.orekit.errors.OrekitParseException
getMessage(Locale) - Method in interface org.orekit.errors.LocalizedException
Gets the message in a specified locale.
getMessage(Locale) - Method in exception org.orekit.errors.OrekitException
Gets the message in a specified locale.
getMessage(Locale) - Method in exception org.orekit.errors.OrekitIllegalArgumentException
Gets the message in a specified locale.
getMessage(Locale) - Method in exception org.orekit.errors.OrekitIllegalStateException
Gets the message in a specified locale.
getMessage(Locale) - Method in exception org.orekit.errors.OrekitInternalError
Gets the message in a specified locale.
getMessage(Locale) - Method in exception org.orekit.errors.OrekitIOException
Gets the message in a specified locale.
getMessage(Locale) - Method in exception org.orekit.errors.OrekitParseException
Gets the message in a specified locale.
getMetaData() - Method in class org.orekit.files.ccsds.OEMFile.EphemeridesBlock
Get the meta-data for the block.
getMetaData() - Method in class org.orekit.files.ccsds.OGMFile
Get the meta data.
getMetaData() - Method in class org.orekit.files.ccsds.OMMFile
Get the meta data.
getMetaData() - Method in class org.orekit.files.ccsds.OPMFile
Get the meta data.
getMetaData() - Method in class org.orekit.files.ccsds.TDMFile.ObservationsBlock
Get the meta-data for the block.
getMetaDataComment() - Method in class org.orekit.files.ccsds.OPMFile
Get the comment for meta-data.
getMHzFrequency() - Method in enum org.orekit.gnss.Frequency
Get the value of the frequency in MHz.
getMilliInWeek() - Method in class org.orekit.time.GPSDate
Get the number of milliseconds since week start.
getMinAlt() - Method in class org.orekit.forces.drag.atmosphere.HarrisPriester
Get the minimal altitude for the model.
getMinDate() - Method in class org.orekit.forces.drag.atmosphere.data.MarshallSolarActivityFutureEstimation
Gets the available data range minimum date.
getMinDate() - Method in interface org.orekit.forces.drag.atmosphere.DTM2000InputParameters
Gets the available data range minimum date.
getMinDate() - Method in interface org.orekit.forces.drag.atmosphere.JB2008InputParameters
Gets the available data range minimum date.
getMinDate() - Method in interface org.orekit.forces.drag.atmosphere.NRLMSISE00InputParameters
Gets the available data range minimum date.
getMinDate() - Method in class org.orekit.propagation.analytical.AggregateBoundedPropagator
 
getMinDate() - Method in class org.orekit.propagation.analytical.Ephemeris
Get the first date of the range.
getMinDate() - Method in interface org.orekit.propagation.BoundedPropagator
Get the first date of the range.
getMinDate() - Method in interface org.orekit.propagation.FieldBoundedPropagator
Get the first date of the range.
getMinDate() - Method in class org.orekit.propagation.integration.FieldIntegratedEphemeris
Get the first date of the range.
getMinDate() - Method in class org.orekit.propagation.integration.IntegratedEphemeris
Get the first date of the range.
getMinElevation() - Method in class org.orekit.gnss.DOPComputer
Get the minimum elevation.
getMinElevation() - Method in class org.orekit.propagation.events.ElevationDetector
Returns the currently configured minimum valid elevation value.
getMinElevation() - Method in class org.orekit.propagation.events.FieldElevationDetector
Returns the currently configured minimum valid elevation value.
getMinute() - Method in class org.orekit.time.TimeComponents
Get the minute number.
getMinutesFromUTC() - Method in class org.orekit.time.TimeComponents
Get the offset between the specified date and UTC.
getMinValue() - Method in class org.orekit.utils.ParameterDriver
Get minimum parameter value.
getMissionReferenceDate() - Method in class org.orekit.files.ccsds.ODMFile
Get reference date for Mission Elapsed Time and Mission Relative Time time systems.
getMissionReferenceDate() - Method in class org.orekit.files.ccsds.ODMParser
Get initial date.
getMissionReferenceDate() - Method in class org.orekit.files.ccsds.TDMParser
Get initial date.
getMjd() - Method in class org.orekit.frames.EOPEntry
Get the entry date (modified julian day, 00h00 UTC scale).
getMJD() - Method in class org.orekit.time.DateComponents
Get the modified julian day.
getMJDRef() - Method in class org.orekit.time.OffsetModel
Get the reference date of the linear model as a modified julian day.
getMOD(boolean) - Static method in class org.orekit.frames.FramesFactory
Get the MOD reference frame.
getMOD(IERSConventions) - Static method in class org.orekit.frames.FramesFactory
Get the MOD reference frame.
getMode() - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData
Getter for the mode.
getMode() - Method in class org.orekit.propagation.AbstractPropagator
Get the current operating mode of the propagator.
getMode() - Method in class org.orekit.propagation.FieldAbstractPropagator
Get the current operating mode of the propagator.
getMode() - Method in interface org.orekit.propagation.FieldPropagator
Get the current operating mode of the propagator.
getMode() - Method in interface org.orekit.propagation.Propagator
Get the current operating mode of the propagator.
getModel() - Method in class org.orekit.propagation.conversion.AbstractPropagatorConverter
Get the Jacobian of the function computing position/velocity at sample points.
getModel() - Method in class org.orekit.propagation.conversion.FiniteDifferencePropagatorConverter
Get the Jacobian of the function computing position/velocity at sample points.
getModel() - Method in class org.orekit.propagation.conversion.JacobianPropagatorConverter
Get the Jacobian of the function computing position/velocity at sample points.
getModelName() - Method in class org.orekit.models.earth.GeoMagneticField
Returns the model name.
getModels() - Method in class org.orekit.models.earth.GeoMagneticModelLoader
Returns a Collection of the GeoMagneticField models that have been successfully loaded.
getModifiedJulianEpoch(Field<T>) - Static method in class org.orekit.time.FieldAbsoluteDate
Reference epoch for modified julian dates: 1858-11-17T00:00:00 Terrestrial Time.
getModifiedRodrigues(double) - Method in class org.orekit.utils.AngularCoordinates
Convert rotation, rate and acceleration to modified Rodrigues vector and derivatives.
getModifiedRodrigues(double) - Method in class org.orekit.utils.FieldAngularCoordinates
Convert rotation, rate and acceleration to modified Rodrigues vector and derivatives.
getModifiers() - Method in class org.orekit.estimation.measurements.AbstractMeasurement
Get the modifiers that apply to a measurement.
getModifiers() - Method in class org.orekit.estimation.measurements.generation.AbstractMeasurementBuilder
Get the modifiers that apply to a measurement.
getModifiers() - Method in interface org.orekit.estimation.measurements.generation.MeasurementBuilder
Get the modifiers that apply to a measurement.
getModifiers() - Method in interface org.orekit.estimation.measurements.ObservedMeasurement
Get the modifiers that apply to a measurement.
getMomentum() - Method in class org.orekit.utils.FieldPVCoordinates
Gets the momentum.
getMomentum() - Method in class org.orekit.utils.PVCoordinates
Gets the momentum.
getMonth() - Method in class org.orekit.time.DateComponents
Get the month.
getMonth(int) - Static method in enum org.orekit.time.Month
Get the month corresponding to a number.
getMonthEnum() - Method in class org.orekit.time.DateComponents
Get the month as an enumerate.
getMoon() - Static method in class org.orekit.bodies.CelestialBodyFactory
Get the Moon singleton body.
getMu() - Method in class org.orekit.files.ccsds.ODMParser
Get gravitational coefficient.
getMu() - Method in class org.orekit.files.ccsds.OEMFile.EphemeridesBlock
 
getMu() - Method in class org.orekit.files.ccsds.OEMFile.OemSatelliteEphemeris
 
getMu() - Method in interface org.orekit.files.general.EphemerisFile.EphemerisSegment
Get the standard gravitational parameter for the satellite.
getMu() - Method in interface org.orekit.files.general.EphemerisFile.SatelliteEphemeris
Get the standard gravitational parameter for the satellite.
getMu() - Method in class org.orekit.files.general.OrekitEphemerisFile.OrekitEphemerisSegment
 
getMu() - Method in class org.orekit.files.general.OrekitEphemerisFile.OrekitSatelliteEphemeris
 
getMu() - Method in class org.orekit.files.sp3.SP3File.SP3Ephemeris
 
getMu() - Method in class org.orekit.forces.gravity.HolmesFeatherstoneAttractionModel
Get the central attraction coefficient μ.
getMu() - Method in class org.orekit.forces.gravity.NewtonianAttraction
Get the central attraction coefficient μ.
getMu() - Method in class org.orekit.forces.gravity.potential.CachedNormalizedSphericalHarmonicsProvider
Get the central body attraction coefficient.
getMu() - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
Get the central body attraction coefficient.
getMu() - Method in interface org.orekit.forces.gravity.potential.SphericalHarmonicsProvider
Get the central body attraction coefficient.
getMu() - Method in class org.orekit.orbits.FieldOrbit
 
getMu() - Method in class org.orekit.orbits.Orbit
Get the central acceleration constant.
getMu() - Method in class org.orekit.propagation.conversion.AbstractPropagatorBuilder
Get the central attraction coefficient (µ - m³/s²) value.
getMu() - Method in class org.orekit.propagation.FieldSpacecraftState
Get the central attraction coefficient.
getMu() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
Get the central attraction coefficient μ.
getMu() - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator
Get the central attraction coefficient μ.
getMu() - Method in class org.orekit.propagation.integration.FieldStateMapper
Get the central attraction coefficient μ.
getMu() - Method in class org.orekit.propagation.integration.StateMapper
Get the central attraction coefficient μ.
getMu() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
Get the central body attraction coefficient.
getMu() - Method in class org.orekit.propagation.SpacecraftState
Get the central attraction coefficient.
getMU() - Static method in class org.orekit.propagation.analytical.gnss.GPSPropagator
Get the Earth gravity coefficient used for GPS propagation.
getMU() - Static method in class org.orekit.propagation.analytical.tle.TLEPropagator
Get the Earth gravity coefficient used for TLE propagation.
getMuCreated() - Method in class org.orekit.files.ccsds.ODMFile
Get the gravitational coefficient created from the knowledge of the central body.
getMuParsed() - Method in class org.orekit.files.ccsds.ODMFile
Get the gravitational coefficient parsed in the ODM File.
getMuSet() - Method in class org.orekit.files.ccsds.ODMFile
Get the gravitational coefficient set by the user.
getMuUsed() - Method in class org.orekit.files.ccsds.ODMFile
Get the used gravitational coefficient.
getN() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.CoefficientsFactory.NSKey
Get n.
getNadir() - Method in class org.orekit.bodies.FieldGeodeticPoint
Get the direction below the point, expressed in parent shape frame.
getNadir() - Method in class org.orekit.bodies.GeodeticPoint
Get the direction below the point, expressed in parent shape frame.
getNadir() - Method in class org.orekit.frames.TopocentricFrame
Get the nadir direction of topocentric frame, expressed in parent shape frame.
getName() - Method in interface org.orekit.bodies.CelestialBody
Get the name of the body.
getName() - Method in class org.orekit.data.NamedData
Get the name of the data.
getName() - Method in class org.orekit.forces.maneuvers.ConstantThrustManeuver
Get the name.
getName() - Method in class org.orekit.frames.Frame
Get the name.
getName() - Method in enum org.orekit.frames.ITRFVersion
Get the name the frame version.
getName() - Method in enum org.orekit.frames.Predefined
Get the name of the frame.
getName() - Method in enum org.orekit.gnss.antenna.SatelliteAntennaCode
Deprecated.
Get the IGS name for the antenna code.
getName() - Method in enum org.orekit.gnss.antenna.SatelliteType
Get the IGS name for the antenna code.
getName() - Method in enum org.orekit.gnss.Frequency
Get the RINEX name for the frequency.
getName() - Method in interface org.orekit.propagation.AdditionalStateProvider
Get the name of the additional state.
getName() - Method in class org.orekit.propagation.analytical.gnss.ClockCorrectionsProvider
Get the name of the additional state.
getName() - Method in interface org.orekit.propagation.FieldAdditionalStateProvider
Get the name of the additional state.
getName() - Method in interface org.orekit.propagation.integration.AdditionalEquations
Get the name of the additional state.
getName() - Method in interface org.orekit.propagation.integration.FieldAdditionalEquations
Get the name of the additional state.
getName() - Method in class org.orekit.propagation.numerical.JacobiansMapper
Get the name of the partial Jacobians.
getName() - Method in class org.orekit.propagation.numerical.PartialDerivativesEquations
Get the name of the additional state.
getName() - Method in class org.orekit.time.BDTScale
Get the name time scale.
getName() - Method in class org.orekit.time.GalileoScale
Get the name time scale.
getName() - Method in class org.orekit.time.GLONASSScale
Get the name time scale.
getName() - Method in class org.orekit.time.GMSTScale
Get the name time scale.
getName() - Method in class org.orekit.time.GPSScale
Get the name time scale.
getName() - Method in class org.orekit.time.IRNSSScale
Get the name time scale.
getName() - Method in class org.orekit.time.QZSSScale
Get the name time scale.
getName() - Method in class org.orekit.time.TAIScale
Get the name time scale.
getName() - Method in class org.orekit.time.TCBScale
Get the name time scale.
getName() - Method in class org.orekit.time.TCGScale
Get the name time scale.
getName() - Method in class org.orekit.time.TDBScale
Get the name time scale.
getName() - Method in interface org.orekit.time.TimeScale
Get the name time scale.
getName() - Method in class org.orekit.time.TTScale
Get the name time scale.
getName() - Method in class org.orekit.time.UT1Scale
Get the name time scale.
getName() - Method in class org.orekit.time.UTCScale
Get the name time scale.
getName() - Method in class org.orekit.utils.ParameterDriver
Get name.
getNbManeuvers() - Method in class org.orekit.files.ccsds.OPMFile
Get the number of maneuvers present in the OPM.
getNbParams() - Method in class org.orekit.utils.ParameterDriversList
Get the number of parameters with different names.
getNbSpecies() - Method in class org.orekit.models.earth.displacement.OceanLoadingCoefficients
Get the number of species.
getNbTides(int) - Method in class org.orekit.models.earth.displacement.OceanLoadingCoefficients
Get the number of tides for one species.
getNeighbors(AbsoluteDate) - Method in class org.orekit.frames.EOPHistory
Get the entries surrounding a central date.
getNeighbors(AbsoluteDate) - Method in class org.orekit.utils.GenericTimeStampedCache
Get the entries surrounding a central date.
getNeighbors(AbsoluteDate) - Method in class org.orekit.utils.ImmutableTimeStampedCache
Get the entries surrounding a central date.
getNeighbors(AbsoluteDate) - Method in interface org.orekit.utils.TimeStampedCache
Get the entries surrounding a central date.
getNeighborsSize() - Method in class org.orekit.utils.GenericTimeStampedCache
Get the fixed size of the arrays to be returned by GenericTimeStampedCache.getNeighbors(AbsoluteDate).
getNeighborsSize() - Method in class org.orekit.utils.ImmutableTimeStampedCache
 
getNeighborsSize() - Method in interface org.orekit.utils.TimeStampedCache
Get the fixed size of the lists returned by TimeStampedCache.getNeighbors(AbsoluteDate).
getNeptune() - Static method in class org.orekit.bodies.CelestialBodyFactory
Get the Neptune singleton body.
getNewSlotQuantumGap() - Method in class org.orekit.utils.GenericTimeStampedCache
Get quantum gap above which a new slot is created instead of extending an existing one.
getNewState() - Method in class org.orekit.propagation.events.EventState.EventOccurrence
Get the new state for a reset action.
getNewState() - Method in class org.orekit.propagation.events.FieldEventState.EventOccurrence
Get the new state for a reset action.
getNewtonianAttractionForceModel() - Method in class org.orekit.propagation.numerical.FieldNumericalPropagator
Deprecated.
as of 9.1, this method is deprecated, the Newtonian attraction force model (if any) is the last in the FieldNumericalPropagator.getAllForceModels()
getNode(AbsoluteDate) - Method in interface org.orekit.bodies.IAUPole
Get the body Q Node direction in ICRF frame.
getNode(FieldAbsoluteDate<T>) - Method in interface org.orekit.bodies.IAUPole
Get the body Q Node direction in ICRF frame.
getNoise() - Method in class org.orekit.estimation.measurements.generation.AbstractMeasurementBuilder
Generate a noise vector.
getNominalTidalDisplacement() - Method in enum org.orekit.utils.IERSConventions
Get the nominal values of the displacement numbers.
getNonInterpolatingEOPHistory() - Method in class org.orekit.frames.EOPHistory
Get non-interpolating version of the instance.
getNonInterpolatingProvider() - Method in interface org.orekit.frames.EOPBasedTransformProvider
Get a version of the provider that does not cache tidal corrections.
getNonInterpolatingProvider() - Method in class org.orekit.frames.GTODProvider
Get a version of the provider that does not cache tidal corrections.
getNonInterpolatingTransform(Frame, Frame, AbsoluteDate) - Static method in class org.orekit.frames.FramesFactory
Get the transform between two frames, suppressing all interpolation.
getNonInterpolatingTransform(Frame, Frame, FieldAbsoluteDate<T>) - Static method in class org.orekit.frames.FramesFactory
Get the transform between two frames, suppressing all interpolation.
getNonPolynomialSize() - Method in class org.orekit.data.PoissonSeries
Get the number of different terms in the non-polynomial part.
getNonRotatinOriginNutationCorrection(AbsoluteDate) - Method in class org.orekit.frames.EOPHistory
Get the correction to the nutation parameters for Non-Rotating Origin paradigm.
getNonRotatinOriginNutationCorrection(FieldAbsoluteDate<T>) - Method in class org.orekit.frames.EOPHistory
Get the correction to the nutation parameters for Non-Rotating Origin paradigm.
getNoradID() - Method in class org.orekit.files.ccsds.OMMFile
Get the NORAD Catalog Number ("Satellite Number").
getNormal() - Method in class org.orekit.forces.BoxAndSolarArraySpacecraft.Facet
Get unit normal vector.
getNormal(AbsoluteDate, Frame, FieldVector3D<DerivativeStructure>, FieldRotation<DerivativeStructure>) - Method in class org.orekit.forces.BoxAndSolarArraySpacecraft
Get solar array normal in spacecraft frame.
getNormal(AbsoluteDate, Frame, Vector3D, Rotation) - Method in class org.orekit.forces.BoxAndSolarArraySpacecraft
Get solar array normal in spacecraft frame.
getNormal(FieldAbsoluteDate<T>, Frame, FieldVector3D<T>, FieldRotation<T>) - Method in class org.orekit.forces.BoxAndSolarArraySpacecraft
Get solar array normal in spacecraft frame.
getNormalGravity(double) - Method in class org.orekit.models.earth.ReferenceEllipsoid
Gets the normal gravity, that is gravity just due to the reference ellipsoid's potential.
getNormalizedCnm(int, int) - Method in interface org.orekit.forces.gravity.potential.NormalizedSphericalHarmonicsProvider.NormalizedSphericalHarmonics
Get a spherical harmonic cosine coefficient.
getNormalizedProvider(double, double, TideSystem, double[][], double[][]) - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory
Create a time-independent NormalizedSphericalHarmonicsProvider from canonical coefficients.
getNormalizedProvider(int, int) - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory
Get the gravity field coefficients provider from the first supported file.
getNormalizedProvider(UnnormalizedSphericalHarmonicsProvider) - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory
getNormalizedSnm(int, int) - Method in interface org.orekit.forces.gravity.potential.NormalizedSphericalHarmonicsProvider.NormalizedSphericalHarmonics
Get a spherical harmonic sine coefficient.
getNormalizedValue() - Method in class org.orekit.utils.ParameterDriver
Get normalized value.
getNorth() - Method in class org.orekit.bodies.FieldGeodeticPoint
Get the direction to the north of point, expressed in parent shape frame.
getNorth() - Method in class org.orekit.bodies.GeodeticPoint
Get the direction to the north of point, expressed in parent shape frame.
getNorth() - Method in class org.orekit.frames.TopocentricFrame
Get the north direction of topocentric frame, expressed in parent shape frame.
getNorthOffsetDriver() - Method in class org.orekit.estimation.measurements.GroundStation
Get a driver allowing to change station position along North axis.
getNumber() - Method in interface org.orekit.estimation.measurements.EstimationsProvider
Get the number of evaluations available.
getNumber() - Method in enum org.orekit.time.Month
Get the month number.
getNumberOfEpochs() - Method in class org.orekit.files.sp3.SP3File
Returns the number of epochs contained in this orbit file.
getNutationArguments(TimeScale) - Method in enum org.orekit.utils.IERSConventions
Get the fundamental nutation arguments.
getNutationCorrectionConverter() - Method in enum org.orekit.utils.IERSConventions
Create a function converting nutation corrections between δX/δY and δΔψ/δΔε.
getNutationFunction() - Method in enum org.orekit.utils.IERSConventions
Get the function computing the nutation angles.
getNutationReferenceEpoch() - Method in enum org.orekit.utils.IERSConventions
Get the reference epoch for fundamental nutation arguments.
getObjectID() - Method in class org.orekit.files.ccsds.ODMMetaData
Get the spacecraft ID for which the orbit state is provided.
getObjectiveFunction() - Method in class org.orekit.propagation.conversion.AbstractPropagatorConverter
Get the function computing position/velocity at sample points.
getObjectiveFunction() - Method in class org.orekit.propagation.conversion.FiniteDifferencePropagatorConverter
Get the function computing position/velocity at sample points.
getObjectiveFunction() - Method in class org.orekit.propagation.conversion.JacobianPropagatorConverter
Get the function computing position/velocity at sample points.
getObjectName() - Method in class org.orekit.files.ccsds.ODMMetaData
Get the spacecraft name for which the orbit state is provided.
getObservationCode() - Method in class org.orekit.gnss.RinexHeader
Get the observation code of the average phasecenter position w/r to antenna reference point.
getObservationData() - Method in class org.orekit.gnss.ObservationDataSet
Get list of observation data.
getObservationDataSets() - Method in class org.orekit.gnss.RinexLoader
Get parsed rinex observations data sets.
getObservations() - Method in class org.orekit.files.ccsds.TDMFile.ObservationsBlock
Get the list of Observations data lines.
getObservations() - Method in class org.orekit.gnss.RinexLoader
Deprecated.
getObservationsBlocks() - Method in class org.orekit.files.ccsds.TDMFile
Get the list of observations blocks as an unmodifiable list.
getObservationsComment() - Method in class org.orekit.files.ccsds.TDMFile.ObservationsBlock
Get the observations data lines comment.
getObservationType() - Method in class org.orekit.gnss.ObservationData
Get the observation type.
getObservedMeasurement() - Method in class org.orekit.estimation.measurements.EstimatedMeasurement
Get the associated observed measurement.
getObservedMeasurement() - Method in class org.orekit.estimation.sequential.MeasurementDecorator
Get the observed measurement.
getObservedValue() - Method in class org.orekit.estimation.measurements.AbstractMeasurement
Get the observed value.
getObservedValue() - Method in interface org.orekit.estimation.measurements.ComparableMeasurement
Get the observed value.
getObservedValue() - Method in class org.orekit.estimation.measurements.EstimatedMeasurement
Get the observed value.
getObserver() - Method in class org.orekit.propagation.events.AngularSeparationDetector
Get the observer for the spacecraft.
getObserverName() - Method in class org.orekit.gnss.RinexHeader
Get name of the observer.
getObservers() - Method in class org.orekit.utils.ParameterDriver
Get the observers for this driver.
getOcculted() - Method in class org.orekit.propagation.events.EclipseDetector
Get the occulted body.
getOcculted() - Method in class org.orekit.propagation.events.FieldEclipseDetector
Get the occulted body.
getOccultedRadius() - Method in class org.orekit.propagation.events.EclipseDetector
Get the occulted body radius (m).
getOccultedRadius() - Method in class org.orekit.propagation.events.FieldEclipseDetector
Get the occulted body radius (m).
getOcculting() - Method in class org.orekit.propagation.events.EclipseDetector
Get the occulting body.
getOcculting() - Method in class org.orekit.propagation.events.FieldEclipseDetector
Get the occulting body.
getOccultingRadius() - Method in class org.orekit.propagation.events.EclipseDetector
Get the occulting body radius (m).
getOccultingRadius() - Method in class org.orekit.propagation.events.FieldEclipseDetector
Get the occulting body radius (m).
getOceanLoadDeformationCoefficients() - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory
Get the configured ocean load deformation coefficients.
getOceanPoleTide(EOPHistory) - Method in enum org.orekit.utils.IERSConventions
Get the function computing ocean pole tide (ΔC₂₁, ΔS₂₁).
getOceanTidesWaves(int, int) - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory
Get the ocean tides waves from the first supported file.
getODMFile() - Method in class org.orekit.files.ccsds.ODMMetaData
Get the ODM file to which these meta-data belong.
getOffset() - Method in class org.orekit.time.OffsetModel
Offset at reference date in seconds (TAI minus UTC).
getOffset(AbsoluteDate) - Method in class org.orekit.forces.gravity.potential.CachedNormalizedSphericalHarmonicsProvider
Get the offset from reference date for the harmonics.
getOffset(AbsoluteDate) - Method in interface org.orekit.forces.gravity.potential.SphericalHarmonicsProvider
Get the offset from reference date for the harmonics.
getOffsetGeodeticPoint() - Method in class org.orekit.estimation.measurements.GroundStation
Deprecated.
getOffsetGeodeticPoint(AbsoluteDate) - Method in class org.orekit.estimation.measurements.GroundStation
Get the geodetic point at the center of the offset frame.
getOffsetToInertial(Frame, AbsoluteDate) - Method in class org.orekit.estimation.measurements.GroundStation
Get the transform between offset frame and inertial frame.
getOffsetToInertial(Frame, AbsoluteDate, DSFactory, Map<String, Integer>) - Method in class org.orekit.estimation.measurements.GroundStation
Get the transform between offset frame and inertial frame with derivatives.
getOffsetToInertial(Frame, FieldAbsoluteDate<DerivativeStructure>, DSFactory, Map<String, Integer>) - Method in class org.orekit.estimation.measurements.GroundStation
Get the transform between offset frame and inertial frame with derivatives.
getOmega() - Method in class org.orekit.data.DelaunayArguments
Get the mean longitude of the ascending node of the Moon.
getOmega() - Method in class org.orekit.data.FieldDelaunayArguments
Get the mean longitude of the ascending node of the Moon.
getOmega0() - Method in class org.orekit.gnss.GPSAlmanac
 
getOmega0() - Method in interface org.orekit.propagation.analytical.gnss.GPSOrbitalElements
Gets the Longitude of Ascending Node of Orbit Plane at Weekly Epoch.
getOmegaDot() - Method in class org.orekit.data.DelaunayArguments
Get the mean longitude of the ascending node of the Moon time derivative.
getOmegaDot() - Method in class org.orekit.data.FieldDelaunayArguments
Get the mean longitude of the ascending node of the Moon time derivative.
getOmegaDot() - Method in class org.orekit.gnss.GPSAlmanac
 
getOmegaDot() - Method in interface org.orekit.propagation.analytical.gnss.GPSOrbitalElements
Gets the Rate of Right Ascension.
getOptimum() - Method in class org.orekit.estimation.leastsquares.BatchLSEstimator
Get the optimum found.
getOrbit() - Method in class org.orekit.propagation.FieldSpacecraftState
Gets the current orbit.
getOrbit() - Method in class org.orekit.propagation.SpacecraftState
Gets the current orbit.
getOrbitalParametersDrivers() - Method in class org.orekit.propagation.conversion.AbstractPropagatorBuilder
Get the drivers for the configurable orbital parameters.
getOrbitalParametersDrivers() - Method in interface org.orekit.propagation.conversion.PropagatorBuilder
Get the drivers for the configurable orbital parameters.
getOrbitalParametersDrivers(boolean) - Method in class org.orekit.estimation.leastsquares.BatchLSEstimator
Get the orbital parameters supported by this estimator.
getOrbitalParametersDrivers(boolean) - Method in class org.orekit.estimation.sequential.KalmanEstimator
Get the orbital parameters supported by this estimator.
getOrbitType() - Method in class org.orekit.files.sp3.SP3File
Returns the SP3File.SP3OrbitType for this SP3 file.
getOrbitType() - Method in class org.orekit.propagation.conversion.AbstractPropagatorBuilder
Get the orbit type expected for the 6 first parameters in PropagatorBuilder.buildPropagator(double[]).
getOrbitType() - Method in interface org.orekit.propagation.conversion.PropagatorBuilder
Get the orbit type expected for the 6 first parameters in PropagatorBuilder.buildPropagator(double[]).
getOrbitType() - Method in class org.orekit.propagation.events.PositionAngleDetector
Get the orbit type defining the angle type.
getOrbitType() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
Get propagation parameter type.
getOrbitType() - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator
Get propagation parameter type.
getOrbitType() - Method in class org.orekit.propagation.integration.FieldStateMapper
Get propagation parameter type.
getOrbitType() - Method in class org.orekit.propagation.integration.StateMapper
Get propagation parameter type.
getOrbitType() - Method in class org.orekit.propagation.numerical.FieldNumericalPropagator
Get propagation parameter type.
getOrbitType() - Method in class org.orekit.propagation.numerical.NumericalPropagator
Get propagation parameter type.
getOrbitTypeKey() - Method in class org.orekit.files.sp3.SP3File
Returns the orbit type key for this SP3 file.
getOrdinateGrid() - Method in class org.orekit.utils.InterpolationTableLoader
Returns a copy of the ordinate grid for the interpolation function.
getOrientation() - Method in class org.orekit.attitudes.Attitude
Get the complete orientation including spin.
getOrientation() - Method in class org.orekit.attitudes.FieldAttitude
Get the complete orientation including spin.
getOrigin() - Method in enum org.orekit.frames.HelmertTransformation.Predefined
Get the origin ITRF.
getOrigin() - Method in class org.orekit.frames.ITRFVersion.Converter
Get the origin ITRF.
getOriginator() - Method in class org.orekit.files.ccsds.ODMFile
Get the file originator.
getOriginator() - Method in class org.orekit.files.ccsds.TDMFile
Get the file originator.
getP() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
Get the y component of inclination vector.
getPa() - Method in class org.orekit.data.BodiesElements
Get the general accumulated precession in longitude.
getPa() - Method in class org.orekit.data.FieldBodiesElements
Get the general accumulated precession in longitude.
getPa() - Method in class org.orekit.files.ccsds.OGMFile
Get the orbit argument of pericenter.
getPa() - Method in class org.orekit.gnss.GPSAlmanac
 
getPa() - Method in interface org.orekit.propagation.analytical.gnss.GPSOrbitalElements
Gets the Argument of Perigee.
getPaDot() - Method in class org.orekit.data.BodiesElements
Get the general accumulated precession in longitude time derivative.
getPaDot() - Method in class org.orekit.data.FieldBodiesElements
Get the general accumulated precession in longitude time derivative.
getParameterDerivatives(ParameterDriver) - Method in class org.orekit.estimation.measurements.EstimatedMeasurement
Get the partial derivatives of the simulated measurement with respect to a parameter.
getParameterDriver(String) - Method in class org.orekit.forces.AbstractForceModel
Get parameter value from its name.
getParameterDriver(String) - Method in interface org.orekit.forces.ForceModel
Get parameter value from its name.
getParameters() - Method in interface org.orekit.forces.ForceModel
Get force model parameters.
getParameters() - Method in interface org.orekit.models.earth.MappingFunction
Get tropospheric model parameters.
getParameters() - Method in class org.orekit.propagation.numerical.JacobiansMapper
Get the number of parameters.
getParameters(Field<T>) - Method in interface org.orekit.forces.ForceModel
Get force model parameters.
getParameters(Field<T>) - Method in interface org.orekit.models.earth.MappingFunction
Get tropospheric model parameters.
getParameters(FieldSpacecraftState<DerivativeStructure>, DiscreteTroposphericModel) - Method in class org.orekit.estimation.measurements.modifiers.TroposphericDSConverter
Get the tropospheric model parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.AbstractMeasurement
Get the drivers for this measurement parameters, including its modifiers parameters.
getParametersDrivers() - Method in interface org.orekit.estimation.measurements.EstimationModifier
Get the drivers for this modifier parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.AngularIonosphericDelayModifier
Get the drivers for this modifier parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.AngularRadioRefractionModifier
Get the drivers for this modifier parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.AngularTroposphericDelayModifier
Get the drivers for this modifier parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.Bias
Get the drivers for this modifier parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.OnBoardAntennaInterSatellitesRangeModifier
Get the drivers for this modifier parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.OnBoardAntennaRangeModifier
Get the drivers for this modifier parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.OnBoardAntennaTurnAroundRangeModifier
Get the drivers for this modifier parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.OutlierFilter
Get the drivers for this modifier parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.PhaseAmbiguityModifier
Get the drivers for this modifier parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.RangeIonosphericDelayModifier
Get the drivers for this modifier parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.RangeRateIonosphericDelayModifier
Get the drivers for this modifier parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.RangeRateTroposphericDelayModifier
Get the drivers for this modifier parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.RangeTroposphericDelayModifier
Get the drivers for this modifier parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.TurnAroundRangeIonosphericDelayModifier
Get the drivers for this modifier parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.TurnAroundRangeTroposphericDelayModifier
Get the drivers for this modifier parameters.
getParametersDrivers() - Method in interface org.orekit.estimation.measurements.ObservedMeasurement
Get the drivers for this measurement parameters, including its modifiers parameters.
getParametersDrivers() - Method in class org.orekit.forces.drag.DragForce
Get the drivers for force model parameters.
getParametersDrivers() - Method in interface org.orekit.forces.ForceModel
Get the drivers for force model parameters.
getParametersDrivers() - Method in class org.orekit.forces.gravity.HolmesFeatherstoneAttractionModel
Get the drivers for force model parameters.
getParametersDrivers() - Method in class org.orekit.forces.gravity.NewtonianAttraction
Get the drivers for force model parameters.
getParametersDrivers() - Method in class org.orekit.forces.gravity.OceanTides
Get the drivers for force model parameters.
getParametersDrivers() - Method in class org.orekit.forces.gravity.Relativity
Get the drivers for force model parameters.
getParametersDrivers() - Method in class org.orekit.forces.gravity.SolidTides
Get the drivers for force model parameters.
getParametersDrivers() - Method in class org.orekit.forces.gravity.ThirdBodyAttraction
Get the drivers for force model parameters.
getParametersDrivers() - Method in class org.orekit.forces.HarmonicParametricAcceleration
Get the drivers for force model parameters.
getParametersDrivers() - Method in class org.orekit.forces.maneuvers.ConstantThrustManeuver
Get the drivers for force model parameters.
getParametersDrivers() - Method in class org.orekit.forces.PolynomialParametricAcceleration
Get the drivers for force model parameters.
getParametersDrivers() - Method in class org.orekit.forces.radiation.SolarRadiationPressure
Get the drivers for force model parameters.
getParametersDrivers() - Method in class org.orekit.models.earth.EstimatedTroposphericModel
 
getParametersDrivers() - Method in class org.orekit.models.earth.GlobalMappingFunctionModel
Get the drivers for tropospheric model parameters.
getParametersDrivers() - Method in interface org.orekit.models.earth.MappingFunction
Get the drivers for tropospheric model parameters.
getParametersDrivers() - Method in class org.orekit.models.earth.MendesPavlisModel
Get the drivers for tropospheric model parameters.
getParametersDrivers() - Method in class org.orekit.models.earth.NiellMappingFunctionModel
 
getParametersDrivers() - Method in interface org.orekit.models.earth.TroposphericModel
Get the drivers for tropospheric model parameters.
getParametersDrivers() - Method in class org.orekit.models.earth.ViennaOneModel
Get the drivers for tropospheric model parameters.
getParametersDrivers() - Method in class org.orekit.models.earth.ViennaThreeModel
Get the drivers for tropospheric model parameters.
getParametersJacobian(SpacecraftState, double[][]) - Method in class org.orekit.propagation.numerical.JacobiansMapper
Get theJacobian with respect to parameters from a one-dimensional additional state array.
getParent() - Method in class org.orekit.frames.Frame
Get the parent frame.
getParentShape() - Method in class org.orekit.frames.TopocentricFrame
Get the body shape on which the local point is defined.
getParticipants() - Method in class org.orekit.estimation.measurements.EstimatedMeasurement
Get the coordinates of the measurements participants in signal travel order.
getParticipants() - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData
Getter for the participants.
getParts() - Method in interface org.orekit.errors.LocalizedException
Get the variable parts of the error message.
getParts() - Method in exception org.orekit.errors.OrekitException
Get the variable parts of the error message.
getParts() - Method in exception org.orekit.errors.OrekitIllegalArgumentException
Get the variable parts of the error message.
getParts() - Method in exception org.orekit.errors.OrekitIllegalStateException
Get the variable parts of the error message.
getParts() - Method in exception org.orekit.errors.OrekitInternalError
Get the variable parts of the error message.
getParts() - Method in exception org.orekit.errors.OrekitIOException
Get the variable parts of the error message.
getParts() - Method in exception org.orekit.errors.OrekitParseException
Get the variable parts of the error message.
getPastInfinity(Field<T>) - Static method in class org.orekit.time.FieldAbsoluteDate
Dummy date at infinity in the past direction.
getPath() - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData
Getter for the path.
getPath1() - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData
Getter for the path1.
getPath2() - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData
Getter for the path2.
getPdop() - Method in class org.orekit.gnss.DOP
Gets the position dilution of precision.
getPendingEvent() - Method in class org.orekit.propagation.events.FieldEventState
Get PendingEvent.
getPerigeeArgument() - Method in class org.orekit.orbits.FieldKeplerianOrbit
Get the perigee argument.
getPerigeeArgument() - Method in class org.orekit.orbits.KeplerianOrbit
Get the perigee argument.
getPerigeeArgument() - Method in class org.orekit.propagation.analytical.tle.TLE
Get the argument of perigee.
getPerigeeArgumentDot() - Method in class org.orekit.orbits.FieldKeplerianOrbit
Get the perigee argument derivative.
getPerigeeArgumentDot() - Method in class org.orekit.orbits.KeplerianOrbit
Get the perigee argument derivative.
getPermanentTide() - Method in enum org.orekit.utils.IERSConventions
Get the permanent tide to be removed from ΔC₂₀ when zero-tide potentials are used.
getPhase(BodiesElements) - Method in class org.orekit.models.earth.displacement.Tide
Get the phase of the tide.
getPhaseCenterVariation(Vector3D) - Method in class org.orekit.gnss.antenna.FrequencyPattern
Get the value of the phase center variation in a signal direction.
getPhaseCenterVariation(Frequency, Vector3D) - Method in class org.orekit.gnss.antenna.Antenna
Get the value of the phase center variation in a signal direction.
getPhaseShiftCorrections() - Method in class org.orekit.gnss.RinexHeader
Get the list of phase shift correction used to generate phases consistent w/r to cycle shifts.
getPhysicalCovariances(double) - Method in class org.orekit.estimation.leastsquares.BatchLSEstimator
Get the covariances matrix in space flight dynamics physical units.
getPhysicalEstimatedCovarianceMatrix() - Method in interface org.orekit.estimation.sequential.KalmanEstimation
Get the "physical" estimated covariance matrix (i.e.
getPhysicalEstimatedCovarianceMatrix() - Method in class org.orekit.estimation.sequential.KalmanEstimator
Get the "physical" estimated covariance matrix (i.e.
getPhysicalEstimatedCovarianceMatrix() - Method in class org.orekit.estimation.sequential.Model
Get the "physical" estimated covariance matrix (i.e.
getPhysicalEstimatedState() - Method in interface org.orekit.estimation.sequential.KalmanEstimation
Get the "physical" estimated state (i.e.
getPhysicalEstimatedState() - Method in class org.orekit.estimation.sequential.KalmanEstimator
Get the "physical" estimated state (i.e.
getPhysicalEstimatedState() - Method in class org.orekit.estimation.sequential.Model
Get the "physical" estimated state (i.e.
getPhysicalInnovationCovarianceMatrix() - Method in interface org.orekit.estimation.sequential.KalmanEstimation
Get the physical innovation covariance matrix.
getPhysicalInnovationCovarianceMatrix() - Method in class org.orekit.estimation.sequential.Model
Get the physical innovation covariance matrix.
getPhysicalKalmanGain() - Method in interface org.orekit.estimation.sequential.KalmanEstimation
Get the physical Kalman gain matrix.
getPhysicalKalmanGain() - Method in class org.orekit.estimation.sequential.Model
Get the physical Kalman gain matrix.
getPhysicalMeasurementJacobian() - Method in interface org.orekit.estimation.sequential.KalmanEstimation
Get the physical Jacobian of the measurement with respect to the state (H matrix).
getPhysicalMeasurementJacobian() - Method in class org.orekit.estimation.sequential.Model
Get the physical Jacobian of the measurement with respect to the state (H matrix).
getPhysicalStateTransitionMatrix() - Method in interface org.orekit.estimation.sequential.KalmanEstimation
Get physical state transition matrix between previous state and estimated (but not yet corrected) state.
getPhysicalStateTransitionMatrix() - Method in class org.orekit.estimation.sequential.Model
Get physical state transition matrix between previous state and estimated (but not yet corrected) state.
getPlaneSection(Vector3D, Vector3D) - Method in class org.orekit.bodies.Ellipsoid
Compute the 2D ellipse at the intersection of the 3D ellipsoid and a plane.
getPlus(int, int) - Method in class org.orekit.utils.LoveNumbers
Get the real part of a nominal Love numbers.
getPluto() - Static method in class org.orekit.bodies.CelestialBodyFactory
Get the Pluto singleton body.
getPoint() - Method in class org.orekit.frames.TopocentricFrame
Get the surface point defining the origin of the frame.
getPoint(Field<T>) - Method in class org.orekit.frames.TopocentricFrame
Get the surface point defining the origin of the frame.
getPolarDriftXDriver() - Method in class org.orekit.estimation.measurements.EstimatedEarthFrameProvider
Get a driver allowing to add a polar drift along X.
getPolarDriftXDriver() - Method in class org.orekit.estimation.measurements.GroundStation
Get a driver allowing to add a polar drift along X.
getPolarDriftYDriver() - Method in class org.orekit.estimation.measurements.EstimatedEarthFrameProvider
Get a driver allowing to add a polar drift along Y.
getPolarDriftYDriver() - Method in class org.orekit.estimation.measurements.GroundStation
Get a driver allowing to add a polar drift along Y.
getPolarOffsetXDriver() - Method in class org.orekit.estimation.measurements.EstimatedEarthFrameProvider
Get a driver allowing to add a polar offset along X.
getPolarOffsetXDriver() - Method in class org.orekit.estimation.measurements.GroundStation
Get a driver allowing to add a polar offset along X.
getPolarOffsetYDriver() - Method in class org.orekit.estimation.measurements.EstimatedEarthFrameProvider
Get a driver allowing to add a polar offset along Y.
getPolarOffsetYDriver() - Method in class org.orekit.estimation.measurements.GroundStation
Get a driver allowing to add a polar offset along Y.
getPolarRadius() - Method in class org.orekit.models.earth.ReferenceEllipsoid
Get the radius of this ellipsoid at the poles.
getPole(AbsoluteDate) - Method in interface org.orekit.bodies.IAUPole
Get the body North pole direction in ICRF frame.
getPole(FieldAbsoluteDate<T>) - Method in interface org.orekit.bodies.IAUPole
Get the body North pole direction in ICRF frame.
getPoleCorrection(AbsoluteDate) - Method in class org.orekit.frames.EOPHistory
Get the pole IERS Reference Pole correction.
getPoleCorrection(FieldAbsoluteDate<T>) - Method in class org.orekit.frames.EOPHistory
Get the pole IERS Reference Pole correction.
getPolynomial() - Method in class org.orekit.data.PoissonSeries
Get the polynomial part of the series.
getPosition() - Method in class org.orekit.estimation.measurements.Position
Get the position.
getPosition() - Method in class org.orekit.estimation.measurements.PV
Get the position.
getPosition() - Method in class org.orekit.files.ccsds.OPMFile
Get position vector.
getPosition() - Method in class org.orekit.utils.FieldPVCoordinates
Gets the position.
getPosition() - Method in class org.orekit.utils.PVCoordinates
Gets the position.
getPositionAngle() - Method in class org.orekit.estimation.sequential.UnivariateProcessNoise
Getter for the positionAngle.
getPositionAngle() - Method in class org.orekit.propagation.conversion.AbstractPropagatorBuilder
Get the position angle type expected for the 6 first parameters in PropagatorBuilder.buildPropagator(double[]).
getPositionAngle() - Method in interface org.orekit.propagation.conversion.PropagatorBuilder
Get the position angle type expected for the 6 first parameters in PropagatorBuilder.buildPropagator(double[]).
getPositionAngle() - Method in class org.orekit.propagation.events.PositionAngleDetector
Get the type of position angle.
getPositionAngleType() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
Get propagation parameter type.
getPositionAngleType() - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator
Get propagation parameter type.
getPositionAngleType() - Method in class org.orekit.propagation.integration.FieldStateMapper
Get propagation parameter type.
getPositionAngleType() - Method in class org.orekit.propagation.integration.StateMapper
Get propagation parameter type.
getPositionAngleType() - Method in class org.orekit.propagation.numerical.FieldNumericalPropagator
Get propagation parameter type.
getPositionAngleType() - Method in class org.orekit.propagation.numerical.NumericalPropagator
Get propagation parameter type.
getPositionScale() - Method in class org.orekit.propagation.conversion.AbstractPropagatorBuilder
Get the position scale.
getPrecessionFunction() - Method in enum org.orekit.utils.IERSConventions
Get the function computing the precession angles.
getPredictedMeasurement() - Method in interface org.orekit.estimation.sequential.KalmanEstimation
Get the predicted measurement.
getPredictedMeasurement() - Method in class org.orekit.estimation.sequential.Model
Get the predicted measurement.
getPredictedSpacecraftStates() - Method in interface org.orekit.estimation.sequential.KalmanEstimation
Get the predicted spacecraft states.
getPredictedSpacecraftStates() - Method in class org.orekit.estimation.sequential.Model
Get the predicted spacecraft states.
getPressure() - Method in class org.orekit.models.earth.EarthStandardAtmosphereRefraction
Get the local pressure at the evaluation location.
getPressure() - Method in class org.orekit.models.earth.GlobalPressureTemperature2Model
Returns the pressure at the station [hPa].
getPressure() - Method in class org.orekit.models.earth.GlobalPressureTemperatureModel
Get the atmospheric pressure of the station depending its position.
getPreviousState() - Method in interface org.orekit.propagation.sampling.FieldOrekitStepInterpolator
Get the state at previous grid point date.
getPreviousState() - Method in interface org.orekit.propagation.sampling.OrekitStepInterpolator
Get the state at previous grid point date.
getPrimeMeridianAngle(AbsoluteDate) - Method in interface org.orekit.bodies.IAUPole
Get the prime meridian angle.
getPrimeMeridianAngle(FieldAbsoluteDate<T>) - Method in interface org.orekit.bodies.IAUPole
Get the prime meridian angle.
getPrimeMeridianDriftDriver() - Method in class org.orekit.estimation.measurements.EstimatedEarthFrameProvider
Get a driver allowing to add a prime meridian rotation rate.
getPrimeMeridianDriftDriver() - Method in class org.orekit.estimation.measurements.GroundStation
Get a driver allowing to add a prime meridian rotation rate.
getPrimeMeridianOffsetDriver() - Method in class org.orekit.estimation.measurements.EstimatedEarthFrameProvider
Get a driver allowing to add a prime meridian rotation.
getPrimeMeridianOffsetDriver() - Method in class org.orekit.estimation.measurements.GroundStation
Get a driver allowing to add a prime meridian rotation.
getPRN() - Method in class org.orekit.gnss.GPSAlmanac
 
getPRN() - Method in interface org.orekit.propagation.analytical.gnss.GPSOrbitalElements
Gets the PRN number of the GPS satellite.
getPrnNumber() - Method in class org.orekit.gnss.antenna.SatelliteAntenna
Get PRN number.
getPrnNumber() - Method in class org.orekit.gnss.ObservationDataSet
Get PRN number.
getPRNNumbers() - Method in class org.orekit.gnss.SEMParser
Gets the PRN numbers of all the GPS almanacs read from the file.
getPRNNumbers() - Method in class org.orekit.gnss.YUMAParser
Gets the PRN numbers of all the GPS almanacs read from the file.
getProcessNoiseMatrix(SpacecraftState, SpacecraftState) - Method in class org.orekit.estimation.sequential.ConstantProcessNoise
Get the process noise matrix between previous and current states.
getProcessNoiseMatrix(SpacecraftState, SpacecraftState) - Method in interface org.orekit.estimation.sequential.CovarianceMatrixProvider
Get the process noise matrix between previous and current states.
getProcessNoiseMatrix(SpacecraftState, SpacecraftState) - Method in class org.orekit.estimation.sequential.UnivariateProcessNoise
Get the process noise matrix between previous and current states.
getProgDCBS() - Method in class org.orekit.gnss.RinexLoader.Parser.AppliedDCBS
Get the program name used to apply DCBs.
getProgPCVS() - Method in class org.orekit.gnss.RinexLoader.Parser.AppliedPCVS
Get the program name used to apply PCVs.
getPropagationParametersDrivers() - Method in class org.orekit.propagation.conversion.AbstractPropagatorBuilder
Get the drivers for the configurable propagation parameters.
getPropagationParametersDrivers() - Method in interface org.orekit.propagation.conversion.PropagatorBuilder
Get the drivers for the configurable propagation parameters.
getPropagationParametersDrivers(boolean) - Method in class org.orekit.estimation.sequential.KalmanEstimator
Get the propagator parameters supported by this estimator.
getPropagationParametersEvolution() - Method in class org.orekit.estimation.sequential.UnivariateProcessNoise
Getter for the propagationParametersEvolution.
getPropagator() - Method in interface org.orekit.files.general.EphemerisFile.EphemerisSegment
View this ephemeris segment as a propagator.
getPropagator() - Method in interface org.orekit.files.general.EphemerisFile.SatelliteEphemeris
View this ephemeris as a propagator, combining data from all segments.
getPropagator() - Method in class org.orekit.files.sp3.SP3File.SP3Ephemeris
 
getPropagator() - Method in class org.orekit.propagation.analytical.AdapterPropagator
Get the reference propagator.
getPropagator(ObservableSatellite) - Method in class org.orekit.estimation.measurements.generation.Generator
Get a registered propagator.
getPropagatorIndex() - Method in class org.orekit.estimation.measurements.ObservableSatellite
Get the index of the propagator related to this satellite.
getPropagatorParametersDrivers(boolean) - Method in class org.orekit.estimation.leastsquares.BatchLSEstimator
Get the propagator parameters supported by this estimator.
getPropagators() - Method in class org.orekit.propagation.PropagatorsParallelizer
Get an unmodifiable list of the underlying mono-satellite propagators.
getPropagatorsIndices() - Method in class org.orekit.estimation.measurements.AbstractMeasurement
Deprecated.
getPropagatorsIndices() - Method in interface org.orekit.estimation.measurements.ObservedMeasurement
Deprecated.
getProvider() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonal
Get the spherical harmonics provider.
getProvider(boolean, int, int) - Method in class org.orekit.forces.gravity.potential.EGMFormatReader
Get a provider for read spherical harmonics coefficients.
getProvider(boolean, int, int) - Method in class org.orekit.forces.gravity.potential.GRGSFormatReader
Get a provider for read spherical harmonics coefficients.
getProvider(boolean, int, int) - Method in class org.orekit.forces.gravity.potential.ICGEMFormatReader
Get a provider for read spherical harmonics coefficients.
getProvider(boolean, int, int) - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
Get a provider for read spherical harmonics coefficients.
getProvider(boolean, int, int) - Method in class org.orekit.forces.gravity.potential.SHMFormatReader
Get a provider for read spherical harmonics coefficients.
getProviders() - Method in class org.orekit.data.DataProvidersManager
Get an unmodifiable view of the list of supported providers.
getProximityAngle() - Method in class org.orekit.propagation.events.AngularSeparationDetector
Get the proximity angle (rad).
getPVCoordinates() - Method in class org.orekit.files.ccsds.OPMFile
Get the position/velocity coordinates contained in the OPM.
getPVCoordinates() - Method in class org.orekit.orbits.FieldOrbit
Get the TimeStampedPVCoordinates in definition frame.
getPVCoordinates() - Method in class org.orekit.orbits.Orbit
Get the TimeStampedPVCoordinates in definition frame.
getPVCoordinates() - Method in class org.orekit.propagation.FieldSpacecraftState
Get the TimeStampedFieldPVCoordinates in orbit definition frame.
getPVCoordinates() - Method in class org.orekit.propagation.SpacecraftState
Get the TimeStampedPVCoordinates in orbit definition frame.
getPVCoordinates(Frame) - Method in class org.orekit.orbits.FieldOrbit
Get the TimeStampedPVCoordinates in a specified frame.
getPVCoordinates(Frame) - Method in class org.orekit.orbits.Orbit
Get the TimeStampedPVCoordinates in a specified frame.
getPVCoordinates(Frame) - Method in class org.orekit.propagation.FieldSpacecraftState
Get the TimeStampedFieldPVCoordinates in given output frame.
getPVCoordinates(Frame) - Method in class org.orekit.propagation.SpacecraftState
Get the TimeStampedPVCoordinates in given output frame.
getPVCoordinates(AbsoluteDate) - Method in class org.orekit.propagation.analytical.tle.TLEPropagator
Get the extrapolated position and velocity from an initial TLE.
getPVCoordinates(AbsoluteDate) - Method in class org.orekit.propagation.analytical.tle.TLESeries
Deprecated.
Get the extrapolated position and velocity from an initial date.
getPVCoordinates(AbsoluteDate, Frame) - Method in class org.orekit.frames.TopocentricFrame
Get the PVCoordinates of the topocentric frame origin in the selected frame.
getPVCoordinates(AbsoluteDate, Frame) - Method in class org.orekit.orbits.Orbit
Get the PVCoordinates of the body in the selected frame.
getPVCoordinates(AbsoluteDate, Frame) - Method in class org.orekit.propagation.AbstractPropagator
Get the PVCoordinates of the body in the selected frame.
getPVCoordinates(AbsoluteDate, Frame) - Method in class org.orekit.propagation.analytical.AggregateBoundedPropagator
 
getPVCoordinates(AbsoluteDate, Frame) - Method in class org.orekit.propagation.analytical.Ephemeris
Get the PVCoordinates of the body in the selected frame.
getPVCoordinates(AbsoluteDate, Frame) - Method in class org.orekit.propagation.integration.IntegratedEphemeris
Get the PVCoordinates of the body in the selected frame.
getPVCoordinates(AbsoluteDate, Frame) - Method in class org.orekit.propagation.numerical.NumericalPropagator
Get the PVCoordinates of the body in the selected frame.
getPVCoordinates(AbsoluteDate, Frame) - Method in interface org.orekit.utils.PVCoordinatesProvider
Get the PVCoordinates of the body in the selected frame.
getPVCoordinates(FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.orbits.FieldOrbit
Get the FieldPVCoordinates of the body in the selected frame.
getPVCoordinates(FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.propagation.FieldAbstractPropagator
Get the FieldPVCoordinates of the body in the selected frame.
getPVCoordinates(FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.propagation.integration.FieldIntegratedEphemeris
Get the FieldPVCoordinates of the body in the selected frame.
getPVCoordinates(FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.propagation.numerical.FieldNumericalPropagator
Get the FieldPVCoordinates of the body in the selected frame.
getPVCoordinates(FieldAbsoluteDate<T>, Frame) - Method in interface org.orekit.utils.ExtendedPVCoordinatesProvider
Get the FieldPVCoordinates of the body in the selected frame.
getPVCoordinates(FieldAbsoluteDate<T>, Frame) - Method in interface org.orekit.utils.FieldPVCoordinatesProvider
Get the FieldPVCoordinates of the body in the selected frame.
getPVCoordinatesProvider() - Method in class org.orekit.propagation.events.AlignmentDetector
Get the body to align.
getPvProvider() - Method in class org.orekit.propagation.analytical.AbstractAnalyticalPropagator
Get PV coordinates provider.
getPvProvider() - Method in class org.orekit.propagation.analytical.FieldAbstractAnalyticalPropagator
Get PV coordinates provider.
getPVTarget() - Method in class org.orekit.propagation.events.CircularFieldOfViewDetector
Get the position/velocity provider of the target .
getPVTarget() - Method in class org.orekit.propagation.events.FieldOfViewDetector
Get the position/velocity provider of the target .
getQ() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
Get the x component of inclination vector.
getQZSS() - Static method in class org.orekit.time.TimeScalesFactory
Get the Quasi-Zenith Satellite System time scale.
getRaan() - Method in class org.orekit.files.ccsds.OGMFile
Get the orbit right ascension of ascending node.
getRaan() - Method in class org.orekit.propagation.analytical.tle.TLE
Get Right Ascension of the Ascending node.
getRadiationParametersDrivers() - Method in class org.orekit.forces.BoxAndSolarArraySpacecraft
Get the drivers for supported parameters.
getRadiationParametersDrivers() - Method in class org.orekit.forces.radiation.IsotropicRadiationClassicalConvention
Get the drivers for supported parameters.
getRadiationParametersDrivers() - Method in class org.orekit.forces.radiation.IsotropicRadiationCNES95Convention
Get the drivers for supported parameters.
getRadiationParametersDrivers() - Method in class org.orekit.forces.radiation.IsotropicRadiationSingleCoefficient
Get the drivers for supported parameters.
getRadiationParametersDrivers() - Method in interface org.orekit.forces.radiation.RadiationSensitive
Get the drivers for supported parameters.
getRange(FieldVector3D<T>, Frame, FieldAbsoluteDate<T>) - Method in class org.orekit.frames.TopocentricFrame
Get the range of a point with regards to the topocentric frame center point.
getRange(Vector3D, Frame, AbsoluteDate) - Method in class org.orekit.frames.TopocentricFrame
Get the range of a point with regards to the topocentric frame center point.
getRange1() - Method in class org.orekit.estimation.iod.IodGooding
Get the range for observation (1).
getRange2() - Method in class org.orekit.estimation.iod.IodGooding
Get the range for observation (2).
getRange3() - Method in class org.orekit.estimation.iod.IodGooding
Get the range for observation (3).
getRangeMode() - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData
Getter for the rangeMode.
getRangeModulus() - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData
Getter for the rangeModulus.
getRangeRate(FieldPVCoordinates<T>, Frame, FieldAbsoluteDate<T>) - Method in class org.orekit.frames.TopocentricFrame
Get the range rate of a point with regards to the topocentric frame center point.
getRangeRate(PVCoordinates, Frame, AbsoluteDate) - Method in class org.orekit.frames.TopocentricFrame
Get the range rate of a point with regards to the topocentric frame center point.
getRangeUnits() - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData
Getter for the rangeUnits.
getRate(BodiesElements) - Method in class org.orekit.models.earth.displacement.Tide
Get the angular rate of the tide.
getRatio() - Method in enum org.orekit.gnss.Frequency
Get the ratio f/f0, where f0 is the common frequency.
getRawCnm(int, int) - Method in interface org.orekit.forces.gravity.potential.RawSphericalHarmonicsProvider.RawSphericalHarmonics
Get a spherical harmonic cosine coefficient.
getRawDrivers() - Method in class org.orekit.utils.ParameterDriversList.DelegatingDriver
Get the raw drivers to which this one delegates.
getRawProvider() - Method in class org.orekit.frames.InterpolatingTransformProvider
Get the underlying provider for raw (non-interpolated) transforms.
getRawProvider() - Method in class org.orekit.frames.ShiftingTransformProvider
Get the underlying provider for raw (non-interpolated) transforms.
getRawPV(AbsoluteDate) - Method in interface org.orekit.bodies.JPLEphemeridesLoader.RawPVProvider
Get the position-velocity at date.
getRawPV(FieldAbsoluteDate<T>) - Method in interface org.orekit.bodies.JPLEphemeridesLoader.RawPVProvider
Get the position-velocity at date.
getRawSnm(int, int) - Method in interface org.orekit.forces.gravity.potential.RawSphericalHarmonicsProvider.RawSphericalHarmonics
Get a spherical harmonic sine coefficient.
getRbar() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTAtmosphericDrag
Get the critical distance.
getRcvrClkOffset() - Method in class org.orekit.gnss.ObservationDataSet
Get receiver clock offset.
getReal(int, int) - Method in class org.orekit.utils.LoveNumbers
Get the real part of a nominal Love numbers.
getReceiveBand() - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData
Getter for the receiveBand.
getReceiveDelays() - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData
Getter for receiveDelays.
getReceiverNumber() - Method in class org.orekit.gnss.RinexHeader
Get the number of the receiver.
getReceiversAntennas() - Method in class org.orekit.gnss.antenna.AntexLoader
Get parsed receivers antennas.
getReceiverType() - Method in class org.orekit.gnss.RinexHeader
Get the type of the receiver.
getReceiverVersion() - Method in class org.orekit.gnss.RinexHeader
Get the version of the receiver.
getReferenceAttitude() - Method in class org.orekit.attitudes.FixedRate
Get the reference attitude.
getReferenceDate() - Method in class org.orekit.forces.gravity.potential.CachedNormalizedSphericalHarmonicsProvider
Get the reference date for the harmonics.
getReferenceDate() - Method in interface org.orekit.forces.gravity.potential.SphericalHarmonicsProvider
Get the reference date for the harmonics.
getReferenceDate() - Method in class org.orekit.propagation.integration.FieldStateMapper
Get reference date.
getReferenceDate() - Method in class org.orekit.propagation.integration.StateMapper
Get reference date.
getReferenceDate() - Method in class org.orekit.utils.ParameterDriver
Get current reference date.
getReferenceDate() - Method in class org.orekit.utils.SecularAndHarmonic
Get the reference date.
getReferenceFrame() - Method in class org.orekit.attitudes.Attitude
Get the reference frame.
getReferenceFrame() - Method in class org.orekit.attitudes.FieldAttitude
Get the reference frame.
getReferenceFrame() - Method in class org.orekit.estimation.measurements.AngularRaDec
Get the reference frame in which the right ascension - declination angles are given.
getReferenceFrame() - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData
Get the the value of REFERENCE_FRAME as an Orekit Frame.
getReferenceFrameString() - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData
Get the reference frame specifier as it appeared in the file.
getReferenceValue() - Method in class org.orekit.utils.ParameterDriver
Get reference parameter value.
getRefFrame() - Method in class org.orekit.files.ccsds.CcsdsModifiedFrame
Get the name of the CCSDS reference frame.
getRefFrame() - Method in class org.orekit.files.ccsds.ODMMetaData
Get the the value of REF_FRAME as an Orekit Frame.
getRefFrame() - Method in class org.orekit.files.ccsds.OPMFile.Maneuver
Get Coordinate system for velocity increment vector, for absolute frames.
getRefLofType() - Method in class org.orekit.files.ccsds.OPMFile.Maneuver
Get coordinate system for velocity increment vector, for Local Orbital Frames.
getRefraction(double) - Method in interface org.orekit.models.AtmosphericRefractionModel
Compute the refraction angle from the true (geometrical) elevation.
getRefraction(double) - Method in class org.orekit.models.earth.EarthITU453AtmosphereRefraction
 
getRefraction(double) - Method in class org.orekit.models.earth.EarthStandardAtmosphereRefraction
 
getRefractionModel() - Method in class org.orekit.propagation.events.ElevationDetector
Returns the currently configured refraction model.
getRefractionModel() - Method in class org.orekit.propagation.events.FieldElevationDetector
Returns the currently configured refraction model.
getRetrogradeFactor() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
Get the retrograde factor.
getRevAtEpoch() - Method in class org.orekit.files.ccsds.OMMFile
Get the revolution rumber.
getReversedProvider(TransformProvider) - Static method in class org.orekit.frames.TransformProviderUtils
Reverse a transform provider.
getRevolutionNumberAtEpoch() - Method in class org.orekit.propagation.analytical.tle.TLE
Get the revolution number.
getRightAscensionOfAscendingNode() - Method in class org.orekit.orbits.CircularOrbit
Get the right ascension of the ascending node.
getRightAscensionOfAscendingNode() - Method in class org.orekit.orbits.FieldCircularOrbit
Get the right ascension of the ascending node.
getRightAscensionOfAscendingNode() - Method in class org.orekit.orbits.FieldKeplerianOrbit
Get the right ascension of the ascending node.
getRightAscensionOfAscendingNode() - Method in class org.orekit.orbits.KeplerianOrbit
Get the right ascension of the ascending node.
getRightAscensionOfAscendingNodeDot() - Method in class org.orekit.orbits.CircularOrbit
Get the right ascension of the ascending node derivative.
getRightAscensionOfAscendingNodeDot() - Method in class org.orekit.orbits.FieldCircularOrbit
Get the right ascension of the ascending node derivative.
getRightAscensionOfAscendingNodeDot() - Method in class org.orekit.orbits.FieldKeplerianOrbit
Get the right ascension of the ascending node derivative.
getRightAscensionOfAscendingNodeDot() - Method in class org.orekit.orbits.KeplerianOrbit
Get the right ascension of the ascending node derivative.
getRinexVersion() - Method in class org.orekit.gnss.RinexHeader
Get Rinex Version.
getRMS() - Method in class org.orekit.propagation.conversion.AbstractPropagatorConverter
Get the Root Mean Square Deviation of the fitting.
getRnml(double, int, int, int, int, int) - Static method in class org.orekit.propagation.semianalytical.dsst.utilities.UpperBounds
Get the upper bound value Rεn,m,l(γ).
getRolloverReference() - Static method in class org.orekit.time.GPSDate
Get the reference date ensuring continuity across GPS week rollover.
getRoot() - Static method in class org.orekit.frames.Frame
Get the unique root frame.
getRotation() - Method in class org.orekit.attitudes.Attitude
Get the attitude rotation.
getRotation() - Method in class org.orekit.attitudes.FieldAttitude
Get the attitude rotation.
getRotation() - Method in class org.orekit.frames.FieldTransform
Get the underlying elementary rotation.
getRotation() - Method in class org.orekit.frames.Transform
Get the underlying elementary rotation.
getRotation() - Method in class org.orekit.utils.AngularCoordinates
Get the rotation.
getRotation() - Method in class org.orekit.utils.FieldAngularCoordinates
Get the rotation.
getRotationAcceleration() - Method in class org.orekit.attitudes.Attitude
Get the satellite rotation acceleration.
getRotationAcceleration() - Method in class org.orekit.attitudes.FieldAttitude
Get the satellite rotation acceleration.
getRotationAcceleration() - Method in class org.orekit.frames.FieldTransform
Get the second time derivative of the rotation.
getRotationAcceleration() - Method in class org.orekit.frames.Transform
Get the second time derivative of the rotation.
getRotationAcceleration() - Method in class org.orekit.utils.AngularCoordinates
Get the rotation acceleration.
getRotationAcceleration() - Method in class org.orekit.utils.FieldAngularCoordinates
Get the rotation acceleration.
getRotationRate() - Method in class org.orekit.frames.FieldTransform
Get the first time derivative of the rotation.
getRotationRate() - Method in class org.orekit.frames.Transform
Get the first time derivative of the rotation.
getRotationRate() - Method in class org.orekit.utils.AngularCoordinates
Get the rotation rate.
getRotationRate() - Method in class org.orekit.utils.FieldAngularCoordinates
Get the rotation rate.
getS() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.CoefficientsFactory.NSKey
Get s.
getS10(AbsoluteDate) - Method in interface org.orekit.forces.drag.atmosphere.JB2008InputParameters
Get the EUV index (26-34 nm) scaled to F10.
getS10B(AbsoluteDate) - Method in interface org.orekit.forces.drag.atmosphere.JB2008InputParameters
Get the EUV 81-day averaged centered index.
getSample() - Method in class org.orekit.propagation.conversion.AbstractPropagatorConverter
Get the states sample.
getSatConfiguration() - Method in class org.orekit.gnss.GPSAlmanac
Gets the satellite configuration.
getSatelliteCode() - Method in class org.orekit.gnss.antenna.SatelliteAntenna
Get satellite code.
getSatelliteCount() - Method in class org.orekit.files.sp3.SP3File
Get the number of satellites contained in this orbit file.
getSatelliteNumber() - Method in class org.orekit.propagation.analytical.tle.TLE
Get the satellite id.
getSatelliteRevolution() - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator
Get the number of satellite revolutions to use for converting osculating to mean elements.
getSatellites() - Method in class org.orekit.estimation.measurements.AbstractMeasurement
Get the satellites related to this measurement.
getSatellites() - Method in class org.orekit.estimation.measurements.generation.AbstractMeasurementBuilder
Get the satellites related to this measurement.
getSatellites() - Method in interface org.orekit.estimation.measurements.ObservedMeasurement
Get the satellites related to this measurement.
getSatellites() - Method in class org.orekit.files.ccsds.OEMFile
 
getSatellites() - Method in interface org.orekit.files.general.EphemerisFile
Get the loaded ephemeris for each satellite in the file.
getSatellites() - Method in class org.orekit.files.general.OrekitEphemerisFile
 
getSatellites() - Method in class org.orekit.files.sp3.SP3File
 
getSatellitesAntennas() - Method in class org.orekit.gnss.antenna.AntexLoader
Get parsed satellites antennas.
getSatelliteSystem() - Method in class org.orekit.gnss.antenna.SatelliteAntenna
Get satellite system.
getSatelliteSystem() - Method in enum org.orekit.gnss.Frequency
Get the satellite system for which this frequency is defined.
getSatelliteSystem() - Method in class org.orekit.gnss.ObservationDataSet
Get Satellite System.
getSatelliteSystem() - Method in class org.orekit.gnss.RinexHeader
Get Satellite System.
getSatelliteSystem() - Method in class org.orekit.gnss.RinexLoader.Parser.AppliedDCBS
Get the satellite system.
getSatelliteSystem() - Method in class org.orekit.gnss.RinexLoader.Parser.AppliedPCVS
Get the satellite system.
getSatelliteSystem() - Method in class org.orekit.gnss.RinexLoader.Parser.PhaseShiftCorrection
Get the Satellite System.
getSatelliteSystem() - Method in class org.orekit.gnss.RinexLoader.Parser.ScaleFactorCorrection
Get the Satellite System.
getSatelliteType() - Method in class org.orekit.gnss.antenna.SatelliteAntenna
Get satellite type.
getSatsCorrected() - Method in class org.orekit.gnss.RinexLoader.Parser.PhaseShiftCorrection
Get the list of satellites involved.
getSaturn() - Static method in class org.orekit.bodies.CelestialBodyFactory
Get the Saturn singleton body.
getScale() - Method in class org.orekit.utils.ParameterDriver
Get scale.
getSecond() - Method in class org.orekit.time.TimeComponents
Get the seconds number.
getSecondsInLocalDay() - Method in class org.orekit.time.TimeComponents
Get the second number within the local day, without applying the offset from UTC.
getSecondsInUTCDay() - Method in class org.orekit.time.TimeComponents
Get the second number within the UTC day, applying the offset from UTC.
getSecondsOfWeek() - Method in class org.orekit.files.sp3.SP3File
Returns the seconds of the GPS week as contained in the SP3 file.
getSegments() - Method in class org.orekit.files.ccsds.OEMFile.OemSatelliteEphemeris
 
getSegments() - Method in interface org.orekit.files.general.EphemerisFile.SatelliteEphemeris
Get the segments of the ephemeris.
getSegments() - Method in class org.orekit.files.general.OrekitEphemerisFile.OrekitSatelliteEphemeris
 
getSegments() - Method in class org.orekit.files.sp3.SP3File.SP3Ephemeris
Returns a list containing only this.
getSelectedCoefficients() - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator
Get the selected short periodic coefficients that must be stored as additional states.
getSelectedNormalizedParameters() - Method in class org.orekit.propagation.conversion.AbstractPropagatorBuilder
Get the current value of selected normalized parameters.
getSelectedNormalizedParameters() - Method in interface org.orekit.propagation.conversion.PropagatorBuilder
Get the current value of selected normalized parameters.
getSelectedParameters() - Method in class org.orekit.propagation.numerical.PartialDerivativesEquations
Get the selected parameters, in Jacobian matrix column order.
getSelector() - Method in class org.orekit.estimation.measurements.generation.AbstractScheduler
Get the dates selector.
getSerialNumber() - Method in class org.orekit.gnss.antenna.ReceiverAntenna
Get the serial number.
getSigma() - Method in class org.orekit.estimation.measurements.modifiers.DynamicOutlierFilter
Get the current value of sigma.
getSignalStrength() - Method in class org.orekit.gnss.ObservationData
Get the signal strength.
getSignalStrengthUnit() - Method in class org.orekit.gnss.RinexHeader
Get the unit of the carrier to noise ratio observables.
getSinexCode() - Method in class org.orekit.gnss.antenna.Antenna
Get the sinex code of the antenna.
getSiteLocation() - Method in class org.orekit.models.earth.displacement.OceanLoadingCoefficients
Get the site location.
getSiteName() - Method in class org.orekit.models.earth.displacement.OceanLoadingCoefficients
Get the site name.
getSites() - Method in class org.orekit.models.earth.displacement.OceanLoadingCoefficientsBLQFactory
Get the list of sites for which we have found coefficients, in lexicographic order ignoring case.
getSize() - Method in class org.orekit.utils.LoveNumbers
Get the size of the arrays.
getSj(int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.CjSjCoefficient
Get the Sj coefficient.
getSlave() - Method in class org.orekit.propagation.events.InterSatDirectViewDetector
Get the provider for the slave satellite.
getSlaveStation() - Method in class org.orekit.estimation.measurements.TurnAroundRange
Get the slave ground station reflecting the signal.
getSlope() - Method in class org.orekit.time.OffsetModel
Offset slope in seconds per UTC day (TAI minus UTC / dUTC).
getSlots() - Method in class org.orekit.utils.GenericTimeStampedCache
Get the number of slots in use.
getSlotsEvictions() - Method in class org.orekit.utils.GenericTimeStampedCache
Get the number of slots evictions.
getSma() - Method in class org.orekit.gnss.GPSAlmanac
 
getSma() - Method in interface org.orekit.propagation.analytical.gnss.GPSOrbitalElements
Gets the Semi-Major Axis.
getSma() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
Get the semi-major axis.
getSolarRadArea() - Method in class org.orekit.files.ccsds.OGMFile
Get the solar radiation pressure area.
getSolarRadCoeff() - Method in class org.orekit.files.ccsds.OGMFile
Get the solar radiation pressure coefficient.
getSolarSystemBarycenter() - Static method in class org.orekit.bodies.CelestialBodyFactory
Get the solar system barycenter aggregated body.
getSolidPoleTide(EOPHistory) - Method in enum org.orekit.utils.IERSConventions
Get the function computing solid pole tide (ΔC₂₁, ΔS₂₁).
getSource() - Method in class org.orekit.gnss.GPSAlmanac
Gets the source of this GPS almanac.
getSourceDCBS() - Method in class org.orekit.gnss.RinexLoader.Parser.AppliedDCBS
Get the source of corrections.
getSourcePCVS() - Method in class org.orekit.gnss.RinexLoader.Parser.AppliedPCVS
Get the source of corrections.
getSourceString() - Method in enum org.orekit.errors.OrekitMessages
getSouth() - Method in class org.orekit.bodies.FieldGeodeticPoint
Get the direction to the south of point, expressed in parent shape frame.
getSouth() - Method in class org.orekit.bodies.GeodeticPoint
Get the direction to the south of point, expressed in parent shape frame.
getSouth() - Method in class org.orekit.frames.TopocentricFrame
Get the south direction of topocentric frame, expressed in parent shape frame.
getSouthAmplitude(int, int) - Method in class org.orekit.models.earth.displacement.OceanLoadingCoefficients
Get the amplitude along South axis.
getSouthPhase(int, int) - Method in class org.orekit.models.earth.displacement.OceanLoadingCoefficients
Get the phase along South axis.
getSpacecraft() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTAtmosphericDrag
Get spacecraft shape.
getSpacecraft() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTSolarRadiationPressure
Get spacecraft shape.
getSpacecraftComment() - Method in class org.orekit.files.ccsds.OGMFile
Get the comment for spacecraft.
getSpan(AbsoluteDate) - Method in class org.orekit.utils.TimeSpanMap
Get the time span containing a specified date.
getSpecifier() - Method in interface org.orekit.errors.LocalizedException
Get the localizable specifier of the error message.
getSpecifier() - Method in exception org.orekit.errors.OrekitException
Get the localizable specifier of the error message.
getSpecifier() - Method in exception org.orekit.errors.OrekitIllegalArgumentException
Get the localizable specifier of the error message.
getSpecifier() - Method in exception org.orekit.errors.OrekitIllegalStateException
Get the localizable specifier of the error message.
getSpecifier() - Method in exception org.orekit.errors.OrekitInternalError
Get the localizable specifier of the error message.
getSpecifier() - Method in exception org.orekit.errors.OrekitIOException
Get the localizable specifier of the error message.
getSpecifier() - Method in exception org.orekit.errors.OrekitParseException
Get the localizable specifier of the error message.
getSpin() - Method in class org.orekit.attitudes.Attitude
Get the satellite spin.
getSpin() - Method in class org.orekit.attitudes.FieldAttitude
Get the satellite spin.
getSpin() - Method in class org.orekit.models.earth.ReferenceEllipsoid
Gets the rotation of the ellipsoid about its axis.
getStandardModel() - Static method in class org.orekit.models.earth.SaastamoinenModel
Create a new Saastamoinen model using a standard atmosphere model.
getStandardModel(double, double) - Static method in class org.orekit.models.earth.MariniMurrayModel
Create a new Marini-Murray model using a standard atmosphere model.
getStandardModel(double, double) - Static method in class org.orekit.models.earth.MendesPavlisModel
Create a new Mendes-Pavlis model using a standard atmosphere model.
getStart() - Method in class org.orekit.estimation.measurements.generation.AbstractMeasurementBuilder
Get the start of the measurements time span.
getStart() - Method in class org.orekit.files.ccsds.OEMFile.EphemeridesBlock
 
getStart() - Method in class org.orekit.files.ccsds.OEMFile.OemSatelliteEphemeris
 
getStart() - Method in interface org.orekit.files.general.EphemerisFile.EphemerisSegment
Get the start date of this ephemeris segment.
getStart() - Method in interface org.orekit.files.general.EphemerisFile.SatelliteEphemeris
Get the start date of the ephemeris.
getStart() - Method in class org.orekit.files.general.OrekitEphemerisFile.OrekitEphemerisSegment
 
getStart() - Method in class org.orekit.files.general.OrekitEphemerisFile.OrekitSatelliteEphemeris
 
getStart() - Method in class org.orekit.files.sp3.SP3File.SP3Ephemeris
 
getStart() - Method in class org.orekit.time.OffsetModel
Get the date of the offset start.
getStart() - Method in class org.orekit.utils.TimeSpanMap.Span
Get the start of this time span.
getStartDate() - Method in class org.orekit.forces.maneuvers.ConstantThrustManeuver
Get the start date.
getStartDate() - Method in class org.orekit.frames.EOPHistory
Get the date of the first available Earth Orientation Parameters.
getStartDate() - Method in class org.orekit.propagation.AbstractPropagator
Get the start date.
getStartDate() - Method in class org.orekit.propagation.FieldAbstractPropagator
Get the start date.
getStartTime() - Method in class org.orekit.files.ccsds.OEMFile.EphemeridesBlock
Get start of total time span covered by ephemerides data and covariance data.
getStartTime() - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData
Getter for the startTime.
getStartTimeString() - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData
Getter for the startTime String.
getState() - Method in class org.orekit.propagation.events.EventsLogger.LoggedEvent
Get the triggering state.
getState() - Method in class org.orekit.propagation.events.FieldEventsLogger.FieldLoggedEvent
Get the triggering state.
getState() - Method in class org.orekit.propagation.events.handlers.RecordAndContinue.Event
Get the spacecraft's state at the event.
getState(DiscreteTroposphericModel) - Method in class org.orekit.estimation.measurements.modifiers.TroposphericDSConverter
Get the state with the number of parameters consistent with tropospheric model.
getStateDerivatives(int) - Method in class org.orekit.estimation.measurements.EstimatedMeasurement
Get the partial derivatives of the simulated measurement with respect to state Cartesian coordinates.
getStateDimension() - Method in class org.orekit.propagation.numerical.JacobiansMapper
Deprecated.
as of 9.0, replaced with JacobiansMapper.STATE_DIMENSION
getStateJacobian(SpacecraftState, double[][]) - Method in class org.orekit.propagation.numerical.JacobiansMapper
Get the Jacobian with respect to state from a one-dimensional additional state array.
getStates() - Method in class org.orekit.estimation.measurements.EstimatedMeasurement
Get the states of the spacecrafts.
getStation() - Method in class org.orekit.estimation.measurements.AngularAzEl
Get the ground station from which measurement is performed.
getStation() - Method in class org.orekit.estimation.measurements.AngularRaDec
Get the ground station from which measurement is performed.
getStation() - Method in class org.orekit.estimation.measurements.Phase
Get the ground station from which measurement is performed.
getStation() - Method in class org.orekit.estimation.measurements.Range
Get the ground station from which measurement is performed.
getStation() - Method in class org.orekit.estimation.measurements.RangeRate
Get the ground station from which measurement is performed.
getStatus() - Method in class org.orekit.estimation.measurements.EstimatedMeasurement
Get the status.
getStep() - Method in class org.orekit.frames.InterpolatingTransformProvider
Get the grid points time step.
getStep() - Method in class org.orekit.frames.ShiftingTransformProvider
Get the grid points time step.
getStepHandler() - Method in class org.orekit.propagation.AbstractPropagator
Get the step handler.
getStepHandler() - Method in class org.orekit.propagation.FieldAbstractPropagator
Get the step handler.
getStop() - Method in class org.orekit.files.ccsds.OEMFile.EphemeridesBlock
 
getStop() - Method in class org.orekit.files.ccsds.OEMFile.OemSatelliteEphemeris
 
getStop() - Method in interface org.orekit.files.general.EphemerisFile.EphemerisSegment
Get the end date of this ephemeris segment.
getStop() - Method in interface org.orekit.files.general.EphemerisFile.SatelliteEphemeris
Get the end date of the ephemeris.
getStop() - Method in class org.orekit.files.general.OrekitEphemerisFile.OrekitEphemerisSegment
 
getStop() - Method in class org.orekit.files.general.OrekitEphemerisFile.OrekitSatelliteEphemeris
 
getStop() - Method in class org.orekit.files.sp3.SP3File.SP3Ephemeris
 
getStopDate() - Method in class org.orekit.propagation.events.EventState.EventOccurrence
Get the new time for a stop action.
getStopDate() - Method in class org.orekit.propagation.events.FieldEventState.EventOccurrence
Get the new time for a stop action.
getStopTime() - Method in class org.orekit.files.ccsds.OEMFile.EphemeridesBlock
Get end of total time span covered by ephemerides data and covariance data.
getStopTime() - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData
Getter for the stopTime.
getStopTimeString() - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData
Getter for the stopTime String.
getStreamOpener() - Method in class org.orekit.data.NamedData
Get the data stream opener.
getStrengthLevel() - Method in class org.orekit.forces.drag.atmosphere.data.MarshallSolarActivityFutureEstimation
Get the strength level for activity.
getSun() - Static method in class org.orekit.bodies.CelestialBodyFactory
Get the Sun singleton body.
getSupportedNames() - Method in class org.orekit.forces.drag.atmosphere.data.MarshallSolarActivityFutureEstimation
Get the supported names for data files.
getSupportedNames() - Method in class org.orekit.forces.gravity.potential.AstronomicalAmplitudeReader
Get the regular expression for supported files names.
getSupportedNames() - Method in class org.orekit.forces.gravity.potential.OceanTidesReader
Get the regular expression for supported files names.
getSupportedNames() - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
Get the regular expression for supported files names.
getSupportedNames() - Method in class org.orekit.gnss.SEMParser
Get the supported names for data files.
getSupportedNames() - Method in class org.orekit.gnss.YUMAParser
Get the supported names for data files.
getSupportedNames() - Method in class org.orekit.models.earth.KlobucharIonoCoefficientsLoader
Returns the supported names of the loader.
getSupportedNames() - Method in class org.orekit.models.earth.ViennaModelCoefficientsLoader
Returns the supported names of the loader.
getSVN() - Method in class org.orekit.gnss.GPSAlmanac
Gets the satellite "SVN" reference number.
getTabDensity() - Method in class org.orekit.forces.drag.atmosphere.HarrisPriester
Get the current density table.
getTable() - Method in class org.orekit.attitudes.TabulatedLofOffset
Get an unmodifiable view of the tabulated attitudes.
getTAI() - Static method in class org.orekit.time.TimeScalesFactory
Get the International Atomic Time scale.
getTargetPV(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.BodyCenterPointing
Compute the target point position/velocity in specified frame.
getTargetPV(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.GroundPointing
Compute the target point position/velocity in specified frame.
getTargetPV(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.LofOffsetPointing
Compute the target point position/velocity in specified frame.
getTargetPV(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.NadirPointing
Compute the target point position/velocity in specified frame.
getTargetPV(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.TargetPointing
Compute the target point position/velocity in specified frame.
getTargetPV(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.YawCompensation
Compute the target point position/velocity in specified frame.
getTargetPV(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.YawSteering
Compute the target point position/velocity in specified frame.
getTargetPV(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.BodyCenterPointing
Compute the target point position/velocity in specified frame.
getTargetPV(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.GroundPointing
Compute the target point position/velocity in specified frame.
getTargetPV(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.LofOffsetPointing
Compute the target point position/velocity in specified frame.
getTargetPV(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.NadirPointing
Compute the target point position/velocity in specified frame.
getTargetPV(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.TargetPointing
Compute the target point position/velocity in specified frame.
getTargetPV(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.YawCompensation
Compute the target point position/velocity in specified frame.
getTargetPV(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.YawSteering
Compute the target point position/velocity in specified frame.
getTargetSize() - Method in class org.orekit.propagation.conversion.AbstractPropagatorConverter
Get the size of the target.
getTauMultiplier() - Method in class org.orekit.models.earth.displacement.Tide
Get the multiplier for the τ Doodson argument.
getTC() - Method in class org.orekit.data.DelaunayArguments
Get the offset in Julian centuries.
getTC() - Method in class org.orekit.data.FieldDelaunayArguments
Get the offset in Julian centuries.
getTCB() - Static method in class org.orekit.time.TimeScalesFactory
Get the Barycentric Coordinate Time scale.
getTCG() - Static method in class org.orekit.time.TimeScalesFactory
Get the Geocentric Coordinate Time scale.
getTDB() - Static method in class org.orekit.time.TimeScalesFactory
Get the Barycentric Dynamic Time scale.
getTdop() - Method in class org.orekit.gnss.DOP
Gets the time dilution of precision.
getTEME() - Static method in class org.orekit.frames.FramesFactory
Get the TEME reference frame.
getTemperature() - Method in class org.orekit.models.earth.EarthStandardAtmosphereRefraction
Get the local temperature at the evaluation location.
getTemperature() - Method in class org.orekit.models.earth.GlobalPressureTemperature2Model
Returns the temperature at the station [K].
getTemperature() - Method in class org.orekit.models.earth.GlobalPressureTemperatureModel
Get the atmospheric temperature of the station depending its position.
getTFirstObs() - Method in class org.orekit.gnss.RinexHeader
Get the time of First observation record.
getTGD() - Method in interface org.orekit.propagation.analytical.gnss.GPSOrbitalElements
Gets the estimated group delay differential TGD for L1-L2 correction.
getTheoreticalStandardDeviation() - Method in class org.orekit.estimation.measurements.AbstractMeasurement
Get the theoretical standard deviation.
getTheoreticalStandardDeviation() - Method in class org.orekit.estimation.measurements.generation.AbstractMeasurementBuilder
Get the theoretical standard deviation.
getTheoreticalStandardDeviation() - Method in interface org.orekit.estimation.measurements.ObservedMeasurement
Get the theoretical standard deviation.
getTheta0() - Method in class org.orekit.models.earth.EarthITU453AtmosphereRefraction
Get the station elevation angle under free-space propagation .
getThetaMin() - Method in class org.orekit.models.earth.EarthITU453AtmosphereRefraction
Get the station minimal elevation angle.
getThreeHourlyKP(AbsoluteDate) - Method in class org.orekit.forces.drag.atmosphere.data.MarshallSolarActivityFutureEstimation
Get the value of the 3 hours geomagnetic index.
getThreeHourlyKP(AbsoluteDate) - Method in interface org.orekit.forces.drag.atmosphere.DTM2000InputParameters
Get the value of the 3 hours geomagnetic index.
getThreshold() - Method in class org.orekit.propagation.events.AbstractDetector
Get the convergence threshold in the event time search.
getThreshold() - Method in class org.orekit.propagation.events.AdapterDetector
Get the convergence threshold in the event time search.
getThreshold() - Method in interface org.orekit.propagation.events.EventDetector
Get the convergence threshold in the event time search.
getThreshold() - Method in class org.orekit.propagation.events.FieldAbstractDetector
Get the convergence threshold in the event time search.
getThreshold() - Method in interface org.orekit.propagation.events.FieldEventDetector
Get the convergence threshold in the event time search.
getThrust() - Method in class org.orekit.forces.maneuvers.ConstantThrustManeuver
Get the thrust.
getTidalDisplacementFrequencyCorrectionDiurnal() - Method in enum org.orekit.utils.IERSConventions
Get the correction function for tidal displacement for diurnal tides.
getTidalDisplacementFrequencyCorrectionDiurnal(String, int, int, int, int, int) - Static method in enum org.orekit.utils.IERSConventions
Get the correction function for tidal displacement for diurnal tides.
getTidalDisplacementFrequencyCorrectionZonal() - Method in enum org.orekit.utils.IERSConventions
Get the correction function for tidal displacement for zonal tides.
getTidalDisplacementFrequencyCorrectionZonal(String, int, int, int, int, int) - Static method in enum org.orekit.utils.IERSConventions
Get the correction function for tidal displacement for zonal tides.
getTide(int, int) - Method in class org.orekit.models.earth.displacement.OceanLoadingCoefficients
Get the tide.
getTideFrequencyDependenceFunction(TimeScale) - Method in enum org.orekit.utils.IERSConventions
Get the function computing frequency dependent terms (ΔC₂₀, ΔC₂₁, ΔS₂₁, ΔC₂₂, ΔS₂₂).
getTideSystem() - Method in class org.orekit.forces.gravity.HolmesFeatherstoneAttractionModel
Get the TideSystem used in the gravity field.
getTideSystem() - Method in class org.orekit.forces.gravity.potential.CachedNormalizedSphericalHarmonicsProvider
Get the TideSystem used in the gravity field.
getTideSystem() - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
Get the TideSystem used in the gravity field.
getTideSystem() - Method in interface org.orekit.forces.gravity.potential.TideSystemProvider
Get the TideSystem used in the gravity field.
getTime() - Method in class org.orekit.estimation.sequential.MeasurementDecorator
getTime() - Method in class org.orekit.gnss.GPSAlmanac
 
getTime() - Method in interface org.orekit.propagation.analytical.gnss.GPSOrbitalElements
Gets the Reference Time of the GPS orbit as a duration from week start.
getTime() - Method in class org.orekit.time.DateTimeComponents
Get the time component.
getTimeOffset() - Method in class org.orekit.estimation.measurements.EstimatedMeasurement
Get the time offset from first state date to measurement date.
getTimeScale() - Method in class org.orekit.files.ccsds.OEMFile.EphemeridesBlock
 
getTimeScale() - Method in interface org.orekit.files.general.EphemerisFile.EphemerisSegment
Get the time scale for this ephemeris segment.
getTimeScale() - Method in class org.orekit.files.general.OrekitEphemerisFile.OrekitEphemerisSegment
 
getTimeScale() - Method in class org.orekit.files.sp3.SP3File.SP3Ephemeris
 
getTimeScale(IERSConventions) - Method in enum org.orekit.files.ccsds.CcsdsTimeScale
Get the corresponding TimeScale.
getTimeScaleString() - Method in class org.orekit.files.ccsds.OEMFile.EphemeridesBlock
 
getTimeScaleString() - Method in interface org.orekit.files.general.EphemerisFile.EphemerisSegment
Get the time scale for this ephemeris segment.
getTimeScaleString() - Method in class org.orekit.files.general.OrekitEphemerisFile.OrekitEphemerisSegment
 
getTimeScaleString() - Method in class org.orekit.files.sp3.SP3File.SP3Ephemeris
 
getTimeSystem() - Method in class org.orekit.files.ccsds.ODMMetaData
Get the Time System that: for OPM, is used for metadata, state vector, maneuver and covariance data, for OMM, is used for metadata, orbit state and covariance data, for OEM, is used for metadata, ephemeris and covariance data.
getTimeSystem() - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData
Get the Time System that: for OPM, is used for metadata, state vector, maneuver and covariance data, for OMM, is used for metadata, orbit state and covariance data, for OEM, is used for metadata, ephemeris and covariance data.
getTimeSystem() - Method in class org.orekit.files.sp3.SP3File
Returns the SP3File.TimeSystem used to time-stamp position entries.
getTimetagRef() - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData
Getter for the timetagRef.
getTIRF(IERSConventions) - Static method in class org.orekit.frames.FramesFactory
Get the TIRF reference frame, ignoring tidal effects.
getTIRF(IERSConventions, boolean) - Static method in class org.orekit.frames.FramesFactory
Get the TIRF reference frame.
getTLastObs() - Method in class org.orekit.gnss.RinexHeader
Get the time of last observation record.
getTLE() - Method in class org.orekit.propagation.analytical.tle.TLEPropagator
Get the underlying TLE.
getTLERelatedParametersComment() - Method in class org.orekit.files.ccsds.OMMFile
Get the comment for TLE related parameters.
getToc() - Method in interface org.orekit.propagation.analytical.gnss.GPSOrbitalElements
Gets the clock correction reference time toc.
getTOD(boolean) - Static method in class org.orekit.frames.FramesFactory
Get the TOD reference frame.
getTOD(IERSConventions, boolean) - Static method in class org.orekit.frames.FramesFactory
Get the TOD reference frame.
getTopocentricFrame() - Method in class org.orekit.propagation.events.ElevationDetector
Returns the currently configured topocentric frame definitions.
getTopocentricFrame() - Method in class org.orekit.propagation.events.ElevationExtremumDetector
Returns the topocentric frame centered on ground point.
getTopocentricFrame() - Method in class org.orekit.propagation.events.FieldElevationDetector
Returns the currently configured topocentric frame definitions.
getTotalEclipse() - Method in class org.orekit.propagation.events.EclipseDetector
Get the total eclipse detection flag.
getTotalEclipse() - Method in class org.orekit.propagation.events.FieldEclipseDetector
Get the total eclipse detection flag.
getTotalIntensity() - Method in class org.orekit.models.earth.GeoMagneticElements
Returns the total intensity of the magnetic field (= norm of the field vector).
getTransform(AbsoluteDate) - Method in class org.orekit.estimation.measurements.EstimatedEarthFrameProvider
Get the Transform corresponding to specified date.
getTransform(AbsoluteDate) - Method in class org.orekit.frames.EclipticProvider
 
getTransform(AbsoluteDate) - Method in class org.orekit.frames.FixedTransformProvider
Get the Transform corresponding to specified date.
getTransform(AbsoluteDate) - Method in class org.orekit.frames.GTODProvider
Get the Transform corresponding to specified date.
getTransform(AbsoluteDate) - Method in class org.orekit.frames.HelmertTransformation
Get the Transform corresponding to specified date.
getTransform(AbsoluteDate) - Method in class org.orekit.frames.InterpolatingTransformProvider
Get the Transform corresponding to specified date.
getTransform(AbsoluteDate) - Method in class org.orekit.frames.ITRFVersion.Converter
Get the Transform corresponding to specified date.
getTransform(AbsoluteDate) - Method in class org.orekit.frames.L1TransformProvider
Get the Transform corresponding to specified date.
getTransform(AbsoluteDate) - Method in class org.orekit.frames.ShiftingTransformProvider
Get the Transform corresponding to specified date.
getTransform(AbsoluteDate) - Method in interface org.orekit.frames.TransformProvider
Get the Transform corresponding to specified date.
getTransform(FieldAbsoluteDate<DerivativeStructure>, DSFactory, Map<String, Integer>) - Method in class org.orekit.estimation.measurements.EstimatedEarthFrameProvider
Get the transform with derivatives.
getTransform(FieldAbsoluteDate<T>) - Method in class org.orekit.estimation.measurements.EstimatedEarthFrameProvider
Get the FieldTransform corresponding to specified date.
getTransform(FieldAbsoluteDate<T>) - Method in class org.orekit.frames.EclipticProvider
 
getTransform(FieldAbsoluteDate<T>) - Method in class org.orekit.frames.FixedTransformProvider
Get the FieldTransform corresponding to specified date.
getTransform(FieldAbsoluteDate<T>) - Method in class org.orekit.frames.GTODProvider
Get the FieldTransform corresponding to specified date.
getTransform(FieldAbsoluteDate<T>) - Method in class org.orekit.frames.HelmertTransformation
Get the FieldTransform corresponding to specified date.
getTransform(FieldAbsoluteDate<T>) - Method in class org.orekit.frames.InterpolatingTransformProvider
Get the FieldTransform corresponding to specified date.
getTransform(FieldAbsoluteDate<T>) - Method in class org.orekit.frames.ITRFVersion.Converter
Get the FieldTransform corresponding to specified date.
getTransform(FieldAbsoluteDate<T>) - Method in class org.orekit.frames.L1TransformProvider
Get the FieldTransform corresponding to specified date.
getTransform(FieldAbsoluteDate<T>) - Method in class org.orekit.frames.ShiftingTransformProvider
Get the FieldTransform corresponding to specified date.
getTransform(FieldAbsoluteDate<T>) - Method in interface org.orekit.frames.TransformProvider
Get the FieldTransform corresponding to specified date.
getTransformation() - Method in enum org.orekit.frames.HelmertTransformation.Predefined
Get the underlying HelmertTransformation.
getTransformProvider() - Method in class org.orekit.frames.Frame
Get the provider for transform from parent frame to instance.
getTransformTo(Frame, AbsoluteDate) - Method in class org.orekit.frames.Frame
Get the transform from the instance to another frame.
getTransformTo(Frame, FieldAbsoluteDate<T>) - Method in class org.orekit.frames.Frame
Get the transform from the instance to another frame.
getTransitions() - Method in class org.orekit.utils.FieldTimeSpanMap
Get an unmodifiable view of the sorted transitions.
getTransitions() - Method in class org.orekit.utils.TimeSpanMap
Get an unmodifiable view of the sorted transitions.
getTranslation() - Method in class org.orekit.frames.FieldTransform
Get the underlying elementary translation.
getTranslation() - Method in class org.orekit.frames.Transform
Get the underlying elementary translation.
getTransmitBand() - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData
Getter for the transmitBand.
getTransmitDelays() - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData
Getter for the transmitDelays.
getTrigger() - Method in class org.orekit.forces.maneuvers.ImpulseManeuver
Get the triggering event.
getTriggeredIncreasing() - Method in enum org.orekit.propagation.events.FilterType
Get the increasing status of triggered events.
getTrueAnomaly() - Method in class org.orekit.orbits.FieldKeplerianOrbit
Get the true anomaly.
getTrueAnomaly() - Method in class org.orekit.orbits.KeplerianOrbit
Get the true anomaly.
getTrueAnomalyDot() - Method in class org.orekit.orbits.FieldKeplerianOrbit
Get the true anomaly derivative.
getTrueAnomalyDot() - Method in class org.orekit.orbits.KeplerianOrbit
Get the true anomaly derivative.
getTT() - Static method in class org.orekit.time.TimeScalesFactory
Get the Terrestrial Time scale.
getTurnaroundDenominator() - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData
Getter for the turnaroundDenominator.
getTurnaroundNumerator() - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData
Getter for the turnaroundNumerator.
getType() - Method in class org.orekit.files.sp3.SP3File
Returns the SP3File.SP3FileType associated with this SP3 file.
getType() - Method in class org.orekit.gnss.antenna.Antenna
Get the type of the antenna.
getType() - Method in class org.orekit.orbits.CartesianOrbit
Get the orbit type.
getType() - Method in class org.orekit.orbits.CircularOrbit
Get the orbit type.
getType() - Method in class org.orekit.orbits.EquinoctialOrbit
Get the orbit type.
getType() - Method in class org.orekit.orbits.FieldCartesianOrbit
Get the orbit type.
getType() - Method in class org.orekit.orbits.FieldCircularOrbit
Get the orbit type.
getType() - Method in class org.orekit.orbits.FieldEquinoctialOrbit
Get the orbit type.
getType() - Method in class org.orekit.orbits.FieldKeplerianOrbit
Get the orbit type.
getType() - Method in class org.orekit.orbits.FieldOrbit
Get the orbit type.
getType() - Method in class org.orekit.orbits.KeplerianOrbit
Get the orbit type.
getType() - Method in class org.orekit.orbits.Orbit
Get the orbit type.
getTypeObs() - Method in class org.orekit.gnss.RinexLoader.Parser.PhaseShiftCorrection
Get the Carrier Phase Observation Code.
getTypesObsScaled() - Method in class org.orekit.gnss.RinexLoader.Parser.ScaleFactorCorrection
Get the list of Observation Types scaled.
getU() - Method in class org.orekit.bodies.Ellipse
Get the unit vector along the major axis.
getUnderlyingAttitudeProvider() - Method in interface org.orekit.attitudes.AttitudeProviderModifier
Get the underlying attitude provider.
getUnderlyingAttitudeProvider() - Method in class org.orekit.attitudes.SpinStabilized
Get the underlying attitude provider.
getUnderlyingAttitudeProvider() - Method in class org.orekit.attitudes.YawCompensation
Get the underlying (ground pointing) attitude provider.
getUnderlyingAttitudeProvider() - Method in class org.orekit.attitudes.YawSteering
Get the underlying (ground pointing) attitude provider.
getUndulation(double, double, AbsoluteDate) - Method in class org.orekit.models.earth.Geoid
Gets the Undulation of the Geoid, N at the given position.
getUnnormalizationFactors(int, int) - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory
Get a un-normalization factors array.
getUnnormalizedCnm(int, int) - Method in interface org.orekit.forces.gravity.potential.UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics
Get a spherical harmonic cosine coefficient.
getUnnormalizedProvider(double, double, TideSystem, double[][], double[][]) - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory
Create a time-independent UnnormalizedSphericalHarmonicsProvider from canonical coefficients.
getUnnormalizedProvider(int, int) - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory
Get the gravity field coefficients provider from the first supported file.
getUnnormalizedProvider(NormalizedSphericalHarmonicsProvider) - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory
getUnnormalizedSnm(int, int) - Method in interface org.orekit.forces.gravity.potential.UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics
Get a spherical harmonic sine coefficient.
getUpperCaseAbbreviation() - Method in enum org.orekit.time.Month
Get the upper case three letters abbreviation.
getUpperCaseName() - Method in enum org.orekit.time.Month
Get the upper case full name.
getURA() - Method in class org.orekit.gnss.GPSAlmanac
Gets the average URA number.
getUranus() - Static method in class org.orekit.bodies.CelestialBodyFactory
Get the Uranus singleton body.
getUseableStartTime() - Method in class org.orekit.files.ccsds.OEMFile.EphemeridesBlock
Get start of useable time span covered by ephemerides data, it may be necessary to allow for proper interpolation.
getUseableStopTime() - Method in class org.orekit.files.ccsds.OEMFile.EphemeridesBlock
Get end of useable time span covered by ephemerides data, it may be necessary to allow for proper interpolation.
getUserDefinedParameters() - Method in class org.orekit.files.ccsds.OGMFile
Get the map of user defined parameter keywords and their corresponding values.
getUT1(EOPHistory) - Static method in class org.orekit.time.TimeScalesFactory
Get the Universal Time 1 scale.
getUT1(IERSConventions, boolean) - Static method in class org.orekit.time.TimeScalesFactory
Get the Universal Time 1 scale.
getUT1MinusUTC() - Method in class org.orekit.frames.EOPEntry
Get the UT1-UTC value.
getUT1MinusUTC(AbsoluteDate) - Method in class org.orekit.frames.EOPHistory
Get the UT1-UTC value.
getUT1MinusUTC(FieldAbsoluteDate<T>) - Method in class org.orekit.frames.EOPHistory
Get the UT1-UTC value.
getUTC() - Static method in class org.orekit.time.TimeScalesFactory
Get the Universal Time Coordinate scale.
getUTCScale() - Method in class org.orekit.time.UT1Scale
Get the associated UTC scale.
getV() - Method in class org.orekit.bodies.Ellipse
Get the unit vector along the minor axis.
getValidFrom() - Method in class org.orekit.gnss.antenna.SatelliteAntenna
Get start of validity.
getValidFUntil() - Method in class org.orekit.gnss.antenna.SatelliteAntenna
Get end of validity.
getValue() - Method in class org.orekit.estimation.sequential.MeasurementDecorator
getValue() - Method in class org.orekit.gnss.ObservationData
Get the observed value.
getValue() - Method in class org.orekit.utils.ParameterDriver
Get current parameter value.
getValue(int, double) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenTesseralLinear
Compute the value of the Hansen coefficient Kj-n-1, s.
getValue(int, double) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenThirdBodyLinear
Compute the value of the Hansen coefficient K₀n, s.
getValue(int, double) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenZonalLinear
Get the K₀-n-1,s coefficient value.
getValue(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GammaMnsFunction
Get Γ function value.
getValue(int, int, int, int) - Static method in class org.orekit.propagation.semianalytical.dsst.utilities.NewcombOperators
Get the Newcomb operator evaluated at n, s, ρ, σ.
getValue(int, int, int, DerivativeStructure) - Static method in class org.orekit.propagation.semianalytical.dsst.utilities.JacobiPolynomials
Returns the value and derivatives of the Jacobi polynomial Plv,w evaluated at γ.
getValue(DSFactory, Map<String, Integer>) - Method in class org.orekit.utils.ParameterDriver
Get the value as a derivative structure.
getValuesSamples() - Method in class org.orekit.utils.InterpolationTableLoader
Returns a copy of the values samples for the interpolation function.
getVdop() - Method in class org.orekit.gnss.DOP
Gets the vertical dilution of precision.
getVectorF() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
Get equinoctial frame vector f.
getVectorG() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
Get equinoctial frame vector g.
getVectorW() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
Get equinoctial frame vector w.
getVeis1950() - Static method in class org.orekit.frames.FramesFactory
Get the VEIS 1950 reference frame.
getVelocity() - Method in class org.orekit.estimation.measurements.PV
Get the velocity.
getVelocity() - Method in class org.orekit.files.ccsds.OPMFile
Get velocity vector.
getVelocity() - Method in class org.orekit.frames.FieldTransform
Get the first time derivative of the translation.
getVelocity() - Method in class org.orekit.frames.Transform
Get the first time derivative of the translation.
getVelocity() - Method in class org.orekit.utils.FieldPVCoordinates
Gets the velocity.
getVelocity() - Method in class org.orekit.utils.PVCoordinates
Gets the velocity.
getVelocity(AbsoluteDate, Vector3D, Frame) - Method in interface org.orekit.forces.drag.atmosphere.Atmosphere
Get the inertial velocity of atmosphere molecules.
getVelocity(FieldAbsoluteDate<T>, FieldVector3D<T>, Frame) - Method in interface org.orekit.forces.drag.atmosphere.Atmosphere
Get the inertial velocity of atmosphere molecules.
getVenus() - Static method in class org.orekit.bodies.CelestialBodyFactory
Get the Venus singleton body.
getVertices() - Method in class org.orekit.models.earth.tessellation.Tile
Get the four vertices.
getVmns(int, int, int) - Static method in class org.orekit.propagation.semianalytical.dsst.utilities.CoefficientsFactory
Get the Vn,sm coefficient from Vn,s.
getWarmup() - Method in class org.orekit.estimation.measurements.modifiers.OutlierFilter
Get the value of warmup iterations.
getWaterVaporPressure() - Method in class org.orekit.models.earth.GlobalPressureTemperature2Model
Returns the water vapor pressure at the station [hPa].
getWaves() - Method in class org.orekit.forces.gravity.potential.OceanTidesReader
Get the loaded waves.
getWeek() - Method in class org.orekit.gnss.GPSAlmanac
 
getWeek() - Method in interface org.orekit.propagation.analytical.gnss.GPSOrbitalElements
Gets the Reference Week of the GPS orbit.
getWeekNumber() - Method in class org.orekit.time.GPSDate
Get the week number since GPS epoch.
getWest() - Method in class org.orekit.bodies.FieldGeodeticPoint
Get the direction to the west of point, expressed in parent shape frame.
getWest() - Method in class org.orekit.bodies.GeodeticPoint
Get the direction to the west of point, expressed in parent shape frame.
getWest() - Method in class org.orekit.frames.TopocentricFrame
Get the west direction of topocentric frame, expressed in parent shape frame.
getWestAmplitude(int, int) - Method in class org.orekit.models.earth.displacement.OceanLoadingCoefficients
Get the amplitude along west axis.
getWestPhase(int, int) - Method in class org.orekit.models.earth.displacement.OceanLoadingCoefficients
Get the phase along West axis.
getWgs84(Frame) - Static method in class org.orekit.models.earth.ReferenceEllipsoid
Get the WGS84 ellipsoid, attached to the given body frame.
getWMM(double) - Static method in class org.orekit.models.earth.GeoMagneticFieldFactory
Get the WMM model for the given year.
getX() - Method in class org.orekit.frames.EOPEntry
Get the X component of the pole motion.
getXM10(AbsoluteDate) - Method in interface org.orekit.forces.drag.atmosphere.JB2008InputParameters
Get the MG2 index scaled to F10.
getXM10B(AbsoluteDate) - Method in interface org.orekit.forces.drag.atmosphere.JB2008InputParameters
Get the MG2 81-day average centered index.
getXp() - Method in class org.orekit.frames.FieldPoleCorrection
Get the xp parameter.
getXp() - Method in class org.orekit.frames.PoleCorrection
Get the xp parameter.
getXYSpXY2Function() - Method in enum org.orekit.utils.IERSConventions
Get the function computing the Celestial Intermediate Pole and Celestial Intermediate Origin components.
getY() - Method in class org.orekit.frames.EOPEntry
Get the Y component of the pole motion.
getY10(AbsoluteDate) - Method in interface org.orekit.forces.drag.atmosphere.JB2008InputParameters
Get the Solar X-Ray & Lya index scaled to F10.
getY10B(AbsoluteDate) - Method in interface org.orekit.forces.drag.atmosphere.JB2008InputParameters
Get the Solar X-Ray & Lya 81-day ave.
getYawAngle(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.YawCompensation
Compute the yaw compensation angle at date.
getYawAngle(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.YawCompensation
Compute the yaw compensation angle at date.
getYear() - Method in enum org.orekit.frames.ITRFVersion
Get the reference year of the frame version.
getYear() - Method in class org.orekit.time.DateComponents
Get the year number.
getYp() - Method in class org.orekit.frames.FieldPoleCorrection
Get the yp parameter.
getYp() - Method in class org.orekit.frames.PoleCorrection
Get the yp parameter.
getZenith() - Method in class org.orekit.bodies.FieldGeodeticPoint
Get the direction above the point, expressed in parent shape frame.
getZenith() - Method in class org.orekit.bodies.GeodeticPoint
Get the direction above the point, expressed in parent shape frame.
getZenith() - Method in class org.orekit.frames.TopocentricFrame
Get the zenith direction of topocentric frame, expressed in parent shape frame.
getZenithAmplitude(int, int) - Method in class org.orekit.models.earth.displacement.OceanLoadingCoefficients
Get the amplitude along zenith axis.
getZenithDelay() - Method in class org.orekit.models.earth.ViennaModelCoefficientsLoader
Returns the zenith delay array.
getZenithOffsetDriver() - Method in class org.orekit.estimation.measurements.GroundStation
Get a driver allowing to change station position along Zenith axis.
getZenithPhase(int, int) - Method in class org.orekit.models.earth.displacement.OceanLoadingCoefficients
Get the phase along zenith axis.
getZero(Field<T>) - Static method in class org.orekit.utils.FieldPVCoordinates
Get fixed position/velocity at origin (both p, v and a are zero vectors).
getZone() - Method in class org.orekit.propagation.events.FieldOfView
Get the interior zone.
getZone() - Method in class org.orekit.propagation.events.FootprintOverlapDetector
Get the geographic zone triggering the events.
getZone() - Method in class org.orekit.propagation.events.GeographicZoneDetector
Get the geographic zone.
GHIJjsPolynomials - Class in org.orekit.propagation.semianalytical.dsst.utilities
Compute the Gjs, Hjs, Ijs and Jjs polynomials in the equinoctial elements h, k and the direction cosines α and β and their partial derivatives with respect to k, h, α and β.
GHIJjsPolynomials(double, double, double, double) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
Create a set of Gjs, Hjs, Ijs and Jjs polynomials.
GHmsjPolynomials - Class in org.orekit.propagation.semianalytical.dsst.utilities
Compute the Gmsj and the Hmsj polynomials in the equinoctial elements h, k and the direction cosines α and β and their partial derivatives with respect to k, h, α and β.
GHmsjPolynomials(double, double, double, double, int) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.GHmsjPolynomials
Create a set of Gmsj and Hmsj polynomials.
GillIntegratorBuilder - Class in org.orekit.propagation.conversion
Builder for GillIntegrator.
GillIntegratorBuilder(double) - Constructor for class org.orekit.propagation.conversion.GillIntegratorBuilder
Build a new instance.
GLO - org.orekit.files.sp3.SP3File.TimeSystem
GLONASS.
GlobalMappingFunctionModel - Class in org.orekit.models.earth
The Global Mapping Function model for radio techniques.
GlobalMappingFunctionModel(double, double) - Constructor for class org.orekit.models.earth.GlobalMappingFunctionModel
Build a new instance.
GlobalPressureTemperature2Model - Class in org.orekit.models.earth
The Global Pressure and Temperature 2 (GPT2) model.
GlobalPressureTemperature2Model(double, double, Geoid) - Constructor for class org.orekit.models.earth.GlobalPressureTemperature2Model
Constructor with default supported names.
GlobalPressureTemperature2Model(String, double, double, Geoid) - Constructor for class org.orekit.models.earth.GlobalPressureTemperature2Model
Constructor with supported names given by user.
GlobalPressureTemperatureModel - Class in org.orekit.models.earth
The Global Pressure and Temperature model.
GlobalPressureTemperatureModel(double, double, Frame) - Constructor for class org.orekit.models.earth.GlobalPressureTemperatureModel
Build a new instance.
Glonass - Class in org.orekit.gnss.attitude
Attitude providers for Glonass navigation satellites.
Glonass(double, AbsoluteDate, AbsoluteDate, ExtendedPVCoordinatesProvider, Frame) - Constructor for class org.orekit.gnss.attitude.Glonass
Simple constructor.
GLONASS - org.orekit.files.sp3.SP3File.SP3FileType
GLONASS only file.
GLONASS - org.orekit.gnss.antenna.SatelliteAntennaCode
Deprecated.
GLONASS : GLONASS no.
GLONASS - org.orekit.gnss.antenna.SatelliteType
GLONASS : GLONASS no.
GLONASS - org.orekit.gnss.SatelliteSystem
GLONASS system.
GLONASS_K1 - org.orekit.gnss.antenna.SatelliteAntennaCode
Deprecated.
GLONASS-K1 : IGS SVN R801-R802 (GLO no.
GLONASS_K1 - org.orekit.gnss.antenna.SatelliteType
GLONASS-K1 : IGS SVN R801-R802 (GLO no.
GLONASS_K2 - org.orekit.gnss.antenna.SatelliteAntennaCode
Deprecated.
GLONASS-K2.
GLONASS_K2 - org.orekit.gnss.antenna.SatelliteType
GLONASS-K2.
GLONASS_M - org.orekit.gnss.antenna.SatelliteAntennaCode
Deprecated.
GLONASS-M : GLONASS no.
GLONASS_M - org.orekit.gnss.antenna.SatelliteType
GLONASS-M : GLONASS no.
GLONASSScale - Class in org.orekit.time
GLONASS time scale.
GM - org.orekit.files.ccsds.Keyword
Gravitational coefficient.
GMST - org.orekit.files.ccsds.CcsdsTimeScale
Greenwich Mean Sidereal Time.
GMSTScale - Class in org.orekit.time
Greenwich Mean Sidereal Time.
GNSSAttitudeProvider - Interface in org.orekit.gnss.attitude
Attitude providers for navigation satellites.
GPS - org.orekit.files.ccsds.CcsdsTimeScale
Global Positioning System.
GPS - org.orekit.files.sp3.SP3File.SP3FileType
GPS only file.
GPS - org.orekit.files.sp3.SP3File.TimeSystem
Global Positioning System.
GPS - org.orekit.gnss.SatelliteSystem
GPS system.
GPS_EPOCH - Static variable in class org.orekit.time.AbsoluteDate
Reference epoch for GPS weeks: 1980-01-06T00:00:00 GPS time.
GPS_EPOCH - Static variable in class org.orekit.time.DateComponents
Reference epoch for GPS weeks: 1980-01-06.
GPS_MU - Static variable in interface org.orekit.propagation.analytical.gnss.GPSOrbitalElements
WGS 84 value of the Earth's universal gravitational parameter for GPS user in m³/s².
GPS_PI - Static variable in interface org.orekit.propagation.analytical.gnss.GPSOrbitalElements
Value of Pi for conversion from semicircles to radian.
GPS_WEEK_IN_SECONDS - Static variable in interface org.orekit.propagation.analytical.gnss.GPSOrbitalElements
Duration of the GPS week in seconds.
GPS_WEEK_NB - Static variable in interface org.orekit.propagation.analytical.gnss.GPSOrbitalElements
Number of weeks in the GPS cycle.
GPSAlmanac - Class in org.orekit.gnss
This class holds a GPS almanac as read from SEM or YUMA files.
GPSAlmanac(String, int, int, int, double, double, double, double, double, double, double, double, double, double, int, int, int) - Constructor for class org.orekit.gnss.GPSAlmanac
Constructor.
GPSBlockIIA - Class in org.orekit.gnss.attitude
Attitude providers for GPS block IIR navigation satellites.
GPSBlockIIA(double, double, AbsoluteDate, AbsoluteDate, ExtendedPVCoordinatesProvider, Frame) - Constructor for class org.orekit.gnss.attitude.GPSBlockIIA
Simple constructor.
GPSBlockIIA(double, double, AbsoluteDate, AbsoluteDate, ExtendedPVCoordinatesProvider, Frame, int) - Constructor for class org.orekit.gnss.attitude.GPSBlockIIA
GPSBlockIIF - Class in org.orekit.gnss.attitude
Attitude providers for GPS block IIF navigation satellites.
GPSBlockIIF(double, double, AbsoluteDate, AbsoluteDate, ExtendedPVCoordinatesProvider, Frame) - Constructor for class org.orekit.gnss.attitude.GPSBlockIIF
Simple constructor.
GPSBlockIIR - Class in org.orekit.gnss.attitude
Attitude providers for GPS block IIF navigation satellites.
GPSBlockIIR(double, AbsoluteDate, AbsoluteDate, ExtendedPVCoordinatesProvider, Frame) - Constructor for class org.orekit.gnss.attitude.GPSBlockIIR
Simple constructor.
GPSDate - Class in org.orekit.time
Container for date in GPS form.
GPSDate(int, double) - Constructor for class org.orekit.time.GPSDate
Build an instance corresponding to a GPS date.
GPSDate(AbsoluteDate) - Constructor for class org.orekit.time.GPSDate
Build an instance from an absolute date.
GPSOrbitalElements - Interface in org.orekit.propagation.analytical.gnss
This interface provides the minimal set of orbital elements needed by the GPSPropagator.
GPSPropagator - Class in org.orekit.propagation.analytical.gnss
This class aims at propagating a GPS orbit from GPSOrbitalElements.
GPSPropagator.Builder - Class in org.orekit.propagation.analytical.gnss
This nested class aims at building a GPSPropagator.
GPSScale - Class in org.orekit.time
GPS time scale.
gradient(AbsoluteDate, Vector3D, double) - Method in class org.orekit.forces.gravity.HolmesFeatherstoneAttractionModel
Compute the gradient of the non-central part of the gravity field.
gradient(FieldAbsoluteDate<T>, FieldVector3D<T>, T) - Method in class org.orekit.forces.gravity.HolmesFeatherstoneAttractionModel
Compute the gradient of the non-central part of the gravity field.
GraggBulirschStoerIntegratorBuilder - Class in org.orekit.propagation.conversion
Builder for GraggBulirschStoerIntegrator.
GraggBulirschStoerIntegratorBuilder(double, double, double) - Constructor for class org.orekit.propagation.conversion.GraggBulirschStoerIntegratorBuilder
Build a new instance.
GRAVITY_FIELD_NORMALIZATION_UNDERFLOW - org.orekit.errors.OrekitMessages
 
GravityFieldFactory - Class in org.orekit.forces.gravity.potential
Factory used to read gravity field files in several supported formats.
GRC - org.orekit.files.ccsds.CCSDSFrame
Greenwich Rotating Coordinates.
GRGS_FILENAME - Static variable in class org.orekit.forces.gravity.potential.GravityFieldFactory
Default regular expression for GRGS files.
GRGSFormatReader - Class in org.orekit.forces.gravity.potential
Reader for the GRGS gravity field format.
GRGSFormatReader(String, boolean) - Constructor for class org.orekit.forces.gravity.potential.GRGSFormatReader
Simple constructor.
GRIM5C1_EARTH_ANGULAR_VELOCITY - Static variable in interface org.orekit.utils.Constants
Earth angular velocity from GRIM5C1 model: 7.292115e-5 rad/s.
GRIM5C1_EARTH_C20 - Static variable in interface org.orekit.utils.Constants
Earth un-normalized second zonal coefficient from GRIM5C1 model: -1.082626110612609e-3.
GRIM5C1_EARTH_C30 - Static variable in interface org.orekit.utils.Constants
Earth un-normalized third zonal coefficient from GRIM5C1 model: 2.536150841690056e-6.
GRIM5C1_EARTH_C40 - Static variable in interface org.orekit.utils.Constants
Earth un-normalized fourth zonal coefficient from GRIM5C1 model: 1.61936352497151e-6.
GRIM5C1_EARTH_C50 - Static variable in interface org.orekit.utils.Constants
Earth un-normalized fifth zonal coefficient from GRIM5C1 model: 2.231013736607540e-7.
GRIM5C1_EARTH_C60 - Static variable in interface org.orekit.utils.Constants
Earth un-normalized sixth zonal coefficient from GRIM5C1 model: -5.402895357302363e-7.
GRIM5C1_EARTH_EQUATORIAL_RADIUS - Static variable in interface org.orekit.utils.Constants
Earth equatorial radius from GRIM5C1 model: 6378136.46 m.
GRIM5C1_EARTH_FLATTENING - Static variable in interface org.orekit.utils.Constants
Earth flattening from GRIM5C1 model: 1.0 / 298.25765.
GRIM5C1_EARTH_MU - Static variable in interface org.orekit.utils.Constants
Earth gravitational constant from GRIM5C1 model: 3.986004415e14 m³/s².
GroundAtNightDetector - Class in org.orekit.propagation.events
Detector for ground location being at night.
GroundAtNightDetector(TopocentricFrame, PVCoordinatesProvider, double, AtmosphericRefractionModel) - Constructor for class org.orekit.propagation.events.GroundAtNightDetector
Simple constructor.
GroundFieldOfViewDetector - Class in org.orekit.propagation.events
Finder for satellite entry/exit events with respect to a sensor Field Of View attached to an arbitrary frame.
GroundFieldOfViewDetector(Frame, FieldOfView) - Constructor for class org.orekit.propagation.events.GroundFieldOfViewDetector
Build a new instance.
GroundPointing - Class in org.orekit.attitudes
Base class for ground pointing attitude providers.
GroundPointing(Frame, Frame) - Constructor for class org.orekit.attitudes.GroundPointing
Default constructor.
GroundStation - Class in org.orekit.estimation.measurements
Class modeling a ground station that can perform some measurements.
GroundStation(TopocentricFrame) - Constructor for class org.orekit.estimation.measurements.GroundStation
Build a ground station ignoring station displacements.
GroundStation(TopocentricFrame, EOPHistory, StationDisplacement...) - Constructor for class org.orekit.estimation.measurements.GroundStation
Simple constructor.
GRS80_EARTH_ANGULAR_VELOCITY - Static variable in interface org.orekit.utils.Constants
Earth angular velocity from GRS80 model: 7.292115e-5 rad/s.
GRS80_EARTH_C20 - Static variable in interface org.orekit.utils.Constants
Earth un-normalized second zonal coefficient from GRS80 model: -1.08263e-3.
GRS80_EARTH_EQUATORIAL_RADIUS - Static variable in interface org.orekit.utils.Constants
Earth equatorial radius from GRS80 model: 6378137.0 m.
GRS80_EARTH_FLATTENING - Static variable in interface org.orekit.utils.Constants
Earth flattening from GRS80 model: 1.0 / 298.257222101.
GRS80_EARTH_MU - Static variable in interface org.orekit.utils.Constants
Earth gravitational constant from GRS80 model: 3.986005e14 m³/s².
GTOD_CONVENTIONS_1996_ACCURATE_EOP - org.orekit.frames.Predefined
GTOD, IERS 1996 conventions, with accurate EOP interpolation.
GTOD_CONVENTIONS_1996_SIMPLE_EOP - org.orekit.frames.Predefined
GTOD, IERS 1996 conventions, with simple EOP interpolation.
GTOD_CONVENTIONS_2003_ACCURATE_EOP - org.orekit.frames.Predefined
GTOD, IERS 2003 conventions, with accurate EOP interpolation.
GTOD_CONVENTIONS_2003_SIMPLE_EOP - org.orekit.frames.Predefined
GTOD, IERS 2003 conventions, with simple EOP interpolation.
GTOD_CONVENTIONS_2010_ACCURATE_EOP - org.orekit.frames.Predefined
GTOD, IERS 2010 conventions, with accurate EOP interpolation.
GTOD_CONVENTIONS_2010_SIMPLE_EOP - org.orekit.frames.Predefined
GTOD, IERS 2010 conventions, with simple EOP interpolation.
GTOD_WITHOUT_EOP_CORRECTIONS - org.orekit.frames.Predefined
GTOD, IERS 1996 conventions without EOP corrections.
GTODProvider - Class in org.orekit.frames
Greenwich True Of Date Frame, also known as True of Date Rotating frame (TDR) or Greenwich Rotating Coordinate frame (GCR).
GTODProvider(IERSConventions, EOPHistory) - Constructor for class org.orekit.frames.GTODProvider
Simple constructor.
GZIP_FILE_PATTERN - Static variable in interface org.orekit.data.DataProvider
Deprecated.
as of 9.2, replaced with GzipFilter
GzipFilter - Class in org.orekit.data
Filter for gzip compressed data.
GzipFilter() - Constructor for class org.orekit.data.GzipFilter
 

H

h - Variable in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution
ey.
H00 - Static variable in class org.orekit.time.TimeComponents
Constant for commonly used hour 00:00:00.
H12 - Static variable in class org.orekit.time.TimeComponents
Constant for commonly used hour 12:00:00.
handleStep(List<OrekitStepInterpolator>, boolean) - Method in interface org.orekit.propagation.sampling.MultiSatStepHandler
Handle the current step.
handleStep(FieldSpacecraftState<T>, boolean) - Method in interface org.orekit.propagation.sampling.FieldOrekitFixedStepHandler
Handle the current step.
handleStep(FieldOrekitStepInterpolator<T>, boolean) - Method in interface org.orekit.propagation.sampling.FieldOrekitStepHandler
Handle the current step.
handleStep(FieldOrekitStepInterpolator<T>, boolean) - Method in class org.orekit.propagation.sampling.FieldOrekitStepHandlerMultiplexer
Handle the current step.
handleStep(FieldOrekitStepInterpolator<T>, boolean) - Method in class org.orekit.propagation.sampling.FieldOrekitStepNormalizer
Handle the last accepted step.
handleStep(OrekitStepInterpolator, boolean) - Method in interface org.orekit.propagation.sampling.OrekitStepHandler
Handle the current step.
handleStep(OrekitStepInterpolator, boolean) - Method in class org.orekit.propagation.sampling.OrekitStepHandlerMultiplexer
Handle the current step.
handleStep(OrekitStepInterpolator, boolean) - Method in class org.orekit.propagation.sampling.OrekitStepNormalizer
Handle the last accepted step.
handleStep(SpacecraftState, boolean) - Method in class org.orekit.files.ccsds.StreamingOemWriter.Segment
 
handleStep(SpacecraftState, boolean) - Method in interface org.orekit.propagation.sampling.OrekitFixedStepHandler
Handle the current step.
HansenTesseralLinear - Class in org.orekit.propagation.semianalytical.dsst.utilities.hansen
Hansen coefficients K(t,n,s) for t!=0 and n < 0.
HansenTesseralLinear(int, int, int, int, int) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenTesseralLinear
Constructor.
HansenThirdBodyLinear - Class in org.orekit.propagation.semianalytical.dsst.utilities.hansen
Hansen coefficients K(t,n,s) for t=0 and n > 0.
HansenThirdBodyLinear(int, int) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenThirdBodyLinear
Constructor.
HansenUtilities - Class in org.orekit.propagation.semianalytical.dsst.utilities.hansen
Utilities class.
HansenZonalLinear - Class in org.orekit.propagation.semianalytical.dsst.utilities.hansen
Hansen coefficients K(t,n,s) for t=0 and n < 0.
HansenZonalLinear(int, int) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenZonalLinear
Constructor.
HarmonicParametricAcceleration - Class in org.orekit.forces
This class implements a parametric acceleration with harmonic signed amplitude.
HarmonicParametricAcceleration(Vector3D, boolean, String, AbsoluteDate, double, int) - Constructor for class org.orekit.forces.HarmonicParametricAcceleration
Simple constructor.
HarmonicParametricAcceleration(Vector3D, AttitudeProvider, String, AbsoluteDate, double, int) - Constructor for class org.orekit.forces.HarmonicParametricAcceleration
Simple constructor.
HarrisPriester - Class in org.orekit.forces.drag.atmosphere
This atmosphere model is the realization of the Modified Harris-Priester model.
HarrisPriester(PVCoordinatesProvider, OneAxisEllipsoid) - Constructor for class org.orekit.forces.drag.atmosphere.HarrisPriester
Simple constructor for Modified Harris-Priester atmosphere model.
HarrisPriester(PVCoordinatesProvider, OneAxisEllipsoid, double) - Constructor for class org.orekit.forces.drag.atmosphere.HarrisPriester
Constructor for Modified Harris-Priester atmosphere model.
HarrisPriester(PVCoordinatesProvider, OneAxisEllipsoid, double[][]) - Constructor for class org.orekit.forces.drag.atmosphere.HarrisPriester
Constructor for Modified Harris-Priester atmosphere model.
HarrisPriester(PVCoordinatesProvider, OneAxisEllipsoid, double[][], double) - Constructor for class org.orekit.forces.drag.atmosphere.HarrisPriester
Constructor for Modified Harris-Priester atmosphere model.
hasAdditionalState(String) - Method in class org.orekit.propagation.FieldSpacecraftState
Check if an additional state is available.
hasAdditionalState(String) - Method in class org.orekit.propagation.SpacecraftState
Check if an additional state is available.
hasCovarianceMatrix() - Method in class org.orekit.files.ccsds.OGMFile
Check whether the OPM contains covariance matrix data.
hasDataFor(AbsoluteDate) - Method in class org.orekit.frames.EOPHistory
Check if the cache has data for the given date using EOPHistory.getStartDate() and EOPHistory.getEndDate().
hasDerivatives() - Method in class org.orekit.orbits.CartesianOrbit
Check if orbit includes derivatives.
hasDerivatives() - Method in class org.orekit.orbits.FieldCartesianOrbit
Check if orbit includes derivatives.
hasDerivatives() - Method in class org.orekit.orbits.FieldCircularOrbit
Check if orbit includes derivatives.
hasDerivatives() - Method in class org.orekit.orbits.FieldEquinoctialOrbit
Check if orbit includes derivatives.
hasDerivatives() - Method in class org.orekit.orbits.FieldKeplerianOrbit
Check if orbit includes derivatives.
hasDerivatives() - Method in class org.orekit.orbits.FieldOrbit
Check if orbit includes derivatives.
hasDerivatives() - Method in class org.orekit.orbits.Orbit
Check if orbit includes derivatives.
hashCode() - Method in class org.orekit.bodies.FieldGeodeticPoint
 
hashCode() - Method in class org.orekit.bodies.GeodeticPoint
 
hashCode() - Method in class org.orekit.models.earth.displacement.Tide
 
hashCode() - Method in class org.orekit.propagation.analytical.tle.TLE
Get a hashcode for this tle.
hashCode() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.CoefficientsFactory.NSKey
hashCode() - Method in class org.orekit.time.AbsoluteDate
Get a hashcode for this date.
hashCode() - Method in class org.orekit.time.DateComponents
hashCode() - Method in class org.orekit.time.DateTimeComponents
hashCode() - Method in class org.orekit.time.FieldAbsoluteDate
Get a hashcode for this date.
hashCode() - Method in class org.orekit.time.TimeComponents
hasKeplerianElements() - Method in class org.orekit.files.ccsds.OGMFile
Check whether the OPM contains Keplerian elements data.
hasNonKeplerianAcceleration(FieldPVCoordinates<T>, double) - Static method in class org.orekit.orbits.FieldOrbit
Check if Cartesian coordinates include non-Keplerian acceleration.
hasNonKeplerianAcceleration(PVCoordinates, double) - Static method in class org.orekit.orbits.Orbit
Check if Cartesian coordinates include non-Keplerian acceleration.
header - org.orekit.files.ccsds.Keyword
Header keyword.
HELIUM - Static variable in class org.orekit.forces.drag.atmosphere.DTM2000
Identifier for helium.
HelmertTransformation - Class in org.orekit.frames
Transformation class for geodetic systems.
HelmertTransformation(AbsoluteDate, double, double, double, double, double, double, double, double, double, double, double, double) - Constructor for class org.orekit.frames.HelmertTransformation
Build a transform from its primitive operations.
HelmertTransformation.Predefined - Enum in org.orekit.frames
Enumerate for predefined Helmert transformations.
HERMITE - org.orekit.files.ccsds.OEMWriter.InterpolationMethod
Hermite interpolation.
HighamHall54IntegratorBuilder - Class in org.orekit.propagation.conversion
Builder for HighamHall54Integrator.
HighamHall54IntegratorBuilder(double, double, double) - Constructor for class org.orekit.propagation.conversion.HighamHall54IntegratorBuilder
Build a new instance.
HLM - org.orekit.files.sp3.SP3File.SP3OrbitType
fitted after applying a Helmert transformation.
HolmesFeatherstoneAttractionModel - Class in org.orekit.forces.gravity
This class represents the gravitational field of a celestial body.
HolmesFeatherstoneAttractionModel(Frame, NormalizedSphericalHarmonicsProvider) - Constructor for class org.orekit.forces.gravity.HolmesFeatherstoneAttractionModel
Creates a new instance.
HYDROGEN - Static variable in class org.orekit.forces.drag.atmosphere.DTM2000
Identifier for hydrogen.
HYPERBOLIC_ORBIT_NOT_HANDLED_AS - org.orekit.errors.OrekitMessages
 
hyperbolicEccentricToMean(double, double) - Static method in class org.orekit.orbits.KeplerianOrbit
Computes the mean anomaly from the hyperbolic eccentric anomaly.
hyperbolicEccentricToMean(T, T) - Static method in class org.orekit.orbits.FieldKeplerianOrbit
Computes the mean anomaly from the hyperbolic eccentric anomaly.
hyperbolicEccentricToTrue(double, double) - Static method in class org.orekit.orbits.KeplerianOrbit
Computes the true anomaly from the hyperbolic eccentric anomaly.
hyperbolicEccentricToTrue(T, T) - Static method in class org.orekit.orbits.FieldKeplerianOrbit
Computes the true anomaly from the hyperbolic eccentric anomaly.
hyperbolicKeplerianToPosition(T, T, T, T, T, T, double) - Static method in class org.orekit.orbits.FieldKeplerianOrbit

I

i - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator
final inclination.
I05 - org.orekit.gnss.Frequency
IRNSS L5.
I09 - org.orekit.gnss.Frequency
IRNSS S (2492.028 MHz).
IAU_2012_ASTRONOMICAL_UNIT - Static variable in interface org.orekit.utils.Constants
Astronomical unit as a conventional unit of length since IAU 2012 resolution B2: 149597870700.0 m.
IAU_2015_NOMINAL_EARTH_EQUATORIAL_RADIUS - Static variable in interface org.orekit.utils.Constants
Earth equatorial radius as defined by IAU 2015 resolution B3: 6.3781e6 (m).
IAU_2015_NOMINAL_EARTH_GM - Static variable in interface org.orekit.utils.Constants
Earth attraction coefficient as defined by IAU 2015 resolution B3: 3.986004e14 (m³/s²).
IAU_2015_NOMINAL_EARTH_POLAR_RADIUS - Static variable in interface org.orekit.utils.Constants
Earth polar radius as defined by IAU 2015 resolution B3: 6.3568e6 (m).
IAU_2015_NOMINAL_JUPITER_EQUATORIAL_RADIUS - Static variable in interface org.orekit.utils.Constants
Jupiter equatorial radius as defined by IAU 2015 resolution B3: 7.1492e7 (m).
IAU_2015_NOMINAL_JUPITER_GM - Static variable in interface org.orekit.utils.Constants
Jupiter attraction coefficient as defined by IAU 2015 resolution B3: 1.2668653e17 (m³/s²).
IAU_2015_NOMINAL_JUPITER_POLAR_RADIUS - Static variable in interface org.orekit.utils.Constants
Jupiter polar radius as defined by IAU 2015 resolution B3: 6.6854e7 (m).
IAU_2015_NOMINAL_SOLAR_RADIUS - Static variable in interface org.orekit.utils.Constants
Solar radius as defined by IAU 2015 resolution B3: 695700000.0 m.
IAU_2015_NOMINAL_SUN_GM - Static variable in interface org.orekit.utils.Constants
Sun attraction coefficient as defined by IAU 2015 resolution B3: 1.3271244e20 (m³/s²).
IAUPole - Interface in org.orekit.bodies
Interface for IAU pole and prime meridian orientations.
ICGEM_FILENAME - Static variable in class org.orekit.forces.gravity.potential.GravityFieldFactory
Default regular expression for ICGEM files.
ICGEMFormatReader - Class in org.orekit.forces.gravity.potential
Reader for the ICGEM gravity field format.
ICGEMFormatReader(String, boolean) - Constructor for class org.orekit.forces.gravity.potential.ICGEMFormatReader
Simple constructor.
ICRF - org.orekit.files.ccsds.CCSDSFrame
International Celestial Reference Frame.
ICRF - org.orekit.frames.Predefined
ICRF frame.
IDENTITY - Static variable in class org.orekit.frames.Transform
Identity transform.
IDENTITY - Static variable in class org.orekit.utils.AngularCoordinates
Fixed orientation parallel with reference frame (identity rotation, zero rotation rate and acceleration).
IDENTITY_PROVIDER - Static variable in class org.orekit.frames.TransformProviderUtils
Identity provider.
IERS_1996 - org.orekit.forces.gravity.potential.OceanLoadDeformationCoefficients
Coefficients from IERS 1996 conventions.
IERS_1996 - org.orekit.utils.IERSConventions
Constant for IERS 1996 conventions.
IERS_2003 - org.orekit.forces.gravity.potential.OceanLoadDeformationCoefficients
Coefficients from IERS 2003 conventions.
IERS_2003 - org.orekit.utils.IERSConventions
Constant for IERS 2003 conventions.
IERS_2010 - org.orekit.forces.gravity.potential.OceanLoadDeformationCoefficients
Coefficients from IERS 2010 conventions.
IERS_2010 - org.orekit.utils.IERSConventions
Constant for IERS 2010 conventions.
IERSConventions - Enum in org.orekit.utils
Supported IERS conventions.
IERSConventions.NutationCorrectionConverter - Interface in org.orekit.utils
Interface for functions converting nutation corrections between δΔψ/δΔε to δX/δY.
IGRF - org.orekit.models.earth.GeoMagneticFieldFactory.FieldModel
International Geomagnetic Reference Field.
ImmutableTimeStampedCache<T extends TimeStamped> - Class in org.orekit.utils
A cache of TimeStamped data that provides concurrency through immutability.
ImmutableTimeStampedCache(int, Collection<? extends T>) - Constructor for class org.orekit.utils.ImmutableTimeStampedCache
Create a new cache with the given neighbors size and data.
ImpulseManeuver<T extends EventDetector> - Class in org.orekit.forces.maneuvers
Impulse maneuver model.
ImpulseManeuver(T, Vector3D, double) - Constructor for class org.orekit.forces.maneuvers.ImpulseManeuver
Build a new instance.
ImpulseManeuver(T, AttitudeProvider, Vector3D, double) - Constructor for class org.orekit.forces.maneuvers.ImpulseManeuver
Build a new instance.
INCLINATION - org.orekit.files.ccsds.Keyword
Orbit inclination.
INCOMPLETE_HEADER - org.orekit.errors.OrekitMessages
 
INCONSISTENT_ASTRONOMICAL_UNIT_IN_FILES - org.orekit.errors.OrekitMessages
 
INCONSISTENT_DATES_IN_IERS_FILE - org.orekit.errors.OrekitMessages
 
INCONSISTENT_EARTH_MOON_RATIO_IN_FILES - org.orekit.errors.OrekitMessages
 
INCONSISTENT_NUMBER_OF_SATS - org.orekit.errors.OrekitMessages
 
INCONSISTENT_SATELLITE_SYSTEM - org.orekit.errors.OrekitMessages
 
InertialProvider - Class in org.orekit.attitudes
This class handles an inertial attitude provider.
InertialProvider(Rotation) - Constructor for class org.orekit.attitudes.InertialProvider
Creates new instance.
init(List<SpacecraftState>, AbsoluteDate) - Method in interface org.orekit.propagation.sampling.MultiSatStepHandler
Initialize step handler at the start of a propagation.
init(FieldSpacecraftState<T>, FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.events.FieldAbstractDetector
Initialize event handler at the start of a propagation.
init(FieldSpacecraftState<T>, FieldAbsoluteDate<T>) - Method in interface org.orekit.propagation.events.FieldEventDetector
Initialize event handler at the start of a propagation.
init(FieldSpacecraftState<T>, FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.events.FieldEventState
Initialize event handler at the start of a propagation.
init(FieldSpacecraftState<T>, FieldAbsoluteDate<T>) - Method in interface org.orekit.propagation.events.handlers.FieldEventHandler
Initialize event handler at the start of a propagation.
init(FieldSpacecraftState<T>, FieldAbsoluteDate<T>) - Method in interface org.orekit.propagation.integration.FieldAbstractIntegratedPropagator.MainStateEquations
Initialize the equations at the start of propagation.
init(FieldSpacecraftState<T>, FieldAbsoluteDate<T>) - Method in interface org.orekit.propagation.integration.FieldAdditionalEquations
Initialize the equations at the start of propagation.
init(FieldSpacecraftState<T>, FieldAbsoluteDate<T>) - Method in interface org.orekit.propagation.sampling.FieldOrekitStepHandler
Initialize step handler at the start of a propagation.
init(FieldSpacecraftState<T>, FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.sampling.FieldOrekitStepHandlerMultiplexer
Initialize step handler at the start of a propagation.
init(FieldSpacecraftState<T>, FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.sampling.FieldOrekitStepNormalizer
Initialize step handler at the start of a propagation.
init(FieldSpacecraftState<T>, FieldAbsoluteDate<T>, T) - Method in interface org.orekit.propagation.sampling.FieldOrekitFixedStepHandler
Initialize step handler at the start of a propagation.
init(SpacecraftState, AbsoluteDate) - Method in interface org.orekit.forces.ForceModel
Initialize the force model at the start of propagation.
init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.forces.HarmonicParametricAcceleration
Initialize the force model at the start of propagation.
init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.forces.maneuvers.ConstantThrustManeuver
Initialize the force model at the start of propagation.
init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.forces.maneuvers.ImpulseManeuver
Initialize event handler at the start of a propagation.
init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.forces.PolynomialParametricAcceleration
Initialize the force model at the start of propagation.
init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.propagation.events.AbstractDetector
Initialize event handler at the start of a propagation.
init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.propagation.events.AdapterDetector
Initialize event handler at the start of a propagation.
init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.propagation.events.BooleanDetector
 
init(SpacecraftState, AbsoluteDate) - Method in interface org.orekit.propagation.events.EventDetector
Initialize event handler at the start of a propagation.
init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.propagation.events.EventEnablingPredicateFilter
Initialize event handler at the start of a propagation.
init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.propagation.events.EventShifter
Initialize event handler at the start of a propagation.
init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.propagation.events.EventSlopeFilter
Initialize event handler at the start of a propagation.
init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.propagation.events.EventState
Initialize event handler at the start of a propagation.
init(SpacecraftState, AbsoluteDate) - Method in interface org.orekit.propagation.events.handlers.EventHandler
Initialize event handler at the start of a propagation.
init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.propagation.events.NegateDetector
 
init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.propagation.events.PositionAngleDetector
Initialize event handler at the start of a propagation.
init(SpacecraftState, AbsoluteDate) - Method in interface org.orekit.propagation.integration.AbstractIntegratedPropagator.MainStateEquations
Initialize the equations at the start of propagation.
init(SpacecraftState, AbsoluteDate) - Method in interface org.orekit.propagation.integration.AdditionalEquations
Initialize the equations at the start of propagation.
init(SpacecraftState, AbsoluteDate) - Method in interface org.orekit.propagation.sampling.OrekitFixedStepHandler
init(SpacecraftState, AbsoluteDate) - Method in interface org.orekit.propagation.sampling.OrekitStepHandler
Initialize step handler at the start of a propagation.
init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.propagation.sampling.OrekitStepHandlerMultiplexer
Initialize step handler at the start of a propagation.
init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.propagation.sampling.OrekitStepNormalizer
Initialize step handler at the start of a propagation.
init(SpacecraftState, AbsoluteDate, double) - Method in class org.orekit.files.ccsds.StreamingOemWriter.Segment
Initialize step handler at the start of a propagation.
init(SpacecraftState, AbsoluteDate, double) - Method in interface org.orekit.propagation.sampling.OrekitFixedStepHandler
Initialize step handler at the start of a propagation.
init(AbsoluteDate, AbsoluteDate) - Method in class org.orekit.estimation.measurements.generation.AbstractMeasurementBuilder
Initialize builder at the start of a measurements generation.
init(AbsoluteDate, AbsoluteDate) - Method in class org.orekit.estimation.measurements.generation.AbstractScheduler
Initialize scheduler at the start of a measurements generation.
init(AbsoluteDate, AbsoluteDate) - Method in interface org.orekit.estimation.measurements.generation.MeasurementBuilder
Initialize builder at the start of a measurements generation.
init(AbsoluteDate, AbsoluteDate) - Method in interface org.orekit.estimation.measurements.generation.Scheduler
Initialize scheduler at the start of a measurements generation.
INITIAL_MATRIX_AND_PARAMETERS_NUMBER_MISMATCH - org.orekit.errors.OrekitMessages
 
INITIAL_STATE_NOT_SPECIFIED_FOR_ORBIT_PROPAGATION - org.orekit.errors.OrekitMessages
 
initialIsOsculating() - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator
Check if the initial state is provided in osculating elements.
initialize(boolean, AbsoluteDate) - Method in interface org.orekit.propagation.integration.ModeHandler
Initialize the mode handler.
initialize(boolean, FieldAbsoluteDate<T>) - Method in interface org.orekit.propagation.integration.FieldModeHandler
Initialize the mode handler.
initialize(AuxiliaryElements, boolean) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution
Performs initialization prior to propagation for the current force model.
initialize(AuxiliaryElements, boolean) - Method in interface org.orekit.propagation.semianalytical.dsst.forces.DSSTForceModel
Performs initialization prior to propagation for the current force model.
initialize(AuxiliaryElements, boolean) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseral
Performs initialization prior to propagation for the current force model.
initialize(AuxiliaryElements, boolean) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBody
Computes the highest power of the eccentricity and the highest power of a/R3 to appear in the truncated analytical power series expansion.
initialize(AuxiliaryElements, boolean) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonal
Performs initialization prior to propagation for the current force model.
initializeStep(AuxiliaryElements) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution
Performs initialization at each integration step for the current force model.
initializeStep(AuxiliaryElements) - Method in interface org.orekit.propagation.semianalytical.dsst.forces.DSSTForceModel
Performs initialization at each integration step for the current force model.
initializeStep(AuxiliaryElements) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseral
Performs initialization at each integration step for the current force model.
initializeStep(AuxiliaryElements) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBody
Performs initialization at each integration step for the current force model.
initializeStep(AuxiliaryElements) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonal
Performs initialization at each integration step for the current force model.
initMapper() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
Initialize the mapper.
initMapper() - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator
Initialize the mapper.
initPVCoordinates() - Method in class org.orekit.orbits.CartesianOrbit
Compute the position/velocity coordinates from the canonical parameters.
initPVCoordinates() - Method in class org.orekit.orbits.CircularOrbit
Compute the position/velocity coordinates from the canonical parameters.
initPVCoordinates() - Method in class org.orekit.orbits.EquinoctialOrbit
Compute the position/velocity coordinates from the canonical parameters.
initPVCoordinates() - Method in class org.orekit.orbits.FieldCartesianOrbit
Compute the position/velocity coordinates from the canonical parameters.
initPVCoordinates() - Method in class org.orekit.orbits.FieldCircularOrbit
Compute the position/velocity coordinates from the canonical parameters.
initPVCoordinates() - Method in class org.orekit.orbits.FieldEquinoctialOrbit
Compute the position/velocity coordinates from the canonical parameters.
initPVCoordinates() - Method in class org.orekit.orbits.FieldKeplerianOrbit
Compute the position/velocity coordinates from the canonical parameters.
initPVCoordinates() - Method in class org.orekit.orbits.FieldOrbit
Compute the position/velocity coordinates from the canonical parameters.
initPVCoordinates() - Method in class org.orekit.orbits.KeplerianOrbit
Compute the position/velocity coordinates from the canonical parameters.
initPVCoordinates() - Method in class org.orekit.orbits.Orbit
Compute the position/velocity coordinates from the canonical parameters.
insideLeap(AbsoluteDate) - Method in class org.orekit.time.GLONASSScale
Check if date is within a leap second introduction in this time scale.
insideLeap(AbsoluteDate) - Method in interface org.orekit.time.TimeScale
Check if date is within a leap second introduction in this time scale.
insideLeap(AbsoluteDate) - Method in class org.orekit.time.UTCScale
Check if date is within a leap second introduction in this time scale.
insideLeap(FieldAbsoluteDate<T>) - Method in class org.orekit.time.GLONASSScale
Check if date is within a leap second introduction in this time scale.
insideLeap(FieldAbsoluteDate<T>) - Method in interface org.orekit.time.TimeScale
Check if date is within a leap second introduction in this time scale.
insideLeap(FieldAbsoluteDate<T>) - Method in class org.orekit.time.UTCScale
Check if date is within a leap second introduction in this time scale.
IntegratedEphemeris - Class in org.orekit.propagation.integration
This class stores sequentially generated orbital parameters for later retrieval.
IntegratedEphemeris(AbsoluteDate, AbsoluteDate, AbsoluteDate, StateMapper, boolean, DenseOutputModel, Map<String, double[]>, List<AdditionalStateProvider>, String[]) - Constructor for class org.orekit.propagation.integration.IntegratedEphemeris
Creates a new instance of IntegratedEphemeris.
INTEGRATION_INTERVAL - org.orekit.files.ccsds.Keyword
Meta-data: Integration interval.
INTEGRATION_REF - org.orekit.files.ccsds.Keyword
Meta-data: Integration reference.
INTERMEDIATE_SUFFIX - Static variable in class org.orekit.estimation.measurements.GroundStation
Suffix for ground station intermediate frame name.
INTERNAL_ERROR - org.orekit.errors.OrekitMessages
 
interpolate(AbsoluteDate, Collection<T>) - Method in interface org.orekit.time.TimeInterpolable
Get an interpolated instance.
interpolate(AbsoluteDate, Stream<Attitude>) - Method in class org.orekit.attitudes.Attitude
Get an interpolated instance.
interpolate(AbsoluteDate, Stream<Transform>) - Method in class org.orekit.frames.Transform
Get an interpolated instance.
interpolate(AbsoluteDate, Stream<Orbit>) - Method in class org.orekit.orbits.CartesianOrbit
Get an interpolated instance.
interpolate(AbsoluteDate, Stream<Orbit>) - Method in class org.orekit.orbits.CircularOrbit
Get an interpolated instance.
interpolate(AbsoluteDate, Stream<Orbit>) - Method in class org.orekit.orbits.EquinoctialOrbit
Get an interpolated instance.
interpolate(AbsoluteDate, Stream<Orbit>) - Method in class org.orekit.orbits.KeplerianOrbit
Get an interpolated instance.
interpolate(AbsoluteDate, Stream<SpacecraftState>) - Method in class org.orekit.propagation.SpacecraftState
Get an interpolated instance.
interpolate(AbsoluteDate, Stream<T>) - Method in interface org.orekit.time.TimeInterpolable
Get an interpolated instance.
interpolate(AbsoluteDate, AngularDerivativesFilter, Collection<TimeStampedAngularCoordinates>) - Static method in class org.orekit.utils.TimeStampedAngularCoordinates
Interpolate angular coordinates.
interpolate(AbsoluteDate, AngularDerivativesFilter, Collection<TimeStampedFieldAngularCoordinates<T>>) - Static method in class org.orekit.utils.TimeStampedFieldAngularCoordinates
Interpolate angular coordinates.
interpolate(AbsoluteDate, CartesianDerivativesFilter, Collection<TimeStampedPVCoordinates>) - Static method in class org.orekit.utils.TimeStampedPVCoordinates
Interpolate position-velocity.
interpolate(AbsoluteDate, CartesianDerivativesFilter, Stream<TimeStampedPVCoordinates>) - Static method in class org.orekit.utils.TimeStampedPVCoordinates
Interpolate position-velocity.
interpolate(AbsoluteDate, CartesianDerivativesFilter, AngularDerivativesFilter, Collection<Transform>) - Static method in class org.orekit.frames.Transform
Interpolate a transform from a sample set of existing transforms.
interpolate(FieldAbsoluteDate<KK>, Collection<T>) - Method in interface org.orekit.time.FieldTimeInterpolable
Get an interpolated instance.
interpolate(FieldAbsoluteDate<KK>, Stream<T>) - Method in interface org.orekit.time.FieldTimeInterpolable
Get an interpolated instance.
interpolate(FieldAbsoluteDate<T>, Collection<FieldTransform<T>>) - Static method in class org.orekit.frames.FieldTransform
Interpolate a transform from a sample set of existing transforms.
interpolate(FieldAbsoluteDate<T>, Stream<FieldAttitude<T>>) - Method in class org.orekit.attitudes.FieldAttitude
Get an interpolated instance.
interpolate(FieldAbsoluteDate<T>, Stream<FieldOrbit<T>>) - Method in class org.orekit.orbits.FieldCartesianOrbit
Get an interpolated instance.
interpolate(FieldAbsoluteDate<T>, Stream<FieldOrbit<T>>) - Method in class org.orekit.orbits.FieldCircularOrbit
Get an interpolated instance.
interpolate(FieldAbsoluteDate<T>, Stream<FieldOrbit<T>>) - Method in class org.orekit.orbits.FieldEquinoctialOrbit
Get an interpolated instance.
interpolate(FieldAbsoluteDate<T>, Stream<FieldOrbit<T>>) - Method in class org.orekit.orbits.FieldKeplerianOrbit
Get an interpolated instance.
interpolate(FieldAbsoluteDate<T>, Stream<FieldSpacecraftState<T>>) - Method in class org.orekit.propagation.FieldSpacecraftState
Get an interpolated instance.
interpolate(FieldAbsoluteDate<T>, AngularDerivativesFilter, Collection<TimeStampedFieldAngularCoordinates<T>>) - Static method in class org.orekit.utils.TimeStampedFieldAngularCoordinates
Interpolate angular coordinates.
interpolate(FieldAbsoluteDate<T>, CartesianDerivativesFilter, Collection<TimeStampedFieldPVCoordinates<T>>) - Static method in class org.orekit.utils.TimeStampedFieldPVCoordinates
Interpolate position-velocity.
interpolate(FieldAbsoluteDate<T>, CartesianDerivativesFilter, Stream<TimeStampedFieldPVCoordinates<T>>) - Static method in class org.orekit.utils.TimeStampedFieldPVCoordinates
Interpolate position-velocity.
interpolate(FieldAbsoluteDate<T>, CartesianDerivativesFilter, AngularDerivativesFilter, Collection<FieldTransform<T>>) - Static method in class org.orekit.frames.FieldTransform
Interpolate a transform from a sample set of existing transforms.
interpolate(FieldAbsoluteDate<T>, CartesianDerivativesFilter, AngularDerivativesFilter, Stream<FieldTransform<T>>) - Static method in class org.orekit.frames.FieldTransform
Interpolate a transform from a sample set of existing transforms.
InterpolatingTransformProvider - Class in org.orekit.frames
Transform provider using thread-safe interpolation on transforms sample.
InterpolatingTransformProvider(TransformProvider, CartesianDerivativesFilter, AngularDerivativesFilter, int, double, int, double, double) - Constructor for class org.orekit.frames.InterpolatingTransformProvider
Simple constructor.
InterpolatingTransformProvider(TransformProvider, CartesianDerivativesFilter, AngularDerivativesFilter, AbsoluteDate, AbsoluteDate, int, double, int, double, double) - Constructor for class org.orekit.frames.InterpolatingTransformProvider
INTERPOLATION - org.orekit.files.ccsds.Keyword
The interpolation method to be used.
INTERPOLATION_DEGREE - org.orekit.files.ccsds.Keyword
The interpolation degree.
InterpolationGrid - Interface in org.orekit.propagation.semianalytical.dsst.utilities
Interface for interpolation grids.
InterpolationTableLoader - Class in org.orekit.utils
Used to read an interpolation table from a data file.
InterpolationTableLoader() - Constructor for class org.orekit.utils.InterpolationTableLoader
 
InterSatDirectViewDetector - Class in org.orekit.propagation.events
Detector for inter-satellites direct view (i.e.
InterSatDirectViewDetector(OneAxisEllipsoid, PVCoordinatesProvider) - Constructor for class org.orekit.propagation.events.InterSatDirectViewDetector
simple constructor.
InterSatellitesRange - Class in org.orekit.estimation.measurements
One-way or two-way range measurements between two satellites.
InterSatellitesRange(int, int, boolean, AbsoluteDate, double, double, double) - Constructor for class org.orekit.estimation.measurements.InterSatellitesRange
InterSatellitesRange(ObservableSatellite, ObservableSatellite, boolean, AbsoluteDate, double, double, double) - Constructor for class org.orekit.estimation.measurements.InterSatellitesRange
Simple constructor.
InterSatellitesRangeBuilder - Class in org.orekit.estimation.measurements.generation
Builder for InterSatellitesRange measurements.
InterSatellitesRangeBuilder(CorrelatedRandomVectorGenerator, ObservableSatellite, ObservableSatellite, boolean, double, double) - Constructor for class org.orekit.estimation.measurements.generation.InterSatellitesRangeBuilder
Simple constructor.
IodGibbs - Class in org.orekit.estimation.iod
Gibbs initial orbit determination.
IodGibbs(double) - Constructor for class org.orekit.estimation.iod.IodGibbs
Creator.
IodGooding - Class in org.orekit.estimation.iod
Gooding angles only initial orbit determination, assuming Keplerian motion.
IodGooding(Frame, double) - Constructor for class org.orekit.estimation.iod.IodGooding
Creator.
IodLambert - Class in org.orekit.estimation.iod
Lambert initial orbit determination, assuming Keplerian motion.
IodLambert(double) - Constructor for class org.orekit.estimation.iod.IodLambert
Creator.
IonosphericModel - Interface in org.orekit.models.earth
Defines a ionospheric model, used to calculate the path delay imposed to electro-magnetic signals between an orbital satellite and a ground station.
IRNSS - org.orekit.gnss.SatelliteSystem
Indian Regional Navigation Satellite System system.
IRNSS_1GEO - org.orekit.gnss.antenna.SatelliteAntennaCode
Deprecated.
IRNSS-1 GEO.
IRNSS_1GEO - org.orekit.gnss.antenna.SatelliteType
IRNSS-1 GEO.
IRNSS_1IGSO - org.orekit.gnss.antenna.SatelliteAntennaCode
Deprecated.
IRNSS-1 IGSO.
IRNSS_1IGSO - org.orekit.gnss.antenna.SatelliteType
IRNSS-1 IGSO.
IRNSSScale - Class in org.orekit.time
IRNSS time scale (also called IRNWT for IRNSS NetWork Time).
IRREGULAR_OR_INCOMPLETE_GRID - org.orekit.errors.OrekitMessages
 
isAdditionalStateManaged(String) - Method in class org.orekit.propagation.AbstractPropagator
Check if an additional state is managed.
isAdditionalStateManaged(String) - Method in class org.orekit.propagation.analytical.Ephemeris
Check if an additional state is managed.
isAdditionalStateManaged(String) - Method in class org.orekit.propagation.FieldAbstractPropagator
Check if an additional state is managed.
isAdditionalStateManaged(String) - Method in interface org.orekit.propagation.FieldPropagator
Check if an additional state is managed.
isAdditionalStateManaged(String) - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
Check if an additional state is managed.
isAdditionalStateManaged(String) - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator
Check if an additional state is managed.
isAdditionalStateManaged(String) - Method in interface org.orekit.propagation.Propagator
Check if an additional state is managed.
isChildOf(Frame) - Method in class org.orekit.frames.Frame
Determine if a Frame is a child of another one.
isCurrentStateInterpolated() - Method in interface org.orekit.propagation.sampling.OrekitStepInterpolator
Determines if the current state is computed directly by the integrator, or if it is calculated using interpolation.
isEnabled() - Method in class org.orekit.estimation.measurements.AbstractMeasurement
Check if a measurement is enabled.
isEnabled() - Method in interface org.orekit.estimation.measurements.ObservedMeasurement
Check if a measurement is enabled.
isFormatOK(String, String) - Static method in class org.orekit.propagation.analytical.tle.TLE
Check the lines format validity.
isForward() - Method in class org.orekit.propagation.events.AbstractDetector
Check if the current propagation is forward or backward.
isForward() - Method in class org.orekit.propagation.events.FieldAbstractDetector
Check if the current propagation is forward or backward.
isForward() - Method in interface org.orekit.propagation.sampling.FieldOrekitStepInterpolator
Check is integration direction is forward in date.
isForward() - Method in interface org.orekit.propagation.sampling.OrekitStepInterpolator
Check is integration direction is forward in date.
isIncreasing() - Method in class org.orekit.propagation.events.EventsLogger.LoggedEvent
Get the Increasing/decreasing status of the event.
isIncreasing() - Method in class org.orekit.propagation.events.FieldEventsLogger.FieldLoggedEvent
Get the Increasing/decreasing status of the event.
isIncreasing() - Method in class org.orekit.propagation.events.handlers.RecordAndContinue.Event
Is the g() function increasing?
isInertial() - Method in class org.orekit.forces.AbstractParametricAcceleration
Check if direction is inertial.
isInside(Vector3D) - Method in class org.orekit.bodies.Ellipsoid
Check if a point is inside the ellipsoid.
isLof() - Method in enum org.orekit.files.ccsds.CCSDSFrame
Check if the frame is a Local Orbital frame.
isMeanOrbit() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
Check if only the mean elements should be used in a semianalitical propagation.
isMeanOrbit() - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator
Check if only the mean elements should be used in a semianalitical propagation.
isOnlyPosition() - Method in class org.orekit.propagation.conversion.AbstractPropagatorConverter
Check if fitting uses only sample positions.
IsotropicDrag - Class in org.orekit.forces.drag
This class models isotropic drag effects.
IsotropicDrag(double, double) - Constructor for class org.orekit.forces.drag.IsotropicDrag
Constructor with drag coefficient min/max set to ±∞.
IsotropicDrag(double, double, double, double) - Constructor for class org.orekit.forces.drag.IsotropicDrag
Constructor with drag coefficient min/max set by user.
IsotropicRadiationClassicalConvention - Class in org.orekit.forces.radiation
This class represents the features of a simplified spacecraft.
IsotropicRadiationClassicalConvention(double, double, double) - Constructor for class org.orekit.forces.radiation.IsotropicRadiationClassicalConvention
Simple constructor.
IsotropicRadiationCNES95Convention - Class in org.orekit.forces.radiation
This class represents the features of a simplified spacecraft.
IsotropicRadiationCNES95Convention(double, double, double) - Constructor for class org.orekit.forces.radiation.IsotropicRadiationCNES95Convention
Simple constructor.
IsotropicRadiationSingleCoefficient - Class in org.orekit.forces.radiation
This class represents the features of a simplified spacecraft.
IsotropicRadiationSingleCoefficient(double, double) - Constructor for class org.orekit.forces.radiation.IsotropicRadiationSingleCoefficient
Constructor with reflection coefficient min/max set to ±∞.
IsotropicRadiationSingleCoefficient(double, double, double, double) - Constructor for class org.orekit.forces.radiation.IsotropicRadiationSingleCoefficient
Constructor with reflection coefficient min/max set by user.
isPreviousStateInterpolated() - Method in interface org.orekit.propagation.sampling.OrekitStepInterpolator
Determines if the previous state is computed directly by the integrator, or if it is calculated using interpolation.
isPseudoInertial() - Method in class org.orekit.frames.Frame
Check if the frame is pseudo-inertial.
isSelected() - Method in class org.orekit.utils.ParameterDriver
Check if parameter is selected.
isSimpleEOP() - Method in class org.orekit.files.ccsds.ODMParser
Get EOP interpolation method.
isSimpleEOP() - Method in class org.orekit.files.ccsds.TDMParser
Get EOP interpolation method.
isSupported(String) - Method in class org.orekit.forces.AbstractForceModel
Check if a parameter is supported.
isSupported(String) - Method in interface org.orekit.forces.ForceModel
Check if a parameter is supported.
isSupported(DataProvider) - Method in class org.orekit.data.DataProvidersManager
Check if some provider is supported.
isTwoWay() - Method in class org.orekit.estimation.measurements.InterSatellitesRange
Check if the instance represents a two-way measurement.
isTwoWay() - Method in class org.orekit.estimation.measurements.Range
Check if the instance represents a two-way measurement.
isTwoWay() - Method in class org.orekit.estimation.measurements.RangeRate
Check if the instance represents a two-way measurement.
ITRF_2000 - org.orekit.frames.ITRFVersion
Constant for ITRF 2000.
ITRF_2005 - org.orekit.frames.ITRFVersion
Constant for ITRF 2005.
ITRF_2008 - org.orekit.frames.ITRFVersion
Constant for ITRF 2008.
ITRF_2008_TO_ITRF_2000 - org.orekit.frames.HelmertTransformation.Predefined
Transformation from ITRF 2008 To ITRF 2000.
ITRF_2008_TO_ITRF_2005 - org.orekit.frames.HelmertTransformation.Predefined
Transformation from ITRF 2008 To ITRF 2005.
ITRF_2008_TO_ITRF_88 - org.orekit.frames.HelmertTransformation.Predefined
Transformation from ITRF 2008 To ITRF 88.
ITRF_2008_TO_ITRF_89 - org.orekit.frames.HelmertTransformation.Predefined
Transformation from ITRF 2008 To ITRF 89.
ITRF_2008_TO_ITRF_90 - org.orekit.frames.HelmertTransformation.Predefined
Transformation from ITRF 2008 To ITRF 90.
ITRF_2008_TO_ITRF_91 - org.orekit.frames.HelmertTransformation.Predefined
Transformation from ITRF 2008 To ITRF 91.
ITRF_2008_TO_ITRF_92 - org.orekit.frames.HelmertTransformation.Predefined
Transformation from ITRF 2008 To ITRF 92.
ITRF_2008_TO_ITRF_93 - org.orekit.frames.HelmertTransformation.Predefined
Transformation from ITRF 2008 To ITRF 93.
ITRF_2008_TO_ITRF_94 - org.orekit.frames.HelmertTransformation.Predefined
Transformation from ITRF 2008 To ITRF 94.
ITRF_2008_TO_ITRF_96 - org.orekit.frames.HelmertTransformation.Predefined
Transformation from ITRF 2008 To ITRF 96.
ITRF_2008_TO_ITRF_97 - org.orekit.frames.HelmertTransformation.Predefined
Transformation from ITRF 2008 To ITRF 97.
ITRF_2014 - org.orekit.frames.ITRFVersion
Constant for ITRF 2014.
ITRF_2014_TO_ITRF_2000 - org.orekit.frames.HelmertTransformation.Predefined
Transformation from ITRF 2014 To ITRF 2000.
ITRF_2014_TO_ITRF_2005 - org.orekit.frames.HelmertTransformation.Predefined
Transformation from ITRF 2014 To ITRF 2005.
ITRF_2014_TO_ITRF_2008 - org.orekit.frames.HelmertTransformation.Predefined
Transformation from ITRF 2014 To ITRF 2008.
ITRF_2014_TO_ITRF_88 - org.orekit.frames.HelmertTransformation.Predefined
Transformation from ITRF 2014 To ITRF 88.
ITRF_2014_TO_ITRF_89 - org.orekit.frames.HelmertTransformation.Predefined
Transformation from ITRF 2014 To ITRF 89.
ITRF_2014_TO_ITRF_90 - org.orekit.frames.HelmertTransformation.Predefined
Transformation from ITRF 2014 To ITRF 90.
ITRF_2014_TO_ITRF_91 - org.orekit.frames.HelmertTransformation.Predefined
Transformation from ITRF 2014 To ITRF 91.
ITRF_2014_TO_ITRF_92 - org.orekit.frames.HelmertTransformation.Predefined
Transformation from ITRF 2014 To ITRF 92.
ITRF_2014_TO_ITRF_93 - org.orekit.frames.HelmertTransformation.Predefined
Transformation from ITRF 2014 To ITRF 93.
ITRF_2014_TO_ITRF_94 - org.orekit.frames.HelmertTransformation.Predefined
Transformation from ITRF 2014 To ITRF 94.
ITRF_2014_TO_ITRF_96 - org.orekit.frames.HelmertTransformation.Predefined
Transformation from ITRF 2014 To ITRF 96.
ITRF_2014_TO_ITRF_97 - org.orekit.frames.HelmertTransformation.Predefined
Transformation from ITRF 2014 To ITRF 97.
ITRF_88 - org.orekit.frames.ITRFVersion
Constant for ITRF 88.
ITRF_89 - org.orekit.frames.ITRFVersion
Constant for ITRF 89.
ITRF_90 - org.orekit.frames.ITRFVersion
Constant for ITRF 90.
ITRF_91 - org.orekit.frames.ITRFVersion
Constant for ITRF 91.
ITRF_92 - org.orekit.frames.ITRFVersion
Constant for ITRF 92.
ITRF_93 - org.orekit.frames.ITRFVersion
Constant for ITRF 93.
ITRF_94 - org.orekit.frames.ITRFVersion
Constant for ITRF 94.
ITRF_96 - org.orekit.frames.ITRFVersion
Constant for ITRF 96.
ITRF_97 - org.orekit.frames.ITRFVersion
Constant for ITRF 97.
ITRF_CIO_CONV_1996_ACCURATE_EOP - org.orekit.frames.Predefined
CIO-based ITRF, IERS 1996 conventions with accurate EOP interpolation.
ITRF_CIO_CONV_1996_SIMPLE_EOP - org.orekit.frames.Predefined
CIO-based ITRF, IERS 1996 conventions with simple EOP interpolation.
ITRF_CIO_CONV_2003_ACCURATE_EOP - org.orekit.frames.Predefined
CIO-based ITRF, IERS 2003 conventions with accurate EOP interpolation.
ITRF_CIO_CONV_2003_SIMPLE_EOP - org.orekit.frames.Predefined
CIO-based ITRF, IERS 2003 conventions with simple EOP interpolation.
ITRF_CIO_CONV_2010_ACCURATE_EOP - org.orekit.frames.Predefined
CIO-based ITRF, IERS 2010 conventions with accurate EOP interpolation.
ITRF_CIO_CONV_2010_SIMPLE_EOP - org.orekit.frames.Predefined
CIO-based ITRF, IERS 2010 conventions with simple EOP interpolation.
ITRF_EQUINOX_CONV_1996_ACCURATE_EOP - org.orekit.frames.Predefined
Equinox-based ITRF, IERS 1996 conventions with accurate EOP interpolation.
ITRF_EQUINOX_CONV_1996_SIMPLE_EOP - org.orekit.frames.Predefined
Equinox-based ITRF, IERS 1996 conventions with simple EOP interpolation.
ITRF_EQUINOX_CONV_2003_ACCURATE_EOP - org.orekit.frames.Predefined
Equinox-based ITRF, IERS 2003 conventions with accurate EOP interpolation.
ITRF_EQUINOX_CONV_2003_SIMPLE_EOP - org.orekit.frames.Predefined
Equinox-based ITRF, IERS 2003 conventions with simple EOP interpolation.
ITRF_EQUINOX_CONV_2010_ACCURATE_EOP - org.orekit.frames.Predefined
Equinox-based ITRF, IERS 2010 conventions with accurate EOP interpolation.
ITRF_EQUINOX_CONV_2010_SIMPLE_EOP - org.orekit.frames.Predefined
Equinox-based ITRF, IERS 2010 conventions with simple EOP interpolation.
ITRF2000 - org.orekit.files.ccsds.CCSDSFrame
International Terrestrial Reference Frame 2000.
ITRF2005 - org.orekit.files.ccsds.CCSDSFrame
International Terrestrial Reference Frame 2005.
ITRF2008 - org.orekit.files.ccsds.CCSDSFrame
International Terrestrial Reference Frame 2008.
ITRF2014 - org.orekit.files.ccsds.CCSDSFrame
International Terrestrial Reference Frame 2014.
ITRF93 - org.orekit.files.ccsds.CCSDSFrame
International Terrestrial Reference Frame 1993.
ITRF97 - org.orekit.files.ccsds.CCSDSFrame
International Terrestrial Reference Frame 1997.
ITRFVersion - Enum in org.orekit.frames
Enumerate for ITRF versions.
ITRFVersion.Converter - Class in org.orekit.frames
Specialized transform provider between ITRF frames.

J

J01 - org.orekit.gnss.Frequency
QZSS L1 (1575.42 MHz).
J02 - org.orekit.gnss.Frequency
QZSS L2 (1227.6 MHz).
J05 - org.orekit.gnss.Frequency
QZSS L5 (1176.45 MHz).
J06 - org.orekit.gnss.Frequency
QZSS LEX (1278.75 MHz).
J2000_EPOCH - Static variable in class org.orekit.time.AbsoluteDate
J2000.0 Reference epoch: 2000-01-01T12:00:00 Terrestrial Time (not UTC).
J2000_EPOCH - Static variable in class org.orekit.time.DateComponents
J2000.0 Reference epoch: 2000-01-01.
J2DifferentialEffect - Class in org.orekit.propagation.analytical
Analytical model for J2 effect.
J2DifferentialEffect(Orbit, Orbit, boolean, double, double, double) - Constructor for class org.orekit.propagation.analytical.J2DifferentialEffect
Simple constructor.
J2DifferentialEffect(Orbit, Orbit, boolean, UnnormalizedSphericalHarmonicsProvider) - Constructor for class org.orekit.propagation.analytical.J2DifferentialEffect
Simple constructor.
J2DifferentialEffect(SpacecraftState, AdapterPropagator.DifferentialEffect, boolean, double, double, double) - Constructor for class org.orekit.propagation.analytical.J2DifferentialEffect
Simple constructor.
J2DifferentialEffect(SpacecraftState, AdapterPropagator.DifferentialEffect, boolean, UnnormalizedSphericalHarmonicsProvider) - Constructor for class org.orekit.propagation.analytical.J2DifferentialEffect
Simple constructor.
JacobianPropagatorConverter - Class in org.orekit.propagation.conversion
Propagator converter using the real Jacobian.
JacobianPropagatorConverter(NumericalPropagatorBuilder, double, int) - Constructor for class org.orekit.propagation.conversion.JacobianPropagatorConverter
Simple constructor.
JacobiansMapper - Class in org.orekit.propagation.numerical
Mapper between two-dimensional Jacobian matrices and one-dimensional additional state arrays.
JacobiPolynomials - Class in org.orekit.propagation.semianalytical.dsst.utilities
Provider of the Jacobi polynomials Plv,w.
JANUARY - org.orekit.time.Month
January.
JAVA_EPOCH - Static variable in class org.orekit.time.AbsoluteDate
Java Reference epoch: 1970-01-01T00:00:00 Universal Time Coordinate.
JAVA_EPOCH - Static variable in class org.orekit.time.DateComponents
Java Reference epoch: 1970-01-01.
JB2008 - Class in org.orekit.forces.drag.atmosphere
This is the realization of the Jacchia-Bowman 2008 atmospheric model.
JB2008(JB2008InputParameters, PVCoordinatesProvider, BodyShape) - Constructor for class org.orekit.forces.drag.atmosphere.JB2008
Constructor with space environment information for internal computation.
JB2008InputParameters - Interface in org.orekit.forces.drag.atmosphere
Interface for solar activity and magnetic activity data.
JPL_SSD_ASTRONOMICAL_UNIT - Static variable in interface org.orekit.utils.Constants
Astronomical Unit: 149597870691 m.
JPL_SSD_EARTH_GM - Static variable in interface org.orekit.utils.Constants
Earth attraction coefficient (m³/s²).
JPL_SSD_EARTH_MOON_MASS_RATIO - Static variable in interface org.orekit.utils.Constants
Earth/Moon mass ratio: 81.30059.
JPL_SSD_EARTH_PLUS_MOON_GM - Static variable in interface org.orekit.utils.Constants
Sun/(Earth + Moon) attraction coefficient (m³/s²).
JPL_SSD_GAUSSIAN_GRAVITATIONAL_CONSTANT - Static variable in interface org.orekit.utils.Constants
Gaussian gravitational constant: 0.01720209895 √(AU³/d²).
JPL_SSD_JUPITER_SYSTEM_GM - Static variable in interface org.orekit.utils.Constants
Sun/(Jupiter system) ttraction coefficient (m³/s²).
JPL_SSD_MARS_SYSTEM_GM - Static variable in interface org.orekit.utils.Constants
Sun/(Mars system) attraction coefficient (m³/s²).
JPL_SSD_MERCURY_GM - Static variable in interface org.orekit.utils.Constants
Sun/Mercury attraction coefficient (m³/s²).
JPL_SSD_MOON_GM - Static variable in interface org.orekit.utils.Constants
Moon attraction coefficient (m³/s²).
JPL_SSD_NEPTUNE_SYSTEM_GM - Static variable in interface org.orekit.utils.Constants
Sun/(Neptune system) attraction coefficient (m³/s²).
JPL_SSD_PLUTO_SYSTEM_GM - Static variable in interface org.orekit.utils.Constants
Sun/(Pluto system) ttraction coefficient (m³/s²).
JPL_SSD_SATURN_SYSTEM_GM - Static variable in interface org.orekit.utils.Constants
Sun/(Saturn system) attraction coefficient (m³/s²).
JPL_SSD_SUN_EARTH_PLUS_MOON_MASS_RATIO - Static variable in interface org.orekit.utils.Constants
Sun/(Earth + Moon) mass ratio: 328900.56.
JPL_SSD_SUN_GM - Static variable in interface org.orekit.utils.Constants
Sun attraction coefficient (m³/s²).
JPL_SSD_SUN_JUPITER_SYSTEM_MASS_RATIO - Static variable in interface org.orekit.utils.Constants
Sun/(Jupiter system) mass ratio: 1047.3486.
JPL_SSD_SUN_MARS_SYSTEM_MASS_RATIO - Static variable in interface org.orekit.utils.Constants
Sun/(Mars system) mass ratio: 3098708.0.
JPL_SSD_SUN_MERCURY_MASS_RATIO - Static variable in interface org.orekit.utils.Constants
Sun/Mercury mass ratio: 6023600.
JPL_SSD_SUN_NEPTUNE_SYSTEM_MASS_RATIO - Static variable in interface org.orekit.utils.Constants
Sun/(Neptune system) mass ratio: 19412.24.
JPL_SSD_SUN_PLUTO_SYSTEM_MASS_RATIO - Static variable in interface org.orekit.utils.Constants
Sun/(Pluto system) mass ratio: 1.35e8.
JPL_SSD_SUN_SATURN_SYSTEM_MASS_RATIO - Static variable in interface org.orekit.utils.Constants
Sun/(Saturn system) mass ratio: 3497.898.
JPL_SSD_SUN_URANUS_SYSTEM_MASS_RATIO - Static variable in interface org.orekit.utils.Constants
Sun/(Uranus system) mass ratio: 22902.98.
JPL_SSD_SUN_VENUS_MASS_RATIO - Static variable in interface org.orekit.utils.Constants
Sun/Venus mass ratio: 408523.71.
JPL_SSD_URANUS_SYSTEM_GM - Static variable in interface org.orekit.utils.Constants
Sun/(Uranus system) attraction coefficient (m³/s²).
JPL_SSD_VENUS_GM - Static variable in interface org.orekit.utils.Constants
Sun/Venus attraction coefficient (m³/s²).
JPLEphemeridesLoader - Class in org.orekit.bodies
Loader for JPL ephemerides binary files (DE 4xx) and similar formats (INPOP 06/08/10).
JPLEphemeridesLoader(String, JPLEphemeridesLoader.EphemerisType) - Constructor for class org.orekit.bodies.JPLEphemeridesLoader
Create a loader for JPL ephemerides binary files.
JPLEphemeridesLoader.EphemerisType - Enum in org.orekit.bodies
List of supported ephemerides types.
JPLEphemeridesLoader.RawPVProvider - Interface in org.orekit.bodies
Interface for raw position-velocity retrieval.
JULIAN_CENTURY - Static variable in interface org.orekit.utils.Constants
Duration of a Julian century: 36525 Constants.JULIAN_DAY.
JULIAN_DAY - Static variable in interface org.orekit.utils.Constants
Duration of a mean solar day: 86400.0 s.
JULIAN_EPOCH - Static variable in class org.orekit.time.AbsoluteDate
Reference epoch for julian dates: -4712-01-01T12:00:00 Terrestrial Time.
JULIAN_EPOCH - Static variable in class org.orekit.time.DateComponents
Reference epoch for julian dates: -4712-01-01.
JULIAN_YEAR - Static variable in interface org.orekit.utils.Constants
Duration of a Julian year: 365.25 Constants.JULIAN_DAY.
JULY - org.orekit.time.Month
July.
JUNE - org.orekit.time.Month
June.
JUPITER - org.orekit.bodies.JPLEphemeridesLoader.EphemerisType
Constant for Jupiter.
JUPITER - org.orekit.files.ccsds.CenterName
Jupiter body.
JUPITER - Static variable in class org.orekit.bodies.CelestialBodyFactory
Predefined name for Jupiter.

K

k - Variable in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution
ex.
K1 - Static variable in class org.orekit.models.earth.displacement.Tide
K₁ tide.
K2 - Static variable in class org.orekit.models.earth.displacement.Tide
K₂ tide.
KalmanEstimation - Interface in org.orekit.estimation.sequential
Interface for accessing Kalman filter estimations.
KalmanEstimator - Class in org.orekit.estimation.sequential
Implementation of a Kalman filter to perform orbit determination.
KalmanEstimatorBuilder - Class in org.orekit.estimation.sequential
Builder for a Kalman filter estimator.
KalmanEstimatorBuilder() - Constructor for class org.orekit.estimation.sequential.KalmanEstimatorBuilder
Default constructor.
KalmanObserver - Interface in org.orekit.estimation.sequential
Observer for Kalman filter estimations.
KEPLERIAN - org.orekit.orbits.OrbitType
Type for propagation in Keplerian parameters.
KeplerianOrbit - Class in org.orekit.orbits
This class handles traditional Keplerian orbital parameters.
KeplerianOrbit(double, double, double, double, double, double, double, double, double, double, double, double, PositionAngle, Frame, AbsoluteDate, double) - Constructor for class org.orekit.orbits.KeplerianOrbit
Creates a new instance.
KeplerianOrbit(double, double, double, double, double, double, PositionAngle, Frame, AbsoluteDate, double) - Constructor for class org.orekit.orbits.KeplerianOrbit
Creates a new instance.
KeplerianOrbit(Orbit) - Constructor for class org.orekit.orbits.KeplerianOrbit
Constructor from any kind of orbital parameters.
KeplerianOrbit(PVCoordinates, Frame, AbsoluteDate, double) - Constructor for class org.orekit.orbits.KeplerianOrbit
Constructor from Cartesian parameters.
KeplerianOrbit(TimeStampedPVCoordinates, Frame, double) - Constructor for class org.orekit.orbits.KeplerianOrbit
Constructor from Cartesian parameters.
KeplerianPropagator - Class in org.orekit.propagation.analytical
Simple Keplerian orbit propagator.
KeplerianPropagator(Orbit) - Constructor for class org.orekit.propagation.analytical.KeplerianPropagator
Build a propagator from orbit only.
KeplerianPropagator(Orbit, double) - Constructor for class org.orekit.propagation.analytical.KeplerianPropagator
Build a propagator from orbit and central attraction coefficient μ.
KeplerianPropagator(Orbit, AttitudeProvider) - Constructor for class org.orekit.propagation.analytical.KeplerianPropagator
Build a propagator from orbit and attitude provider.
KeplerianPropagator(Orbit, AttitudeProvider, double) - Constructor for class org.orekit.propagation.analytical.KeplerianPropagator
Build a propagator from orbit, attitude provider and central attraction coefficient μ.
KeplerianPropagator(Orbit, AttitudeProvider, double, double) - Constructor for class org.orekit.propagation.analytical.KeplerianPropagator
Build propagator from orbit, attitude provider, central attraction coefficient μ and mass.
KeplerianPropagatorBuilder - Class in org.orekit.propagation.conversion
Builder for Keplerian propagator.
KeplerianPropagatorBuilder(Orbit, PositionAngle, double) - Constructor for class org.orekit.propagation.conversion.KeplerianPropagatorBuilder
Build a new instance.
KEYVALUE - org.orekit.files.ccsds.TDMParser.TDMFileFormat
Keyvalue (text file with Key = Value lines).
Keyword - Enum in org.orekit.files.ccsds
Keywords for CCSDS Navigation Data Messages.
KLOBUCHAR_ALPHA_BETA_NOT_AVAILABLE_FOR_DATE - org.orekit.errors.OrekitMessages
 
KLOBUCHAR_ALPHA_BETA_NOT_LOADED - org.orekit.errors.OrekitMessages
 
KlobucharIonoCoefficientsLoader - Class in org.orekit.models.earth
Loads Klobuchar-Style ionospheric coefficients a given input stream.
KlobucharIonoCoefficientsLoader() - Constructor for class org.orekit.models.earth.KlobucharIonoCoefficientsLoader
Constructor with default supported names.
KlobucharIonoCoefficientsLoader(String) - Constructor for class org.orekit.models.earth.KlobucharIonoCoefficientsLoader
Constructor with supported names given by user.
KlobucharIonoModel - Class in org.orekit.models.earth
Klobuchar ionospheric delay model.
KlobucharIonoModel(double[], double[]) - Constructor for class org.orekit.models.earth.KlobucharIonoModel
Create a new Klobuchar ionospheric delay model, when single L1 frequency system is used.
KlobucharIonoModel(double[], double[], double) - Constructor for class org.orekit.models.earth.KlobucharIonoModel
Create a new Klobuchar ionospheric delay model, when a single frequency system is used.

L

L1 - org.orekit.gnss.ObservationType
Carrier-phase GPS L1 / GLONASS G1 / Galileo E2-L1-E1 / SBAS L1 for Rinex2.
L1A - org.orekit.gnss.ObservationType
Carrier-phase Galileo E1 A for Rinex3.
L1B - org.orekit.gnss.ObservationType
Carrier-phase Galileo E1 I/NAV OS/CS/SoL for Rinex3.
L1C - org.orekit.gnss.ObservationType
Carrier-phase GPS L1 C/A / GLONASS G1 C/A / Galileo E1 C / SBAS L1 C/A / QZSS L1 C/A for Rinex3.
L1Frame - Class in org.orekit.frames
Class to create a L1 centered frame with L1TransformProvider.
L1Frame(CelestialBody, CelestialBody) - Constructor for class org.orekit.frames.L1Frame
Simple constructor.
L1I - org.orekit.gnss.ObservationType
Carrier-phase Beidou B1 I for Rinex3.
L1L - org.orekit.gnss.ObservationType
Carrier-phase GPS L1 L1C(P) / QZSS L1 L1C(P) for Rinex3.
L1M - org.orekit.gnss.ObservationType
Carrier-phase GPS L2 M for Rinex3.
L1N - org.orekit.gnss.ObservationType
Carrier-phase GPS L1 codeless for Rinex3.
L1P - org.orekit.gnss.ObservationType
Carrier-phase GPS L2 P(AS off) / GLONASS G2 P for Rinex3.
L1S - org.orekit.gnss.ObservationType
Carrier-phase GPS L1 L1C(D) / QZSS L1 L1C(D) for Rinex3.
L1TransformProvider - Class in org.orekit.frames
L1 Transform provider for a frame on the L1 Lagrange point of two celestial bodies.
L1TransformProvider(CelestialBody, CelestialBody) - Constructor for class org.orekit.frames.L1TransformProvider
Simple constructor.
L1W - org.orekit.gnss.ObservationType
Carrier-phase GPS L1 Z-tracking and similar (AS on) for Rinex3.
L1X - org.orekit.gnss.ObservationType
Carrier-phase GPS L1 L1C (D+P) / Galileo E1 B+C / QZSS L1 L1C(D+P) for Rinex3.
L1Y - org.orekit.gnss.ObservationType
Carrier-phase GPS L1 Y for Rinex3.
L1Z - org.orekit.gnss.ObservationType
Carrier-phase Galileo E1 C1Z A+B+C / QZSS L1 L1-SAIF for Rinex3.
L2 - org.orekit.gnss.ObservationType
Carrier-phase GPS L2 / GLONASS G2 / Beidou B02 for Rinex2.
L2C - org.orekit.gnss.ObservationType
Carrier-phase GPS L2 C/A / GLONASS G2 C/A for Rinex3.
L2D - org.orekit.gnss.ObservationType
Carrier-phase GPS L1(C/A)+(P2-P1) (semi-codeless) for Rinex3.
L2Frame - Class in org.orekit.frames
Class to create a L2 centered frame with L2TransformProvider.
L2Frame(CelestialBody, CelestialBody) - Constructor for class org.orekit.frames.L2Frame
Simple constructor.
L2I - org.orekit.gnss.ObservationType
Carrier-phase Beidou B1 I for Rinex3.03.
L2L - org.orekit.gnss.ObservationType
Carrier-phase GPS L2 L2C(L) / QZSS L2 L2C(2) for Rinex3.
L2M - org.orekit.gnss.ObservationType
Carrier-phase GPS L2 M for Rinex3.
L2N - org.orekit.gnss.ObservationType
Carrier-phase GPS L2 codeless for Rinex3.
L2P - org.orekit.gnss.ObservationType
Carrier-phase GPS L2 P(AS off) / GLONASS G2 P for Rinex3.
L2Q - org.orekit.gnss.ObservationType
Carrier-phase Beidou B1 Q for Rinex3.03.
L2S - org.orekit.gnss.ObservationType
Carrier-phase GPS L2 L2C(M) / QZSS L2 L2C(M) for Rinex3.
L2W - org.orekit.gnss.ObservationType
Carrier-phase GPS L2 Z-tracking and similar (AS on) for Rinex3.
L2X - org.orekit.gnss.ObservationType
Carrier-phase GPS L2 L2C (M+L) / QZSS L2 L2C(M+L) for Rinex3.
L2Y - org.orekit.gnss.ObservationType
Carrier-phase GPS L2 Y for Rinex3.
L3I - org.orekit.gnss.ObservationType
Carrier-phase GLONASS G3 I for Rinex3.
L3Q - org.orekit.gnss.ObservationType
Carrier-phase GLONASS G3 Q for Rinex3.
L3X - org.orekit.gnss.ObservationType
Carrier-phase GLONASS G3 I+Q for Rinex3.
L5 - org.orekit.gnss.ObservationType
Carrier-phase GPS L5 / Galileo E5a / SBAS L5 for Rinex2.
L5A - org.orekit.gnss.ObservationType
Carrier-phase IRNSS L5 A for Rinex3.
L5B - org.orekit.gnss.ObservationType
Carrier-phase IRNSS L5 B for Rinex3.
L5C - org.orekit.gnss.ObservationType
Carrier-phase IRNSS L5 C for Rinex3.
L5I - org.orekit.gnss.ObservationType
Carrier-phase GPS L5 I/ Galileo E5a F/NAV OS / SBAS L5 I / QZSS L5 I for Rinex3.
L5Q - org.orekit.gnss.ObservationType
Carrier-phase GPS L5 Q/ Galileo E5a Q / SBAS L5 Q / QZSS L5 Q for Rinex3.
L5X - org.orekit.gnss.ObservationType
Carrier-phase GPS L5 I+Q/ Galileo E5a I+Q / SBAS L5 I+Q / QZSS L5 I+Q / IRNSS L5 B+C for Rinex3.
L6 - org.orekit.gnss.ObservationType
Carrier-phase Galileo E6 / Beidou B03 for Rinex2.
L6A - org.orekit.gnss.ObservationType
Carrier-phase Galileo E6 A PRS for Rinex3.
L6B - org.orekit.gnss.ObservationType
Carrier-phase Galileo E6 B C/NAV CS for Rinex3.
L6C - org.orekit.gnss.ObservationType
Carrier-phase Galileo E6 C no data for Rinex3.
L6I - org.orekit.gnss.ObservationType
Carrier-phase Beidou B3 I for Rinex3.
L6L - org.orekit.gnss.ObservationType
Carrier-phase QZSS LEX(6) L for Rinex3.
L6Q - org.orekit.gnss.ObservationType
Carrier-phase Beidou B3 Q for Rinex3.
L6S - org.orekit.gnss.ObservationType
Carrier-phase QZSS LEX(6) S for Rinex3.
L6X - org.orekit.gnss.ObservationType
Carrier-phase Galileo E6 B+C / QZSS LEX(6) S+L / Beidou B3 I+Q for Rinex3.
L6Z - org.orekit.gnss.ObservationType
Carrier-phase Galileo E6 A+B+C for Rinex3.
L7 - org.orekit.gnss.ObservationType
Carrier-phase Galileo E5b / Beidou B02 for Rinex2.
L7I - org.orekit.gnss.ObservationType
Carrier-phase Galileo E5b I I/NAV OS/CS/SoL / Beidou B2 I for Rinex3.
L7Q - org.orekit.gnss.ObservationType
Carrier-phase Galileo Q no data / Beidou B2 Q for Rinex3.
L7X - org.orekit.gnss.ObservationType
Carrier-phase Galileo E5b I+Q / Beidou B2 I+Q for Rinex3.
L8 - org.orekit.gnss.ObservationType
Carrier-phase Galileo E5a+b for Rinex2.
L8I - org.orekit.gnss.ObservationType
Carrier-phase Galileo E5(E5a+E5b) I for Rinex3.
L8Q - org.orekit.gnss.ObservationType
Carrier-phase Galileo E5(E5a+E5b) Q for Rinex3.
L8X - org.orekit.gnss.ObservationType
Carrier-phase Galileo E5(E5a+E5b) I+Q for Rinex3.
L9A - org.orekit.gnss.ObservationType
Carrier-phase IRNSS S A for Rinex3.
L9B - org.orekit.gnss.ObservationType
Carrier-phase IRNSS S B for Rinex3.
L9C - org.orekit.gnss.ObservationType
Carrier-phase IRNSS S C for Rinex3.
L9X - org.orekit.gnss.ObservationType
Carrier-phase IRNSS S B+C for Rinex3.
LA - org.orekit.gnss.ObservationType
Carrier-phase GPS L1 C/A / GLONASS G1 C/A for Rinex2.
LAGRANGE - org.orekit.files.ccsds.OEMWriter.InterpolationMethod
Lagrange interpolation.
LatitudeCrossingDetector - Class in org.orekit.propagation.events
Detector for geographic latitude crossing.
LatitudeCrossingDetector(double, double, OneAxisEllipsoid, double) - Constructor for class org.orekit.propagation.events.LatitudeCrossingDetector
Build a detector.
LatitudeCrossingDetector(OneAxisEllipsoid, double) - Constructor for class org.orekit.propagation.events.LatitudeCrossingDetector
Build a new detector.
LatitudeExtremumDetector - Class in org.orekit.propagation.events
Detector for geographic latitude extremum.
LatitudeExtremumDetector(double, double, OneAxisEllipsoid) - Constructor for class org.orekit.propagation.events.LatitudeExtremumDetector
Build a detector.
LatitudeExtremumDetector(OneAxisEllipsoid) - Constructor for class org.orekit.propagation.events.LatitudeExtremumDetector
Build a new detector.
LB - org.orekit.gnss.ObservationType
Carrier-phase GPS L1C for Rinex2.
LC - org.orekit.gnss.ObservationType
Carrier-phase GPS L2C for Rinex2.
LD - org.orekit.gnss.ObservationType
Carrier-phase GLONASS G2 for Rinex2.
LEO - org.orekit.files.sp3.SP3File.SP3FileType
LEO only file.
LIFT_RATIO - Static variable in interface org.orekit.forces.drag.DragSensitive
Parameter name for lift ration enabling Jacobian processing.
LINEAR - org.orekit.files.ccsds.OEMWriter.InterpolationMethod
Linear interpolation.
lm - Variable in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution
Mean longitude.
LnsCoefficients - Class in org.orekit.propagation.semianalytical.dsst.utilities
Compute the Lns(γ).
LnsCoefficients(int, int, double[][], TreeMap<CoefficientsFactory.NSKey, Double>, double) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.LnsCoefficients
Create a set of Lns(γ) coefficients.
loadCelestialBody(String) - Method in interface org.orekit.bodies.CelestialBodyLoader
Load celestial body.
loadCelestialBody(String) - Method in class org.orekit.bodies.JPLEphemeridesLoader
Load celestial body.
loadData() - Method in class org.orekit.gnss.SEMParser
Loads almanacs.
loadData() - Method in class org.orekit.gnss.YUMAParser
Loads almanacs.
loadData(InputStream, String) - Method in interface org.orekit.data.DataLoader
Load data from a stream.
loadData(InputStream, String) - Method in class org.orekit.forces.drag.atmosphere.data.MarshallSolarActivityFutureEstimation
Load data from a stream.
loadData(InputStream, String) - Method in class org.orekit.forces.gravity.potential.AstronomicalAmplitudeReader
Load data from a stream.
loadData(InputStream, String) - Method in class org.orekit.forces.gravity.potential.EGMFormatReader
Load data from a stream.
loadData(InputStream, String) - Method in class org.orekit.forces.gravity.potential.FESCHatEpsilonReader
Load data from a stream.
loadData(InputStream, String) - Method in class org.orekit.forces.gravity.potential.FESCnmSnmReader
Load data from a stream.
loadData(InputStream, String) - Method in class org.orekit.forces.gravity.potential.GRGSFormatReader
Load data from a stream.
loadData(InputStream, String) - Method in class org.orekit.forces.gravity.potential.ICGEMFormatReader
Load data from a stream.
loadData(InputStream, String) - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
Load data from a stream.
loadData(InputStream, String) - Method in class org.orekit.forces.gravity.potential.SHMFormatReader
Load data from a stream.
loadData(InputStream, String) - Method in class org.orekit.gnss.RinexLoader.Parser
Load data from a stream.
loadData(InputStream, String) - Method in class org.orekit.gnss.SEMParser
 
loadData(InputStream, String) - Method in class org.orekit.gnss.YUMAParser
 
loadData(InputStream, String) - Method in class org.orekit.models.earth.GeoMagneticModelLoader
Load data from a stream.
loadData(InputStream, String) - Method in class org.orekit.models.earth.KlobucharIonoCoefficientsLoader
Load Klobuchar-Style ionospheric coefficients read from some file.
loadData(InputStream, String) - Method in class org.orekit.models.earth.ViennaModelCoefficientsLoader
 
loadData(InputStream, String) - Method in class org.orekit.propagation.analytical.tle.TLESeries
Deprecated.
Load data from a stream.
loadData(InputStream, String) - Method in class org.orekit.utils.InterpolationTableLoader
Loads an bi-variate interpolation table from the given InputStream.
loadKlobucharIonosphericCoefficients() - Method in class org.orekit.models.earth.KlobucharIonoCoefficientsLoader
Load the data using supported names .
loadKlobucharIonosphericCoefficients(DateComponents) - Method in class org.orekit.models.earth.KlobucharIonoCoefficientsLoader
Load the data for a given day.
loadLoveNumbers(String) - Method in enum org.orekit.utils.IERSConventions
Load the Love numbers.
loadOffsets() - Method in class org.orekit.time.TAIUTCDatFilesLoader
Load UTC-TAI offsets entries.
loadOffsets() - Method in class org.orekit.time.UTCTAIBulletinAFilesLoader
Load UTC-TAI offsets entries.
loadOffsets() - Method in class org.orekit.time.UTCTAIHistoryFilesLoader
Load UTC-TAI offsets entries.
loadOffsets() - Method in interface org.orekit.time.UTCTAIOffsetsLoader
Load UTC-TAI offsets entries.
loadTLEData() - Method in class org.orekit.propagation.analytical.tle.TLESeries
Deprecated.
Load TLE data for a specified object.
loadTLEData(int) - Method in class org.orekit.propagation.analytical.tle.TLESeries
Deprecated.
Load TLE data for a specified object.
loadTLEData(int, int, String) - Method in class org.orekit.propagation.analytical.tle.TLESeries
Deprecated.
Load TLE data for a specified object.
loadViennaCoefficients() - Method in class org.orekit.models.earth.ViennaModelCoefficientsLoader
Load the data using supported names .
loadViennaCoefficients(DateTimeComponents) - Method in class org.orekit.models.earth.ViennaModelCoefficientsLoader
Load the data for a given day.
LocalizedException - Interface in org.orekit.errors
This interface specified methods implemented by localized exception classes.
LocalOrbitalFrame - Class in org.orekit.frames
Class for frames moving with an orbiting satellite.
LocalOrbitalFrame(Frame, LOFType, PVCoordinatesProvider, String) - Constructor for class org.orekit.frames.LocalOrbitalFrame
Build a new instance.
LofOffset - Class in org.orekit.attitudes
Attitude law defined by fixed Roll, Pitch and Yaw angles (in any order) with respect to a local orbital frame.
LofOffset(Frame, LOFType) - Constructor for class org.orekit.attitudes.LofOffset
Create a LOF-aligned attitude.
LofOffset(Frame, LOFType, RotationOrder, double, double, double) - Constructor for class org.orekit.attitudes.LofOffset
Creates new instance.
LofOffsetPointing - Class in org.orekit.attitudes
This class provides a default attitude provider.
LofOffsetPointing(Frame, BodyShape, AttitudeProvider, Vector3D) - Constructor for class org.orekit.attitudes.LofOffsetPointing
Creates new instance.
LOFType - Enum in org.orekit.frames
Enumerate for different types of Local Orbital Frames.
LongitudeCrossingDetector - Class in org.orekit.propagation.events
Detector for geographic longitude crossing.
LongitudeCrossingDetector(double, double, OneAxisEllipsoid, double) - Constructor for class org.orekit.propagation.events.LongitudeCrossingDetector
Build a detector.
LongitudeCrossingDetector(OneAxisEllipsoid, double) - Constructor for class org.orekit.propagation.events.LongitudeCrossingDetector
Build a new detector.
LongitudeExtremumDetector - Class in org.orekit.propagation.events
Detector for geographic longitude extremum.
LongitudeExtremumDetector(double, double, OneAxisEllipsoid) - Constructor for class org.orekit.propagation.events.LongitudeExtremumDetector
Build a detector.
LongitudeExtremumDetector(OneAxisEllipsoid) - Constructor for class org.orekit.propagation.events.LongitudeExtremumDetector
Build a new detector.
LoveNumbers - Class in org.orekit.utils
Container for Love numbers.
LoveNumbers(double[][], double[][], double[][]) - Constructor for class org.orekit.utils.LoveNumbers
Simple constructor.
luniSolarTermsComputation() - Method in class org.orekit.propagation.analytical.tle.DeepSDP4
Computes luni - solar terms from initial coordinates and epoch.
LutherIntegratorBuilder - Class in org.orekit.propagation.conversion
Builder for LutherIntegrator.
LutherIntegratorBuilder(double) - Constructor for class org.orekit.propagation.conversion.LutherIntegratorBuilder
Build a new instance.
LVLH - org.orekit.frames.LOFType
Constant for Local Vertical, Local Horizontal frame (X axis aligned with position, Z axis aligned with orbital momentum).

M

M2 - Static variable in class org.orekit.models.earth.displacement.Tide
M₂ tide.
MAN_DELTA_MASS - org.orekit.files.ccsds.Keyword
Mass change during maneuver (value is < 0).
MAN_DURATION - org.orekit.files.ccsds.Keyword
Maneuver duration (If = 0, impulsive maneuver).
MAN_DV_1 - org.orekit.files.ccsds.Keyword
First component of the velocity increment.
MAN_DV_2 - org.orekit.files.ccsds.Keyword
Second component of the velocity increment.
MAN_DV_3 - org.orekit.files.ccsds.Keyword
Third component of the velocity increment.
MAN_EPOCH_IGNITION - org.orekit.files.ccsds.Keyword
Epoch of ignition.
MAN_REF_FRAME - org.orekit.files.ccsds.Keyword
Coordinate system for velocity increment vector.
Maneuver() - Constructor for class org.orekit.files.ccsds.OPMFile.Maneuver
Simple constructor.
mapArrayToOrbit(double[], double[], PositionAngle, AbsoluteDate, double, Frame) - Method in enum org.orekit.orbits.OrbitType
Convert state array to orbital parameters.
mapArrayToOrbit(T[], T[], PositionAngle, FieldAbsoluteDate<T>, double, Frame) - Method in enum org.orekit.orbits.OrbitType
Convert state array to orbital parameters.
mapArrayToState(double, double[], double[], boolean) - Method in class org.orekit.propagation.integration.StateMapper
Map the raw double components to a spacecraft state.
mapArrayToState(AbsoluteDate, double[], double[], boolean) - Method in class org.orekit.propagation.integration.StateMapper
Map the raw double components to a spacecraft state.
mapArrayToState(FieldAbsoluteDate<T>, T[], T[], boolean) - Method in class org.orekit.propagation.integration.FieldStateMapper
Map the raw double components to a spacecraft state.
mapArrayToState(T, T[], T[], boolean) - Method in class org.orekit.propagation.integration.FieldStateMapper
Map the raw double components to a spacecraft state.
mapDateToDouble(AbsoluteDate) - Method in class org.orekit.propagation.integration.StateMapper
Map a date to a raw double time offset.
mapDateToDouble(FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.integration.FieldStateMapper
Map a date to a raw double time offset.
mapDoubleToDate(double) - Method in class org.orekit.propagation.integration.StateMapper
Map the raw double time offset to a date.
mapDoubleToDate(double, AbsoluteDate) - Method in class org.orekit.propagation.integration.StateMapper
Map the raw double time offset to a date.
mapDoubleToDate(T) - Method in class org.orekit.propagation.integration.FieldStateMapper
Map the raw double time offset to a date.
mapDoubleToDate(T, FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.integration.FieldStateMapper
Map the raw double time offset to a date.
mapOrbitToArray(FieldOrbit<T>, PositionAngle, T[], T[]) - Method in enum org.orekit.orbits.OrbitType
Convert orbit to state array.
mapOrbitToArray(Orbit, PositionAngle, double[], double[]) - Method in enum org.orekit.orbits.OrbitType
Convert orbit to state array.
mappingFactors(double, double, double[], AbsoluteDate) - Method in class org.orekit.models.earth.EstimatedTroposphericModel
 
mappingFactors(double, double, double[], AbsoluteDate) - Method in class org.orekit.models.earth.GlobalMappingFunctionModel
This method allows the computation of the hydrostatic and wet mapping functions.
mappingFactors(double, double, double[], AbsoluteDate) - Method in interface org.orekit.models.earth.MappingFunction
This method allows the computation of the hydrostatic and wet mapping functions.
mappingFactors(double, double, double[], AbsoluteDate) - Method in class org.orekit.models.earth.MendesPavlisModel
With the Mendes Pavlis tropospheric model, the mapping function is not split into hydrostatic and wet component.
mappingFactors(double, double, double[], AbsoluteDate) - Method in class org.orekit.models.earth.NiellMappingFunctionModel
 
mappingFactors(double, double, double[], AbsoluteDate) - Method in interface org.orekit.models.earth.TroposphericModel
This method allows the computation of the hydrostatic and wet mapping functions.
mappingFactors(double, double, double[], AbsoluteDate) - Method in class org.orekit.models.earth.ViennaOneModel
This method allows the computation of the hydrostatic and wet mapping functions.
mappingFactors(double, double, double[], AbsoluteDate) - Method in class org.orekit.models.earth.ViennaThreeModel
This method allows the computation of the hydrostatic and wet mapping functions.
mappingFactors(T, T, T[], FieldAbsoluteDate<T>) - Method in class org.orekit.models.earth.EstimatedTroposphericModel
 
mappingFactors(T, T, T[], FieldAbsoluteDate<T>) - Method in class org.orekit.models.earth.GlobalMappingFunctionModel
This method allows the computation of the hydrostatic and wet mapping functions.
mappingFactors(T, T, T[], FieldAbsoluteDate<T>) - Method in interface org.orekit.models.earth.MappingFunction
This method allows the computation of the hydrostatic and wet mapping functions.
mappingFactors(T, T, T[], FieldAbsoluteDate<T>) - Method in class org.orekit.models.earth.MendesPavlisModel
This method allows the computation of the hydrostatic and wet mapping functions.
mappingFactors(T, T, T[], FieldAbsoluteDate<T>) - Method in class org.orekit.models.earth.NiellMappingFunctionModel
 
mappingFactors(T, T, T[], FieldAbsoluteDate<T>) - Method in interface org.orekit.models.earth.TroposphericModel
This method allows the computation of the hydrostatic and wet mapping functions.
mappingFactors(T, T, T[], FieldAbsoluteDate<T>) - Method in class org.orekit.models.earth.ViennaOneModel
This method allows the computation of the hydrostatic and wet mapping functions.
mappingFactors(T, T, T[], FieldAbsoluteDate<T>) - Method in class org.orekit.models.earth.ViennaThreeModel
This method allows the computation of the hydrostatic and wet mapping functions.
MappingFunction - Interface in org.orekit.models.earth
Interface for mapping functions used in the tropospheric delay computation.
mapStateToArray(FieldSpacecraftState<T>, T[], T[]) - Method in class org.orekit.propagation.integration.FieldStateMapper
Map a spacecraft state to raw double components.
mapStateToArray(SpacecraftState, double[], double[]) - Method in class org.orekit.propagation.integration.StateMapper
Map a spacecraft state to raw double components.
MARCH - org.orekit.time.Month
March.
MariniMurrayModel - Class in org.orekit.models.earth
The Marini-Murray tropospheric delay model for laser ranging.
MariniMurrayModel(double, double, double, double, double) - Constructor for class org.orekit.models.earth.MariniMurrayModel
Create a new Marini-Murray model for the troposphere using the given environmental conditions.
MARS - org.orekit.bodies.JPLEphemeridesLoader.EphemerisType
Constant for Mars.
MARS - org.orekit.files.ccsds.CenterName
Mars body.
MARS - Static variable in class org.orekit.bodies.CelestialBodyFactory
Predefined name for Mars.
MarshallSolarActivityFutureEstimation - Class in org.orekit.forces.drag.atmosphere.data
This class reads and provides solar activity data needed by atmospheric models: F107 solar flux, Ap and Kp indexes.
MarshallSolarActivityFutureEstimation(String, MarshallSolarActivityFutureEstimation.StrengthLevel) - Constructor for class org.orekit.forces.drag.atmosphere.data.MarshallSolarActivityFutureEstimation
Simple constructor.
MarshallSolarActivityFutureEstimation.StrengthLevel - Enum in org.orekit.forces.drag.atmosphere.data
Strength level of activity.
mass(double) - Method in class org.orekit.propagation.analytical.gnss.GPSPropagator.Builder
Sets the mass.
MASS - org.orekit.files.ccsds.Keyword
Spacecraft mass.
MASTER_MODE - Static variable in interface org.orekit.propagation.FieldPropagator
Indicator for master mode.
MASTER_MODE - Static variable in interface org.orekit.propagation.Propagator
Indicator for master mode.
MAX_EPOCH - Static variable in class org.orekit.time.DateComponents
Maximum supported date.
MaxGapInterpolationGrid - Class in org.orekit.propagation.semianalytical.dsst.utilities
Interpolation grid where points obey a maximum time gap.
MaxGapInterpolationGrid(double) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.MaxGapInterpolationGrid
Constructor.
maxValueChanged(double, ParameterDriver) - Method in interface org.orekit.utils.ParameterObserver
Notify that a parameter maximum value has been changed.
MAY - org.orekit.time.Month
May.
MCI - org.orekit.files.ccsds.CCSDSFrame
Mars Centered Inertial.
MEAN - org.orekit.orbits.PositionAngle
Mean angle.
MEAN_ANOMALY - org.orekit.files.ccsds.Keyword
Orbit mean anomaly.
MEAN_ELEMENT_THEORY - org.orekit.files.ccsds.Keyword
Mean element theory.
MEAN_MOTION - org.orekit.files.ccsds.Keyword
Mean Motion.
MEAN_MOTION_DDOT - org.orekit.files.ccsds.Keyword
Second Time Derivative of the Mean Motion.
MEAN_MOTION_DOT - org.orekit.files.ccsds.Keyword
First Time Derivative of the Mean Motion.
meanDerivative(AbsoluteDate, int, int) - Method in class org.orekit.utils.SecularAndHarmonic
Get mean derivative, truncated to first components.
meanSecondDerivative(AbsoluteDate, int, int) - Method in class org.orekit.utils.SecularAndHarmonic
Get mean second derivative, truncated to first components.
meanToEccentric(double, double, double) - Static method in class org.orekit.orbits.CircularOrbit
Computes the eccentric latitude argument from the mean latitude argument.
meanToEccentric(double, double, double) - Static method in class org.orekit.orbits.EquinoctialOrbit
Computes the eccentric longitude argument from the mean longitude argument.
meanToEccentric(T, T, T) - Static method in class org.orekit.orbits.FieldCircularOrbit
Computes the eccentric latitude argument from the mean latitude argument.
meanToEccentric(T, T, T) - Static method in class org.orekit.orbits.FieldEquinoctialOrbit
Computes the eccentric longitude argument from the mean longitude argument.
meanToEllipticEccentric(double, double) - Static method in class org.orekit.orbits.KeplerianOrbit
Computes the elliptic eccentric anomaly from the mean anomaly.
meanToEllipticEccentric(T, T) - Static method in class org.orekit.orbits.FieldKeplerianOrbit
Computes the elliptic eccentric anomaly from the mean anomaly.
meanToHyperbolicEccentric(double, double) - Static method in class org.orekit.orbits.KeplerianOrbit
Computes the hyperbolic eccentric anomaly from the mean anomaly.
meanToHyperbolicEccentric(T, T) - Static method in class org.orekit.orbits.FieldKeplerianOrbit
Computes the hyperbolic eccentric anomaly from the mean anomaly.
meanValue(AbsoluteDate, int, int) - Method in class org.orekit.utils.SecularAndHarmonic
Get mean value, truncated to first components.
MeasurementBuilder<T extends ObservedMeasurement<T>> - Interface in org.orekit.estimation.measurements.generation
Interface for generating individual measurements.
MeasurementDecorator - Class in org.orekit.estimation.sequential
Decorator adding Measurement API to an ObservedMeasurement.
MeasurementDecorator(ObservedMeasurement<?>, RealMatrix, AbsoluteDate) - Constructor for class org.orekit.estimation.sequential.MeasurementDecorator
Simple constructor.
measurementIsFeasible(double) - Method in enum org.orekit.estimation.measurements.generation.SignSemantic
Check if measurement is feasible.
MeasurementType - Enum in org.orekit.gnss
Enumerate for measurement type.
MendesPavlisModel - Class in org.orekit.models.earth
The Mendes - Pavlis tropospheric delay model for optical techniques.
MendesPavlisModel(double, double, double, double, double) - Constructor for class org.orekit.models.earth.MendesPavlisModel
Create a new Mendes-Pavlis model for the troposphere.
MERCURY - org.orekit.bodies.JPLEphemeridesLoader.EphemerisType
Constant for Mercury.
MERCURY - org.orekit.files.ccsds.CenterName
Mercury body.
MERCURY - Static variable in class org.orekit.bodies.CelestialBodyFactory
Predefined name for Mercury.
MET - org.orekit.files.ccsds.CcsdsTimeScale
Mission Elapsed Time.
META_START - org.orekit.files.ccsds.Keyword
Keyword used to delineate the start of a Meta-data block.
META_STOP - org.orekit.files.ccsds.Keyword
Keyword used to delineate the end of a Meta-data block.
metadata - org.orekit.files.ccsds.Keyword
Meta-data keyword.
MF - Static variable in class org.orekit.models.earth.displacement.Tide
Mf tide.
MICRO_ARC_SECONDS - org.orekit.data.PolynomialParser.Unit
Micro arc-seconds angles.
MidpointIntegratorBuilder - Class in org.orekit.propagation.conversion
Builder for MidpointIntegrator.
MidpointIntegratorBuilder(double) - Constructor for class org.orekit.propagation.conversion.MidpointIntegratorBuilder
Build a new instance.
MILLI_ARC_SECONDS - org.orekit.data.PolynomialParser.Unit
Milli arc-seconds angles.
MIN_EPOCH - Static variable in class org.orekit.time.DateComponents
Maximum supported date.
minuteDuration(AbsoluteDate) - Method in class org.orekit.time.GLONASSScale
Check length of the current minute in this time scale.
minuteDuration(AbsoluteDate) - Method in interface org.orekit.time.TimeScale
Check length of the current minute in this time scale.
minuteDuration(AbsoluteDate) - Method in class org.orekit.time.UTCScale
Check length of the current minute in this time scale.
minuteDuration(FieldAbsoluteDate<T>) - Method in class org.orekit.time.GLONASSScale
Check length of the current minute in this time scale.
minuteDuration(FieldAbsoluteDate<T>) - Method in interface org.orekit.time.TimeScale
Check length of the current minute in this time scale.
minuteDuration(FieldAbsoluteDate<T>) - Method in class org.orekit.time.UTCScale
Check length of the current minute in this time scale.
minValueChanged(double, ParameterDriver) - Method in interface org.orekit.utils.ParameterObserver
Notify that a parameter minimum value has been changed.
MISMATCHED_FREQUENCIES - org.orekit.errors.OrekitMessages
 
MISSING_EARTH_ORIENTATION_PARAMETERS_BETWEEN_DATES - org.orekit.errors.OrekitMessages
 
MISSING_GRAVITY_FIELD_COEFFICIENT_IN_FILE - org.orekit.errors.OrekitMessages
 
MISSING_SECOND_TLE_LINE - org.orekit.errors.OrekitMessages
 
MISSING_SERIE_J_IN_FILE - org.orekit.errors.OrekitMessages
 
missingCoefficientsAllowed() - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
Check if missing coefficients are allowed in the input data.
MIXED - org.orekit.files.sp3.SP3File.SP3FileType
Mixed file.
MIXED - org.orekit.gnss.SatelliteSystem
Mixed system.
MM - Static variable in class org.orekit.models.earth.displacement.Tide
Mm tide.
MOD_CONVENTIONS_1996 - org.orekit.frames.Predefined
MOD, IERS 1996 conventions.
MOD_CONVENTIONS_2003 - org.orekit.frames.Predefined
MOD, IERS 2003 conventions.
MOD_CONVENTIONS_2010 - org.orekit.frames.Predefined
MOD, IERS 2010 conventions.
MOD_WITHOUT_EOP_CORRECTIONS - org.orekit.frames.Predefined
MOD, IERS 1996 conventions without EOP corrections.
MODE - org.orekit.files.ccsds.Keyword
Meta-data: Tracking mode associated with data section of the segment.
ModeHandler - Interface in org.orekit.propagation.integration
Common interface for all propagator mode handlers initialization.
Model - Class in org.orekit.estimation.sequential
Class defining the process model dynamics to use with a KalmanEstimator.
MODIFIED_JULIAN_EPOCH - Static variable in class org.orekit.time.AbsoluteDate
Reference epoch for modified julian dates: 1858-11-17T00:00:00 Terrestrial Time.
MODIFIED_JULIAN_EPOCH - Static variable in class org.orekit.time.DateComponents
Reference epoch for modified julian dates: 1858-11-17.
modify(EstimatedMeasurement<AngularAzEl>) - Method in class org.orekit.estimation.measurements.modifiers.AngularIonosphericDelayModifier
 
modify(EstimatedMeasurement<AngularAzEl>) - Method in class org.orekit.estimation.measurements.modifiers.AngularRadioRefractionModifier
 
modify(EstimatedMeasurement<AngularAzEl>) - Method in class org.orekit.estimation.measurements.modifiers.AngularTroposphericDelayModifier
 
modify(EstimatedMeasurement<InterSatellitesRange>) - Method in class org.orekit.estimation.measurements.modifiers.OnBoardAntennaInterSatellitesRangeModifier
Apply a modifier to an estimated measurement.
modify(EstimatedMeasurement<Phase>) - Method in class org.orekit.estimation.measurements.modifiers.PhaseAmbiguityModifier
 
modify(EstimatedMeasurement<Range>) - Method in class org.orekit.estimation.measurements.modifiers.OnBoardAntennaRangeModifier
Apply a modifier to an estimated measurement.
modify(EstimatedMeasurement<Range>) - Method in class org.orekit.estimation.measurements.modifiers.RangeIonosphericDelayModifier
 
modify(EstimatedMeasurement<Range>) - Method in class org.orekit.estimation.measurements.modifiers.RangeTroposphericDelayModifier
Apply a modifier to an estimated measurement.
modify(EstimatedMeasurement<RangeRate>) - Method in class org.orekit.estimation.measurements.modifiers.RangeRateIonosphericDelayModifier
Apply a modifier to an estimated measurement.
modify(EstimatedMeasurement<RangeRate>) - Method in class org.orekit.estimation.measurements.modifiers.RangeRateTroposphericDelayModifier
Apply a modifier to an estimated measurement.
modify(EstimatedMeasurement<TurnAroundRange>) - Method in class org.orekit.estimation.measurements.modifiers.OnBoardAntennaTurnAroundRangeModifier
Apply a modifier to an estimated measurement.
modify(EstimatedMeasurement<TurnAroundRange>) - Method in class org.orekit.estimation.measurements.modifiers.TurnAroundRangeIonosphericDelayModifier
 
modify(EstimatedMeasurement<TurnAroundRange>) - Method in class org.orekit.estimation.measurements.modifiers.TurnAroundRangeTroposphericDelayModifier
Apply a modifier to an estimated measurement.
modify(EstimatedMeasurement<T>) - Method in interface org.orekit.estimation.measurements.EstimationModifier
Apply a modifier to an estimated measurement.
modify(EstimatedMeasurement<T>) - Method in class org.orekit.estimation.measurements.modifiers.Bias
Apply a modifier to an estimated measurement.
modify(EstimatedMeasurement<T>) - Method in class org.orekit.estimation.measurements.modifiers.DynamicOutlierFilter
Apply a modifier to an estimated measurement.
modify(EstimatedMeasurement<T>) - Method in class org.orekit.estimation.measurements.modifiers.OutlierFilter
Apply a modifier to an estimated measurement.
MOLECULAR_NITROGEN - Static variable in class org.orekit.forces.drag.atmosphere.DTM2000
Identifier for molecular nitrogen.
MOLECULAR_OXYGEN - Static variable in class org.orekit.forces.drag.atmosphere.DTM2000
Identifier for molecular oxygen.
monitorDetector(D) - Method in class org.orekit.propagation.events.FieldEventsLogger
Monitor an event detector.
monitorDetector(T) - Method in class org.orekit.propagation.events.EventsLogger
Monitor an event detector.
Month - Enum in org.orekit.time
Enumerate representing a calendar month.
MOON - org.orekit.bodies.JPLEphemeridesLoader.EphemerisType
Constant for the Moon.
MOON - org.orekit.files.ccsds.CenterName
Moon body.
MOON - Static variable in class org.orekit.bodies.CelestialBodyFactory
Predefined name for Moon.
MOON_EQUATORIAL_RADIUS - Static variable in interface org.orekit.utils.Constants
Moon equatorial radius: 1737400 m.
MRT - org.orekit.files.ccsds.CcsdsTimeScale
Mission Relative Time.
mu - Variable in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution
μ .
multiply(PolynomialFunctionMatrix) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.PolynomialFunctionMatrix
Multiply the argument matrix with the current matrix.
MultiSatStepHandler - Interface in org.orekit.propagation.sampling
This interface is a space-dynamics aware step handler for multi-sat propagation.

N

n - Variable in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution
Kepler mean motion: n = sqrt(μ / a³).
N2 - Static variable in class org.orekit.models.earth.displacement.Tide
N₂ tide.
NadirPointing - Class in org.orekit.attitudes
This class handles nadir pointing attitude provider.
NadirPointing(Frame, BodyShape) - Constructor for class org.orekit.attitudes.NadirPointing
Creates new instance.
nameChanged(String, ParameterDriver) - Method in interface org.orekit.utils.ParameterObserver
Notify that a parameter name has been changed.
NamedData - Class in org.orekit.data
Container for holding named data that can be filtered.
NamedData(String, NamedData.StreamOpener) - Constructor for class org.orekit.data.NamedData
Simple constructor.
NamedData.StreamOpener - Interface in org.orekit.data
Interface for lazy-opening a stream.
NAUTICAL_DAWN_DUSK_ELEVATION - Static variable in class org.orekit.propagation.events.GroundAtNightDetector
Sun elevation at nautical dawn/dusk (12° below horizon).
negate() - Method in class org.orekit.utils.FieldPVCoordinates
Get the opposite of the instance.
negate() - Method in class org.orekit.utils.PVCoordinates
Get the opposite of the instance.
NegateDetector - Class in org.orekit.propagation.events
An event detector that negates the sign on another event detector's g function.
NegateDetector(EventDetector) - Constructor for class org.orekit.propagation.events.NegateDetector
Create a new event detector that negates an existing event detector.
NEITHER_DIRECTORY_NOR_ZIP_OR_JAR - org.orekit.errors.OrekitMessages
 
NEPTUNE - org.orekit.bodies.JPLEphemeridesLoader.EphemerisType
Constant for Neptune.
NEPTUNE - org.orekit.files.ccsds.CenterName
Neptune body.
NEPTUNE - Static variable in class org.orekit.bodies.CelestialBodyFactory
Predefined name for Neptune.
NetworkCrawler - Class in org.orekit.data
Provider for data files directly fetched from network.
NetworkCrawler(URL...) - Constructor for class org.orekit.data.NetworkCrawler
Build a data classpath crawler.
newBundle(String, Locale, String, ClassLoader, boolean) - Method in class org.orekit.errors.OrekitMessages.UTF8Control
NewcombOperators - Class in org.orekit.propagation.semianalytical.dsst.utilities
Implementation of the Modified Newcomb Operators.
newSegment(Frame, Map<Keyword, String>) - Method in class org.orekit.files.ccsds.StreamingOemWriter
Create a writer for a new OEM ephemeris segment.
NewtonianAttraction - Class in org.orekit.forces.gravity
Force model for Newtonian central body attraction.
NewtonianAttraction(double) - Constructor for class org.orekit.forces.gravity.NewtonianAttraction
Simple constructor.
NiellMappingFunctionModel - Class in org.orekit.models.earth
The Niell Mapping Function model for radio wavelengths.
NiellMappingFunctionModel(double) - Constructor for class org.orekit.models.earth.NiellMappingFunctionModel
Buils a new instance.
NO_CACHED_ENTRIES - org.orekit.errors.OrekitMessages
 
NO_DATA_GENERATED - org.orekit.errors.OrekitMessages
 
NO_DATA_LOADED_FOR_CELESTIAL_BODY - org.orekit.errors.OrekitMessages
 
NO_EARTH_ORIENTATION_PARAMETERS - org.orekit.errors.OrekitMessages
 
NO_EARTH_ORIENTATION_PARAMETERS_LOADED - org.orekit.errors.OrekitMessages
 
NO_ENTRIES_IN_IERS_UTC_TAI_HISTORY_FILE - org.orekit.errors.OrekitMessages
 
NO_GRAVITY_FIELD_DATA_LOADED - org.orekit.errors.OrekitMessages
 
NO_IERS_UTC_TAI_HISTORY_DATA_LOADED - org.orekit.errors.OrekitMessages
 
NO_JPL_EPHEMERIDES_BINARY_FILES_FOUND - org.orekit.errors.OrekitMessages
 
NO_KLOBUCHAR_ALPHA_BETA_IN_FILE - org.orekit.errors.OrekitMessages
 
NO_OCEAN_TIDE_DATA_LOADED - org.orekit.errors.OrekitMessages
 
NO_PROPAGATOR_CONFIGURED - org.orekit.errors.OrekitMessages
 
NO_REFERENCE_DATE_FOR_PARAMETER - org.orekit.errors.OrekitMessages
 
NO_SEM_ALMANAC_AVAILABLE - org.orekit.errors.OrekitMessages
 
NO_SOLAR_ACTIVITY_AT_DATE - org.orekit.errors.OrekitMessages
 
NO_SUCH_ITRF_FRAME - org.orekit.errors.OrekitMessages
 
NO_TLE_DATA_AVAILABLE - org.orekit.errors.OrekitMessages
 
NO_TLE_FOR_LAUNCH_YEAR_NUMBER_PIECE - org.orekit.errors.OrekitMessages
 
NO_TLE_FOR_OBJECT - org.orekit.errors.OrekitMessages
 
NO_UNITS - org.orekit.data.PolynomialParser.Unit
No units.
NO_VIENNA_ACOEF_OR_ZENITH_DELAY_IN_FILE - org.orekit.errors.OrekitMessages
 
NO_YUMA_ALMANAC_AVAILABLE - org.orekit.errors.OrekitMessages
 
NodeDetector - Class in org.orekit.propagation.events
Finder for node crossing events.
NodeDetector(double, Orbit, Frame) - Constructor for class org.orekit.propagation.events.NodeDetector
Build a new instance.
NodeDetector(Orbit, Frame) - Constructor for class org.orekit.propagation.events.NodeDetector
Build a new instance.
NON_CHRONOLOGICAL_DATES_IN_FILE - org.orekit.errors.OrekitMessages
 
NON_CHRONOLOGICALLY_SORTED_ENTRIES - org.orekit.errors.OrekitMessages
 
NON_EXISTENT_DATE - org.orekit.errors.OrekitMessages
 
NON_EXISTENT_DAY_NUMBER_IN_YEAR - org.orekit.errors.OrekitMessages
 
NON_EXISTENT_GEOMAGNETIC_MODEL - org.orekit.errors.OrekitMessages
 
NON_EXISTENT_HMS_TIME - org.orekit.errors.OrekitMessages
 
NON_EXISTENT_MONTH - org.orekit.errors.OrekitMessages
 
NON_EXISTENT_TIME - org.orekit.errors.OrekitMessages
 
NON_EXISTENT_WEEK_DATE - org.orekit.errors.OrekitMessages
 
NON_EXISTENT_YEAR_MONTH_DAY - org.orekit.errors.OrekitMessages
 
NON_PSEUDO_INERTIAL_FRAME - org.orekit.errors.OrekitMessages
 
NON_RESETABLE_STATE - org.orekit.errors.OrekitMessages
 
nonCentralPart(AbsoluteDate, Vector3D, double) - Method in class org.orekit.forces.gravity.HolmesFeatherstoneAttractionModel
Compute the non-central part of the gravity field.
NORAD_CAT_ID - org.orekit.files.ccsds.Keyword
NORAD catalogue number.
normalize() - Method in class org.orekit.utils.FieldPVCoordinates
Normalize the position part of the instance.
normalize() - Method in class org.orekit.utils.PVCoordinates
Normalize the position part of the instance.
normalizeAngle(T, T) - Static method in class org.orekit.orbits.FieldCircularOrbit
Normalize an angle in a 2π wide interval around a center value.
normalizeAngle(T, T) - Static method in class org.orekit.orbits.FieldEquinoctialOrbit
Normalize an angle in a 2π wide interval around a center value.
normalizeAngle(T, T) - Static method in class org.orekit.orbits.FieldKeplerianOrbit
Normalize an angle in a 2π wide interval around a center value.
normalizeAngle(T, T) - Static method in class org.orekit.propagation.analytical.FieldEcksteinHechlerPropagator
Normalize an angle in a 2π wide interval around a center value.
NormalizedSphericalHarmonicsProvider - Interface in org.orekit.forces.gravity.potential
Interface used to provide normalized spherical harmonics coefficients.
NormalizedSphericalHarmonicsProvider.NormalizedSphericalHarmonics - Interface in org.orekit.forces.gravity.potential
The normalized geopotential coefficients at a specific instance in time.
NOT_A_DIRECTORY - org.orekit.errors.OrekitMessages
 
NOT_A_JPL_EPHEMERIDES_BINARY_FILE - org.orekit.errors.OrekitMessages
 
NOT_A_MARSHALL_SOLAR_ACTIVITY_FUTURE_ESTIMATION_FILE - org.orekit.errors.OrekitMessages
 
NOT_A_SUPPORTED_IERS_DATA_FILE - org.orekit.errors.OrekitMessages
 
NOT_A_SUPPORTED_SEM_ALMANAC_FILE - org.orekit.errors.OrekitMessages
 
NOT_A_SUPPORTED_UNIX_COMPRESSED_FILE - org.orekit.errors.OrekitMessages
 
NOT_A_SUPPORTED_YUMA_ALMANAC_FILE - org.orekit.errors.OrekitMessages
 
NOT_ENOUGH_CACHED_NEIGHBORS - org.orekit.errors.OrekitMessages
 
NOT_ENOUGH_DATA_FOR_INTERPOLATION - org.orekit.errors.OrekitMessages
 
NOT_ENOUGH_GNSS_FOR_DOP - org.orekit.errors.OrekitMessages
 
NOT_ENOUGH_PROPAGATORS - org.orekit.errors.OrekitMessages
 
NOT_POSITIVE_SPACECRAFT_MASS - org.orekit.errors.OrekitMessages
 
NOT_TLE_LINES - org.orekit.errors.OrekitMessages
 
notCombine(EventDetector) - Static method in class org.orekit.propagation.events.BooleanDetector
Create a new event detector that negates the g function of another detector.
NOVEMBER - org.orekit.time.Month
November.
NRLMSISE00 - Class in org.orekit.forces.drag.atmosphere
This class implements the mathematical representation of the 2001 Naval Research Laboratory Mass Spectrometer and Incoherent Scatter Radar Exosphere (NRLMSISE-00) of the MSIS® class model.
NRLMSISE00(NRLMSISE00InputParameters, PVCoordinatesProvider, BodyShape) - Constructor for class org.orekit.forces.drag.atmosphere.NRLMSISE00
Constructor.
NRLMSISE00.FieldOutput<T extends org.hipparchus.RealFieldElement<T>> - Class in org.orekit.forces.drag.atmosphere
This class is a placeholder for the computed densities and temperatures.
NRLMSISE00InputParameters - Interface in org.orekit.forces.drag.atmosphere
Container for solar activity data, compatible with NRLMSISE-00 atmosphere model.
NSKey(int, int) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.CoefficientsFactory.NSKey
Simple constructor.
NULL_ARGUMENT - org.orekit.errors.OrekitMessages
 
NULL_CORRECTION - Static variable in class org.orekit.frames.PoleCorrection
Null correction (xp = 0, yp = 0).
NULL_PARENT_FOR_FRAME - org.orekit.errors.OrekitMessages
 
NumericalPropagator - Class in org.orekit.propagation.numerical
This class propagates orbits using numerical integration.
NumericalPropagator(ODEIntegrator) - Constructor for class org.orekit.propagation.numerical.NumericalPropagator
Create a new instance of NumericalPropagator, based on orbit definition mu.
NumericalPropagatorBuilder - Class in org.orekit.propagation.conversion
Builder for numerical propagator.
NumericalPropagatorBuilder(Orbit, ODEIntegratorBuilder, PositionAngle, double) - Constructor for class org.orekit.propagation.conversion.NumericalPropagatorBuilder
Build a new instance.

O

O1 - Static variable in class org.orekit.models.earth.displacement.Tide
O₁ tide.
OBJECT_ID - org.orekit.files.ccsds.Keyword
Object identifier of the object for which the orbit state is provided.
OBJECT_NAME - org.orekit.files.ccsds.Keyword
Spacecraft name for which the orbit state is provided.
ObservableSatellite - Class in org.orekit.estimation.measurements
Class modeling a satellite that can be observed.
ObservableSatellite(int) - Constructor for class org.orekit.estimation.measurements.ObservableSatellite
Simple constructor.
observation - org.orekit.files.ccsds.Keyword
Observation keyword.
ObservationData - Class in org.orekit.gnss
Observation Data.
ObservationData(ObservationType, double, int, int) - Constructor for class org.orekit.gnss.ObservationData
Simple constructor.
ObservationDataSet - Class in org.orekit.gnss
Observation Data set.
ObservationDataSet(RinexHeader, SatelliteSystem, int, AbsoluteDate, double, List<ObservationData>) - Constructor for class org.orekit.gnss.ObservationDataSet
Simple constructor.
ObservationsBlock() - Constructor for class org.orekit.files.ccsds.TDMFile.ObservationsBlock
ObservationsBlock constructor.
ObservationType - Enum in org.orekit.gnss
Enumerate for all the Observation Types for Rinex 2 and 3.
ObservedMeasurement<T extends ObservedMeasurement<T>> - Interface in org.orekit.estimation.measurements
Interface for measurements used for orbit determination.
OCEAN_TIDE_DATA_DEGREE_ORDER_LIMITS - org.orekit.errors.OrekitMessages
 
OCEAN_TIDE_LOAD_DEFORMATION_LIMITS - org.orekit.errors.OrekitMessages
 
OceanLoadDeformationCoefficients - Enum in org.orekit.forces.gravity.potential
Supported Ocean load Deformation coefficients (Love numbers k'i).
OceanLoading - Class in org.orekit.models.earth.displacement
Modeling of displacement of reference points due to ocean loading.
OceanLoading(OneAxisEllipsoid, OceanLoadingCoefficients) - Constructor for class org.orekit.models.earth.displacement.OceanLoading
Simple constructor.
OceanLoadingCoefficients - Class in org.orekit.models.earth.displacement
Site specific coefficients for ocean loading.
OceanLoadingCoefficients(String, GeodeticPoint, Tide[][], double[][], double[][], double[][], double[][], double[][], double[][]) - Constructor for class org.orekit.models.earth.displacement.OceanLoadingCoefficients
Simple constructor.
OceanLoadingCoefficientsBLQFactory - Class in org.orekit.models.earth.displacement
Factory for ocean loading coefficients, using Onsala Space Observatory files in BLQ format.
OceanLoadingCoefficientsBLQFactory(String) - Constructor for class org.orekit.models.earth.displacement.OceanLoadingCoefficientsBLQFactory
Simple constructor.
OceanTides - Class in org.orekit.forces.gravity
Ocean tides force model.
OceanTides(Frame, double, double, boolean, double, int, int, int, IERSConventions, UT1Scale) - Constructor for class org.orekit.forces.gravity.OceanTides
Simple constructor.
OceanTides(Frame, double, double, int, int, IERSConventions, UT1Scale) - Constructor for class org.orekit.forces.gravity.OceanTides
Simple constructor.
OceanTidesReader - Class in org.orekit.forces.gravity.potential
Reader for ocean tides coefficients.
OceanTidesReader(String) - Constructor for class org.orekit.forces.gravity.potential.OceanTidesReader
Simple constructor.
OceanTidesWave - Class in org.orekit.forces.gravity.potential
Container for ocen tides coefficients for one tide wave.
OceanTidesWave(int, int, int, double[][][]) - Constructor for class org.orekit.forces.gravity.potential.OceanTidesWave
Simple constructor.
OCTOBER - org.orekit.time.Month
October.
ODEIntegratorBuilder - Interface in org.orekit.propagation.conversion
This interface is the top-level abstraction to build first order integrators for propagators conversion.
ODMFile - Class in org.orekit.files.ccsds
The ODMFile (Orbit Data Message) class represents any of the three orbit messages used by the CCSDS, i.e.
ODMFile() - Constructor for class org.orekit.files.ccsds.ODMFile
ODMFile constructor.
ODMMetaData - Class in org.orekit.files.ccsds
This class gathers the meta-data present in the Orbital Data Message (ODM).
ODMParser - Class in org.orekit.files.ccsds
Base class for all CCSDS Orbit Data Message parsers.
ODMParser(AbsoluteDate, double, IERSConventions, boolean, int, int, String) - Constructor for class org.orekit.files.ccsds.ODMParser
Complete constructor.
OEMFile - Class in org.orekit.files.ccsds
This class stocks all the information of the OEM File parsed by OEMParser.
OEMFile() - Constructor for class org.orekit.files.ccsds.OEMFile
OEMFile constructor.
OEMFile.CovarianceMatrix - Class in org.orekit.files.ccsds
The CovarianceMatrix class represents a covariance matrix and its metadata: epoch and frame.
OEMFile.EphemeridesBlock - Class in org.orekit.files.ccsds
The Ephemerides Blocks class contain metadata, the list of ephemerides data lines and optional covariance matrices (and their metadata).
OEMFile.OemSatelliteEphemeris - Class in org.orekit.files.ccsds
OEM ephemeris blocks for a single satellite.
OEMParser - Class in org.orekit.files.ccsds
A parser for the CCSDS OEM (Orbit Ephemeris Message).
OEMParser() - Constructor for class org.orekit.files.ccsds.OEMParser
Simple constructor.
OEMWriter - Class in org.orekit.files.ccsds
An OEM Writer class that can take in a general EphemerisFile object and export it as a valid OEM file.
OEMWriter() - Constructor for class org.orekit.files.ccsds.OEMWriter
Standard default constructor that creates a writer with default configurations.
OEMWriter(OEMWriter.InterpolationMethod, String, String, String) - Constructor for class org.orekit.files.ccsds.OEMWriter
Constructor used to create a new OEM writer configured with the necessary parameters to successfully fill in all required fields that aren't part of a standard @{link EphemerisFile} object.
OEMWriter.InterpolationMethod - Enum in org.orekit.files.ccsds
OEM interpolation method.
OFFSET_SUFFIX - Static variable in class org.orekit.estimation.measurements.GroundStation
Suffix for ground station position and clock offset parameters names.
offsetFrom(AbsoluteDate, TimeScale) - Method in class org.orekit.time.AbsoluteDate
Compute the apparent clock offset between two instant in the perspective of a specific time scale.
offsetFrom(DateTimeComponents) - Method in class org.orekit.time.DateTimeComponents
Compute the seconds offset between two instances.
offsetFrom(FieldAbsoluteDate<T>, TimeScale) - Method in class org.orekit.time.FieldAbsoluteDate
Compute the apparent clock offset between two instant in the perspective of a specific time scale.
offsetFromBoundary(Vector3D) - Method in class org.orekit.propagation.events.FieldOfView
Get the angular offset of target point with respect to the Field Of View Boundary.
offsetFromTAI(AbsoluteDate) - Method in class org.orekit.time.BDTScale
Get the offset to convert locations from TAIScale to instance.
offsetFromTAI(AbsoluteDate) - Method in class org.orekit.time.GalileoScale
Get the offset to convert locations from TAIScale to instance.
offsetFromTAI(AbsoluteDate) - Method in class org.orekit.time.GLONASSScale
Get the offset to convert locations from TAIScale to instance.
offsetFromTAI(AbsoluteDate) - Method in class org.orekit.time.GMSTScale
Get the offset to convert locations from TAIScale to instance.
offsetFromTAI(AbsoluteDate) - Method in class org.orekit.time.GPSScale
Get the offset to convert locations from TAIScale to instance.
offsetFromTAI(AbsoluteDate) - Method in class org.orekit.time.IRNSSScale
Get the offset to convert locations from TAIScale to instance.
offsetFromTAI(AbsoluteDate) - Method in class org.orekit.time.QZSSScale
Get the offset to convert locations from TAIScale to instance.
offsetFromTAI(AbsoluteDate) - Method in class org.orekit.time.TAIScale
Get the offset to convert locations from TAIScale to instance.
offsetFromTAI(AbsoluteDate) - Method in class org.orekit.time.TCBScale
Get the offset to convert locations from TAIScale to instance.
offsetFromTAI(AbsoluteDate) - Method in class org.orekit.time.TCGScale
Get the offset to convert locations from TAIScale to instance.
offsetFromTAI(AbsoluteDate) - Method in class org.orekit.time.TDBScale
Get the offset to convert locations from TAIScale to instance.
offsetFromTAI(AbsoluteDate) - Method in interface org.orekit.time.TimeScale
Get the offset to convert locations from TAIScale to instance.
offsetFromTAI(AbsoluteDate) - Method in class org.orekit.time.TTScale
Get the offset to convert locations from TAIScale to instance.
offsetFromTAI(AbsoluteDate) - Method in class org.orekit.time.UT1Scale
Get the offset to convert locations from TAIScale to instance.
offsetFromTAI(AbsoluteDate) - Method in class org.orekit.time.UTCScale
Get the offset to convert locations from TAIScale to instance.
offsetFromTAI(FieldAbsoluteDate<T>) - Method in class org.orekit.time.BDTScale
Get the offset to convert locations from TAIScale to instance.
offsetFromTAI(FieldAbsoluteDate<T>) - Method in class org.orekit.time.GalileoScale
Get the offset to convert locations from TAIScale to instance.
offsetFromTAI(FieldAbsoluteDate<T>) - Method in class org.orekit.time.GLONASSScale
Get the offset to convert locations from TAIScale to instance.
offsetFromTAI(FieldAbsoluteDate<T>) - Method in class org.orekit.time.GMSTScale
Get the offset to convert locations from TAIScale to instance.
offsetFromTAI(FieldAbsoluteDate<T>) - Method in class org.orekit.time.GPSScale
Get the offset to convert locations from TAIScale to instance.
offsetFromTAI(FieldAbsoluteDate<T>) - Method in class org.orekit.time.IRNSSScale
Get the offset to convert locations from TAIScale to instance.
offsetFromTAI(FieldAbsoluteDate<T>) - Method in class org.orekit.time.QZSSScale
Get the offset to convert locations from TAIScale to instance.
offsetFromTAI(FieldAbsoluteDate<T>) - Method in class org.orekit.time.TAIScale
Get the offset to convert locations from TAIScale to instance.
offsetFromTAI(FieldAbsoluteDate<T>) - Method in class org.orekit.time.TCBScale
Get the offset to convert locations from TAIScale to instance.
offsetFromTAI(FieldAbsoluteDate<T>) - Method in class org.orekit.time.TCGScale
Get the offset to convert locations from TAIScale to instance.
offsetFromTAI(FieldAbsoluteDate<T>) - Method in class org.orekit.time.TDBScale
Get the offset to convert locations from TAIScale to instance.
offsetFromTAI(FieldAbsoluteDate<T>) - Method in interface org.orekit.time.TimeScale
Get the offset to convert locations from TAIScale to instance.
offsetFromTAI(FieldAbsoluteDate<T>) - Method in class org.orekit.time.TTScale
Get the offset to convert locations from TAIScale to instance.
offsetFromTAI(FieldAbsoluteDate<T>) - Method in class org.orekit.time.UT1Scale
Get the offset to convert locations from TAIScale to instance.
offsetFromTAI(FieldAbsoluteDate<T>) - Method in class org.orekit.time.UTCScale
Get the offset to convert locations from TAIScale to instance.
OffsetModel - Class in org.orekit.time
TAI UTC offset model.
OffsetModel(DateComponents, int) - Constructor for class org.orekit.time.OffsetModel
Constructor for a constant offset model.
OffsetModel(DateComponents, int, double, double) - Constructor for class org.orekit.time.OffsetModel
Constructor for a linear offset model.
offsetToTAI(DateComponents, TimeComponents) - Method in class org.orekit.time.BDTScale
Get the offset to convert locations from instance to TAIScale.
offsetToTAI(DateComponents, TimeComponents) - Method in class org.orekit.time.GalileoScale
Get the offset to convert locations from instance to TAIScale.
offsetToTAI(DateComponents, TimeComponents) - Method in class org.orekit.time.GLONASSScale
Get the offset to convert locations from instance to TAIScale.
offsetToTAI(DateComponents, TimeComponents) - Method in class org.orekit.time.GPSScale
Get the offset to convert locations from instance to TAIScale.
offsetToTAI(DateComponents, TimeComponents) - Method in class org.orekit.time.IRNSSScale
Get the offset to convert locations from instance to TAIScale.
offsetToTAI(DateComponents, TimeComponents) - Method in class org.orekit.time.QZSSScale
Get the offset to convert locations from instance to TAIScale.
offsetToTAI(DateComponents, TimeComponents) - Method in class org.orekit.time.TAIScale
Get the offset to convert locations from instance to TAIScale.
offsetToTAI(DateComponents, TimeComponents) - Method in interface org.orekit.time.TimeScale
Get the offset to convert locations from instance to TAIScale.
offsetToTAI(DateComponents, TimeComponents) - Method in class org.orekit.time.TTScale
Get the offset to convert locations from instance to TAIScale.
offsetToTAI(DateComponents, TimeComponents) - Method in class org.orekit.time.UTCScale
Get the offset to convert locations from instance to TAIScale.
OGMFile - Class in org.orekit.files.ccsds
This class gathers the general state data present in both OPM and OMM files.
omega - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator
final perigee argument.
omgdot - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator
common parameter for perigee argument (omega) computation.
OMMFile - Class in org.orekit.files.ccsds
This class gathers the informations present in the Orbital Mean-Elements Message (OMM), and contains methods to generate a CartesianOrbit, a KeplerianOrbit, a SpacecraftState and, eventually, a TLE.
OMMFile.OMMMetaData - Class in org.orekit.files.ccsds
 
OMMParser - Class in org.orekit.files.ccsds
A parser for the CCSDS OMM (Orbiter Mean-Elements Message).
OMMParser() - Constructor for class org.orekit.files.ccsds.OMMParser
Simple constructor.
OnBoardAntennaInterSatellitesRangeModifier - Class in org.orekit.estimation.measurements.modifiers
On-board antenna offset effect on inter-satellites range measurements.
OnBoardAntennaInterSatellitesRangeModifier(Vector3D, Vector3D) - Constructor for class org.orekit.estimation.measurements.modifiers.OnBoardAntennaInterSatellitesRangeModifier
Simple constructor.
OnBoardAntennaRangeModifier - Class in org.orekit.estimation.measurements.modifiers
On-board antenna offset effect on range measurements.
OnBoardAntennaRangeModifier(Vector3D) - Constructor for class org.orekit.estimation.measurements.modifiers.OnBoardAntennaRangeModifier
Simple constructor.
OnBoardAntennaTurnAroundRangeModifier - Class in org.orekit.estimation.measurements.modifiers
On-board antenna offset effect on turn around range measurements.
OnBoardAntennaTurnAroundRangeModifier(Vector3D) - Constructor for class org.orekit.estimation.measurements.modifiers.OnBoardAntennaTurnAroundRangeModifier
Simple constructor.
onDate(AbsoluteDate) - Method in class org.orekit.forces.gravity.potential.CachedNormalizedSphericalHarmonicsProvider
Get the normalized spherical harmonic coefficients at a specific instance in time.
onDate(AbsoluteDate) - Method in interface org.orekit.forces.gravity.potential.NormalizedSphericalHarmonicsProvider
Get the normalized spherical harmonic coefficients at a specific instance in time.
onDate(AbsoluteDate) - Method in interface org.orekit.forces.gravity.potential.RawSphericalHarmonicsProvider
Get the raw spherical harmonic coefficients on a specific date.
onDate(AbsoluteDate) - Method in interface org.orekit.forces.gravity.potential.UnnormalizedSphericalHarmonicsProvider
Get the un-normalized spherical harmonic coefficients at a specific instance in time.
ONE - Static variable in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenUtilities
1 represented as a polynomial.
OneAxisEllipsoid - Class in org.orekit.bodies
Modeling of a one-axis ellipsoid.
OneAxisEllipsoid(double, double, Frame) - Constructor for class org.orekit.bodies.OneAxisEllipsoid
Simple constructor.
ooA - Variable in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution
1 / A .
ooAB - Variable in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution
1 / (A * B) .
ooBpo - Variable in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution
1 / (1 + B) .
ooMu - Variable in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution
1 / μ .
openStream() - Method in interface org.orekit.data.NamedData.StreamOpener
Open the stream.
OPMFile - Class in org.orekit.files.ccsds
This class gathers the informations present in the Orbital Parameter Message (OPM), and contains methods to generate CartesianOrbit, KeplerianOrbit or SpacecraftState.
OPMFile.Maneuver - Class in org.orekit.files.ccsds
Maneuver in an OPM file.
OPMParser - Class in org.orekit.files.ccsds
A parser for the CCSDS OPM (Orbit Parameter Message).
OPMParser() - Constructor for class org.orekit.files.ccsds.OPMParser
Simple constructor.
Orbit - Class in org.orekit.orbits
This class handles orbital parameters.
Orbit(Frame, AbsoluteDate, double) - Constructor for class org.orekit.orbits.Orbit
Default constructor.
Orbit(TimeStampedPVCoordinates, Frame, double) - Constructor for class org.orekit.orbits.Orbit
Set the orbit from Cartesian parameters.
ORBIT_A_E_MISMATCH_WITH_CONIC_TYPE - org.orekit.errors.OrekitMessages
 
ORBIT_AND_ATTITUDE_DATES_MISMATCH - org.orekit.errors.OrekitMessages
 
ORBIT_ANOMALY_OUT_OF_HYPERBOLIC_RANGE - org.orekit.errors.OrekitMessages
 
ORBIT_TYPE_NOT_ALLOWED - org.orekit.errors.OrekitMessages
 
OrbitType - Enum in org.orekit.orbits
Enumerate for orbital parameters types.
orCombine(Collection<? extends EventDetector>) - Static method in class org.orekit.propagation.events.BooleanDetector
Create a new event detector that is the logical OR or the given event detectors.
orCombine(EventDetector...) - Static method in class org.orekit.propagation.events.BooleanDetector
Create a new event detector that is the logical OR or the given event detectors.
OREKIT_DATA_PATH - Static variable in class org.orekit.data.DataProvidersManager
Name of the property defining the root directories or zip/jar files path for default configuration.
OrekitConfiguration - Class in org.orekit.utils
Utility class for setting global configuration parameters.
OrekitEphemerisFile - Class in org.orekit.files.general
A class for encapsulating Orekit propagators within an EphemerisFile complaint object that makes for easy serialization to external ephemeris formats like OEM.
OrekitEphemerisFile() - Constructor for class org.orekit.files.general.OrekitEphemerisFile
Standard default constructor.
OrekitEphemerisFile.OrekitEphemerisSegment - Class in org.orekit.files.general
 
OrekitEphemerisFile.OrekitSatelliteEphemeris - Class in org.orekit.files.general
Inner class of OrekitEphemerisFile that defines the OrekitEphemerisFile.OrekitSatelliteEphemeris corresponding object for this ephemeris type.
OrekitEphemerisSegment(List<TimeStampedPVCoordinates>, Frame, String, double, TimeScale, int) - Constructor for class org.orekit.files.general.OrekitEphemerisFile.OrekitEphemerisSegment
constructor for OrekitEphemerisSegment.
OrekitException - Exception in org.orekit.errors
This class is the base class for all specific exceptions thrown by the Orekit classes.
OrekitException(Throwable, Localizable, Object...) - Constructor for exception org.orekit.errors.OrekitException
Simple constructor.
OrekitException(Localizable, Object...) - Constructor for exception org.orekit.errors.OrekitException
Simple constructor.
OrekitException(Localizable, Throwable) - Constructor for exception org.orekit.errors.OrekitException
Simple constructor.
OrekitException(MathRuntimeException) - Constructor for exception org.orekit.errors.OrekitException
Simple constructor.
OrekitException(OrekitException) - Constructor for exception org.orekit.errors.OrekitException
Copy constructor.
OrekitExceptionWrapper - Exception in org.orekit.errors
Deprecated.
as of 9.3, this class is not used anymore, as OrekitException is now an unchecked exception
OrekitExceptionWrapper(OrekitException) - Constructor for exception org.orekit.errors.OrekitExceptionWrapper
Deprecated.
Simple constructor.
OrekitFixedStepHandler - Interface in org.orekit.propagation.sampling
This interface is a space-dynamics aware fixed size step handler.
OrekitIllegalArgumentException - Exception in org.orekit.errors
Extension of IllegalArgumentException with localized message.
OrekitIllegalArgumentException(Localizable, Object...) - Constructor for exception org.orekit.errors.OrekitIllegalArgumentException
Create an exception with localized message.
OrekitIllegalStateException - Exception in org.orekit.errors
Extension of IllegalStateException with localized message.
OrekitIllegalStateException(Localizable, Object...) - Constructor for exception org.orekit.errors.OrekitIllegalStateException
Create an exception with localized message.
OrekitInternalError - Exception in org.orekit.errors
Extension of Runtime with localized message for internal errors only.
OrekitInternalError(Throwable) - Constructor for exception org.orekit.errors.OrekitInternalError
Create an exception with localized message.
OrekitIOException - Exception in org.orekit.errors
Extension of IOException with localized message.
OrekitIOException(Localizable, Object...) - Constructor for exception org.orekit.errors.OrekitIOException
Create an exception with localized message.
OrekitMessages - Enum in org.orekit.errors
Enumeration for localized messages formats.
OrekitMessages.UTF8Control - Class in org.orekit.errors
Control class loading properties in UTF-8 encoding.
OrekitParseException - Exception in org.orekit.errors
Extension of ParseException with localized message.
OrekitParseException(Localizable, Object...) - Constructor for exception org.orekit.errors.OrekitParseException
Create an exception with localized message.
OrekitSatelliteEphemeris(String) - Constructor for class org.orekit.files.general.OrekitEphemerisFile.OrekitSatelliteEphemeris
Standard constructor for building the satellite Ephemeris object.
OrekitStepHandler - Interface in org.orekit.propagation.sampling
This interface is a space-dynamics aware step handler.
OrekitStepHandlerMultiplexer - Class in org.orekit.propagation.sampling
This class gathers several OrekitStepHandler instances into one.
OrekitStepHandlerMultiplexer() - Constructor for class org.orekit.propagation.sampling.OrekitStepHandlerMultiplexer
Simple constructor.
OrekitStepInterpolator - Interface in org.orekit.propagation.sampling
This interface is a space-dynamics aware step interpolator.
OrekitStepNormalizer - Class in org.orekit.propagation.sampling
This class wraps an object implementing OrekitFixedStepHandler into a OrekitStepHandler.
OrekitStepNormalizer(double, OrekitFixedStepHandler) - Constructor for class org.orekit.propagation.sampling.OrekitStepNormalizer
Simple constructor.
org.orekit.attitudes - package org.orekit.attitudes
This package provides classes to represent simple attitudes.
org.orekit.bodies - package org.orekit.bodies
This package provides interface to represent the position and geometry of space objects such as stars, planets or asteroids.
org.orekit.data - package org.orekit.data
This package provide base classes for exploring the configured data directory tree and read external data that can be used by the library.
org.orekit.errors - package org.orekit.errors
This package provides classes to generate and handle exceptions.
org.orekit.estimation - package org.orekit.estimation
This package is the top level package for orbit determination.
org.orekit.estimation.iod - package org.orekit.estimation.iod
 
org.orekit.estimation.leastsquares - package org.orekit.estimation.leastsquares
The leastsquares package provides an implementation of a batch least squares estimator engine to perform an orbit determination.
org.orekit.estimation.measurements - package org.orekit.estimation.measurements
The measurements package defines everything that is related to orbit determination measurements.
org.orekit.estimation.measurements.generation - package org.orekit.estimation.measurements.generation
This package provides Orbit Determination measurements generation.
org.orekit.estimation.measurements.modifiers - package org.orekit.estimation.measurements.modifiers
 
org.orekit.estimation.sequential - package org.orekit.estimation.sequential
 
org.orekit.files - package org.orekit.files
Top level package for various parsers.
org.orekit.files.ccsds - package org.orekit.files.ccsds
This package provides a parser for orbit data stored in CCSDS Orbit Data Message format.
org.orekit.files.general - package org.orekit.files.general
This package provides interfaces for orbit file representations and corresponding parsers.
org.orekit.files.sp3 - package org.orekit.files.sp3
This package provides a parser for orbit data stored in SP3 format.
org.orekit.forces - package org.orekit.forces
This package provides the interface for force models that will be used by the NumericalPropagator, as well as some classical spacecraft models for surface forces (spherical, box and solar array ...).
org.orekit.forces.drag - package org.orekit.forces.drag
This package provides all drag-related forces.
org.orekit.forces.drag.atmosphere - package org.orekit.forces.drag.atmosphere
This package provides the atmosphere model interface and several implementations.
org.orekit.forces.drag.atmosphere.data - package org.orekit.forces.drag.atmosphere.data
This package provides classes to get atmospheric data, including solar flux and planetary geomagnetic indices.
org.orekit.forces.gravity - package org.orekit.forces.gravity
This package provides all gravity-related forces.
org.orekit.forces.gravity.potential - package org.orekit.forces.gravity.potential
This package provides classes to read gravity field files and supports several different formats.
org.orekit.forces.maneuvers - package org.orekit.forces.maneuvers
This package provides models of simple maneuvers.
org.orekit.forces.radiation - package org.orekit.forces.radiation
This package provides all radiation pressure related forces.
org.orekit.frames - package org.orekit.frames
This package provides classes to handle frames and transforms between them.
org.orekit.gnss - package org.orekit.gnss
This package provides classes related to GNSS applications.
org.orekit.gnss.antenna - package org.orekit.gnss.antenna
This package provides classes related to receiver and satellites antenna modeling.
org.orekit.gnss.attitude - package org.orekit.gnss.attitude
This package provides classes related to navigation satellites attitude modeling.
org.orekit.models - package org.orekit.models
Top level package for physical models.
org.orekit.models.earth - package org.orekit.models.earth
This package provides models that simulate certain physical phenomena of Earth and the near-Earth environment.
org.orekit.models.earth.displacement - package org.orekit.models.earth.displacement
This package provides models computing reference points displacements on Earth surface.
org.orekit.models.earth.tessellation - package org.orekit.models.earth.tessellation
This package provides ways to do tessellation and sampling of zones of interest over an ellipsoid surface.
org.orekit.orbits - package org.orekit.orbits
This package provides classes to represent orbits.
org.orekit.propagation - package org.orekit.propagation
Propagation
org.orekit.propagation.analytical - package org.orekit.propagation.analytical
Top level package for analytical propagators.
org.orekit.propagation.analytical.gnss - package org.orekit.propagation.analytical.gnss
This package provides classes to propagate GNSS orbits.
org.orekit.propagation.analytical.tle - package org.orekit.propagation.analytical.tle
This package provides classes to read and extrapolate tle's.
org.orekit.propagation.conversion - package org.orekit.propagation.conversion
This package provides tools to convert a given propagator or a set of SpacecraftState into another propagator.
org.orekit.propagation.events - package org.orekit.propagation.events
This package provides interfaces and classes dealing with events occurring during propagation.
org.orekit.propagation.events.handlers - package org.orekit.propagation.events.handlers
This package provides an interface and classes dealing with events occurrence only.
org.orekit.propagation.integration - package org.orekit.propagation.integration
Utilities for integration-based propagators (both numerical and semi-analytical).
org.orekit.propagation.numerical - package org.orekit.propagation.numerical
Top level package for numerical propagators.
org.orekit.propagation.sampling - package org.orekit.propagation.sampling
This package provides interfaces and classes dealing with step handling during propagation.
org.orekit.propagation.semianalytical - package org.orekit.propagation.semianalytical
Top level package for semi-analytical propagators.
org.orekit.propagation.semianalytical.dsst - package org.orekit.propagation.semianalytical.dsst
This package provides an implementation of the Draper Semi-analytical Satellite Theory (DSST).
org.orekit.propagation.semianalytical.dsst.forces - package org.orekit.propagation.semianalytical.dsst.forces
This package provides force models for Draper Semi-analytical Satellite Theory (DSST).
org.orekit.propagation.semianalytical.dsst.utilities - package org.orekit.propagation.semianalytical.dsst.utilities
This package provides utilities for Draper Semi-analytical Satellite Theory (DSST).
org.orekit.propagation.semianalytical.dsst.utilities.hansen - package org.orekit.propagation.semianalytical.dsst.utilities.hansen
This package provides Hansen coefficient related utilities for Draper Semi-analytical Satellite Theory (DSST).
org.orekit.time - package org.orekit.time
This independent package provides classes to handle epochs, time scales, and to compare instants together.
org.orekit.utils - package org.orekit.utils
This package provides useful objects.
ORIGINATOR - org.orekit.files.ccsds.Keyword
Creating agency or operator.
OrphanFrame - Class in org.orekit.frames
Prototype frame that can be built from leaf to roots and later attached to a tree.
OrphanFrame(String) - Constructor for class org.orekit.frames.OrphanFrame
Simple constructor.
osculatingDerivative(AbsoluteDate) - Method in class org.orekit.utils.SecularAndHarmonic
Get fitted osculating derivative.
osculatingSecondDerivative(AbsoluteDate) - Method in class org.orekit.utils.SecularAndHarmonic
Get fitted osculating second derivative.
OsculatingToMeanElementsConverter - Class in org.orekit.propagation.conversion
This class converts osculating orbital elements into mean elements.
OsculatingToMeanElementsConverter(SpacecraftState, int, Propagator, double) - Constructor for class org.orekit.propagation.conversion.OsculatingToMeanElementsConverter
Constructor.
osculatingValue(AbsoluteDate) - Method in class org.orekit.utils.SecularAndHarmonic
Get fitted osculating value.
OTHER - org.orekit.files.sp3.SP3File.SP3OrbitType
other type, defined by SP3 file producing agency.
OUT_OF_RANGE_BODY_EPHEMERIDES_DATE - org.orekit.errors.OrekitMessages
 
OUT_OF_RANGE_DERIVATION_ORDER - org.orekit.errors.OrekitMessages
 
OUT_OF_RANGE_EPHEMERIDES_DATE - org.orekit.errors.OrekitMessages
 
OUT_OF_RANGE_LATITUDE - org.orekit.errors.OrekitMessages
 
OUT_OF_RANGE_SECONDS_NUMBER - org.orekit.errors.OrekitMessages
 
OUT_OF_RANGE_TIME_TRANSFORM - org.orekit.errors.OrekitMessages
 
OutlierFilter<T extends ObservedMeasurement<T>> - Class in org.orekit.estimation.measurements.modifiers
Modifier that sets estimated measurement weight to 0 if residual is too far from expected domain.
OutlierFilter(int, double) - Constructor for class org.orekit.estimation.measurements.modifiers.OutlierFilter
Simple constructor.

P

p - Variable in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution
hy.
P1 - org.orekit.gnss.ObservationType
Pseudorange GPS L1 / GLONASS G1 for Rinex2.
P1 - Static variable in class org.orekit.models.earth.displacement.Tide
P₁ tide.
P2 - org.orekit.gnss.ObservationType
Pseudorange GPS L2 / GLONASS G2 for Rinex2.
ParameterDriver - Class in org.orekit.utils
Class allowing to drive the value of a parameter.
ParameterDriver(String, double, double, double, double) - Constructor for class org.orekit.utils.ParameterDriver
Simple constructor.
ParameterDriversList - Class in org.orekit.utils
Class managing several parameter drivers, taking care of duplicated names.
ParameterDriversList() - Constructor for class org.orekit.utils.ParameterDriversList
Creates an empty list.
ParameterDriversList.DelegatingDriver - Class in org.orekit.utils
Specialized driver delegating to several other managing the same parameter name.
ParameterFunction - Interface in org.orekit.utils
Interface representing a scalar function depending on a ParameterDriver.
ParameterObserver - Interface in org.orekit.utils
Interface for observing parameters changes.
parse(BufferedReader, String) - Method in class org.orekit.files.ccsds.OEMParser
 
parse(BufferedReader, String) - Method in interface org.orekit.files.general.EphemerisFileParser
Parse an ephemeris file from a stream.
parse(BufferedReader, String) - Method in class org.orekit.files.sp3.SP3Parser
 
parse(InputStream) - Method in class org.orekit.files.ccsds.ODMParser
Parse a CCSDS Orbit Data Message.
parse(InputStream) - Method in class org.orekit.files.ccsds.OEMParser
Parse a CCSDS Orbit Data Message.
parse(InputStream) - Method in class org.orekit.files.ccsds.OMMParser
Parse a CCSDS Orbit Data Message.
parse(InputStream) - Method in class org.orekit.files.ccsds.OPMParser
Parse a CCSDS Orbit Data Message.
parse(InputStream) - Method in class org.orekit.files.ccsds.TDMParser
Parse a CCSDS Tracking Data Message.
parse(InputStream) - Method in class org.orekit.files.sp3.SP3Parser
Parse a SP3 file from an input stream using the UTF-8 charset.
parse(InputStream, String) - Method in class org.orekit.data.PoissonSeriesParser
Parse a stream.
parse(InputStream, String) - Method in class org.orekit.data.SimpleTimeStampedTableParser
Parse a stream.
parse(InputStream, String) - Method in class org.orekit.files.ccsds.ODMParser
Parse a CCSDS Orbit Data Message.
parse(InputStream, String) - Method in class org.orekit.files.ccsds.OEMParser
Parse a CCSDS Orbit Data Message.
parse(InputStream, String) - Method in class org.orekit.files.ccsds.OMMParser
Parse a CCSDS Orbit Data Message.
parse(InputStream, String) - Method in class org.orekit.files.ccsds.OPMParser
Parse a CCSDS Orbit Data Message.
parse(InputStream, String) - Method in class org.orekit.files.ccsds.TDMParser
Parse a CCSDS Tracking Data Message.
parse(String) - Method in class org.orekit.data.PolynomialParser
Parse a polynomial expression.
parse(String) - Method in class org.orekit.files.ccsds.ODMParser
Parse a CCSDS Orbit Data Message.
parse(String) - Method in class org.orekit.files.ccsds.OEMParser
Parse a CCSDS Orbit Data Message.
parse(String) - Method in class org.orekit.files.ccsds.OMMParser
Parse a CCSDS Orbit Data Message.
parse(String) - Method in class org.orekit.files.ccsds.OPMParser
Parse a CCSDS Orbit Data Message.
parse(String) - Method in class org.orekit.files.ccsds.TDMParser
Parse a CCSDS Tracking Data Message.
parse(String) - Method in interface org.orekit.files.general.EphemerisFileParser
Parse an ephemeris file from a file on the local file system.
parse(String) - Method in class org.orekit.files.sp3.SP3Parser
 
parseCCSDSCalendarSegmentedTimeCode(byte, byte[]) - Static method in class org.orekit.time.AbsoluteDate
Build an instance from a CCSDS Calendar Segmented Time Code (CCS).
parseCCSDSCalendarSegmentedTimeCode(byte, byte[]) - Method in class org.orekit.time.FieldAbsoluteDate
Build an instance from a CCSDS Calendar Segmented Time Code (CCS).
parseCCSDSDaySegmentedTimeCode(byte, byte[], DateComponents) - Static method in class org.orekit.time.AbsoluteDate
Build an instance from a CCSDS Day Segmented Time Code (CDS).
parseCCSDSDaySegmentedTimeCode(Field<T>, byte, byte[], DateComponents) - Static method in class org.orekit.time.FieldAbsoluteDate
Build an instance from a CCSDS Day Segmented Time Code (CDS).
parseCCSDSFrame(String) - Method in class org.orekit.files.ccsds.ODMParser
Parse a CCSDS frame.
parseCCSDSUnsegmentedTimeCode(byte, byte, byte[], AbsoluteDate) - Static method in class org.orekit.time.AbsoluteDate
Build an instance from a CCSDS Unsegmented Time Code (CUC).
parseCCSDSUnsegmentedTimeCode(Field<T>, byte, byte, byte[], FieldAbsoluteDate<T>) - Static method in class org.orekit.time.FieldAbsoluteDate
Build an instance from a CCSDS Unsegmented Time Code (CUC).
parseCoefficient(String, double[][], int, int, String, String) - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
Parse a coefficient.
parseCoefficient(String, List<List<Double>>, int, int, String, String) - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
Parse a coefficient.
parseComment(KeyValue, List<String>) - Method in class org.orekit.files.ccsds.ODMParser
Parse a comment line.
parseDate(String) - Static method in class org.orekit.time.DateComponents
Parse a string in ISO-8601 format to build a date.
parseDate(String, CcsdsTimeScale) - Method in class org.orekit.files.ccsds.ODMParser
Parse a date.
parseDate(String, IERSConventions, AbsoluteDate) - Method in enum org.orekit.files.ccsds.CcsdsTimeScale
Parse a date in this time scale.
parseDateTime(String) - Static method in class org.orekit.time.DateTimeComponents
Parse a string in ISO-8601 format to build a date/time.
parseDouble(String) - Static method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
Parse a double from a string.
parseGeneralStateDataEntry(KeyValue, OGMFile, List<String>) - Method in class org.orekit.files.ccsds.ODMParser
Parse a general state data key = value entry.
parseHeaderEntry(KeyValue, ODMFile, List<String>) - Method in class org.orekit.files.ccsds.ODMParser
Parse an entry from the header.
parseKeyValue(InputStream, String) - Method in class org.orekit.files.ccsds.TDMParser
Parse a CCSDS Tracking Data Message with KEYVALUE format.
parseMetaDataEntry(KeyValue, ODMMetaData, List<String>) - Method in class org.orekit.files.ccsds.ODMParser
Parse a meta-data key = value entry.
parseMonth(String) - Static method in enum org.orekit.time.Month
Parse the string to get the month.
Parser() - Constructor for class org.orekit.gnss.RinexLoader.Parser
 
parseSatelliteAntennaCode(String) - Static method in enum org.orekit.gnss.antenna.SatelliteAntennaCode
Deprecated.
Parse a string to get the satellite antenna code.
parseSatelliteSystem(String) - Static method in enum org.orekit.gnss.SatelliteSystem
Parse a string to get the satellite system.
parseSatelliteType(String) - Static method in enum org.orekit.gnss.antenna.SatelliteType
Parse a string to get the satellite type.
parseTime(String) - Static method in class org.orekit.time.TimeComponents
Parse a string in ISO-8601 format to build a time.
parseType(String) - Static method in enum org.orekit.files.sp3.SP3File.SP3OrbitType
Parse a string to get the type.
parseXml(InputStream, String) - Method in class org.orekit.files.ccsds.TDMParser
Parse a CCSDS Tracking Data Message with XML format.
PartialDerivativesEquations - Class in org.orekit.propagation.numerical
Set of additional equations computing the partial derivatives of the state (orbit) with respect to initial state and force models parameters.
PartialDerivativesEquations(String, NumericalPropagator) - Constructor for class org.orekit.propagation.numerical.PartialDerivativesEquations
Simple constructor.
PARTICIPANT_1 - org.orekit.files.ccsds.Keyword
Meta-data: PARTICIPANT_n, n = {1, 2, 3, 4, 5}.
PARTICIPANT_2 - org.orekit.files.ccsds.Keyword
Participant 2.
PARTICIPANT_3 - org.orekit.files.ccsds.Keyword
Participant 3.
PARTICIPANT_4 - org.orekit.files.ccsds.Keyword
Participant 4.
PARTICIPANT_5 - org.orekit.files.ccsds.Keyword
Participant 5.
PAST_INFINITY - Static variable in class org.orekit.time.AbsoluteDate
Dummy date at infinity in the past direction.
PATH - org.orekit.files.ccsds.Keyword
Meta-data: The PATH keywords shall reflect the signal path by listing the index of each PARTICIPANT in order, separated by commas, with no inserted white space.
PATH_1 - org.orekit.files.ccsds.Keyword
Path 1.
PATH_2 - org.orekit.files.ccsds.Keyword
Path 2.
pathDelay(double, double) - Method in class org.orekit.models.earth.FixedTroposphericDelay
Calculates the tropospheric path delay for the signal path from a ground station to a satellite.
pathDelay(double, double) - Method in class org.orekit.models.earth.MariniMurrayModel
 
pathDelay(double, double) - Method in class org.orekit.models.earth.SaastamoinenModel
Calculates the tropospheric path delay for the signal path from a ground station to a satellite.
pathDelay(double, double) - Method in interface org.orekit.models.earth.TroposphericModel
Calculates the tropospheric path delay for the signal path from a ground station to a satellite.
pathDelay(double, double, double[], AbsoluteDate) - Method in interface org.orekit.models.earth.DiscreteTroposphericModel
Calculates the tropospheric path delay for the signal path from a ground station to a satellite.
pathDelay(double, double, double[], AbsoluteDate) - Method in class org.orekit.models.earth.EstimatedTroposphericModel
 
pathDelay(double, double, double[], AbsoluteDate) - Method in class org.orekit.models.earth.MendesPavlisModel
Calculates the tropospheric path delay for the signal path from a ground station to a satellite.
pathDelay(double, double, double[], AbsoluteDate) - Method in interface org.orekit.models.earth.TroposphericModel
Calculates the tropospheric path delay for the signal path from a ground station to a satellite.
pathDelay(double, double, double[], AbsoluteDate) - Method in class org.orekit.models.earth.ViennaOneModel
Calculates the tropospheric path delay for the signal path from a ground station to a satellite.
pathDelay(double, double, double[], AbsoluteDate) - Method in class org.orekit.models.earth.ViennaThreeModel
Calculates the tropospheric path delay for the signal path from a ground station to a satellite.
pathDelay(AbsoluteDate, GeodeticPoint, double, double) - Method in interface org.orekit.models.earth.IonosphericModel
Calculates the ionospheric path delay for the signal path from a ground station to a satellite.
pathDelay(AbsoluteDate, GeodeticPoint, double, double) - Method in class org.orekit.models.earth.KlobucharIonoModel
Calculates the ionospheric path delay for the signal path from a ground station to a satellite.
pathDelay(T, T) - Method in interface org.orekit.models.earth.TroposphericModel
Calculates the tropospheric path delay for the signal path from a ground station to a satellite.
pathDelay(T, T, T[], FieldAbsoluteDate<T>) - Method in interface org.orekit.models.earth.DiscreteTroposphericModel
Calculates the tropospheric path delay for the signal path from a ground station to a satellite.
pathDelay(T, T, T[], FieldAbsoluteDate<T>) - Method in class org.orekit.models.earth.EstimatedTroposphericModel
 
pathDelay(T, T, T[], FieldAbsoluteDate<T>) - Method in class org.orekit.models.earth.MendesPavlisModel
Calculates the tropospheric path delay for the signal path from a ground station to a satellite.
pathDelay(T, T, T[], FieldAbsoluteDate<T>) - Method in interface org.orekit.models.earth.TroposphericModel
Calculates the tropospheric path delay for the signal path from a ground station to a satellite.
pathDelay(T, T, T[], FieldAbsoluteDate<T>) - Method in class org.orekit.models.earth.ViennaOneModel
Calculates the tropospheric path delay for the signal path from a ground station to a satellite.
pathDelay(T, T, T[], FieldAbsoluteDate<T>) - Method in class org.orekit.models.earth.ViennaThreeModel
Calculates the tropospheric path delay for the signal path from a ground station to a satellite.
PC_N0 - org.orekit.files.ccsds.Keyword
Data: Carrier power to noise spectral density ratio (Pc/No) [dBHz].
perige - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator
perigee, expressed in KM and ALTITUDE.
Phase - Class in org.orekit.estimation.measurements
Class modeling a phase measurement from a ground station.
Phase(GroundStation, AbsoluteDate, double, double, double, double) - Constructor for class org.orekit.estimation.measurements.Phase
Phase(GroundStation, AbsoluteDate, double, double, double, double, int) - Constructor for class org.orekit.estimation.measurements.Phase
Phase(GroundStation, AbsoluteDate, double, double, double, double, ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.Phase
Simple constructor.
PhaseAmbiguityModifier - Class in org.orekit.estimation.measurements.modifiers
Class modifying theoretical phase measurement with ambiguity.
PhaseAmbiguityModifier(int, double) - Constructor for class org.orekit.estimation.measurements.modifiers.PhaseAmbiguityModifier
Constructor.
PhaseCenterVariationFunction - Interface in org.orekit.gnss.antenna
Model for antennas phase center variations.
PLUTO - org.orekit.bodies.JPLEphemeridesLoader.EphemerisType
Constant for Pluto.
PLUTO - org.orekit.files.ccsds.CenterName
Pluto body.
PLUTO - Static variable in class org.orekit.bodies.CelestialBodyFactory
Predefined name for Pluto.
POINT_INSIDE_ELLIPSOID - org.orekit.errors.OrekitMessages
 
pointAt(double) - Method in class org.orekit.bodies.Ellipse
Get a point of the 2D ellipse.
pointAtDistance(double, double, double) - Method in class org.orekit.frames.TopocentricFrame
Compute the point observed from the station at some specified distance.
pointOnLimb(Vector3D, Vector3D) - Method in class org.orekit.bodies.Ellipsoid
Find a point on ellipsoid limb, as seen by an external observer.
PoissonSeries - Class in org.orekit.data
Class representing a Poisson series for nutation or ephemeris computations.
PoissonSeries(PolynomialNutation, Map<Long, SeriesTerm>) - Constructor for class org.orekit.data.PoissonSeries
Build a Poisson series from an IERS table file.
PoissonSeries.CompiledSeries - Interface in org.orekit.data
This interface represents a fast evaluator for Poisson series.
PoissonSeriesParser - Class in org.orekit.data
Parser for Poisson series files.
PoissonSeriesParser(int) - Constructor for class org.orekit.data.PoissonSeriesParser
Build a parser for a Poisson series from an IERS table file.
POLAR_TRAJECTORY - org.orekit.errors.OrekitMessages
 
PoleCorrection - Class in org.orekit.frames
Simple container class for pole correction parameters.
PoleCorrection(double, double) - Constructor for class org.orekit.frames.PoleCorrection
Simple constructor.
PolynomialFunctionMatrix - Class in org.orekit.propagation.semianalytical.dsst.utilities.hansen
A quadratic matrix of PolynomialFunction.
PolynomialNutation - Class in org.orekit.data
Polynomial nutation function.
PolynomialNutation(double...) - Constructor for class org.orekit.data.PolynomialNutation
Build a polynomial from its coefficients.
PolynomialParametricAcceleration - Class in org.orekit.forces
This class implements a parametric acceleration with polynomial signed amplitude.
PolynomialParametricAcceleration(Vector3D, boolean, String, AbsoluteDate, int) - Constructor for class org.orekit.forces.PolynomialParametricAcceleration
Simple constructor.
PolynomialParametricAcceleration(Vector3D, AttitudeProvider, String, AbsoluteDate, int) - Constructor for class org.orekit.forces.PolynomialParametricAcceleration
Simple constructor.
PolynomialParser - Class in org.orekit.data
Parser for polynomials in IERS tables.
PolynomialParser(char, PolynomialParser.Unit) - Constructor for class org.orekit.data.PolynomialParser
Simple constructor.
PolynomialParser.Unit - Enum in org.orekit.data
Unit for the coefficients.
Position - Class in org.orekit.estimation.measurements
Class modeling a position only measurement.
Position(AbsoluteDate, Vector3D, double[][], double) - Constructor for class org.orekit.estimation.measurements.Position
Position(AbsoluteDate, Vector3D, double[][], double, int) - Constructor for class org.orekit.estimation.measurements.Position
Position(AbsoluteDate, Vector3D, double[][], double, ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.Position
Constructor with full covariance matrix and all inputs.
Position(AbsoluteDate, Vector3D, double[], double) - Constructor for class org.orekit.estimation.measurements.Position
Position(AbsoluteDate, Vector3D, double[], double, int) - Constructor for class org.orekit.estimation.measurements.Position
Position(AbsoluteDate, Vector3D, double[], double, ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.Position
Constructor with one vector for the standard deviation.
Position(AbsoluteDate, Vector3D, double, double) - Constructor for class org.orekit.estimation.measurements.Position
Position(AbsoluteDate, Vector3D, double, double, int) - Constructor for class org.orekit.estimation.measurements.Position
Position(AbsoluteDate, Vector3D, double, double, ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.Position
Constructor with one double for the standard deviation.
PositionAngle - Enum in org.orekit.orbits
Enumerate for true, eccentric and mean position angles.
PositionAngleDetector - Class in org.orekit.propagation.events
Detector for in-orbit position angle.
PositionAngleDetector(double, double, OrbitType, PositionAngle, double) - Constructor for class org.orekit.propagation.events.PositionAngleDetector
Build a detector.
PositionAngleDetector(OrbitType, PositionAngle, double) - Constructor for class org.orekit.propagation.events.PositionAngleDetector
Build a new detector.
PositionBuilder - Class in org.orekit.estimation.measurements.generation
Builder for Position measurements.
PositionBuilder(CorrelatedRandomVectorGenerator, double, double, ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.generation.PositionBuilder
Simple constructor.
POSITIVE_FLOW_RATE - org.orekit.errors.OrekitMessages
 
PotentialCoefficientsReader - Class in org.orekit.forces.gravity.potential
This abstract class represents a Gravitational Potential Coefficients file reader.
PotentialCoefficientsReader(String, boolean) - Constructor for class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
Simple constructor.
PR_N0 - org.orekit.files.ccsds.Keyword
Data: Ranging power to noise spectral density ratio (Pr/No) [dBHz].
Predefined - Enum in org.orekit.frames
Predefined frames provided by FramesFactory.
PRESSURE - org.orekit.files.ccsds.Keyword
Data: Pressure [hPa].
PROCESSED - org.orekit.estimation.measurements.EstimatedMeasurement.Status
Status for processed measurements.
processMeasurements(Iterable<ObservedMeasurement<?>>) - Method in class org.orekit.estimation.sequential.KalmanEstimator
Process several measurements.
projectToEllipse(Vector2D) - Method in class org.orekit.bodies.Ellipse
Find the closest ellipse point.
projectToEllipse(TimeStampedPVCoordinates) - Method in class org.orekit.bodies.Ellipse
Project position-velocity-acceleration on an ellipse.
projectToGround(Vector3D, AbsoluteDate, Frame) - Method in interface org.orekit.bodies.BodyShape
Project a point to the ground.
projectToGround(Vector3D, AbsoluteDate, Frame) - Method in class org.orekit.bodies.OneAxisEllipsoid
Project a point to the ground.
projectToGround(Vector3D, AbsoluteDate, Frame) - Method in class org.orekit.models.earth.Geoid
 
projectToGround(TimeStampedPVCoordinates, Frame) - Method in interface org.orekit.bodies.BodyShape
Project a moving point to the ground.
projectToGround(TimeStampedPVCoordinates, Frame) - Method in class org.orekit.bodies.OneAxisEllipsoid
Project a moving point to the ground.
projectToGround(TimeStampedPVCoordinates, Frame) - Method in class org.orekit.models.earth.Geoid
 
propagate(AbsoluteDate) - Method in class org.orekit.propagation.AbstractPropagator
Propagate towards a target date.
propagate(AbsoluteDate) - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
Propagate towards a target date.
propagate(AbsoluteDate) - Method in interface org.orekit.propagation.Propagator
Propagate towards a target date.
propagate(AbsoluteDate, boolean) - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
Propagation with or without event detection.
propagate(AbsoluteDate, AbsoluteDate) - Method in class org.orekit.propagation.analytical.AbstractAnalyticalPropagator
Propagate from a start date towards a target date.
propagate(AbsoluteDate, AbsoluteDate) - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
Propagate from a start date towards a target date.
propagate(AbsoluteDate, AbsoluteDate) - Method in interface org.orekit.propagation.Propagator
Propagate from a start date towards a target date.
propagate(AbsoluteDate, AbsoluteDate) - Method in class org.orekit.propagation.PropagatorsParallelizer
Propagate from a start date towards a target date.
propagate(FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.FieldAbstractPropagator
Propagate towards a target date.
propagate(FieldAbsoluteDate<T>) - Method in interface org.orekit.propagation.FieldPropagator
Propagate towards a target date.
propagate(FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator
Propagate towards a target date.
propagate(FieldAbsoluteDate<T>, boolean) - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator
Propagation with or without event detection.
propagate(FieldAbsoluteDate<T>, FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.analytical.FieldAbstractAnalyticalPropagator
Propagate from a start date towards a target date.
propagate(FieldAbsoluteDate<T>, FieldAbsoluteDate<T>) - Method in interface org.orekit.propagation.FieldPropagator
Propagate from a start date towards a target date.
propagate(FieldAbsoluteDate<T>, FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator
Propagate from a start date towards a target date.
propagateInEcef(AbsoluteDate) - Method in class org.orekit.propagation.analytical.gnss.GPSPropagator
Gets the PVCoordinates of the GPS SV in ECEF frame.
propagateOrbit(AbsoluteDate) - Method in class org.orekit.propagation.analytical.AbstractAnalyticalPropagator
Extrapolate an orbit up to a specific target date.
propagateOrbit(AbsoluteDate) - Method in class org.orekit.propagation.analytical.AdapterPropagator
Extrapolate an orbit up to a specific target date.
propagateOrbit(AbsoluteDate) - Method in class org.orekit.propagation.analytical.AggregateBoundedPropagator
 
propagateOrbit(AbsoluteDate) - Method in class org.orekit.propagation.analytical.EcksteinHechlerPropagator
Extrapolate an orbit up to a specific target date.
propagateOrbit(AbsoluteDate) - Method in class org.orekit.propagation.analytical.Ephemeris
Extrapolate an orbit up to a specific target date.
propagateOrbit(AbsoluteDate) - Method in class org.orekit.propagation.analytical.gnss.GPSPropagator
Extrapolate an orbit up to a specific target date.
propagateOrbit(AbsoluteDate) - Method in class org.orekit.propagation.analytical.KeplerianPropagator
Extrapolate an orbit up to a specific target date.
propagateOrbit(AbsoluteDate) - Method in class org.orekit.propagation.analytical.tle.TLEPropagator
Extrapolate an orbit up to a specific target date.
propagateOrbit(AbsoluteDate) - Method in class org.orekit.propagation.integration.IntegratedEphemeris
Extrapolate an orbit up to a specific target date.
propagateOrbit(FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.analytical.FieldAbstractAnalyticalPropagator
Extrapolate an orbit up to a specific target date.
propagateOrbit(FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.analytical.FieldEcksteinHechlerPropagator
Extrapolate an orbit up to a specific target date.
propagateOrbit(FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.analytical.FieldKeplerianPropagator
Extrapolate an orbit up to a specific target date.
propagateOrbit(FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.integration.FieldIntegratedEphemeris
Extrapolate an orbit up to a specific target date.
Propagator - Interface in org.orekit.propagation
This interface provides a way to propagate an orbit at any time.
PROPAGATOR_NOT_IN_EPHEMERIS_GENERATION_MODE - org.orekit.errors.OrekitMessages
 
PropagatorBuilder - Interface in org.orekit.propagation.conversion
This interface is the top-level abstraction to build propagators for conversion.
PropagatorConverter - Interface in org.orekit.propagation.conversion
This interface is the top-level abstraction for propagators conversions.
PropagatorsParallelizer - Class in org.orekit.propagation
This class provides a way to propagate simultaneously several orbits.
PropagatorsParallelizer(List<Propagator>, MultiSatStepHandler) - Constructor for class org.orekit.propagation.PropagatorsParallelizer
Simple constructor.
PSEUDO_RANGE - org.orekit.gnss.MeasurementType
Pseudo-range measurement.
PV - Class in org.orekit.estimation.measurements
Class modeling a position-velocity measurement.
PV(AbsoluteDate, Vector3D, Vector3D, double[][], double) - Constructor for class org.orekit.estimation.measurements.PV
PV(AbsoluteDate, Vector3D, Vector3D, double[][], double[][], double) - Constructor for class org.orekit.estimation.measurements.PV
PV(AbsoluteDate, Vector3D, Vector3D, double[][], double[][], double, int) - Constructor for class org.orekit.estimation.measurements.PV
PV(AbsoluteDate, Vector3D, Vector3D, double[][], double[][], double, ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.PV
Constructor with 2 smaller covariance matrices.
PV(AbsoluteDate, Vector3D, Vector3D, double[][], double, int) - Constructor for class org.orekit.estimation.measurements.PV
PV(AbsoluteDate, Vector3D, Vector3D, double[][], double, ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.PV
Constructor with full covariance matrix and all inputs.
PV(AbsoluteDate, Vector3D, Vector3D, double[], double) - Constructor for class org.orekit.estimation.measurements.PV
PV(AbsoluteDate, Vector3D, Vector3D, double[], double[], double) - Constructor for class org.orekit.estimation.measurements.PV
PV(AbsoluteDate, Vector3D, Vector3D, double[], double[], double, int) - Constructor for class org.orekit.estimation.measurements.PV
PV(AbsoluteDate, Vector3D, Vector3D, double[], double[], double, ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.PV
Constructor with two vectors for the standard deviations.
PV(AbsoluteDate, Vector3D, Vector3D, double[], double, int) - Constructor for class org.orekit.estimation.measurements.PV
PV(AbsoluteDate, Vector3D, Vector3D, double[], double, ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.PV
Constructor with one vector for the standard deviations.
PV(AbsoluteDate, Vector3D, Vector3D, double, double, double) - Constructor for class org.orekit.estimation.measurements.PV
PV(AbsoluteDate, Vector3D, Vector3D, double, double, double, int) - Constructor for class org.orekit.estimation.measurements.PV
PV(AbsoluteDate, Vector3D, Vector3D, double, double, double, ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.PV
Constructor with two double for the standard deviations.
PVBuilder - Class in org.orekit.estimation.measurements.generation
Builder for PV measurements.
PVBuilder(CorrelatedRandomVectorGenerator, double, double, double, ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.generation.PVBuilder
Simple constructor.
PVCoordinates - Class in org.orekit.utils
Simple container for Position/Velocity/Acceleration triplets.
PVCoordinates() - Constructor for class org.orekit.utils.PVCoordinates
Simple constructor.
PVCoordinates(double, PVCoordinates) - Constructor for class org.orekit.utils.PVCoordinates
Multiplicative constructor.
PVCoordinates(double, PVCoordinates, double, PVCoordinates) - Constructor for class org.orekit.utils.PVCoordinates
Linear constructor.
PVCoordinates(double, PVCoordinates, double, PVCoordinates, double, PVCoordinates) - Constructor for class org.orekit.utils.PVCoordinates
Linear constructor.
PVCoordinates(double, PVCoordinates, double, PVCoordinates, double, PVCoordinates, double, PVCoordinates) - Constructor for class org.orekit.utils.PVCoordinates
Linear constructor.
PVCoordinates(FieldVector3D<DerivativeStructure>) - Constructor for class org.orekit.utils.PVCoordinates
Builds a PVCoordinates triplet from a FieldVector3D<DerivativeStructure>.
PVCoordinates(Vector3D, Vector3D) - Constructor for class org.orekit.utils.PVCoordinates
Builds a PVCoordinates triplet with zero acceleration.
PVCoordinates(Vector3D, Vector3D, Vector3D) - Constructor for class org.orekit.utils.PVCoordinates
Builds a PVCoordinates triplet.
PVCoordinates(PVCoordinates, PVCoordinates) - Constructor for class org.orekit.utils.PVCoordinates
Subtractive constructor.
PVCoordinatesProvider - Interface in org.orekit.utils
Interface for PV coordinates providers.

Q

q - Variable in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution
hx.
Q1 - Static variable in class org.orekit.models.earth.displacement.Tide
Q₁ tide.
QSW - org.orekit.frames.LOFType
Constant for QSW frame (X axis aligned with position, Z axis aligned with orbital momentum).
QZS - org.orekit.files.sp3.SP3File.TimeSystem
Quasi-Zenith System.
QZSS - org.orekit.files.sp3.SP3File.SP3FileType
QZSS only file.
QZSS - org.orekit.gnss.antenna.SatelliteAntennaCode
Deprecated.
QZSS Block I (Michibiki-1).
QZSS - org.orekit.gnss.antenna.SatelliteType
QZSS Block I (Michibiki-1).
QZSS - org.orekit.gnss.SatelliteSystem
Quasi-Zenith Satellite System system.
QZSS_2G - org.orekit.gnss.antenna.SatelliteAntennaCode
Deprecated.
QZSS Block II GEO (Michibiki-3).
QZSS_2G - org.orekit.gnss.antenna.SatelliteType
QZSS Block II GEO (Michibiki-3).
QZSS_2I - org.orekit.gnss.antenna.SatelliteAntennaCode
Deprecated.
QZSS Block II IGSO (Michibiki-2,4).
QZSS_2I - org.orekit.gnss.antenna.SatelliteType
QZSS Block II IGSO (Michibiki-2,4).
QZSSScale - Class in org.orekit.time
QZSS time scale.

R

R01 - org.orekit.gnss.Frequency
GLONASS, "G1" (1602 MHZ).
R02 - org.orekit.gnss.Frequency
GLONASS, "G2" (1246 MHz).
R03 - org.orekit.gnss.Frequency
GLONASS, "G3" (1202.025 MHz).
RA_OF_ASC_NODE - org.orekit.files.ccsds.Keyword
Orbit right ascension of ascending node.
RADIANS - org.orekit.data.PolynomialParser.Unit
Radians angles.
radiationPressureAcceleration(AbsoluteDate, Frame, Vector3D, Rotation, double, Vector3D, double[]) - Method in class org.orekit.forces.BoxAndSolarArraySpacecraft
Compute the acceleration due to radiation pressure.
radiationPressureAcceleration(AbsoluteDate, Frame, Vector3D, Rotation, double, Vector3D, double[]) - Method in class org.orekit.forces.radiation.IsotropicRadiationClassicalConvention
Compute the acceleration due to radiation pressure.
radiationPressureAcceleration(AbsoluteDate, Frame, Vector3D, Rotation, double, Vector3D, double[]) - Method in class org.orekit.forces.radiation.IsotropicRadiationCNES95Convention
Compute the acceleration due to radiation pressure.
radiationPressureAcceleration(AbsoluteDate, Frame, Vector3D, Rotation, double, Vector3D, double[]) - Method in class org.orekit.forces.radiation.IsotropicRadiationSingleCoefficient
Compute the acceleration due to radiation pressure.
radiationPressureAcceleration(AbsoluteDate, Frame, Vector3D, Rotation, double, Vector3D, double[]) - Method in interface org.orekit.forces.radiation.RadiationSensitive
Compute the acceleration due to radiation pressure.
radiationPressureAcceleration(AbsoluteDate, Frame, Vector3D, Rotation, double, Vector3D, double[], String) - Method in class org.orekit.forces.BoxAndSolarArraySpacecraft
Compute the acceleration due to radiation pressure, with parameters derivatives.
radiationPressureAcceleration(AbsoluteDate, Frame, Vector3D, Rotation, double, Vector3D, double[], String) - Method in class org.orekit.forces.radiation.IsotropicRadiationClassicalConvention
Compute the acceleration due to radiation pressure, with parameters derivatives.
radiationPressureAcceleration(AbsoluteDate, Frame, Vector3D, Rotation, double, Vector3D, double[], String) - Method in class org.orekit.forces.radiation.IsotropicRadiationCNES95Convention
Compute the acceleration due to radiation pressure, with parameters derivatives.
radiationPressureAcceleration(AbsoluteDate, Frame, Vector3D, Rotation, double, Vector3D, double[], String) - Method in class org.orekit.forces.radiation.IsotropicRadiationSingleCoefficient
Compute the acceleration due to radiation pressure, with parameters derivatives.
radiationPressureAcceleration(AbsoluteDate, Frame, Vector3D, Rotation, double, Vector3D, double[], String) - Method in interface org.orekit.forces.radiation.RadiationSensitive
Compute the acceleration due to radiation pressure, with parameters derivatives.
radiationPressureAcceleration(FieldAbsoluteDate<T>, Frame, FieldVector3D<T>, FieldRotation<T>, T, FieldVector3D<T>, T[]) - Method in class org.orekit.forces.BoxAndSolarArraySpacecraft
Compute the acceleration due to radiation pressure.
radiationPressureAcceleration(FieldAbsoluteDate<T>, Frame, FieldVector3D<T>, FieldRotation<T>, T, FieldVector3D<T>, T[]) - Method in class org.orekit.forces.radiation.IsotropicRadiationClassicalConvention
Compute the acceleration due to radiation pressure.
radiationPressureAcceleration(FieldAbsoluteDate<T>, Frame, FieldVector3D<T>, FieldRotation<T>, T, FieldVector3D<T>, T[]) - Method in class org.orekit.forces.radiation.IsotropicRadiationCNES95Convention
Compute the acceleration due to radiation pressure.
radiationPressureAcceleration(FieldAbsoluteDate<T>, Frame, FieldVector3D<T>, FieldRotation<T>, T, FieldVector3D<T>, T[]) - Method in class org.orekit.forces.radiation.IsotropicRadiationSingleCoefficient
Compute the acceleration due to radiation pressure.
radiationPressureAcceleration(FieldAbsoluteDate<T>, Frame, FieldVector3D<T>, FieldRotation<T>, T, FieldVector3D<T>, T[]) - Method in interface org.orekit.forces.radiation.RadiationSensitive
Compute the acceleration due to radiation pressure.
RadiationSensitive - Interface in org.orekit.forces.radiation
Interface for spacecraft that are sensitive to radiation pressure forces.
Range - Class in org.orekit.estimation.measurements
Class modeling a range measurement from a ground station.
Range(GroundStation, boolean, AbsoluteDate, double, double, double, int) - Constructor for class org.orekit.estimation.measurements.Range
Range(GroundStation, boolean, AbsoluteDate, double, double, double, ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.Range
Simple constructor.
Range(GroundStation, AbsoluteDate, double, double, double) - Constructor for class org.orekit.estimation.measurements.Range
Range(GroundStation, AbsoluteDate, double, double, double, boolean) - Constructor for class org.orekit.estimation.measurements.Range
Range(GroundStation, AbsoluteDate, double, double, double, int) - Constructor for class org.orekit.estimation.measurements.Range
RANGE - org.orekit.files.ccsds.Keyword
Data: Range value [km, s or RU].
RANGE_MODE - org.orekit.files.ccsds.Keyword
Meta-data: Range mode.
RANGE_MODULUS - org.orekit.files.ccsds.Keyword
Meta-data: Range modulus.
RANGE_UNITS - org.orekit.files.ccsds.Keyword
Meta-data: The RANGE_UNITS keyword specifies the units for the range observable.
RangeBuilder - Class in org.orekit.estimation.measurements.generation
Builder for Range measurements.
RangeBuilder(CorrelatedRandomVectorGenerator, GroundStation, boolean, double, double, ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.generation.RangeBuilder
Simple constructor.
RangeIonosphericDelayModifier - Class in org.orekit.estimation.measurements.modifiers
Class modifying theoretical range measurement with ionospheric delay.
RangeIonosphericDelayModifier(IonosphericModel) - Constructor for class org.orekit.estimation.measurements.modifiers.RangeIonosphericDelayModifier
Constructor.
RangeRate - Class in org.orekit.estimation.measurements
Class modeling one-way or two-way range rate measurement between two vehicles.
RangeRate(GroundStation, AbsoluteDate, double, double, double, boolean) - Constructor for class org.orekit.estimation.measurements.RangeRate
RangeRate(GroundStation, AbsoluteDate, double, double, double, boolean, int) - Constructor for class org.orekit.estimation.measurements.RangeRate
RangeRate(GroundStation, AbsoluteDate, double, double, double, boolean, ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.RangeRate
Simple constructor.
RangeRateBuilder - Class in org.orekit.estimation.measurements.generation
Builder for RangeRate measurements.
RangeRateBuilder(CorrelatedRandomVectorGenerator, GroundStation, boolean, double, double, ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.generation.RangeRateBuilder
Simple constructor.
rangeRateErrorTroposphericModel(GroundStation, FieldSpacecraftState<T>, T[]) - Method in class org.orekit.estimation.measurements.modifiers.RangeRateTroposphericDelayModifier
Compute the measurement error due to Troposphere.
rangeRateErrorTroposphericModel(GroundStation, SpacecraftState) - Method in class org.orekit.estimation.measurements.modifiers.RangeRateTroposphericDelayModifier
Compute the measurement error due to Troposphere.
RangeRateIonosphericDelayModifier - Class in org.orekit.estimation.measurements.modifiers
Class modifying theoretical range-rate measurement with ionospheric delay.
RangeRateIonosphericDelayModifier(IonosphericModel, boolean) - Constructor for class org.orekit.estimation.measurements.modifiers.RangeRateIonosphericDelayModifier
Constructor.
RangeRateTroposphericDelayModifier - Class in org.orekit.estimation.measurements.modifiers
Class modifying theoretical range-rate measurements with tropospheric delay.
RangeRateTroposphericDelayModifier(DiscreteTroposphericModel, boolean) - Constructor for class org.orekit.estimation.measurements.modifiers.RangeRateTroposphericDelayModifier
Constructor.
RangeTroposphericDelayModifier - Class in org.orekit.estimation.measurements.modifiers
Class modifying theoretical range measurement with tropospheric delay.
RangeTroposphericDelayModifier(DiscreteTroposphericModel) - Constructor for class org.orekit.estimation.measurements.modifiers.RangeTroposphericDelayModifier
Constructor.
RAPID_DATA_PREDICITON_COLUMNS_2000_FILENAME - Static variable in class org.orekit.frames.FramesFactory
Default regular expression for the Rapid Data and Prediction EOP columns files (IAU2000 compatibles).
RAPID_DATA_PREDICITON_XML_2000_FILENAME - Static variable in class org.orekit.frames.FramesFactory
Default regular expression for the Rapid Data and Prediction EOP XML files (IAU2000 compatibles).
RAPID_DATA_PREDICTION_COLUMNS_1980_FILENAME - Static variable in class org.orekit.frames.FramesFactory
Default regular expression for the Rapid Data and Prediction EOP columns files (IAU1980 compatibles).
RAPID_DATA_PREDICTION_XML_1980_FILENAME - Static variable in class org.orekit.frames.FramesFactory
Default regular expression for the Rapid Data and Prediction EOP XML files (IAU1980 compatibles).
RawSphericalHarmonicsProvider - Interface in org.orekit.forces.gravity.potential
Interface used to provide raw spherical harmonics coefficients.
RawSphericalHarmonicsProvider.RawSphericalHarmonics - Interface in org.orekit.forces.gravity.potential
The raw spherical harmonics at a particular instant.
readGravityField(int, int) - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory
Read a gravity field coefficients provider from the first supported file.
rebuildZone() - Method in class org.orekit.utils.SphericalPolygonsSetTransferObject
Rebuild the zone from saved data.
RECEIVE_BAND - org.orekit.files.ccsds.Keyword
Meta-data: Frequency band for received frequencies.
RECEIVE_DELAY_1 - org.orekit.files.ccsds.Keyword
Meta-data: Receive delays list.
RECEIVE_DELAY_2 - org.orekit.files.ccsds.Keyword
Second.
RECEIVE_DELAY_3 - org.orekit.files.ccsds.Keyword
Second.
RECEIVE_DELAY_4 - org.orekit.files.ccsds.Keyword
Second.
RECEIVE_DELAY_5 - org.orekit.files.ccsds.Keyword
Second.
RECEIVE_FREQ - org.orekit.files.ccsds.Keyword
Data: Received frequency [Hz].
RECEIVE_FREQ_1 - org.orekit.files.ccsds.Keyword
Data: Received frequencies [Hz].
RECEIVE_FREQ_2 - org.orekit.files.ccsds.Keyword
Received frequency 2.
RECEIVE_FREQ_3 - org.orekit.files.ccsds.Keyword
Received frequency 3.
RECEIVE_FREQ_4 - org.orekit.files.ccsds.Keyword
Received frequency 4.
RECEIVE_FREQ_5 - org.orekit.files.ccsds.Keyword
Received frequency 5.
ReceiverAntenna - Class in org.orekit.gnss.antenna
GNSS receiver antenna model.
ReceiverAntenna(String, String, Map<Frequency, FrequencyPattern>, String) - Constructor for class org.orekit.gnss.antenna.ReceiverAntenna
Simple constructor.
RecordAndContinue<T extends EventDetector> - Class in org.orekit.propagation.events.handlers
Handler that will record every time an event occurs and always return EventHandler.Action.CONTINUE.
RecordAndContinue() - Constructor for class org.orekit.propagation.events.handlers.RecordAndContinue
Create a new handler using an ArrayList to store events.
RecordAndContinue(List<RecordAndContinue.Event<T>>) - Constructor for class org.orekit.propagation.events.handlers.RecordAndContinue
Create a handler using the given collection to store events.
RecordAndContinue.Event<T> - Class in org.orekit.propagation.events.handlers
A single event detected during propagation.
REF_FRAME - org.orekit.files.ccsds.Keyword
Name of the reference frame in which the state vector and optional Keplerian element data are given.
REF_FRAME_EPOCH - org.orekit.files.ccsds.Keyword
Epoch of reference frame, if not intrinsic to the definition of the reference frame.
REFERENCE_FRAME - org.orekit.files.ccsds.Keyword
Reference frame in which data are given: used in combination with ANGLE_TYPE=RADEC.
referenceDateChanged(AbsoluteDate, ParameterDriver) - Method in interface org.orekit.utils.ParameterObserver
Notify that a parameter reference date has been changed.
ReferenceEllipsoid - Class in org.orekit.models.earth
A Reference Ellipsoid for use in geodesy.
ReferenceEllipsoid(double, double, Frame, double, double) - Constructor for class org.orekit.models.earth.ReferenceEllipsoid
Creates a new geodetic Reference Ellipsoid from four defining parameters.
referenceValueChanged(double, ParameterDriver) - Method in interface org.orekit.utils.ParameterObserver
Notify that a parameter reference value has been changed.
REFLECTION_COEFFICIENT - Static variable in interface org.orekit.forces.radiation.RadiationSensitive
Parameter name for reflection coefficient.
registerAttitudeProvider(AttitudeProvider) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution
Register an attitude provider.
registerAttitudeProvider(AttitudeProvider) - Method in interface org.orekit.propagation.semianalytical.dsst.forces.DSSTForceModel
Register an attitude provider.
registerAttitudeProvider(AttitudeProvider) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseral
Register an attitude provider.
registerAttitudeProvider(AttitudeProvider) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBody
Register an attitude provider.
registerAttitudeProvider(AttitudeProvider) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonal
Register an attitude provider.
registerSwitchEvents(Field<T>, FieldPropagator<T>) - Method in class org.orekit.attitudes.AttitudesSequence
Register all wrapped switch events to the propagator.
registerSwitchEvents(Propagator) - Method in class org.orekit.attitudes.AttitudesSequence
Register all wrapped switch events to the propagator.
reinitializeBegin(FieldOrekitStepInterpolator<T>) - Method in class org.orekit.propagation.events.FieldEventState
Reinitialize the beginning of the step.
reinitializeBegin(OrekitStepInterpolator) - Method in class org.orekit.propagation.events.EventState
Reinitialize the beginning of the step.
REJECTED - org.orekit.estimation.measurements.EstimatedMeasurement.Status
Status for rejected measurements.
Relativity - Class in org.orekit.forces.gravity
Post-Newtonian correction force due to general relativity.
Relativity(double) - Constructor for class org.orekit.forces.gravity.Relativity
Create a force model to add post-Newtonian acceleration corrections to an Earth orbit.
removeForceModels() - Method in class org.orekit.propagation.numerical.FieldNumericalPropagator
Remove all perturbing force models from the global perturbation model.
removeForceModels() - Method in class org.orekit.propagation.numerical.NumericalPropagator
Remove all force models (except central attraction).
removeForceModels() - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator
Remove all perturbing force models from the global perturbation model.
removeObserver(ParameterObserver) - Method in class org.orekit.utils.ParameterDriver
Remove an observer.
removeProvider(DataProvider) - Method in class org.orekit.data.DataProvidersManager
Remove one provider.
requiresDenseOutput() - Method in class org.orekit.propagation.sampling.FieldOrekitStepNormalizer
Determines whether this handler needs dense output.
requiresDenseOutput() - Method in class org.orekit.propagation.sampling.OrekitStepNormalizer
Determines whether this handler needs dense output.
rescale(double, boolean, double[][], double[][], boolean, double[][], double[][]) - Static method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
Rescale coefficients arrays.
RESET_DERIVATIVES - org.orekit.propagation.events.handlers.EventHandler.Action
Reset derivatives indicator.
RESET_DERIVATIVES - org.orekit.propagation.events.handlers.FieldEventHandler.Action
Reset derivatives indicator.
RESET_STATE - org.orekit.propagation.events.handlers.EventHandler.Action
Reset state indicator.
RESET_STATE - org.orekit.propagation.events.handlers.FieldEventHandler.Action
Reset state indicator.
resetActiveProvider(AttitudeProvider) - Method in class org.orekit.attitudes.AttitudesSequence
Reset the active provider.
resetFitting(AbsoluteDate, double...) - Method in class org.orekit.utils.SecularAndHarmonic
Reset fitting.
resetInitialState(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.analytical.FieldEcksteinHechlerPropagator
Reset the propagator initial state.
resetInitialState(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.analytical.FieldKeplerianPropagator
Reset the propagator initial state.
resetInitialState(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.FieldAbstractPropagator
Reset the propagator initial state.
resetInitialState(FieldSpacecraftState<T>) - Method in interface org.orekit.propagation.FieldPropagator
Reset the propagator initial state.
resetInitialState(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.integration.FieldIntegratedEphemeris
Reset the propagator initial state.
resetInitialState(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.numerical.FieldNumericalPropagator
Reset the propagator initial state.
resetInitialState(SpacecraftState) - Method in class org.orekit.propagation.AbstractPropagator
Reset the propagator initial state.
resetInitialState(SpacecraftState) - Method in class org.orekit.propagation.analytical.AdapterPropagator
Reset the propagator initial state.
resetInitialState(SpacecraftState) - Method in class org.orekit.propagation.analytical.AggregateBoundedPropagator
 
resetInitialState(SpacecraftState) - Method in class org.orekit.propagation.analytical.EcksteinHechlerPropagator
Reset the propagator initial state.
resetInitialState(SpacecraftState) - Method in class org.orekit.propagation.analytical.Ephemeris
Try (and fail) to reset the initial state.
resetInitialState(SpacecraftState) - Method in class org.orekit.propagation.analytical.gnss.GPSPropagator
Reset the propagator initial state.
resetInitialState(SpacecraftState) - Method in class org.orekit.propagation.analytical.KeplerianPropagator
Reset the propagator initial state.
resetInitialState(SpacecraftState) - Method in class org.orekit.propagation.analytical.tle.TLEPropagator
Reset the propagator initial state.
resetInitialState(SpacecraftState) - Method in class org.orekit.propagation.integration.IntegratedEphemeris
Reset the propagator initial state.
resetInitialState(SpacecraftState) - Method in class org.orekit.propagation.numerical.NumericalPropagator
Reset the propagator initial state.
resetInitialState(SpacecraftState) - Method in interface org.orekit.propagation.Propagator
Reset the propagator initial state.
resetInitialState(SpacecraftState) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator
Reset the initial state.
resetIntermediateState(FieldSpacecraftState<T>, boolean) - Method in class org.orekit.propagation.analytical.FieldAbstractAnalyticalPropagator
Reset an intermediate state.
resetIntermediateState(FieldSpacecraftState<T>, boolean) - Method in class org.orekit.propagation.analytical.FieldEcksteinHechlerPropagator
Reset an intermediate state.
resetIntermediateState(FieldSpacecraftState<T>, boolean) - Method in class org.orekit.propagation.analytical.FieldKeplerianPropagator
Reset an intermediate state.
resetIntermediateState(FieldSpacecraftState<T>, boolean) - Method in class org.orekit.propagation.integration.FieldIntegratedEphemeris
Reset an intermediate state.
resetIntermediateState(SpacecraftState, boolean) - Method in class org.orekit.propagation.analytical.AbstractAnalyticalPropagator
Reset an intermediate state.
resetIntermediateState(SpacecraftState, boolean) - Method in class org.orekit.propagation.analytical.AdapterPropagator
Reset an intermediate state.
resetIntermediateState(SpacecraftState, boolean) - Method in class org.orekit.propagation.analytical.AggregateBoundedPropagator
 
resetIntermediateState(SpacecraftState, boolean) - Method in class org.orekit.propagation.analytical.EcksteinHechlerPropagator
Reset an intermediate state.
resetIntermediateState(SpacecraftState, boolean) - Method in class org.orekit.propagation.analytical.Ephemeris
Reset an intermediate state.
resetIntermediateState(SpacecraftState, boolean) - Method in class org.orekit.propagation.analytical.gnss.GPSPropagator
Reset an intermediate state.
resetIntermediateState(SpacecraftState, boolean) - Method in class org.orekit.propagation.analytical.KeplerianPropagator
Reset an intermediate state.
resetIntermediateState(SpacecraftState, boolean) - Method in class org.orekit.propagation.analytical.tle.TLEPropagator
Reset an intermediate state.
resetIntermediateState(SpacecraftState, boolean) - Method in class org.orekit.propagation.integration.IntegratedEphemeris
Reset an intermediate state.
resetOrbit(Orbit) - Method in class org.orekit.propagation.conversion.AbstractPropagatorBuilder
Reset the orbit in the propagator builder.
resetState(KK, FieldSpacecraftState<T>) - Method in interface org.orekit.propagation.events.handlers.FieldEventHandler
Reset the state prior to continue propagation.
resetState(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.events.FieldAbstractDetector
Reset the state prior to continue propagation.
resetState(FieldSpacecraftState<T>) - Method in interface org.orekit.propagation.events.FieldEventDetector
Reset the state prior to continue propagation.
resetState(SpacecraftState) - Method in class org.orekit.propagation.events.AbstractDetector
Reset the state prior to continue propagation.
resetState(SpacecraftState) - Method in class org.orekit.propagation.events.AdapterDetector
Reset the state prior to continue propagation.
resetState(SpacecraftState) - Method in interface org.orekit.propagation.events.EventDetector
Reset the state prior to continue propagation.
resetState(T, SpacecraftState) - Method in interface org.orekit.propagation.events.handlers.EventHandler
Reset the state prior to continue propagation.
resetState(T, SpacecraftState) - Method in class org.orekit.propagation.events.handlers.RecordAndContinue
 
restrictStep(SpacecraftState, SpacecraftState) - Method in interface org.orekit.propagation.sampling.OrekitStepInterpolator
Create a new restricted version of the instance.
REV_AT_EPOCH - org.orekit.files.ccsds.Keyword
Revolution Number.
revert() - Method in class org.orekit.utils.AngularCoordinates
Revert a rotation/rotation rate/ rotation acceleration triplet.
revert() - Method in class org.orekit.utils.FieldAngularCoordinates
Revert a rotation / rotation rate / rotation acceleration triplet.
revert() - Method in class org.orekit.utils.TimeStampedAngularCoordinates
Revert a rotation/rotation rate pair.
revert() - Method in class org.orekit.utils.TimeStampedFieldAngularCoordinates
Revert a rotation/rotation rate pair.
RHUMIDITY - org.orekit.files.ccsds.Keyword
Data: Relative humidity [%].
RinexHeader - Class in org.orekit.gnss
Container for Rinex file header.
RinexHeader(double, SatelliteSystem, String, String, String, String, String, String, String, String, String, String, Vector3D, double, Vector2D, Vector3D, String, Vector3D, Vector3D, double, Vector3D, Vector3D, String, double, AbsoluteDate, AbsoluteDate, int, List<RinexLoader.Parser.AppliedDCBS>, List<RinexLoader.Parser.AppliedPCVS>, List<RinexLoader.Parser.PhaseShiftCorrection>, int, int, int, int) - Constructor for class org.orekit.gnss.RinexHeader
Simple constructor, for Rinex 3 Header.
RinexHeader(double, SatelliteSystem, String, String, String, String, String, String, String, String, String, String, Vector3D, double, Vector2D, Vector3D, Vector3D, Vector3D, double, AbsoluteDate, AbsoluteDate, int, int) - Constructor for class org.orekit.gnss.RinexHeader
Simple constructor, for Rinex 2 Header.
RinexLoader - Class in org.orekit.gnss
Loader for Rinex measurements files.
RinexLoader(InputStream, String) - Constructor for class org.orekit.gnss.RinexLoader
Simple constructor.
RinexLoader(String) - Constructor for class org.orekit.gnss.RinexLoader
Simple constructor.
RinexLoader.Parser - Class in org.orekit.gnss
Parser for rinex files.
RinexLoader.Parser.AppliedDCBS - Class in org.orekit.gnss
Corrections of Differential Code Biases (DCBs) applied.
RinexLoader.Parser.AppliedPCVS - Class in org.orekit.gnss
Corrections of antenna phase center variations (PCVs) applied.
RinexLoader.Parser.PhaseShiftCorrection - Class in org.orekit.gnss
Phase Shift corrections.
RinexLoader.Parser.ScaleFactorCorrection - Class in org.orekit.gnss
Scale Factor to be applied.
rotationFromInertial(Field<T>, FieldPVCoordinates<T>) - Method in enum org.orekit.frames.LOFType
Get the rotation from inertial frame to local orbital frame.
rotationFromInertial(PVCoordinates) - Method in enum org.orekit.frames.LOFType
Get the rotation from inertial frame to local orbital frame.
RSW - org.orekit.files.ccsds.CCSDSFrame
Another name for Radial, Transverse (along-track) and Normal.
RTN - org.orekit.files.ccsds.CCSDSFrame
Radial, Transverse (along-track) and Normal.

S

S01 - org.orekit.gnss.Frequency
SBAS L1 (1575.42 MHz).
S05 - org.orekit.gnss.Frequency
SBAS L5 (1176.45 MHz).
S1 - org.orekit.gnss.ObservationType
Doppler GPS L1 / GLONASS G1 / Galileo E2-L1-E1 / SBAS L1 for Rinex2.
S1A - org.orekit.gnss.ObservationType
Signal-strength Galileo E1 A for Rinex3.
S1B - org.orekit.gnss.ObservationType
Signal-strength Galileo E1 I/NAV OS/CS/SoL for Rinex3.
S1C - org.orekit.gnss.ObservationType
Signal-strength GPS L1 C/A / GLONASS G1 C/A / Galileo E1 C / SBAS L1 C/A / QZSS L1 C/A for Rinex3.
S1I - org.orekit.gnss.ObservationType
Signal-strength Beidou B1 I for Rinex3.
S1L - org.orekit.gnss.ObservationType
Signal-strength GPS L1 L1C(P) / QZSS L1 L1C(P) for Rinex3.
S1M - org.orekit.gnss.ObservationType
Signal-strength GPS L2 M for Rinex3.
S1N - org.orekit.gnss.ObservationType
Signal-strength GPS L1 codeless for Rinex3.
S1P - org.orekit.gnss.ObservationType
Signal-strength GPS L2 P(AS off) / GLONASS G2 P for Rinex3.
S1S - org.orekit.gnss.ObservationType
Signal-strength GPS L1 L1C(D) / QZSS L1 L1C(D) for Rinex3.
S1W - org.orekit.gnss.ObservationType
Signal-strength GPS L1 Z-tracking and similar (AS on) for Rinex3.
S1X - org.orekit.gnss.ObservationType
Signal-strength GPS L1 L1C (D+P) / Galileo E1 B+C / QZSS L1 L1C(D+P) for Rinex3.
S1Y - org.orekit.gnss.ObservationType
Signal-strength GPS L1 Y for Rinex3.
S1Z - org.orekit.gnss.ObservationType
Signal-strength Galileo E1 C1Z A+B+C / QZSS L1 L1-SAIF for Rinex3.
S2 - org.orekit.gnss.ObservationType
Signal Strength GPS L2 / GLONASS G2 / Beidou B02 for Rinex2.
S2 - Static variable in class org.orekit.models.earth.displacement.Tide
S₂ tide.
S2C - org.orekit.gnss.ObservationType
Signal-strength GPS L2 C/A / GLONASS G2 C/A for Rinex3.
S2D - org.orekit.gnss.ObservationType
Signal-strength GPS L1(C/A)+(P2-P1) (semi-codeless) for Rinex3.
S2I - org.orekit.gnss.ObservationType
Signal-strength Beidou B1 I for Rinex3.03.
S2L - org.orekit.gnss.ObservationType
Signal-strength GPS L2 L2C(L) / QZSS L2 L2C(2) for Rinex3.
S2M - org.orekit.gnss.ObservationType
Signal-strength GPS L2 M for Rinex3.
S2N - org.orekit.gnss.ObservationType
Signal-strength GPS L2 codeless for Rinex3.
S2P - org.orekit.gnss.ObservationType
Signal-strength GPS L2 P(AS off) / GLONASS G2 P for Rinex3.
S2Q - org.orekit.gnss.ObservationType
Signal-strength Beidou B1 Q for Rinex3.03.
S2S - org.orekit.gnss.ObservationType
Signal-strength GPS L2 L2C(M) / QZSS L2 L2C(M) for Rinex3.
S2W - org.orekit.gnss.ObservationType
Signal-strength GPS L2 Z-tracking and similar (AS on) for Rinex3.
S2X - org.orekit.gnss.ObservationType
Signal-strength GPS L2 L2C (M+L) / QZSS L2 L2C(M+L) for Rinex3.
S2Y - org.orekit.gnss.ObservationType
Signal-strength GPS L2 Y for Rinex3.
S3I - org.orekit.gnss.ObservationType
Signal-strength GLONASS G3 I for Rinex3.
S3Q - org.orekit.gnss.ObservationType
Signal-strength GLONASS G3 Q for Rinex3.
S3X - org.orekit.gnss.ObservationType
Signal-strength GLONASS G3 I+Q for Rinex3.
s4 - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator
s* new value for the contant s.
S5 - org.orekit.gnss.ObservationType
Signal Strength GPS L5 / Galileo E5a / SBAS L5 for Rinex2.
S5A - org.orekit.gnss.ObservationType
Signal-strength IRNSS L5 A for Rinex3.
S5B - org.orekit.gnss.ObservationType
Signal-strength IRNSS L5 B for Rinex3.
S5C - org.orekit.gnss.ObservationType
Signal-strength IRNSS L5 C for Rinex3.
S5I - org.orekit.gnss.ObservationType
Signal-strength GPS L5 I/ Galileo E5a F/NAV OS / SBAS L5 I / QZSS L5 I for Rinex3.
S5Q - org.orekit.gnss.ObservationType
Signal-strength GPS L5 Q/ Galileo E5a Q / SBAS L5 Q / QZSS L5 Q for Rinex3.
S5X - org.orekit.gnss.ObservationType
Signal-strength GPS L5 I+Q/ Galileo E5a I+Q / SBAS L5 I+Q / QZSS L5 I+Q / IRNSS L5 B+C for Rinex3.
S6 - org.orekit.gnss.ObservationType
Signal Strength Galileo E6 / Beidou B03 for Rinex2.
S6A - org.orekit.gnss.ObservationType
Signal-strength Galileo E6 A PRS for Rinex3.
S6B - org.orekit.gnss.ObservationType
Signal-strength Galileo E6 B C/NAV CS for Rinex3.
S6C - org.orekit.gnss.ObservationType
Signal-strength Galileo E6 C no data for Rinex3.
S6I - org.orekit.gnss.ObservationType
Signal-strength Beidou B3 I for Rinex3.
S6L - org.orekit.gnss.ObservationType
Signal-strength QZSS LEX(6) L for Rinex3.
S6Q - org.orekit.gnss.ObservationType
Signal-strength Beidou B3 Q for Rinex3.
S6S - org.orekit.gnss.ObservationType
Signal-strength QZSS LEX(6) S for Rinex3.
S6X - org.orekit.gnss.ObservationType
Signal-strength Galileo E6 B+C / QZSS LEX(6) S+L / Beidou B3 I+Q for Rinex3.
S6Z - org.orekit.gnss.ObservationType
Signal-strength Galileo E6 A+B+C for Rinex3.
S7 - org.orekit.gnss.ObservationType
Signal Strength Galileo E5b / Beidou B02 for Rinex2.
S7I - org.orekit.gnss.ObservationType
Signal-strength Galileo E5b I I/NAV OS/CS/SoL / Beidou B2 I for Rinex3.
S7Q - org.orekit.gnss.ObservationType
Signal-strength Galileo Q no data / Beidou B2 Q for Rinex3.
S7X - org.orekit.gnss.ObservationType
Signal-strength Galileo E5b I+Q / Beidou B2 I+Q for Rinex3.
S8 - org.orekit.gnss.ObservationType
Signal Strength Galileo E5a+b for Rinex2.
S8I - org.orekit.gnss.ObservationType
Signal-strength Galileo E5(E5a+E5b) I for Rinex3.
S8Q - org.orekit.gnss.ObservationType
Signal-strength Galileo E5(E5a+E5b) Q for Rinex3.
S8X - org.orekit.gnss.ObservationType
Signal-strength Galileo E5(E5a+E5b) I+Q for Rinex3.
S9A - org.orekit.gnss.ObservationType
Signal-strength IRNSS S A for Rinex3.
S9B - org.orekit.gnss.ObservationType
Signal-strength IRNSS S B for Rinex3.
S9C - org.orekit.gnss.ObservationType
Signal-strength IRNSS S C for Rinex3.
S9X - org.orekit.gnss.ObservationType
Signal-strength IRNSS S B+C for Rinex3.
SA - org.orekit.gnss.ObservationType
Signal-strength GPS L1 C/A / GLONASS G1 C/A for Rinex2.
SaastamoinenModel - Class in org.orekit.models.earth
The modified Saastamoinen model.
SaastamoinenModel(double, double, double, String) - Constructor for class org.orekit.models.earth.SaastamoinenModel
Create a new Saastamoinen model for the troposphere using the given environmental conditions.
sample(SphericalPolygonsSet, double, double) - Method in class org.orekit.models.earth.tessellation.EllipsoidTessellator
Sample a zone of interest into a grid sample of geodetic points.
SATELLITE_COLLIDED_WITH_TARGET - org.orekit.errors.OrekitMessages
 
SatelliteAntenna - Class in org.orekit.gnss.antenna
GNSS satellite antenna model.
SatelliteAntenna(String, String, Map<Frequency, FrequencyPattern>, SatelliteSystem, int, int, String, AbsoluteDate, AbsoluteDate) - Constructor for class org.orekit.gnss.antenna.SatelliteAntenna
SatelliteAntenna(String, String, Map<Frequency, FrequencyPattern>, SatelliteSystem, int, SatelliteType, int, String, AbsoluteDate, AbsoluteDate) - Constructor for class org.orekit.gnss.antenna.SatelliteAntenna
Simple constructor.
SatelliteAntennaCode - Enum in org.orekit.gnss.antenna
Deprecated.
as of 9.3 replaced by SatelliteType
SatelliteSystem - Enum in org.orekit.gnss
Enumerate for satellite system.
SatelliteType - Enum in org.orekit.gnss.antenna
Enumerate for satellite types.
SATURN - org.orekit.bodies.JPLEphemeridesLoader.EphemerisType
Constant for Saturn.
SATURN - org.orekit.files.ccsds.CenterName
Saturn body.
SATURN - Static variable in class org.orekit.bodies.CelestialBodyFactory
Predefined name for Saturn.
SB - org.orekit.gnss.ObservationType
Signal-strength GPS L1C for Rinex2.
SBAS - org.orekit.gnss.SatelliteSystem
SBAS system.
SC - org.orekit.gnss.ObservationType
Signal-strength GPS L2C for Rinex2.
scale(double, Orbit) - Method in enum org.orekit.orbits.OrbitType
Compute scaling factor for parameters drivers.
scaleChanged(double, ParameterDriver) - Method in interface org.orekit.utils.ParameterObserver
Notify that a parameter scale has been changed.
Scheduler<T extends ObservedMeasurement<T>> - Interface in org.orekit.estimation.measurements.generation
Interface for generating measurements sequences.
SCLK - org.orekit.files.ccsds.CcsdsTimeScale
Spacecraft Clock.
SD - org.orekit.gnss.ObservationType
Signal-strength GLONASS G2 for Rinex2.
SDP4 - Static variable in class org.orekit.propagation.analytical.tle.TLE
Identifier for SDP4 type of ephemeris.
SDP8 - Static variable in class org.orekit.propagation.analytical.tle.TLE
Identifier for SDP8 type of ephemeris.
SecularAndHarmonic - Class in org.orekit.utils
Class for fitting evolution of osculating orbital parameters.
SecularAndHarmonic(int, double...) - Constructor for class org.orekit.utils.SecularAndHarmonic
Simple constructor.
segment - org.orekit.files.ccsds.Keyword
Segment keyword.
selectDates(AbsoluteDate, AbsoluteDate) - Method in class org.orekit.time.BurstSelector
Select dates within an interval.
selectDates(AbsoluteDate, AbsoluteDate) - Method in interface org.orekit.time.DatesSelector
Select dates within an interval.
selectDates(AbsoluteDate, AbsoluteDate) - Method in class org.orekit.time.FixedStepSelector
Select dates within an interval.
selectExtrapolator(TLE) - Static method in class org.orekit.propagation.analytical.tle.TLEPropagator
Selects the extrapolator to use with the selected TLE.
selectExtrapolator(TLE, AttitudeProvider, double) - Static method in class org.orekit.propagation.analytical.tle.TLEPropagator
Selects the extrapolator to use with the selected TLE.
selectionChanged(boolean, ParameterDriver) - Method in interface org.orekit.utils.ParameterObserver
Notify that a parameter selection status has been changed.
selectTransformer(Transformer, double, boolean) - Method in enum org.orekit.propagation.events.FilterType
Get next function transformer in the specified direction.
SEMI_MAJOR_AXIS - org.orekit.files.ccsds.Keyword
Orbit semi-major axis.
SEMParser - Class in org.orekit.gnss
This class reads SEM almanac files and provides GPS almanacs.
SEMParser(String) - Constructor for class org.orekit.gnss.SEMParser
Simple constructor.
SEPTEMBER - org.orekit.time.Month
September.
setAe(double) - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
Set the central body reference radius.
setAngleType(String) - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData
Setter for the angleType.
setAngularThreshold(double) - Method in class org.orekit.bodies.OneAxisEllipsoid
Set the angular convergence threshold.
setAttitudeProvider(AttitudeProvider) - Method in class org.orekit.propagation.AbstractPropagator
Set attitude provider.
setAttitudeProvider(AttitudeProvider) - Method in class org.orekit.propagation.conversion.NumericalPropagatorBuilder
Set the attitude provider.
setAttitudeProvider(AttitudeProvider) - Method in class org.orekit.propagation.FieldAbstractPropagator
Set attitude provider.
setAttitudeProvider(AttitudeProvider) - Method in interface org.orekit.propagation.FieldPropagator
Set attitude provider.
setAttitudeProvider(AttitudeProvider) - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
Set attitude provider.
setAttitudeProvider(AttitudeProvider) - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator
Set attitude provider.
setAttitudeProvider(AttitudeProvider) - Method in interface org.orekit.propagation.Propagator
Set attitude provider.
setAttitudeProvider(AttitudeProvider) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator
Set attitude provider.
setCacheSlotsNumber(int) - Static method in class org.orekit.utils.OrekitConfiguration
Set the number of slots to use in caches.
setComment(List<String>) - Method in class org.orekit.files.ccsds.OPMFile.Maneuver
Set the maneuvers data comment, each string in the list corresponds to one line of comment.
setComment(List<String>) - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData
Set the meta-data comment.
setCorrectionAngle1(double) - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData
Setter for the correctionAngle1.
setCorrectionAngle2(double) - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData
Setter for the correctionAngle2.
setCorrectionDoppler(double) - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData
Setter for the correctionDoppler.
setCorrectionRange(double) - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData
Setter for the correctionRange.
setCorrectionReceive(double) - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData
Setter for the correctionReceive.
setCorrectionsApplied(String) - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData
Setter for the correctionApplied.
setCorrectionTransmit(double) - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData
Setter for the correctionTransmit.
setCreationDate(AbsoluteDate) - Method in class org.orekit.files.ccsds.TDMFile
Set the file creation date and time in UTC.
setCurrentWeight(double...) - Method in class org.orekit.estimation.measurements.EstimatedMeasurement
Deprecated.
as of 9.2, weight should not be changed anymore, rejected measurements are identified by their status
setDataQuality(String) - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData
Setter for the dataQuality.
setDeltaMass(double) - Method in class org.orekit.files.ccsds.OPMFile.Maneuver
Set mass change during maneuver (value is < 0).
setDuration(double) - Method in class org.orekit.files.ccsds.OPMFile.Maneuver
Set duration (value is 0 for impulsive maneuver).
setdV(Vector3D) - Method in class org.orekit.files.ccsds.OPMFile.Maneuver
Set velocity increment.
setElem(int, int, PolynomialFunction) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.PolynomialFunctionMatrix
Set an element of the matrix.
setEnabled(boolean) - Method in class org.orekit.estimation.measurements.AbstractMeasurement
Enable or disable a measurement.
setEnabled(boolean) - Method in interface org.orekit.estimation.measurements.ObservedMeasurement
Enable or disable a measurement.
setEOPContinuityThreshold(double) - Static method in class org.orekit.frames.FramesFactory
Set the threshold to check EOP continuity.
setEphemerisMode() - Method in class org.orekit.propagation.AbstractPropagator
Set the propagator to ephemeris generation mode.
setEphemerisMode() - Method in class org.orekit.propagation.FieldAbstractPropagator
Set the propagator to ephemeris generation mode.
setEphemerisMode() - Method in interface org.orekit.propagation.FieldPropagator
Set the propagator to ephemeris generation mode.
setEphemerisMode() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
Set the propagator to ephemeris generation mode.
setEphemerisMode() - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator
Set the propagator to ephemeris generation mode.
setEphemerisMode() - Method in interface org.orekit.propagation.Propagator
Set the propagator to ephemeris generation mode.
setEphemerisMode(OrekitStepHandler) - Method in class org.orekit.propagation.AbstractPropagator
Set the propagator to ephemeris generation mode with the specified handler for each integration step.
setEphemerisMode(OrekitStepHandler) - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
Set the propagator to ephemeris generation mode with the specified handler for each integration step.
setEphemerisMode(OrekitStepHandler) - Method in interface org.orekit.propagation.Propagator
Set the propagator to ephemeris generation mode with the specified handler for each integration step.
setEpoch(AbsoluteDate) - Method in class org.orekit.files.ccsds.TDMFile.Observation
Setter for the epoch.
setEstimatedValue(double...) - Method in class org.orekit.estimation.measurements.EstimatedMeasurement
Set the estimated value.
setFormatVersion(double) - Method in class org.orekit.files.ccsds.TDMFile
Set the CCSDS ODM (OPM, OMM or OEM) format version.
setFreqOffset(double) - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData
Setter for the freqOffset.
setHeaderComment(List<String>) - Method in class org.orekit.files.ccsds.TDMFile
Set the header comment.
setInitialJacobians(SpacecraftState) - Method in class org.orekit.propagation.numerical.PartialDerivativesEquations
Set the initial value of the Jacobian with respect to state and parameter.
setInitialJacobians(SpacecraftState, double[][], double[][]) - Method in class org.orekit.propagation.numerical.PartialDerivativesEquations
Set the initial value of the Jacobian with respect to state and parameter.
setInitialJacobians(SpacecraftState, int) - Method in class org.orekit.propagation.numerical.PartialDerivativesEquations
setInitialState(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.numerical.FieldNumericalPropagator
Set the initial state.
setInitialState(SpacecraftState) - Method in class org.orekit.propagation.numerical.NumericalPropagator
Set the initial state.
setInitialState(SpacecraftState) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator
Set the initial state with osculating orbital elements.
setInitialState(SpacecraftState, boolean) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator
Set the initial state.
setIntegrationInterval(double) - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData
Setter for the integrationInterval.
setIntegrationRef(String) - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData
Setter for the integrationRef.
setInterpolationGridToFixedNumberOfPoints(int) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator
Set the interpolation grid generator.
setInterpolationGridToMaxTimeGap(double) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator
Set the interpolation grid generator.
setKeyword(String) - Method in class org.orekit.files.ccsds.TDMFile.Observation
Setter for the keyword.
setMainFieldCoefficients(int, int, double, double) - Method in class org.orekit.models.earth.GeoMagneticField
Set the given main field coefficients.
setMass(double) - Method in class org.orekit.propagation.conversion.NumericalPropagatorBuilder
Set the initial mass.
setMasterMode(double, OrekitFixedStepHandler) - Method in class org.orekit.propagation.AbstractPropagator
Set the propagator to master mode with fixed steps.
setMasterMode(double, OrekitFixedStepHandler) - Method in interface org.orekit.propagation.Propagator
Set the propagator to master mode with fixed steps.
setMasterMode(FieldOrekitStepHandler<T>) - Method in class org.orekit.propagation.FieldAbstractPropagator
Set the propagator to master mode with variable steps.
setMasterMode(FieldOrekitStepHandler<T>) - Method in interface org.orekit.propagation.FieldPropagator
Set the propagator to master mode with variable steps.
setMasterMode(FieldOrekitStepHandler<T>) - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator
Set the propagator to master mode with variable steps.
setMasterMode(OrekitStepHandler) - Method in class org.orekit.propagation.AbstractPropagator
Set the propagator to master mode with variable steps.
setMasterMode(OrekitStepHandler) - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
Set the propagator to master mode with variable steps.
setMasterMode(OrekitStepHandler) - Method in interface org.orekit.propagation.Propagator
Set the propagator to master mode with variable steps.
setMasterMode(T, FieldOrekitFixedStepHandler<T>) - Method in class org.orekit.propagation.FieldAbstractPropagator
Set the propagator to master mode with fixed steps.
setMasterMode(T, FieldOrekitFixedStepHandler<T>) - Method in interface org.orekit.propagation.FieldPropagator
Set the propagator to master mode with fixed steps.
setMatrix(PolynomialFunction[][]) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.PolynomialFunctionMatrix
Set values for all elements.
setMatrixLine(int, PolynomialFunction[]) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.PolynomialFunctionMatrix
Set the value of a line of the matrix.
setMaxEvaluations(int) - Method in class org.orekit.estimation.leastsquares.BatchLSEstimator
Set the maximum number of model evaluations.
setMaxIterations(int) - Method in class org.orekit.estimation.leastsquares.BatchLSEstimator
Set the maximum number of iterations.
setMaxParseDegree(int) - Method in class org.orekit.forces.gravity.potential.OceanTidesReader
Set the degree limit for the next file parsing.
setMaxParseDegree(int) - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
Set the degree limit for the next file parsing.
setMaxParseOrder(int) - Method in class org.orekit.forces.gravity.potential.OceanTidesReader
Set the order limit for the next file parsing.
setMaxParseOrder(int) - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
Set the order limit for the next file parsing.
setMaxValue(double) - Method in class org.orekit.utils.ParameterDriver
Set maximum parameter value.
setMeasurement(double) - Method in class org.orekit.files.ccsds.TDMFile.Observation
Setter for the measurement.
setMetaData(TDMFile.TDMMetaData) - Method in class org.orekit.files.ccsds.TDMFile.ObservationsBlock
Set the meta-data for the block.
setMinValue(double) - Method in class org.orekit.utils.ParameterDriver
Set minimum parameter value.
setMode(String) - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData
Setter for the mode.
setMu(double) - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
Set the central body attraction coefficient.
setMu(double) - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
Set the central attraction coefficient μ.
setMu(double) - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator
Set the central attraction coefficient μ.
setMu(double) - Method in class org.orekit.propagation.numerical.FieldNumericalPropagator
Set the central attraction coefficient μ.
setMu(double) - Method in class org.orekit.propagation.numerical.NumericalPropagator
Set the central attraction coefficient μ.
setMuUsed() - Method in class org.orekit.files.ccsds.ODMFile
Set the gravitational coefficient created from the knowledge of the central body.
setName(String) - Method in class org.orekit.utils.ParameterDriver
Change the name of this parameter driver.
setNormalizedValue(double) - Method in class org.orekit.utils.ParameterDriver
Set normalized value.
setObservations(List<TDMFile.Observation>) - Method in class org.orekit.files.ccsds.TDMFile.ObservationsBlock
Set the list of Observations Data Lines.
setObservationsBlocks(List<TDMFile.ObservationsBlock>) - Method in class org.orekit.files.ccsds.TDMFile
Set the list of Observations Blocks.
setObservationsComment(List<String>) - Method in class org.orekit.files.ccsds.TDMFile.ObservationsBlock
Set the observations data lines comment.
setObserver(BatchLSObserver) - Method in class org.orekit.estimation.leastsquares.BatchLSEstimator
Set an observer for iterations.
setObserver(KalmanObserver) - Method in class org.orekit.estimation.sequential.KalmanEstimator
Set the observer.
setOrbitType(OrbitType) - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
Set propagation orbit type.
setOrbitType(OrbitType) - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator
Set propagation orbit type.
setOrbitType(OrbitType) - Method in class org.orekit.propagation.numerical.FieldNumericalPropagator
Set propagation orbit type.
setOrbitType(OrbitType) - Method in class org.orekit.propagation.numerical.NumericalPropagator
Set propagation orbit type.
setOriginator(String) - Method in class org.orekit.files.ccsds.TDMFile
Set the file originator.
setParameterDerivatives(ParameterDriver, double...) - Method in class org.orekit.estimation.measurements.EstimatedMeasurement
Set the partial derivatives of the simulated measurement with respect to parameter.
setParameters(double[]) - Method in class org.orekit.propagation.conversion.AbstractPropagatorBuilder
Set the selected parameters.
setParametersConvergenceThreshold(double) - Method in class org.orekit.estimation.leastsquares.BatchLSEstimator
Set convergence threshold.
setParticipants(Map<Integer, String>) - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData
Setter for the participants.
setPath(String) - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData
Setter for the path.
setPath1(String) - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData
Setter for the path1.
setPath2(String) - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData
Setter for the path2.
setPositionAngleType() - Method in class org.orekit.propagation.integration.FieldStateMapper
Set position angle type.
setPositionAngleType() - Method in class org.orekit.propagation.integration.StateMapper
Set position angle type.
setPositionAngleType(PositionAngle) - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
Set position angle type.
setPositionAngleType(PositionAngle) - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator
Set position angle type.
setPositionAngleType(PositionAngle) - Method in class org.orekit.propagation.numerical.FieldNumericalPropagator
Set position angle type.
setPositionAngleType(PositionAngle) - Method in class org.orekit.propagation.numerical.NumericalPropagator
Set position angle type.
setPressure(double) - Method in class org.orekit.models.earth.EarthStandardAtmosphereRefraction
Set the local pressure at the evaluation location
setRangeMode(String) - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData
Setter for the rangeMode.
setRangeModulus(double) - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData
Setter for the rangeModulus.
setRangeUnits(String) - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData
Setter for the rangeUnits.
setRawCoefficients(boolean, double[][], double[][], String) - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
Set the tesseral-sectorial coefficients matrix.
setReadComplete(boolean) - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
Set the indicator for completed read.
setReceiveBand(String) - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData
Setter for the receiveBand.
setReceiveDelays(Map<Integer, Double>) - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData
Setter for the receiveDelays.
setReferenceDate(AbsoluteDate) - Method in class org.orekit.utils.ParameterDriver
Set reference date.
setReferenceFrame(Frame) - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData
Set the reference frame in which data are given: used for RADEC tracking data.
setReferenceFrameString(String) - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData
Set the reference frame name.
setReferenceValue(double) - Method in class org.orekit.utils.ParameterDriver
Set reference parameter value.
setRefFrame(Frame) - Method in class org.orekit.files.ccsds.OPMFile.Maneuver
Set Coordinate system for velocity increment vector, for absolute frames.
setRefLofType(LOFType) - Method in class org.orekit.files.ccsds.OPMFile.Maneuver
Set coordinate system for velocity increment vector, for Local Orbital Frames.
setResetAtEnd(boolean) - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
Allow/disallow resetting the initial state at end of propagation.
setResetAtEnd(boolean) - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator
Allow/disallow resetting the initial state at end of propagation.
setRolloverReference(DateComponents) - Static method in class org.orekit.time.GPSDate
Set a reference date for ensuring continuity across GPS week rollover.
setSatelliteRevolution(int) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator
Override the default value of the parameter.
setScale(double) - Method in class org.orekit.utils.ParameterDriver
Set scale.
setSecularVariationCoefficients(int, int, double, double) - Method in class org.orekit.models.earth.GeoMagneticField
Set the given secular variation coefficients.
setSelected(boolean) - Method in class org.orekit.utils.ParameterDriver
Configure a parameter selection status.
setSelectedCoefficients(Set<String>) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator
Set the selected short periodic coefficients that must be stored as additional states.
setSigma(double[]) - Method in class org.orekit.estimation.measurements.modifiers.DynamicOutlierFilter
Set the current value of sigma.
setSlaveMode() - Method in class org.orekit.propagation.AbstractPropagator
Set the propagator to slave mode.
setSlaveMode() - Method in class org.orekit.propagation.FieldAbstractPropagator
Set the propagator to slave mode.
setSlaveMode() - Method in interface org.orekit.propagation.FieldPropagator
Set the propagator to slave mode.
setSlaveMode() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
Set the propagator to slave mode.
setSlaveMode() - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator
Set the propagator to slave mode.
setSlaveMode() - Method in interface org.orekit.propagation.Propagator
Set the propagator to slave mode.
setStartDate(AbsoluteDate) - Method in class org.orekit.propagation.AbstractPropagator
Set a start date.
setStartDate(FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.FieldAbstractPropagator
Set a start date.
setStartTime(AbsoluteDate) - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData
Setter for the startTime.
setStartTimeString(String) - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData
Setter for the startTime String.
setStateDerivatives(int, double[]...) - Method in class org.orekit.estimation.measurements.EstimatedMeasurement
Set the partial derivatives of the simulated measurement with respect to state Cartesian coordinates.
setStatus(EstimatedMeasurement.Status) - Method in class org.orekit.estimation.measurements.EstimatedMeasurement
Set the status.
setStopTime(AbsoluteDate) - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData
Setter for the stopTime.
setStopTimeString(String) - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData
Setter for the stopTime String.
setTemperature(double) - Method in class org.orekit.models.earth.EarthStandardAtmosphereRefraction
Set the local temperature at the evaluation location
setTideSystem(TideSystem) - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
Set the TideSystem used in the gravity field.
setTimeout(int) - Method in class org.orekit.data.NetworkCrawler
Set the timeout for connection.
setTimeSystem(CcsdsTimeScale) - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData
Set the Time System that: for OPM, is used for metadata, state vector, maneuver and covariance data, for OMM, is used for metadata, orbit state and covariance data, for OEM, is used for metadata, ephemeris and covariance data.
setTimetagRef(String) - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData
Setter for the timetagRef.
setTransmitBand(String) - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData
Setter for the transmitBand.
setTransmitDelays(Map<Integer, Double>) - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData
Setter for the transmitDelays.
setTurnaroundDenominator(int) - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData
Setter for the turnaroundDenominator.
setTurnaroundNumerator(int) - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData
Setter for the turnaroundNumerator.
setUpEventDetector(FieldODEIntegrator<T>, FieldEventDetector<T>) - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator
Wrap an Orekit event detector and register it to the integrator.
setUpEventDetector(ODEIntegrator, EventDetector) - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
Wrap an Orekit event detector and register it to the integrator.
setUpUserEventDetectors() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
Set up all user defined event detectors.
setUpUserEventDetectors() - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator
Set up all user defined event detectors.
setValue(double) - Method in class org.orekit.utils.ParameterDriver
Set parameter value.
SEVERAL_REFERENCE_DATES_IN_GRAVITY_FIELD - org.orekit.errors.OrekitMessages
 
SGP - Static variable in class org.orekit.propagation.analytical.tle.TLE
Identifier for SGP type of ephemeris.
SGP4 - Class in org.orekit.propagation.analytical.tle
This class contains methods to compute propagated coordinates with the SGP4 model.
SGP4 - Static variable in class org.orekit.propagation.analytical.tle.TLE
Identifier for SGP4 type of ephemeris.
SGP4(TLE, AttitudeProvider, double) - Constructor for class org.orekit.propagation.analytical.tle.SGP4
Constructor for a unique initial TLE.
SGP8 - Static variable in class org.orekit.propagation.analytical.tle.TLE
Identifier for SGP8 type of ephemeris.
shiftedBy(double) - Method in class org.orekit.attitudes.Attitude
Get a time-shifted attitude.
shiftedBy(double) - Method in class org.orekit.attitudes.FieldAttitude
Get a time-shifted attitude.
shiftedBy(double) - Method in class org.orekit.frames.FieldTransform
Get a time-shifted instance.
shiftedBy(double) - Method in class org.orekit.frames.Transform
Get a time-shifted instance.
shiftedBy(double) - Method in class org.orekit.orbits.CartesianOrbit
Get a time-shifted orbit.
shiftedBy(double) - Method in class org.orekit.orbits.CircularOrbit
Get a time-shifted orbit.
shiftedBy(double) - Method in class org.orekit.orbits.EquinoctialOrbit
Get a time-shifted orbit.
shiftedBy(double) - Method in class org.orekit.orbits.FieldCartesianOrbit
Get a time-shifted instance.
shiftedBy(double) - Method in class org.orekit.orbits.FieldCircularOrbit
Get a time-shifted instance.
shiftedBy(double) - Method in class org.orekit.orbits.FieldEquinoctialOrbit
Get a time-shifted instance.
shiftedBy(double) - Method in class org.orekit.orbits.FieldKeplerianOrbit
Get a time-shifted instance.
shiftedBy(double) - Method in class org.orekit.orbits.KeplerianOrbit
Get a time-shifted orbit.
shiftedBy(double) - Method in class org.orekit.orbits.Orbit
Get a time-shifted orbit.
shiftedBy(double) - Method in class org.orekit.propagation.FieldSpacecraftState
Get a time-shifted state.
shiftedBy(double) - Method in class org.orekit.propagation.SpacecraftState
Get a time-shifted state.
shiftedBy(double) - Method in class org.orekit.time.AbsoluteDate
Get a time-shifted date.
shiftedBy(double) - Method in class org.orekit.time.FieldAbsoluteDate
Get a time-shifted date.
shiftedBy(double) - Method in interface org.orekit.time.FieldTimeShiftable
Get a time-shifted instance.
shiftedBy(double) - Method in interface org.orekit.time.TimeShiftable
Get a time-shifted instance.
shiftedBy(double) - Method in class org.orekit.utils.AngularCoordinates
Get a time-shifted state.
shiftedBy(double) - Method in class org.orekit.utils.FieldAngularCoordinates
Get a time-shifted state.
shiftedBy(double) - Method in class org.orekit.utils.FieldPVCoordinates
Get a time-shifted state.
shiftedBy(double) - Method in class org.orekit.utils.PVCoordinates
Get a time-shifted state.
shiftedBy(double) - Method in class org.orekit.utils.TimeStampedAngularCoordinates
Get a time-shifted state.
shiftedBy(double) - Method in class org.orekit.utils.TimeStampedFieldAngularCoordinates
Get a time-shifted state.
shiftedBy(double) - Method in class org.orekit.utils.TimeStampedFieldPVCoordinates
Get a time-shifted state.
shiftedBy(double) - Method in class org.orekit.utils.TimeStampedPVCoordinates
Get a time-shifted state.
shiftedBy(KK) - Method in interface org.orekit.time.FieldTimeShiftable
Get a time-shifted instance.
shiftedBy(T) - Method in class org.orekit.attitudes.FieldAttitude
Get a time-shifted attitude.
shiftedBy(T) - Method in class org.orekit.frames.FieldTransform
Get a time-shifted instance.
shiftedBy(T) - Method in class org.orekit.orbits.FieldCartesianOrbit
Get a time-shifted orbit.
shiftedBy(T) - Method in class org.orekit.orbits.FieldCircularOrbit
Get a time-shifted orbit.
shiftedBy(T) - Method in class org.orekit.orbits.FieldEquinoctialOrbit
Get a time-shifted orbit.
shiftedBy(T) - Method in class org.orekit.orbits.FieldKeplerianOrbit
Get a time-shifted orbit.
shiftedBy(T) - Method in class org.orekit.orbits.FieldOrbit
Get a time-shifted orbit.
shiftedBy(T) - Method in class org.orekit.propagation.FieldSpacecraftState
Get a time-shifted state.
shiftedBy(T) - Method in class org.orekit.time.FieldAbsoluteDate
Get a time-shifted date.
shiftedBy(T) - Method in class org.orekit.utils.FieldAngularCoordinates
Get a time-shifted state.
shiftedBy(T) - Method in class org.orekit.utils.FieldPVCoordinates
Get a time-shifted state.
shiftedBy(T) - Method in class org.orekit.utils.TimeStampedFieldAngularCoordinates
Get a time-shifted state.
shiftedBy(T) - Method in class org.orekit.utils.TimeStampedFieldPVCoordinates
Get a time-shifted state.
ShiftingTransformProvider - Class in org.orekit.frames
Transform provider using thread-safe shifts on transforms sample.
ShiftingTransformProvider(TransformProvider, CartesianDerivativesFilter, AngularDerivativesFilter, int, double, int, double, double) - Constructor for class org.orekit.frames.ShiftingTransformProvider
Simple constructor.
ShiftingTransformProvider(TransformProvider, CartesianDerivativesFilter, AngularDerivativesFilter, AbsoluteDate, AbsoluteDate, int, double, int, double, double) - Constructor for class org.orekit.frames.ShiftingTransformProvider
SHM_FILENAME - Static variable in class org.orekit.forces.gravity.potential.GravityFieldFactory
Default regular expression for SHM files.
SHMFormatReader - Class in org.orekit.forces.gravity.potential
Reader for the SHM gravity field format.
SHMFormatReader(String, boolean) - Constructor for class org.orekit.forces.gravity.potential.SHMFormatReader
Simple constructor.
ShortPeriodicsInterpolatedCoefficient - Class in org.orekit.propagation.semianalytical.dsst.utilities
Interpolated short periodics coefficients.
ShortPeriodicsInterpolatedCoefficient(int) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.ShortPeriodicsInterpolatedCoefficient
Simple constructor.
ShortPeriodTerms - Interface in org.orekit.propagation.semianalytical.dsst.forces
Additive short period terms contributing to the mean to osculating orbit mapping.
SIGNAL_STRENGTH - org.orekit.gnss.MeasurementType
Signal-strength measurement.
signalTimeOfFlight(TimeStampedFieldPVCoordinates<T>, FieldVector3D<T>, FieldAbsoluteDate<T>) - Static method in class org.orekit.estimation.measurements.AbstractMeasurement
Compute propagation delay on a link leg (typically downlink or uplink).
signalTimeOfFlight(TimeStampedPVCoordinates, Vector3D, AbsoluteDate) - Static method in class org.orekit.estimation.measurements.AbstractMeasurement
Compute propagation delay on a link leg (typically downlink or uplink).
signedAmplitude(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.AbstractParametricAcceleration
Compute the signed amplitude of the acceleration.
signedAmplitude(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.HarmonicParametricAcceleration
Compute the signed amplitude of the acceleration.
signedAmplitude(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.PolynomialParametricAcceleration
Compute the signed amplitude of the acceleration.
signedAmplitude(SpacecraftState, double[]) - Method in class org.orekit.forces.AbstractParametricAcceleration
Compute the signed amplitude of the acceleration.
signedAmplitude(SpacecraftState, double[]) - Method in class org.orekit.forces.HarmonicParametricAcceleration
Compute the signed amplitude of the acceleration.
signedAmplitude(SpacecraftState, double[]) - Method in class org.orekit.forces.PolynomialParametricAcceleration
Compute the signed amplitude of the acceleration.
SignSemantic - Enum in org.orekit.estimation.measurements.generation
Enumerate for the semantic of the g function sign during measurements generation.
SimpleExponentialAtmosphere - Class in org.orekit.forces.drag.atmosphere
Simple exponential atmospheric model.
SimpleExponentialAtmosphere(BodyShape, double, double, double) - Constructor for class org.orekit.forces.drag.atmosphere.SimpleExponentialAtmosphere
Create an exponential atmosphere.
SimpleTimeStampedTableParser<T extends TimeStamped> - Class in org.orekit.data
Parser for simple tables containing time stamped data.
SimpleTimeStampedTableParser(int, SimpleTimeStampedTableParser.RowConverter<T>) - Constructor for class org.orekit.data.SimpleTimeStampedTableParser
Simple constructor.
SimpleTimeStampedTableParser.RowConverter<S extends TimeStamped> - Interface in org.orekit.data
Interface for converting a table row into time-stamped data.
SINGULAR_JACOBIAN_FOR_ORBIT_TYPE - org.orekit.errors.OrekitMessages
 
sini0 - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator
sinus original inclination.
SLAVE_MODE - Static variable in interface org.orekit.propagation.FieldPropagator
Indicator for slave mode.
SLAVE_MODE - Static variable in interface org.orekit.propagation.Propagator
Indicator for slave mode.
SmallManeuverAnalyticalModel - Class in org.orekit.forces.maneuvers
Analytical model for small maneuvers.
SmallManeuverAnalyticalModel(SpacecraftState, Vector3D, double) - Constructor for class org.orekit.forces.maneuvers.SmallManeuverAnalyticalModel
Build a maneuver defined in spacecraft frame.
SmallManeuverAnalyticalModel(SpacecraftState, Frame, Vector3D, double) - Constructor for class org.orekit.forces.maneuvers.SmallManeuverAnalyticalModel
Build a maneuver defined in user-specified frame.
SOLAR_RAD_AREA - org.orekit.files.ccsds.Keyword
Solar radiation pressure area.
SOLAR_RAD_COEFF - org.orekit.files.ccsds.Keyword
Solar radiation pressure coefficient.
SOLAR_SYSTEM_BARYCENTER - org.orekit.bodies.JPLEphemeridesLoader.EphemerisType
Constant for solar system barycenter.
SOLAR_SYSTEM_BARYCENTER - org.orekit.files.ccsds.CenterName
Solar system barycenter aggregated body.
SOLAR_SYSTEM_BARYCENTER - Static variable in class org.orekit.bodies.CelestialBodyFactory
Predefined name for solar system barycenter.
SolarRadiationPressure - Class in org.orekit.forces.radiation
Solar radiation pressure force model.
SolarRadiationPressure(double, double, ExtendedPVCoordinatesProvider, double, RadiationSensitive) - Constructor for class org.orekit.forces.radiation.SolarRadiationPressure
Complete constructor.
SolarRadiationPressure(double, double, PVCoordinatesProvider, double, RadiationSensitive) - Constructor for class org.orekit.forces.radiation.SolarRadiationPressure
SolarRadiationPressure(ExtendedPVCoordinatesProvider, double, RadiationSensitive) - Constructor for class org.orekit.forces.radiation.SolarRadiationPressure
Simple constructor with default reference values.
SolarRadiationPressure(PVCoordinatesProvider, double, RadiationSensitive) - Constructor for class org.orekit.forces.radiation.SolarRadiationPressure
SolidTides - Class in org.orekit.forces.gravity
Solid tides force model.
SolidTides(Frame, double, double, TideSystem, boolean, double, int, IERSConventions, UT1Scale, CelestialBody...) - Constructor for class org.orekit.forces.gravity.SolidTides
Simple constructor.
SolidTides(Frame, double, double, TideSystem, IERSConventions, UT1Scale, CelestialBody...) - Constructor for class org.orekit.forces.gravity.SolidTides
Simple constructor.
sort() - Method in class org.orekit.utils.ParameterDriversList
Sort the parameters lexicographically.
SP3_FRAME_CENTER_STRING - Static variable in class org.orekit.files.sp3.SP3File
String representation of the center of ephemeris coordinate system.
SP3_NUMBER_OF_EPOCH_MISMATCH - org.orekit.errors.OrekitMessages
 
SP3_UNEXPECTED_END_OF_FILE - org.orekit.errors.OrekitMessages
 
SP3_UNSUPPORTED_VERSION - org.orekit.errors.OrekitMessages
 
SP3File - Class in org.orekit.files.sp3
Represents a parsed SP3 orbit file.
SP3File.SP3Coordinate - Class in org.orekit.files.sp3
A single record of position clock and possibly derivatives in an SP3 file.
SP3File.SP3Ephemeris - Class in org.orekit.files.sp3
An ephemeris for a single satellite in a SP3 file.
SP3File.SP3FileType - Enum in org.orekit.files.sp3
File type indicator.
SP3File.SP3OrbitType - Enum in org.orekit.files.sp3
Orbit type indicator.
SP3File.TimeSystem - Enum in org.orekit.files.sp3
Time system used throughout this SP3 file.
SP3Parser - Class in org.orekit.files.sp3
A parser for the SP3 orbit file format.
SP3Parser() - Constructor for class org.orekit.files.sp3.SP3Parser
Create an SP3 parser using default values.
SP3Parser(double, int, Function<? super String, ? extends Frame>) - Constructor for class org.orekit.files.sp3.SP3Parser
Create an SP3 parser and specify the extra information needed to create a Propagator from the ephemeris data.
SPACECRAFT_MASS_BECOMES_NEGATIVE - org.orekit.errors.OrekitMessages
 
SpacecraftState - Class in org.orekit.propagation
This class is the representation of a complete state holding orbit, attitude and mass information at a given date.
SpacecraftState(Orbit) - Constructor for class org.orekit.propagation.SpacecraftState
Build a spacecraft state from orbit only.
SpacecraftState(Orbit, double) - Constructor for class org.orekit.propagation.SpacecraftState
Create a new instance from orbit and mass.
SpacecraftState(Orbit, double, Map<String, double[]>) - Constructor for class org.orekit.propagation.SpacecraftState
Create a new instance from orbit and mass.
SpacecraftState(Orbit, Map<String, double[]>) - Constructor for class org.orekit.propagation.SpacecraftState
Build a spacecraft state from orbit only.
SpacecraftState(Orbit, Attitude) - Constructor for class org.orekit.propagation.SpacecraftState
Build a spacecraft state from orbit and attitude provider.
SpacecraftState(Orbit, Attitude, double) - Constructor for class org.orekit.propagation.SpacecraftState
Build a spacecraft state from orbit, attitude provider and mass.
SpacecraftState(Orbit, Attitude, double, Map<String, double[]>) - Constructor for class org.orekit.propagation.SpacecraftState
Build a spacecraft state from orbit, attitude provider and mass.
SpacecraftState(Orbit, Attitude, Map<String, double[]>) - Constructor for class org.orekit.propagation.SpacecraftState
Build a spacecraft state from orbit and attitude provider.
SPEED_OF_LIGHT - Static variable in interface org.orekit.utils.Constants
Speed of light: 299792458.0 m/s.
SphericalHarmonicsProvider - Interface in org.orekit.forces.gravity.potential
Interface used to provide spherical harmonics coefficients.
SphericalPolygonsSetTransferObject - Class in org.orekit.utils
Transfer object for serializing SphericalPolygonsSet instances.
SphericalPolygonsSetTransferObject(SphericalPolygonsSet) - Constructor for class org.orekit.utils.SphericalPolygonsSetTransferObject
Simple constructor.
SpinStabilized - Class in org.orekit.attitudes
This class handles a spin stabilized attitude provider.
SpinStabilized(AttitudeProvider, AbsoluteDate, Vector3D, double) - Constructor for class org.orekit.attitudes.SpinStabilized
Creates a new instance.
SSA - Static variable in class org.orekit.models.earth.displacement.Tide
Ssa tide.
STANDARD_ATM_PRESSURE - Static variable in class org.orekit.models.earth.EarthStandardAtmosphereRefraction
NIST standard atmospheric pressure (Pa).
STANDARD_ATM_TEMPERATURE - Static variable in class org.orekit.models.earth.EarthStandardAtmosphereRefraction
NIST standard atmospheric temperature (K).
START_TIME - org.orekit.files.ccsds.Keyword
Start of total time span covered by:
startParse(String) - Method in class org.orekit.forces.gravity.potential.OceanTidesReader
Start parsing.
STATE_AND_PARAMETERS_JACOBIANS_ROWS_MISMATCH - org.orekit.errors.OrekitMessages
 
STATE_DIMENSION - Static variable in class org.orekit.propagation.numerical.JacobiansMapper
State dimension, fixed to 6.
STATE_JACOBIAN_NOT_6X6 - org.orekit.errors.OrekitMessages
 
STATE_JACOBIAN_NOT_INITIALIZED - org.orekit.errors.OrekitMessages
 
StateFunction - Interface in org.orekit.utils
Interface representing a vector function depending on SpacecraftState.
StateJacobian - Interface in org.orekit.utils
Interface representing the Jacobian of a vector function depending on SpacecraftState.
StateMapper - Class in org.orekit.propagation.integration
This class maps between raw double elements and SpacecraftState instances.
StateMapper(AbsoluteDate, double, OrbitType, PositionAngle, AttitudeProvider, Frame) - Constructor for class org.orekit.propagation.integration.StateMapper
Simple constructor.
STATION_NOT_FOUND - org.orekit.errors.OrekitMessages
 
StationDisplacement - Interface in org.orekit.models.earth.displacement
Interface for computing reference points displacement.
STEC - org.orekit.files.ccsds.Keyword
Data: STEC - Slant Total Electron Count [TECU].
stillAcceptsData() - Method in interface org.orekit.data.DataLoader
Check if the loader still accepts new data.
stillAcceptsData() - Method in class org.orekit.forces.drag.atmosphere.data.MarshallSolarActivityFutureEstimation
Check if the loader still accepts new data.
stillAcceptsData() - Method in class org.orekit.forces.gravity.potential.AstronomicalAmplitudeReader
Check if the loader still accepts new data.
stillAcceptsData() - Method in class org.orekit.forces.gravity.potential.OceanTidesReader
Check if the loader still accepts new data.
stillAcceptsData() - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
Check if the loader still accepts new data.
stillAcceptsData() - Method in class org.orekit.gnss.RinexLoader.Parser
Check if the loader still accepts new data.
stillAcceptsData() - Method in class org.orekit.gnss.SEMParser
 
stillAcceptsData() - Method in class org.orekit.gnss.YUMAParser
 
stillAcceptsData() - Method in class org.orekit.models.earth.GeoMagneticModelLoader
Check if the loader still accepts new data.
stillAcceptsData() - Method in class org.orekit.models.earth.KlobucharIonoCoefficientsLoader
Check if the loader still accepts new data.
stillAcceptsData() - Method in class org.orekit.models.earth.ViennaModelCoefficientsLoader
 
stillAcceptsData() - Method in class org.orekit.propagation.analytical.tle.TLESeries
Deprecated.
Check if the loader still accepts new data.
stillAcceptsData() - Method in class org.orekit.utils.InterpolationTableLoader
Check if the loader still accepts new data.
STOP - org.orekit.propagation.events.handlers.EventHandler.Action
Stop indicator.
STOP - org.orekit.propagation.events.handlers.FieldEventHandler.Action
Stop indicator.
STOP_TIME - org.orekit.files.ccsds.Keyword
End of total time span covered by:
StopOnDecreasing<T extends EventDetector> - Class in org.orekit.propagation.events.handlers
Handle a detection event and choose what to do next.
StopOnDecreasing() - Constructor for class org.orekit.propagation.events.handlers.StopOnDecreasing
 
StopOnEvent<T extends EventDetector> - Class in org.orekit.propagation.events.handlers
Event handler which will always return stop as a state.
StopOnEvent() - Constructor for class org.orekit.propagation.events.handlers.StopOnEvent
 
StopOnIncreasing<T extends EventDetector> - Class in org.orekit.propagation.events.handlers
Handle a detection event and choose what to do next.
StopOnIncreasing() - Constructor for class org.orekit.propagation.events.handlers.StopOnIncreasing
 
StreamingOemWriter - Class in org.orekit.files.ccsds
A writer for OEM files.
StreamingOemWriter(Appendable, TimeScale, Map<Keyword, String>) - Constructor for class org.orekit.files.ccsds.StreamingOemWriter
Create an OEM writer than streams data to the given output stream.
StreamingOemWriter.Segment - Class in org.orekit.files.ccsds
A writer for a segment of an OEM.
STRONG - org.orekit.forces.drag.atmosphere.data.MarshallSolarActivityFutureEstimation.StrengthLevel
Strong level of activity.
subtractOffset(AngularCoordinates) - Method in class org.orekit.utils.AngularCoordinates
Subtract an offset from the instance.
subtractOffset(AngularCoordinates) - Method in class org.orekit.utils.TimeStampedAngularCoordinates
Subtract an offset from the instance.
subtractOffset(FieldAngularCoordinates<T>) - Method in class org.orekit.utils.FieldAngularCoordinates
Subtract an offset from the instance.
subtractOffset(FieldAngularCoordinates<T>) - Method in class org.orekit.utils.TimeStampedFieldAngularCoordinates
Subtract an offset from the instance.
SUN - org.orekit.bodies.JPLEphemeridesLoader.EphemerisType
Constant for the Sun.
SUN - org.orekit.files.ccsds.CenterName
Sun body.
SUN - Static variable in class org.orekit.bodies.CelestialBodyFactory
Predefined name for Sun.
SUN_RADIUS - Static variable in interface org.orekit.utils.Constants
Sun radius: 695500000 m.
supportsTimeTransform() - Method in class org.orekit.models.earth.GeoMagneticField
Indicates whether this model supports time transformation or not.
switchOccurred(AttitudeProvider, AttitudeProvider, SpacecraftState) - Method in interface org.orekit.attitudes.AttitudesSequence.SwitchHandler
Method called when attitude is switched from one law to another law.
sxpInitialize() - Method in class org.orekit.propagation.analytical.tle.SGP4
Initialization proper to each propagator (SGP or SDP).
sxpInitialize() - Method in class org.orekit.propagation.analytical.tle.TLEPropagator
Initialization proper to each propagator (SGP or SDP).
sxpPropagate(double) - Method in class org.orekit.propagation.analytical.tle.SGP4
Propagation proper to each propagator (SGP or SDP).
sxpPropagate(double) - Method in class org.orekit.propagation.analytical.tle.TLEPropagator
Propagation proper to each propagator (SGP or SDP).

T

t2cof - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator
3/2 * C1.
TabulatedLofOffset - Class in org.orekit.attitudes
This class handles an attitude provider interpolating from a predefined table containing offsets from a Local Orbital Frame.
TabulatedLofOffset(Frame, LOFType, List<TimeStampedAngularCoordinates>, int, AngularDerivativesFilter) - Constructor for class org.orekit.attitudes.TabulatedLofOffset
Creates new instance.
TabulatedProvider - Class in org.orekit.attitudes
This class handles an attitude provider interpolating from a predefined table.
TabulatedProvider(Frame, List<TimeStampedAngularCoordinates>, int, AngularDerivativesFilter) - Constructor for class org.orekit.attitudes.TabulatedProvider
Creates new instance.
TAI - org.orekit.files.ccsds.CcsdsTimeScale
International Atomic Time.
TAI - org.orekit.files.sp3.SP3File.TimeSystem
International Atomic Time.
TAIScale - Class in org.orekit.time
International Atomic Time.
TAIUTCDatFilesLoader - Class in org.orekit.time
Loader for UTC-TAI extracted from tai-utc.dat file from USNO.
TAIUTCDatFilesLoader(String) - Constructor for class org.orekit.time.TAIUTCDatFilesLoader
Build a loader for tai-utc.dat file from USNO.
TargetPointing - Class in org.orekit.attitudes
This class handles target pointing attitude provider.
TargetPointing(Frame, GeodeticPoint, BodyShape) - Constructor for class org.orekit.attitudes.TargetPointing
Creates a new instance from body shape and target expressed in geodetic coordinates.
TargetPointing(Frame, Frame, Vector3D) - Constructor for class org.orekit.attitudes.TargetPointing
Creates a new instance from body frame and target expressed in Cartesian coordinates.
TCB - org.orekit.files.ccsds.CcsdsTimeScale
Barycentric Coordinate Time.
TCBScale - Class in org.orekit.time
Barycentric Coordinate Time.
TCG - org.orekit.files.ccsds.CcsdsTimeScale
Geocentric Coordinate Time.
TCGScale - Class in org.orekit.time
Geocentric Coordinate Time.
TDB - org.orekit.files.ccsds.CcsdsTimeScale
Barycentric Dynamical Time.
TDBScale - Class in org.orekit.time
Barycentric Dynamic Time.
tdm - org.orekit.files.ccsds.Keyword
TDM first keyword.
TDMFile - Class in org.orekit.files.ccsds
This class stocks all the information of the CCSDS Tracking Data Message file parsed by TDMParser or TDMXMLParser.
TDMFile() - Constructor for class org.orekit.files.ccsds.TDMFile
OEMFile constructor.
TDMFile.Observation - Class in org.orekit.files.ccsds
The Observation class contains the data from an observation line.
TDMFile.ObservationsBlock - Class in org.orekit.files.ccsds
The Observations Block class contain metadata and the list of observation data lines.
TDMFile.TDMMetaData - Class in org.orekit.files.ccsds
The TDMMetadata class gathers the meta-data present in the Tracking Data Message (TDM).
TDMMetaData() - Constructor for class org.orekit.files.ccsds.TDMFile.TDMMetaData
Create a new TDM meta-data.
TDMParser - Class in org.orekit.files.ccsds
Class for CCSDS Tracking Data Message parsers.
TDMParser() - Constructor for class org.orekit.files.ccsds.TDMParser
Simple constructor.
TDMParser.TDMFileFormat - Enum in org.orekit.files.ccsds
Enumerate for the format.
TDR - org.orekit.files.ccsds.CCSDSFrame
True of Date, Rotating.
TEME - org.orekit.files.ccsds.CCSDSFrame
True Equator Mean Equinox.
TEME - org.orekit.frames.Predefined
TEME frame.
TEMPERATURE - org.orekit.files.ccsds.Keyword
Data: Temperature [K].
tessellate(SphericalPolygonsSet, double, double, double, double, boolean, boolean) - Method in class org.orekit.models.earth.tessellation.EllipsoidTessellator
Tessellate a zone of interest into tiles.
theoreticalEvaluation(int, int, SpacecraftState[]) - Method in class org.orekit.estimation.measurements.AbstractMeasurement
Estimate the theoretical value.
theoreticalEvaluation(int, int, SpacecraftState[]) - Method in class org.orekit.estimation.measurements.AngularAzEl
Estimate the theoretical value.
theoreticalEvaluation(int, int, SpacecraftState[]) - Method in class org.orekit.estimation.measurements.AngularRaDec
Estimate the theoretical value.
theoreticalEvaluation(int, int, SpacecraftState[]) - Method in class org.orekit.estimation.measurements.InterSatellitesRange
Estimate the theoretical value.
theoreticalEvaluation(int, int, SpacecraftState[]) - Method in class org.orekit.estimation.measurements.Phase
Estimate the theoretical value.
theoreticalEvaluation(int, int, SpacecraftState[]) - Method in class org.orekit.estimation.measurements.Position
Estimate the theoretical value.
theoreticalEvaluation(int, int, SpacecraftState[]) - Method in class org.orekit.estimation.measurements.PV
Estimate the theoretical value.
theoreticalEvaluation(int, int, SpacecraftState[]) - Method in class org.orekit.estimation.measurements.Range
Estimate the theoretical value.
theoreticalEvaluation(int, int, SpacecraftState[]) - Method in class org.orekit.estimation.measurements.RangeRate
Estimate the theoretical value.
theoreticalEvaluation(int, int, SpacecraftState[]) - Method in class org.orekit.estimation.measurements.TurnAroundRange
Estimate the theoretical value.
theta2 - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator
cos io squared.
ThirdBodyAttraction - Class in org.orekit.forces.gravity
Third body attraction force model.
ThirdBodyAttraction(CelestialBody) - Constructor for class org.orekit.forces.gravity.ThirdBodyAttraction
Simple constructor.
ThreeEighthesIntegratorBuilder - Class in org.orekit.propagation.conversion
Builder for ThreeEighthesIntegrator.
ThreeEighthesIntegratorBuilder(double) - Constructor for class org.orekit.propagation.conversion.ThreeEighthesIntegratorBuilder
Build a new instance.
THRUST - Static variable in class org.orekit.forces.maneuvers.ConstantThrustManeuver
Parameter name for thrust.
TidalDisplacement - Class in org.orekit.models.earth.displacement
Modeling of displacement of reference points due to tidal effects.
TidalDisplacement(double, double, double, PVCoordinatesProvider, PVCoordinatesProvider, IERSConventions, boolean) - Constructor for class org.orekit.models.earth.displacement.TidalDisplacement
Simple constructor.
Tide - Class in org.orekit.models.earth.displacement
Class representing a tide.
Tide(int) - Constructor for class org.orekit.models.earth.displacement.Tide
Simple constructor.
Tide(int, int, int, int, int, int) - Constructor for class org.orekit.models.earth.displacement.Tide
Simple constructor.
TIDE_FREE - org.orekit.forces.gravity.potential.TideSystem
Constant for tide-free gravity fields.
TideSystem - Enum in org.orekit.forces.gravity.potential
Enumerate for tie systems.
TideSystemProvider - Interface in org.orekit.forces.gravity.potential
Interface used to provide tide systems.
Tile - Class in org.orekit.models.earth.tessellation
Simple data structure for a quadrilateral tile shape on a body surface.
Tile(GeodeticPoint, GeodeticPoint, GeodeticPoint, GeodeticPoint) - Constructor for class org.orekit.models.earth.tessellation.Tile
Create a tile.
TileAiming - Interface in org.orekit.models.earth.tessellation
Interface defining the aiming direction of tiles.
TIME_SYSTEM - org.orekit.files.ccsds.Keyword
Time system used for state vector, maneuver, and covariance data.
TimeComponents - Class in org.orekit.time
Class representing a time within the day broken up as hour, minute and second components.
TimeComponents(double) - Constructor for class org.orekit.time.TimeComponents
Build a time from the second number within the day.
TimeComponents(int, double) - Constructor for class org.orekit.time.TimeComponents
Build a time from the second number within the day.
TimeComponents(int, int, double) - Constructor for class org.orekit.time.TimeComponents
Build a time from its clock elements.
TimeComponents(int, int, double, int) - Constructor for class org.orekit.time.TimeComponents
Build a time from its clock elements.
TimeDerivativesEquations - Interface in org.orekit.propagation.numerical
Interface summing up the contribution of several forces into orbit and mass derivatives.
TimeInterpolable<T extends TimeInterpolable<T>> - Interface in org.orekit.time
This interface represents objects that can be interpolated in time.
TimeScalarFunction - Interface in org.orekit.time
This interface represents a scalar function of time.
TimeScale - Interface in org.orekit.time
Interface for time scales.
TimeScalesFactory - Class in org.orekit.time
Factory for predefined time scales.
timeScalesOffset(TimeScale, TimeScale) - Method in class org.orekit.time.AbsoluteDate
Compute the offset between two time scales at the current instant.
timeScalesOffset(TimeScale, TimeScale) - Method in class org.orekit.time.FieldAbsoluteDate
Compute the offset between two time scales at the current instant.
TimeShiftable<T extends TimeShiftable<T>> - Interface in org.orekit.time
This interface represents objects that can be shifted in time.
TimeSpanMap<T> - Class in org.orekit.utils
Container for objects that apply to spans of time.
TimeSpanMap(T) - Constructor for class org.orekit.utils.TimeSpanMap
Create a map containing a single object, initially valid throughout the timeline.
TimeSpanMap.Span<S> - Class in org.orekit.utils
Holder for one time span.
TimeSpanMap.Transition<S> - Class in org.orekit.utils
Class holding transition times.
TimeStamped - Interface in org.orekit.time
This interface represents objects that have a AbsoluteDate date attached to them.
TimeStampedAngularCoordinates - Class in org.orekit.utils
TimeStampedAngularCoordinates(AbsoluteDate, FieldRotation<DerivativeStructure>) - Constructor for class org.orekit.utils.TimeStampedAngularCoordinates
Builds a TimeStampedAngularCoordinates from a FieldRotation<DerivativeStructure>.
TimeStampedAngularCoordinates(AbsoluteDate, Rotation, Vector3D, Vector3D) - Constructor for class org.orekit.utils.TimeStampedAngularCoordinates
Builds a rotation/rotation rate pair.
TimeStampedAngularCoordinates(AbsoluteDate, PVCoordinates, PVCoordinates) - Constructor for class org.orekit.utils.TimeStampedAngularCoordinates
Build one of the rotations that transform one pv coordinates into another one.
TimeStampedAngularCoordinates(AbsoluteDate, PVCoordinates, PVCoordinates, PVCoordinates, PVCoordinates, double) - Constructor for class org.orekit.utils.TimeStampedAngularCoordinates
Build the rotation that transforms a pair of pv coordinates into another pair.
TimeStampedCache<T extends TimeStamped> - Interface in org.orekit.utils
Interface for a data structure that can provide concurrent access to TimeStamped data surrounding a given date.
TimeStampedCacheException - Exception in org.orekit.errors
This class is the base class for all specific exceptions thrown by during the GenericTimeStampedCache.
TimeStampedCacheException(Throwable, Localizable, Object...) - Constructor for exception org.orekit.errors.TimeStampedCacheException
Simple constructor.
TimeStampedCacheException(Localizable, Object...) - Constructor for exception org.orekit.errors.TimeStampedCacheException
Simple constructor.
TimeStampedCacheException(MathRuntimeException) - Constructor for exception org.orekit.errors.TimeStampedCacheException
Simple constructor.
TimeStampedCacheException(OrekitException) - Constructor for exception org.orekit.errors.TimeStampedCacheException
Simple constructor.
TimeStampedFieldAngularCoordinates<T extends org.hipparchus.RealFieldElement<T>> - Class in org.orekit.utils
TimeStampedFieldAngularCoordinates(Field<T>, TimeStampedAngularCoordinates) - Constructor for class org.orekit.utils.TimeStampedFieldAngularCoordinates
Builds an instance for a regular TimeStampedAngularCoordinates.
TimeStampedFieldAngularCoordinates(AbsoluteDate, FieldRotation<T>, FieldVector3D<T>, FieldVector3D<T>) - Constructor for class org.orekit.utils.TimeStampedFieldAngularCoordinates
Builds a rotation/rotation rate pair.
TimeStampedFieldAngularCoordinates(AbsoluteDate, FieldPVCoordinates<T>, FieldPVCoordinates<T>, FieldPVCoordinates<T>, FieldPVCoordinates<T>, double) - Constructor for class org.orekit.utils.TimeStampedFieldAngularCoordinates
Build the rotation that transforms a pair of pv coordinates into another pair.
TimeStampedFieldAngularCoordinates(FieldAbsoluteDate<T>, FieldRotation<FieldDerivativeStructure<T>>) - Constructor for class org.orekit.utils.TimeStampedFieldAngularCoordinates
Builds a TimeStampedFieldAngularCoordinates from a FieldRotation<FieldDerivativeStructure>.
TimeStampedFieldAngularCoordinates(FieldAbsoluteDate<T>, FieldRotation<T>, FieldVector3D<T>, FieldVector3D<T>) - Constructor for class org.orekit.utils.TimeStampedFieldAngularCoordinates
Builds a rotation/rotation rate pair.
TimeStampedFieldAngularCoordinates(FieldAbsoluteDate<T>, FieldPVCoordinates<T>, FieldPVCoordinates<T>, FieldPVCoordinates<T>, FieldPVCoordinates<T>, double) - Constructor for class org.orekit.utils.TimeStampedFieldAngularCoordinates
Build the rotation that transforms a pair of pv coordinates into another pair.
TimeStampedFieldPVCoordinates<T extends org.hipparchus.RealFieldElement<T>> - Class in org.orekit.utils
TimeStampedFieldPVCoordinates(AbsoluteDate, double, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates
Multiplicative constructor
TimeStampedFieldPVCoordinates(AbsoluteDate, double, FieldPVCoordinates<T>, double, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates
Linear constructor
TimeStampedFieldPVCoordinates(AbsoluteDate, double, FieldPVCoordinates<T>, double, FieldPVCoordinates<T>, double, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates
Linear constructor
TimeStampedFieldPVCoordinates(AbsoluteDate, double, FieldPVCoordinates<T>, double, FieldPVCoordinates<T>, double, FieldPVCoordinates<T>, double, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates
Linear constructor
TimeStampedFieldPVCoordinates(AbsoluteDate, FieldVector3D<T>, FieldVector3D<T>, FieldVector3D<T>) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates
Builds a PVCoordinates pair.
TimeStampedFieldPVCoordinates(AbsoluteDate, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates
Basic constructor.
TimeStampedFieldPVCoordinates(AbsoluteDate, FieldPVCoordinates<T>, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates
Subtractive constructor
TimeStampedFieldPVCoordinates(AbsoluteDate, T, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates
Multiplicative constructor
TimeStampedFieldPVCoordinates(AbsoluteDate, T, FieldPVCoordinates<T>, T, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates
Linear constructor
TimeStampedFieldPVCoordinates(AbsoluteDate, T, FieldPVCoordinates<T>, T, FieldPVCoordinates<T>, T, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates
Linear constructor
TimeStampedFieldPVCoordinates(AbsoluteDate, T, FieldPVCoordinates<T>, T, FieldPVCoordinates<T>, T, FieldPVCoordinates<T>, T, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates
Linear constructor
TimeStampedFieldPVCoordinates(AbsoluteDate, T, PVCoordinates) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates
Multiplicative constructor
TimeStampedFieldPVCoordinates(AbsoluteDate, T, PVCoordinates, T, PVCoordinates) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates
Linear constructor
TimeStampedFieldPVCoordinates(AbsoluteDate, T, PVCoordinates, T, PVCoordinates, T, PVCoordinates) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates
Linear constructor
TimeStampedFieldPVCoordinates(AbsoluteDate, T, PVCoordinates, T, PVCoordinates, T, PVCoordinates, T, PVCoordinates) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates
Linear constructor
TimeStampedFieldPVCoordinates(FieldAbsoluteDate<T>, double, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates
Multiplicative constructor
TimeStampedFieldPVCoordinates(FieldAbsoluteDate<T>, double, FieldPVCoordinates<T>, double, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates
Linear constructor
TimeStampedFieldPVCoordinates(FieldAbsoluteDate<T>, double, FieldPVCoordinates<T>, double, FieldPVCoordinates<T>, double, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates
Linear constructor
TimeStampedFieldPVCoordinates(FieldAbsoluteDate<T>, double, FieldPVCoordinates<T>, double, FieldPVCoordinates<T>, double, FieldPVCoordinates<T>, double, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates
Linear constructor
TimeStampedFieldPVCoordinates(FieldAbsoluteDate<T>, FieldVector3D<FieldDerivativeStructure<T>>) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates
Builds a TimeStampedFieldPVCoordinates triplet from a FieldVector3D<FieldDerivativeStructure>.
TimeStampedFieldPVCoordinates(FieldAbsoluteDate<T>, FieldVector3D<T>, FieldVector3D<T>, FieldVector3D<T>) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates
Builds a PVCoordinates pair.
TimeStampedFieldPVCoordinates(FieldAbsoluteDate<T>, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates
Basic constructor.
TimeStampedFieldPVCoordinates(FieldAbsoluteDate<T>, FieldPVCoordinates<T>, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates
Subtractive constructor
TimeStampedFieldPVCoordinates(FieldAbsoluteDate<T>, T, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates
Multiplicative constructor
TimeStampedFieldPVCoordinates(FieldAbsoluteDate<T>, T, FieldPVCoordinates<T>, T, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates
Linear constructor
TimeStampedFieldPVCoordinates(FieldAbsoluteDate<T>, T, FieldPVCoordinates<T>, T, FieldPVCoordinates<T>, T, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates
Linear constructor
TimeStampedFieldPVCoordinates(FieldAbsoluteDate<T>, T, FieldPVCoordinates<T>, T, FieldPVCoordinates<T>, T, FieldPVCoordinates<T>, T, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates
Linear constructor
TimeStampedFieldPVCoordinates(FieldAbsoluteDate<T>, T, PVCoordinates) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates
Multiplicative constructor
TimeStampedFieldPVCoordinates(FieldAbsoluteDate<T>, T, PVCoordinates, T, PVCoordinates) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates
Linear constructor
TimeStampedFieldPVCoordinates(FieldAbsoluteDate<T>, T, PVCoordinates, T, PVCoordinates, T, PVCoordinates) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates
Linear constructor
TimeStampedFieldPVCoordinates(FieldAbsoluteDate<T>, T, PVCoordinates, T, PVCoordinates, T, PVCoordinates, T, PVCoordinates) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates
Linear constructor
TimeStampedGenerator<T extends TimeStamped> - Interface in org.orekit.utils
Generator to use for creating entries in time stamped caches.
TimeStampedPVCoordinates - Class in org.orekit.utils
TimeStampedPVCoordinates(AbsoluteDate, double, PVCoordinates) - Constructor for class org.orekit.utils.TimeStampedPVCoordinates
Multiplicative constructor
TimeStampedPVCoordinates(AbsoluteDate, double, PVCoordinates, double, PVCoordinates) - Constructor for class org.orekit.utils.TimeStampedPVCoordinates
Linear constructor
TimeStampedPVCoordinates(AbsoluteDate, double, PVCoordinates, double, PVCoordinates, double, PVCoordinates) - Constructor for class org.orekit.utils.TimeStampedPVCoordinates
Linear constructor
TimeStampedPVCoordinates(AbsoluteDate, double, PVCoordinates, double, PVCoordinates, double, PVCoordinates, double, PVCoordinates) - Constructor for class org.orekit.utils.TimeStampedPVCoordinates
Linear constructor
TimeStampedPVCoordinates(AbsoluteDate, FieldVector3D<DerivativeStructure>) - Constructor for class org.orekit.utils.TimeStampedPVCoordinates
Builds a TimeStampedPVCoordinates triplet from a FieldVector3D<DerivativeStructure>.
TimeStampedPVCoordinates(AbsoluteDate, Vector3D, Vector3D) - Constructor for class org.orekit.utils.TimeStampedPVCoordinates
Build from position and velocity.
TimeStampedPVCoordinates(AbsoluteDate, Vector3D, Vector3D, Vector3D) - Constructor for class org.orekit.utils.TimeStampedPVCoordinates
Builds a TimeStampedPVCoordinates pair.
TimeStampedPVCoordinates(AbsoluteDate, PVCoordinates) - Constructor for class org.orekit.utils.TimeStampedPVCoordinates
Build from position velocity acceleration coordinates.
TimeStampedPVCoordinates(AbsoluteDate, PVCoordinates, PVCoordinates) - Constructor for class org.orekit.utils.TimeStampedPVCoordinates
Subtractive constructor
TIMETAG_REF - org.orekit.files.ccsds.Keyword
Meta-data: Timetag reference.
TimeVectorFunction - Interface in org.orekit.time
This interface represents a multi-valued function of time.
TIRF_CONVENTIONS_1996_ACCURATE_EOP - org.orekit.frames.Predefined
TIRF, IERS 996 conventions, with accurate EOP interpolation.
TIRF_CONVENTIONS_1996_SIMPLE_EOP - org.orekit.frames.Predefined
TIRF, IERS 1996 conventions, with simple EOP interpolation.
TIRF_CONVENTIONS_2003_ACCURATE_EOP - org.orekit.frames.Predefined
TIRF, IERS 2003 conventions, with accurate EOP interpolation.
TIRF_CONVENTIONS_2003_SIMPLE_EOP - org.orekit.frames.Predefined
TIRF, IERS 2003 conventions, with simple EOP interpolation.
TIRF_CONVENTIONS_2010_ACCURATE_EOP - org.orekit.frames.Predefined
TIRF, IERS 2010 conventions, with accurate EOP interpolation.
TIRF_CONVENTIONS_2010_SIMPLE_EOP - org.orekit.frames.Predefined
TIRF, IERS 2010 conventions, with simple EOP interpolation.
tle - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator
Initial state.
TLE - Class in org.orekit.propagation.analytical.tle
This class is a container for a single set of TLE data.
TLE(int, char, int, int, String, int, int, AbsoluteDate, double, double, double, double, double, double, double, double, int, double) - Constructor for class org.orekit.propagation.analytical.tle.TLE
Simple constructor from already parsed elements.
TLE(String, String) - Constructor for class org.orekit.propagation.analytical.tle.TLE
Simple constructor from unparsed two lines.
TLE_CHECKSUM_ERROR - org.orekit.errors.OrekitMessages
 
TLE_INVALID_PARAMETER - org.orekit.errors.OrekitMessages
 
TLE_LINES_DO_NOT_REFER_TO_SAME_OBJECT - org.orekit.errors.OrekitMessages
 
TLEPropagator - Class in org.orekit.propagation.analytical.tle
This class provides elements to propagate TLE's.
TLEPropagator(TLE, AttitudeProvider, double) - Constructor for class org.orekit.propagation.analytical.tle.TLEPropagator
Protected constructor for derived classes.
TLEPropagatorBuilder - Class in org.orekit.propagation.conversion
Builder for TLEPropagator.
TLEPropagatorBuilder(TLE, PositionAngle, double) - Constructor for class org.orekit.propagation.conversion.TLEPropagatorBuilder
Build a new instance.
TLESeries - Class in org.orekit.propagation.analytical.tle
Deprecated.
as of 9.0, this class is deprecated without replacement. The file format used was considered to be too specific and the API not really well designed. Users are encouraged to use their own parser for series of TLE
TLESeries(String, boolean) - Constructor for class org.orekit.propagation.analytical.tle.TLESeries
Deprecated.
Simple constructor with a TLE file.
TNW - org.orekit.files.ccsds.CCSDSFrame
TNW : x-axis along the velocity vector, W along the orbital angular momentum vector and N completes the right handed system.
TNW - org.orekit.frames.LOFType
Constant for TNW frame (X axis aligned with velocity, Z axis aligned with orbital momentum).
toAbsoluteDate() - Method in class org.orekit.time.FieldAbsoluteDate
Transform the FieldAbsoluteDate in an AbsoluteDate.
toAngularCoordinates() - Method in class org.orekit.utils.FieldAngularCoordinates
Convert to a regular angular coordinates.
toArray(List<List<Double>>) - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
Convert a list of list into an array.
toAttitude() - Method in class org.orekit.attitudes.FieldAttitude
Converts to an Attitude instance.
TOD - org.orekit.files.ccsds.CCSDSFrame
True of Date.
TOD_CONVENTIONS_1996_ACCURATE_EOP - org.orekit.frames.Predefined
TOD, IERS 1996 conventions, with accurate EOP interpolation.
TOD_CONVENTIONS_1996_SIMPLE_EOP - org.orekit.frames.Predefined
TOD, IERS 1996 conventions, with simple EOP interpolation.
TOD_CONVENTIONS_2003_ACCURATE_EOP - org.orekit.frames.Predefined
TOD, IERS 2003 conventions, with accurate EOP interpolation.
TOD_CONVENTIONS_2003_SIMPLE_EOP - org.orekit.frames.Predefined
TOD, IERS 2003 conventions, with simple EOP interpolation.
TOD_CONVENTIONS_2010_ACCURATE_EOP - org.orekit.frames.Predefined
TOD, IERS 2010 conventions, with accurate EOP interpolation.
TOD_CONVENTIONS_2010_SIMPLE_EOP - org.orekit.frames.Predefined
TOD, IERS 2010 conventions, with simple EOP interpolation.
TOD_WITHOUT_EOP_CORRECTIONS - org.orekit.frames.Predefined
TOD, IERS 1996 conventions without EOP corrections.
toDate(TimeScale) - Method in class org.orekit.time.AbsoluteDate
Convert the instance to a Java Date.
toDate(TimeScale) - Method in class org.orekit.time.FieldAbsoluteDate
Convert the instance to a Java Date.
toDerivativeStructurePV(int) - Method in class org.orekit.utils.FieldPVCoordinates
Transform the instance to a FieldPVCoordinates<FieldDerivativeStructure>.
toDerivativeStructurePV(int) - Method in class org.orekit.utils.PVCoordinates
Transform the instance to a FieldPVCoordinates<DerivativeStructure>.
toDerivativeStructureRotation(int) - Method in class org.orekit.utils.AngularCoordinates
Transform the instance to a FieldRotation<DerivativeStructure>.
toDerivativeStructureRotation(int) - Method in class org.orekit.utils.FieldAngularCoordinates
Transform the instance to a FieldRotation<FieldDerivativeStructure>.
toDerivativeStructureVector(int) - Method in class org.orekit.utils.FieldPVCoordinates
Transform the instance to a FieldVector3D<FieldDerivativeStructure>.
toDerivativeStructureVector(int) - Method in class org.orekit.utils.PVCoordinates
Transform the instance to a FieldVector3D<DerivativeStructure>.
toEquinox(AbsoluteDate, double, double) - Method in interface org.orekit.utils.IERSConventions.NutationCorrectionConverter
Convert nutation corrections.
toFieldPVCoordinatesProvider(Field<T>) - Method in interface org.orekit.utils.ExtendedPVCoordinatesProvider
Convert to a FieldPVCoordinatesProvider with a specific type.
toGeodetic(S2Point) - Method in class org.orekit.models.earth.tessellation.EllipsoidTessellator
Convert a point on the unit 2-sphere to geodetic coordinates.
tolerances(double, Orbit) - Static method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator
Estimate tolerance vectors for an AdaptativeStepsizeIntegrator.
tolerances(double, Orbit, OrbitType) - Static method in class org.orekit.propagation.numerical.NumericalPropagator
Estimate tolerance vectors for integrators.
tolerances(T, FieldOrbit<T>, OrbitType) - Static method in class org.orekit.propagation.numerical.FieldNumericalPropagator
Estimate tolerance vectors for integrators.
ton2a - Variable in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution
2 / (n² * a) .
toNonRotating(AbsoluteDate, double, double) - Method in interface org.orekit.utils.IERSConventions.NutationCorrectionConverter
Convert nutation corrections.
TOO_LARGE_DEGREE_FOR_GRAVITY_FIELD - org.orekit.errors.OrekitMessages
 
TOO_LARGE_ECCENTRICITY_FOR_PROPAGATION_MODEL - org.orekit.errors.OrekitMessages
 
TOO_LARGE_ORDER_FOR_GRAVITY_FIELD - org.orekit.errors.OrekitMessages
 
TOO_SHORT_TRANSITION_TIME_FOR_ATTITUDES_SWITCH - org.orekit.errors.OrekitMessages
 
TOO_SMALL_SCALE_FOR_PARAMETER - org.orekit.errors.OrekitMessages
 
toOrbit() - Method in class org.orekit.orbits.FieldCartesianOrbit
 
toOrbit() - Method in class org.orekit.orbits.FieldCircularOrbit
 
toOrbit() - Method in class org.orekit.orbits.FieldEquinoctialOrbit
 
toOrbit() - Method in class org.orekit.orbits.FieldKeplerianOrbit
 
toOrbit() - Method in class org.orekit.orbits.FieldOrbit
Transforms the FieldOrbit instance into an Orbit instance.
toPlane(Vector3D) - Method in class org.orekit.bodies.Ellipse
Project a point to the ellipse plane.
TopocentricFrame - Class in org.orekit.frames
Topocentric frame.
TopocentricFrame(BodyShape, GeodeticPoint, String) - Constructor for class org.orekit.frames.TopocentricFrame
Simple constructor.
toPVCoordinates() - Method in class org.orekit.utils.FieldPVCoordinates
Convert to a constant position-velocity.
toSI(double) - Method in enum org.orekit.data.PolynomialParser.Unit
Convert value from instance unit to corresponding SI unit.
toSpace(Vector2D) - Method in class org.orekit.bodies.Ellipse
Create a point from its ellipse-relative coordinates.
toSpacecraftState() - Method in class org.orekit.propagation.FieldSpacecraftState
To convert a FieldSpacecraftState instance into a SpacecraftState instance.
toString() - Method in class org.orekit.bodies.FieldGeodeticPoint
 
toString() - Method in class org.orekit.bodies.GeodeticPoint
 
toString() - Method in class org.orekit.frames.Frame
New definition of the java.util toString() method.
toString() - Method in class org.orekit.frames.OrphanFrame
toString() - Method in class org.orekit.models.earth.GeoMagneticElements
 
toString() - Method in class org.orekit.orbits.CartesianOrbit
Returns a string representation of this Orbit object.
toString() - Method in class org.orekit.orbits.CircularOrbit
Returns a string representation of this Orbit object.
toString() - Method in class org.orekit.orbits.EquinoctialOrbit
Returns a string representation of this equinoctial parameters object.
toString() - Method in class org.orekit.orbits.FieldCartesianOrbit
Returns a string representation of this Orbit object.
toString() - Method in class org.orekit.orbits.FieldCircularOrbit
Returns a string representation of this Orbit object.
toString() - Method in class org.orekit.orbits.FieldEquinoctialOrbit
Returns a string representation of this equinoctial parameters object.
toString() - Method in class org.orekit.orbits.FieldKeplerianOrbit
Returns a string representation of this Keplerian parameters object.
toString() - Method in class org.orekit.orbits.KeplerianOrbit
Returns a string representation of this Keplerian parameters object.
toString() - Method in class org.orekit.propagation.analytical.tle.TLE
Get a string representation of this TLE set.
toString() - Method in class org.orekit.time.AbsoluteDate
Get a String representation of the instant location in UTC time scale.
toString() - Method in class org.orekit.time.BDTScale
toString() - Method in class org.orekit.time.DateComponents
Get a string representation (ISO-8601) of the date.
toString() - Method in class org.orekit.time.DateTimeComponents
Return a string representation of this pair.
toString() - Method in class org.orekit.time.FieldAbsoluteDate
Get a String representation of the instant location in UTC time scale.
toString() - Method in class org.orekit.time.GalileoScale
toString() - Method in class org.orekit.time.GLONASSScale
toString() - Method in class org.orekit.time.GMSTScale
toString() - Method in class org.orekit.time.GPSScale
toString() - Method in class org.orekit.time.IRNSSScale
toString() - Method in class org.orekit.time.QZSSScale
toString() - Method in class org.orekit.time.TAIScale
toString() - Method in class org.orekit.time.TCBScale
toString() - Method in class org.orekit.time.TCGScale
toString() - Method in class org.orekit.time.TDBScale
toString() - Method in class org.orekit.time.TimeComponents
Get a string representation of the time.
toString() - Method in class org.orekit.time.TTScale
toString() - Method in class org.orekit.time.UT1Scale
toString() - Method in class org.orekit.time.UTCScale
toString() - Method in class org.orekit.utils.FieldPVCoordinates
Return a string representation of this position/velocity pair.
toString() - Method in class org.orekit.utils.ImmutableTimeStampedCache
toString() - Method in class org.orekit.utils.ParameterDriver
Get a text representation of the parameter.
toString() - Method in class org.orekit.utils.PVCoordinates
Return a string representation of this position/velocity pair.
toString() - Method in class org.orekit.utils.TimeStampedFieldPVCoordinates
Return a string representation of this position/velocity pair.
toString() - Method in class org.orekit.utils.TimeStampedPVCoordinates
Return a string representation of this position/velocity pair.
toString(int) - Method in class org.orekit.time.AbsoluteDate
Get a String representation of the instant location for a local time.
toString(int) - Method in class org.orekit.time.DateTimeComponents
Return a string representation of this pair.
toString(int) - Method in class org.orekit.time.FieldAbsoluteDate
Get a String representation of the instant location for a local time.
toString(TimeZone) - Method in class org.orekit.time.AbsoluteDate
Get a String representation of the instant location for a time zone.
toString(TimeZone) - Method in class org.orekit.time.FieldAbsoluteDate
Get a String representation of the instant location for a time zone.
toString(TimeScale) - Method in class org.orekit.time.AbsoluteDate
Get a String representation of the instant location.
toString(TimeScale) - Method in class org.orekit.time.FieldAbsoluteDate
Get a String representation of the instant location.
TOTAL_ZENITH_DELAY - Static variable in class org.orekit.models.earth.EstimatedTroposphericModel
Name of the parameter of this model: the total zenith delay.
toTaylorProvider(Frame) - Method in class org.orekit.utils.TimeStampedPVCoordinates
Create a local provider using simply Taylor expansion through TimeStampedPVCoordinates.shiftedBy(double).
toTimeStampedPVCoordinates() - Method in class org.orekit.utils.TimeStampedFieldPVCoordinates
Convert to a constant position-velocity.
toTransform() - Method in class org.orekit.propagation.FieldSpacecraftState
Compute the transform from orbite/attitude reference frame to spacecraft frame.
toTransform() - Method in class org.orekit.propagation.SpacecraftState
Compute the transform from orbite/attitude reference frame to spacecraft frame.
TRAJECTORY_INSIDE_BRILLOUIN_SPHERE - org.orekit.errors.OrekitMessages
 
transform(FieldVector3D<T>, Frame, FieldAbsoluteDate<T>) - Method in interface org.orekit.bodies.BodyShape
Transform a Cartesian point to a surface-relative point.
transform(FieldVector3D<T>, Frame, FieldAbsoluteDate<T>) - Method in class org.orekit.bodies.OneAxisEllipsoid
Transform a Cartesian point to a surface-relative point.
transform(FieldVector3D<T>, Frame, FieldAbsoluteDate<T>) - Method in class org.orekit.models.earth.Geoid
Transform a Cartesian point to a surface-relative point.
transform(Vector3D, Frame, AbsoluteDate) - Method in interface org.orekit.bodies.BodyShape
Transform a Cartesian point to a surface-relative point.
transform(Vector3D, Frame, AbsoluteDate) - Method in class org.orekit.bodies.OneAxisEllipsoid
Transform a Cartesian point to a surface-relative point.
transform(Vector3D, Frame, AbsoluteDate) - Method in class org.orekit.models.earth.Geoid
Transform a Cartesian point to a surface-relative point.
transform(FieldGeodeticPoint<T>) - Method in interface org.orekit.bodies.BodyShape
Transform a surface-relative point to a Cartesian point.
transform(FieldGeodeticPoint<T>) - Method in class org.orekit.bodies.OneAxisEllipsoid
Transform a surface-relative point to a Cartesian point.
transform(FieldGeodeticPoint<T>) - Method in class org.orekit.models.earth.Geoid
Transform a surface-relative point to a Cartesian point.
transform(GeodeticPoint) - Method in interface org.orekit.bodies.BodyShape
Transform a surface-relative point to a Cartesian point.
transform(GeodeticPoint) - Method in class org.orekit.bodies.OneAxisEllipsoid
Transform a surface-relative point to a Cartesian point.
transform(GeodeticPoint) - Method in class org.orekit.models.earth.Geoid
Transform a surface-relative point to a Cartesian point.
transform(PVCoordinates, Frame, AbsoluteDate) - Method in class org.orekit.bodies.OneAxisEllipsoid
Transform a Cartesian point to a surface-relative point.
Transform - Class in org.orekit.frames
Transformation class in three dimensional space.
Transform(AbsoluteDate, Rotation) - Constructor for class org.orekit.frames.Transform
Build a rotation transform.
Transform(AbsoluteDate, Rotation, Vector3D) - Constructor for class org.orekit.frames.Transform
Build a rotation transform.
Transform(AbsoluteDate, Rotation, Vector3D, Vector3D) - Constructor for class org.orekit.frames.Transform
Build a rotation transform.
Transform(AbsoluteDate, Vector3D) - Constructor for class org.orekit.frames.Transform
Build a translation transform.
Transform(AbsoluteDate, Vector3D, Vector3D) - Constructor for class org.orekit.frames.Transform
Build a translation transform, with its first time derivative.
Transform(AbsoluteDate, Vector3D, Vector3D, Vector3D) - Constructor for class org.orekit.frames.Transform
Build a translation transform, with its first and second time derivatives.
Transform(AbsoluteDate, Transform, Transform) - Constructor for class org.orekit.frames.Transform
Build a transform by combining two existing ones.
Transform(AbsoluteDate, AngularCoordinates) - Constructor for class org.orekit.frames.Transform
Build a rotation transform.
Transform(AbsoluteDate, PVCoordinates) - Constructor for class org.orekit.frames.Transform
Build a translation transform, with its first time derivative.
transformFromInertial(AbsoluteDate, PVCoordinates) - Method in enum org.orekit.frames.LOFType
Get the transform from an inertial frame defining position-velocity and the local orbital frame.
transformFromInertial(FieldAbsoluteDate<T>, FieldPVCoordinates<T>) - Method in enum org.orekit.frames.LOFType
Get the transform from an inertial frame defining position-velocity and the local orbital frame.
TransformGenerator - Class in org.orekit.frames
Generator to use transforms in GenericTimeStampedCache.
TransformGenerator(int, TransformProvider, double) - Constructor for class org.orekit.frames.TransformGenerator
simple constructor.
transformLine(FieldLine<T>) - Method in class org.orekit.frames.FieldTransform
Transform a line.
transformLine(Line) - Method in class org.orekit.frames.FieldTransform
Transform a line.
transformLine(Line) - Method in class org.orekit.frames.Transform
Transform a line.
transformModel(double) - Method in class org.orekit.models.earth.GeoMagneticField
Time transform the model coefficients from the base year of the model using secular variation coefficients.
transformModel(GeoMagneticField, double) - Method in class org.orekit.models.earth.GeoMagneticField
Time transform the model coefficients from the base year of the model using a linear interpolation with a second model.
transformPosition(FieldVector3D<T>) - Method in class org.orekit.frames.FieldTransform
Transform a position vector (including translation effects).
transformPosition(FieldVector3D<T>) - Method in class org.orekit.frames.Transform
Transform a position vector (including translation effects).
transformPosition(Vector3D) - Method in class org.orekit.frames.FieldTransform
Transform a position vector (including translation effects).
transformPosition(Vector3D) - Method in class org.orekit.frames.Transform
Transform a position vector (including translation effects).
TransformProvider - Interface in org.orekit.frames
Interface for Transform providers.
TransformProviderUtils - Class in org.orekit.frames
Utility for Transform providers.
transformPVCoordinates(FieldPVCoordinates<T>) - Method in class org.orekit.frames.FieldTransform
Transform TimeStampedFieldPVCoordinates including kinematic effects.
transformPVCoordinates(FieldPVCoordinates<T>) - Method in class org.orekit.frames.Transform
Transform FieldPVCoordinates including kinematic effects.
transformPVCoordinates(PVCoordinates) - Method in class org.orekit.frames.FieldTransform
Transform TimeStampedPVCoordinates including kinematic effects.
transformPVCoordinates(PVCoordinates) - Method in class org.orekit.frames.Transform
Transform PVCoordinates including kinematic effects.
transformPVCoordinates(TimeStampedFieldPVCoordinates<T>) - Method in class org.orekit.frames.FieldTransform
Transform TimeStampedFieldPVCoordinates including kinematic effects.
transformPVCoordinates(TimeStampedFieldPVCoordinates<T>) - Method in class org.orekit.frames.Transform
Transform TimeStampedFieldPVCoordinates including kinematic effects.
transformPVCoordinates(TimeStampedPVCoordinates) - Method in class org.orekit.frames.FieldTransform
Transform TimeStampedPVCoordinates including kinematic effects.
transformPVCoordinates(TimeStampedPVCoordinates) - Method in class org.orekit.frames.Transform
Transform TimeStampedPVCoordinates including kinematic effects.
transformVector(FieldVector3D<T>) - Method in class org.orekit.frames.FieldTransform
Transform a vector (ignoring translation effects).
transformVector(FieldVector3D<T>) - Method in class org.orekit.frames.Transform
Transform a vector (ignoring translation effects).
transformVector(Vector3D) - Method in class org.orekit.frames.FieldTransform
Transform a vector (ignoring translation effects).
transformVector(Vector3D) - Method in class org.orekit.frames.Transform
Transform a vector (ignoring translation effects).
TRANSMIT_BAND - org.orekit.files.ccsds.Keyword
Frequency band for transmitted frequencies.
TRANSMIT_DELAY_1 - org.orekit.files.ccsds.Keyword
Meta-data: Transmit delays list (up to 5).
TRANSMIT_DELAY_2 - org.orekit.files.ccsds.Keyword
Second.
TRANSMIT_DELAY_3 - org.orekit.files.ccsds.Keyword
Second.
TRANSMIT_DELAY_4 - org.orekit.files.ccsds.Keyword
Second.
TRANSMIT_DELAY_5 - org.orekit.files.ccsds.Keyword
Second.
TRANSMIT_FREQ_1 - org.orekit.files.ccsds.Keyword
Data: Transmitted frequencies [Hz].
TRANSMIT_FREQ_2 - org.orekit.files.ccsds.Keyword
Transmitted frequency 2.
TRANSMIT_FREQ_3 - org.orekit.files.ccsds.Keyword
Transmitted frequency 3.
TRANSMIT_FREQ_4 - org.orekit.files.ccsds.Keyword
Transmitted frequency 4.
TRANSMIT_FREQ_5 - org.orekit.files.ccsds.Keyword
Transmitted frequency 5.
TRANSMIT_FREQ_RATE_1 - org.orekit.files.ccsds.Keyword
Data: Transmitted frequencies rates [Hz/s].
TRANSMIT_FREQ_RATE_2 - org.orekit.files.ccsds.Keyword
Transmitted frequency rate 2.
TRANSMIT_FREQ_RATE_3 - org.orekit.files.ccsds.Keyword
Transmitted frequency rate 3.
TRANSMIT_FREQ_RATE_4 - org.orekit.files.ccsds.Keyword
Transmitted frequency rate 4.
TRANSMIT_FREQ_RATE_5 - org.orekit.files.ccsds.Keyword
Transmitted frequency rate 5.
TRIGGER_ONLY_DECREASING_EVENTS - org.orekit.propagation.events.FilterType
Constant for triggering only decreasing events.
TRIGGER_ONLY_INCREASING_EVENTS - org.orekit.propagation.events.FilterType
Constant for triggering only increasing events.
TROPO_DRY - org.orekit.files.ccsds.Keyword
Data: TROPO DRY [m].
TROPO_WET - org.orekit.files.ccsds.Keyword
Data: TROPO WET [m].
TroposphericDSConverter - Class in org.orekit.estimation.measurements.modifiers
Converter for states and parameters arrays.
TroposphericDSConverter(SpacecraftState, int, AttitudeProvider) - Constructor for class org.orekit.estimation.measurements.modifiers.TroposphericDSConverter
Simple constructor.
TroposphericModel - Interface in org.orekit.models.earth
Defines a tropospheric model, used to calculate the path delay imposed to electro-magnetic signals between an orbital satellite and a ground station.
TRUE - org.orekit.orbits.PositionAngle
True angle.
TRUE_ANOMALY - org.orekit.files.ccsds.Keyword
Orbit true anomaly.
trueToEccentric(double, double, double) - Static method in class org.orekit.orbits.CircularOrbit
Computes the eccentric latitude argument from the true latitude argument.
trueToEccentric(double, double, double) - Static method in class org.orekit.orbits.EquinoctialOrbit
Computes the eccentric longitude argument from the true longitude argument.
trueToEccentric(T, T, T) - Static method in class org.orekit.orbits.FieldCircularOrbit
Computes the eccentric latitude argument from the true latitude argument.
trueToEccentric(T, T, T) - Static method in class org.orekit.orbits.FieldEquinoctialOrbit
Computes the eccentric longitude argument from the true longitude argument.
trueToEllipticEccentric(double, double) - Static method in class org.orekit.orbits.KeplerianOrbit
Computes the elliptic eccentric anomaly from the true anomaly.
trueToEllipticEccentric(T, T) - Static method in class org.orekit.orbits.FieldKeplerianOrbit
Computes the elliptic eccentric anomaly from the true anomaly.
trueToHyperbolicEccentric(double, double) - Static method in class org.orekit.orbits.KeplerianOrbit
Computes the hyperbolic eccentric anomaly from the true anomaly.
trueToHyperbolicEccentric(T, T) - Static method in class org.orekit.orbits.FieldKeplerianOrbit
Computes the hyperbolic eccentric anomaly from the true anomaly.
tryAdvance(FieldSpacecraftState<T>, FieldOrekitStepInterpolator<T>) - Method in class org.orekit.propagation.events.FieldEventState
Try to accept the current history up to the given time.
tryAdvance(SpacecraftState, OrekitStepInterpolator) - Method in class org.orekit.propagation.events.EventState
Try to accept the current history up to the given time.
tsi - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator
tsi from SPTRCK #3.
TT - org.orekit.files.ccsds.CcsdsTimeScale
Terrestrial Time.
TTScale - Class in org.orekit.time
Terrestrial Time as defined by IAU(1991) recommendation IV.
TURNAROUND_DENOMINATOR - org.orekit.files.ccsds.Keyword
Meta-data: Turn-around ratio denominator.
TURNAROUND_NUMERATOR - org.orekit.files.ccsds.Keyword
Meta-data: Turn-around ratio numerator.
TurnAroundRange - Class in org.orekit.estimation.measurements
Class modeling a turn-around range measurement using a master ground station and a slave ground station.
TurnAroundRange(GroundStation, GroundStation, AbsoluteDate, double, double, double) - Constructor for class org.orekit.estimation.measurements.TurnAroundRange
TurnAroundRange(GroundStation, GroundStation, AbsoluteDate, double, double, double, int) - Constructor for class org.orekit.estimation.measurements.TurnAroundRange
TurnAroundRange(GroundStation, GroundStation, AbsoluteDate, double, double, double, ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.TurnAroundRange
Simple constructor.
TurnAroundRangeBuilder - Class in org.orekit.estimation.measurements.generation
Builder for TurnAroundRange measurements.
TurnAroundRangeBuilder(CorrelatedRandomVectorGenerator, GroundStation, GroundStation, double, double, ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.generation.TurnAroundRangeBuilder
Simple constructor.
TurnAroundRangeIonosphericDelayModifier - Class in org.orekit.estimation.measurements.modifiers
Class modifying theoretical TurnAroundRange measurement with ionospheric delay.
TurnAroundRangeIonosphericDelayModifier(IonosphericModel) - Constructor for class org.orekit.estimation.measurements.modifiers.TurnAroundRangeIonosphericDelayModifier
Constructor.
TurnAroundRangeTroposphericDelayModifier - Class in org.orekit.estimation.measurements.modifiers
Class modifying theoretical turn-around TurnAroundRange measurement with tropospheric delay.
TurnAroundRangeTroposphericDelayModifier(DiscreteTroposphericModel) - Constructor for class org.orekit.estimation.measurements.modifiers.TurnAroundRangeTroposphericDelayModifier
Constructor.

U

UNABLE_TO_COMPUTE_DSST_MEAN_PARAMETERS - org.orekit.errors.OrekitMessages
 
UNABLE_TO_COMPUTE_ECKSTEIN_HECHLER_MEAN_PARAMETERS - org.orekit.errors.OrekitMessages
 
UNABLE_TO_COMPUTE_HYPERBOLIC_ECCENTRIC_ANOMALY - org.orekit.errors.OrekitMessages
 
UNABLE_TO_FIND_FILE - org.orekit.errors.OrekitMessages
 
UNABLE_TO_FIND_RESOURCE - org.orekit.errors.OrekitMessages
 
UNABLE_TO_GENERATE_NEW_DATA_AFTER - org.orekit.errors.OrekitMessages
 
UNABLE_TO_GENERATE_NEW_DATA_BEFORE - org.orekit.errors.OrekitMessages
 
UNABLE_TO_PARSE_LINE_IN_FILE - org.orekit.errors.OrekitMessages
 
UNABLE_TO_READ_JPL_HEADER - org.orekit.errors.OrekitMessages
 
UNDEFINED - org.orekit.files.sp3.SP3File.SP3FileType
undefined file format.
UNEXPECTED_DATA_AFTER_LINE_IN_FILE - org.orekit.errors.OrekitMessages
 
UNEXPECTED_END_OF_FILE - org.orekit.errors.OrekitMessages
 
UNEXPECTED_END_OF_FILE_AFTER_LINE - org.orekit.errors.OrekitMessages
 
UNEXPECTED_FILE_FORMAT_ERROR_FOR_LOADER - org.orekit.errors.OrekitMessages
 
UNEXPECTED_TWO_ELEVATION_VALUES_FOR_ONE_AZIMUTH - org.orekit.errors.OrekitMessages
 
UnivariateProcessNoise - Class in org.orekit.estimation.sequential
Provider for a temporal evolution of the process noise matrix.
UnivariateProcessNoise(RealMatrix, LOFType, PositionAngle, UnivariateFunction[], UnivariateFunction[]) - Constructor for class org.orekit.estimation.sequential.UnivariateProcessNoise
Simple constructor.
UnixCompressFilter - Class in org.orekit.data
Filter for Unix compressed data.
UnixCompressFilter() - Constructor for class org.orekit.data.UnixCompressFilter
 
UNKNOWN - org.orekit.files.ccsds.TDMParser.TDMFileFormat
UKNOWN file format, default format, throw an Orekit Exception if kept this way.
UNKNOWN - org.orekit.forces.gravity.potential.TideSystem
Constant for unknown tide system.
UNKNOWN_ADDITIONAL_STATE - org.orekit.errors.OrekitMessages
 
UNKNOWN_MONTH - org.orekit.errors.OrekitMessages
 
UNKNOWN_RINEX_FREQUENCY - org.orekit.errors.OrekitMessages
 
UNKNOWN_SATELLITE_ANTENNA_CODE - org.orekit.errors.OrekitMessages
 
UNKNOWN_SATELLITE_SYSTEM - org.orekit.errors.OrekitMessages
 
UnnormalizedSphericalHarmonicsProvider - Interface in org.orekit.forces.gravity.potential
Interface used to provide un-normalized spherical harmonics coefficients.
UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics - Interface in org.orekit.forces.gravity.potential
Un-normalized spherical harmonics coefficients evaluated at a specific instant.
UNSUPPORTED_FILE_FORMAT - org.orekit.errors.OrekitMessages
 
UNSUPPORTED_LOCAL_ORBITAL_FRAME - org.orekit.errors.OrekitMessages
 
UNSUPPORTED_PARAMETER_NAME - org.orekit.errors.OrekitMessages
 
UNSUPPORTED_TIME_TRANSFORM - org.orekit.errors.OrekitMessages
 
unwrap(MathRuntimeException) - Static method in exception org.orekit.errors.OrekitException
Recover a OrekitException, possibly embedded in a MathRuntimeException.
unwrap(MathRuntimeException) - Static method in exception org.orekit.errors.TimeStampedCacheException
Recover a TimeStampedCacheException, possibly embedded in a MathRuntimeException.
unwrap(OrekitException) - Static method in exception org.orekit.errors.TimeStampedCacheException
Recover a TimeStampedCacheException, possibly embedded in a OrekitException.
UpdatableFrame - Class in org.orekit.frames
Frame whose transform from its parent can be updated.
UpdatableFrame(Frame, Transform, String) - Constructor for class org.orekit.frames.UpdatableFrame
Build a non-inertial frame from its transform with respect to its parent.
UpdatableFrame(Frame, Transform, String, boolean) - Constructor for class org.orekit.frames.UpdatableFrame
Build a frame from its transform with respect to its parent.
updateAdditionalStates(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.FieldAbstractPropagator
Update state by adding all additional states.
updateAdditionalStates(SpacecraftState) - Method in class org.orekit.propagation.AbstractPropagator
Update state by adding all additional states.
updateMass(double) - Method in class org.orekit.forces.maneuvers.SmallManeuverAnalyticalModel
Update a spacecraft mass due to maneuver.
updateShortPeriodTerms(SpacecraftState...) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution
Update the short period terms.
updateShortPeriodTerms(SpacecraftState...) - Method in interface org.orekit.propagation.semianalytical.dsst.forces.DSSTForceModel
Update the short period terms.
updateShortPeriodTerms(SpacecraftState...) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseral
Update the short period terms.
updateShortPeriodTerms(SpacecraftState...) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBody
Update the short period terms.
updateShortPeriodTerms(SpacecraftState...) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonal
Update the short period terms.
updateTransform(Frame, Frame, Transform, AbsoluteDate) - Method in class org.orekit.frames.UpdatableFrame
Update the transform from parent frame implicitly according to two other frames.
UpperBounds - Class in org.orekit.propagation.semianalytical.dsst.utilities
Utility class to compute upper bounds for truncation algorithms.
URANUS - org.orekit.bodies.JPLEphemeridesLoader.EphemerisType
Constant for Uranus.
URANUS - org.orekit.files.ccsds.CenterName
Uranus body.
URANUS - Static variable in class org.orekit.bodies.CelestialBodyFactory
Predefined name for Uranus.
USE_P - org.orekit.utils.CartesianDerivativesFilter
Use only positions, ignoring velocities.
USE_PV - org.orekit.utils.CartesianDerivativesFilter
Use positions and velocities.
USE_PVA - org.orekit.utils.CartesianDerivativesFilter
Use positions, velocities and accelerations.
USE_R - org.orekit.utils.AngularDerivativesFilter
Use only rotations, ignoring rotation rates.
USE_RR - org.orekit.utils.AngularDerivativesFilter
Use rotations and rotation rates.
USE_RRA - org.orekit.utils.AngularDerivativesFilter
Use rotations, rotation rates and acceleration.
USEABLE_START_TIME - org.orekit.files.ccsds.Keyword
Start of useable time span covered by ephemerides data, it may be necessary to allow for proper interpolation.
USEABLE_STOP_TIME - org.orekit.files.ccsds.Keyword
End of useable time span covered by ephemerides data, it may be necessary to allow for proper interpolation.
USER_DEFINED_X - org.orekit.files.ccsds.Keyword
User defined parameter, where X is replaced by a variable length user specified character string.
usesInterpolation() - Method in class org.orekit.frames.EOPHistory
Check if the instance uses interpolation on tidal corrections.
UT1 - org.orekit.files.ccsds.CcsdsTimeScale
Universal Time.
UT1Scale - Class in org.orekit.time
Universal Time 1.
UT1Scale(EOPHistory, UTCScale) - Constructor for class org.orekit.time.UT1Scale
Simple constructor.
UTC - org.orekit.files.ccsds.CcsdsTimeScale
Universal Coordinated Time.
UTC - org.orekit.files.sp3.SP3File.TimeSystem
Coordinated Universal Time.
UTCScale - Class in org.orekit.time
Coordinated Universal Time.
UTCTAIBulletinAFilesLoader - Class in org.orekit.time
Loader for UTC-TAI extracted from bulletin A files.
UTCTAIBulletinAFilesLoader(String) - Constructor for class org.orekit.time.UTCTAIBulletinAFilesLoader
Build a loader for IERS bulletins A files.
UTCTAIHistoryFilesLoader - Class in org.orekit.time
Loader for UTC versus TAI history files.
UTCTAIHistoryFilesLoader() - Constructor for class org.orekit.time.UTCTAIHistoryFilesLoader
Build a loader for UTC-TAI history file.
UTCTAIOffsetsLoader - Interface in org.orekit.time
Interface for loading UTC-TAI offsets data files.
UTF8Control() - Constructor for class org.orekit.errors.OrekitMessages.UTF8Control
 

V

validFrom() - Method in class org.orekit.models.earth.GeoMagneticField
Returns the start of the validity period for this model.
validityEnd() - Method in class org.orekit.gnss.attitude.AbstractGNSSAttitudeProvider
Get end of validity for this provider.
validityEnd() - Method in interface org.orekit.gnss.attitude.GNSSAttitudeProvider
Get end of validity for this provider.
validityStart() - Method in class org.orekit.gnss.attitude.AbstractGNSSAttitudeProvider
Get start of validity for this provider.
validityStart() - Method in interface org.orekit.gnss.attitude.GNSSAttitudeProvider
Get start of validity for this provider.
validTo() - Method in class org.orekit.models.earth.GeoMagneticField
Returns the end of the validity period for this model.
value(double) - Method in class org.orekit.data.PolynomialNutation
Evaluate the value of the polynomial.
value(double, double) - Method in interface org.orekit.gnss.antenna.PhaseCenterVariationFunction
Evaluate phase center variation in one signal direction.
value(BodiesElements) - Method in interface org.orekit.data.PoissonSeries.CompiledSeries
Evaluate a set of Poisson series.
value(BodiesElements) - Method in class org.orekit.data.PoissonSeries
Evaluate the value of the series.
value(FieldBodiesElements<S>) - Method in interface org.orekit.data.PoissonSeries.CompiledSeries
Evaluate a set of Poisson series.
value(FieldBodiesElements<T>) - Method in class org.orekit.data.PoissonSeries
Evaluate the value of the series.
value(Orbit) - Method in interface org.orekit.propagation.semianalytical.dsst.forces.ShortPeriodTerms
Evaluate the contributions of the short period terms.
value(SpacecraftState) - Method in interface org.orekit.utils.StateFunction
Evaluate the function.
value(SpacecraftState) - Method in interface org.orekit.utils.StateJacobian
Evaluate the Jacobian of the function.
value(AbsoluteDate) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.ShortPeriodicsInterpolatedCoefficient
Compute the value of the coefficient.
value(AbsoluteDate) - Method in interface org.orekit.time.TimeScalarFunction
Compute a function of time.
value(AbsoluteDate) - Method in interface org.orekit.time.TimeVectorFunction
Compute a function of time.
value(AbsoluteDate, Vector3D, double) - Method in class org.orekit.forces.gravity.HolmesFeatherstoneAttractionModel
Compute the value of the gravity field.
value(FieldAbsoluteDate<T>) - Method in interface org.orekit.time.TimeScalarFunction
Compute a function of time.
value(FieldAbsoluteDate<T>) - Method in interface org.orekit.time.TimeVectorFunction
Compute a function of time.
value(ParameterDriver) - Method in interface org.orekit.utils.ParameterFunction
Evaluate the function.
value(T) - Method in class org.orekit.data.PolynomialNutation
Evaluate the value of the polynomial.
VALUE_NOT_FOUND - org.orekit.errors.OrekitMessages
 
valueChanged(double, ParameterDriver) - Method in interface org.orekit.utils.ParameterObserver
Notify that a parameter value has been changed.
valueOf(String) - Static method in enum org.orekit.bodies.JPLEphemeridesLoader.EphemerisType
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.data.PolynomialParser.Unit
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.errors.OrekitMessages
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.estimation.measurements.EstimatedMeasurement.Status
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.estimation.measurements.generation.SignSemantic
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.CCSDSFrame
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.CcsdsTimeScale
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.CenterName
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.Keyword
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.OEMWriter.InterpolationMethod
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.TDMParser.TDMFileFormat
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.sp3.SP3File.SP3FileType
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.sp3.SP3File.SP3OrbitType
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.sp3.SP3File.TimeSystem
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.forces.drag.atmosphere.data.MarshallSolarActivityFutureEstimation.StrengthLevel
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.forces.gravity.potential.OceanLoadDeformationCoefficients
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.forces.gravity.potential.TideSystem
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.frames.HelmertTransformation.Predefined
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.frames.ITRFVersion
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.frames.LOFType
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.frames.Predefined
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.gnss.antenna.SatelliteAntennaCode
Deprecated.
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.gnss.antenna.SatelliteType
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.gnss.Frequency
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.gnss.MeasurementType
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.gnss.ObservationType
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.gnss.SatelliteSystem
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.models.earth.GeoMagneticFieldFactory.FieldModel
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.models.earth.ViennaModelType
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.orbits.OrbitType
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.orbits.PositionAngle
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.propagation.events.FilterType
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.propagation.events.handlers.EventHandler.Action
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.propagation.events.handlers.FieldEventHandler.Action
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.time.Month
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.utils.AngularDerivativesFilter
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.utils.CartesianDerivativesFilter
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.utils.IERSConventions
Returns the enum constant of this type with the specified name.
values() - Static method in enum org.orekit.bodies.JPLEphemeridesLoader.EphemerisType
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.data.PolynomialParser.Unit
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.errors.OrekitMessages
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.estimation.measurements.EstimatedMeasurement.Status
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.estimation.measurements.generation.SignSemantic
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.CCSDSFrame
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.CcsdsTimeScale
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.CenterName
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.Keyword
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.OEMWriter.InterpolationMethod
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.ccsds.TDMParser.TDMFileFormat
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.sp3.SP3File.SP3FileType
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.sp3.SP3File.SP3OrbitType
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.files.sp3.SP3File.TimeSystem
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.forces.drag.atmosphere.data.MarshallSolarActivityFutureEstimation.StrengthLevel
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.forces.gravity.potential.OceanLoadDeformationCoefficients
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.forces.gravity.potential.TideSystem
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.frames.HelmertTransformation.Predefined
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.frames.ITRFVersion
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.frames.LOFType
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.frames.Predefined
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.gnss.antenna.SatelliteAntennaCode
Deprecated.
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.gnss.antenna.SatelliteType
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.gnss.Frequency
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.gnss.MeasurementType
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.gnss.ObservationType
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.gnss.SatelliteSystem
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.models.earth.GeoMagneticFieldFactory.FieldModel
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.models.earth.ViennaModelType
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.orbits.OrbitType
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.orbits.PositionAngle
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.propagation.events.FilterType
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.propagation.events.handlers.EventHandler.Action
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.propagation.events.handlers.FieldEventHandler.Action
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.time.Month
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.utils.AngularDerivativesFilter
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.utils.CartesianDerivativesFilter
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.utils.IERSConventions
Returns an array containing the constants of this enum type, in the order they are declared.
VEIS_1950 - org.orekit.frames.Predefined
Veis 1950.
VENUS - org.orekit.bodies.JPLEphemeridesLoader.EphemerisType
Constant for Venus.
VENUS - org.orekit.files.ccsds.CenterName
Venus body.
VENUS - Static variable in class org.orekit.bodies.CelestialBodyFactory
Predefined name for Venus.
VersionedITRF - Class in org.orekit.frames
Specific version of International Terrestrial Reference Frame.
VIENNA_ACOEF_OR_ZENITH_DELAY_NOT_AVAILABLE_FOR_DATE - org.orekit.errors.OrekitMessages
 
VIENNA_ACOEF_OR_ZENITH_DELAY_NOT_LOADED - org.orekit.errors.OrekitMessages
 
VIENNA_ONE - org.orekit.models.earth.ViennaModelType
Vienna one tropospheric model.
VIENNA_THREE - org.orekit.models.earth.ViennaModelType
Vienna three tropospheric model.
ViennaModelCoefficientsLoader - Class in org.orekit.models.earth
Loads Vienna tropospheric coefficients a given input stream.
ViennaModelCoefficientsLoader(double, double, ViennaModelType) - Constructor for class org.orekit.models.earth.ViennaModelCoefficientsLoader
Constructor with default supported names.
ViennaModelCoefficientsLoader(String, double, double, ViennaModelType) - Constructor for class org.orekit.models.earth.ViennaModelCoefficientsLoader
Constructor with supported names given by user.
ViennaModelType - Enum in org.orekit.models.earth
Enumerate for Vienna tropospheric model 1 and 3.
ViennaOneModel - Class in org.orekit.models.earth
The Vienna1 tropospheric delay model for radio techniques.
ViennaOneModel(double[], double[], double) - Constructor for class org.orekit.models.earth.ViennaOneModel
Build a new instance.
ViennaThreeModel - Class in org.orekit.models.earth
The Vienna3 tropospheric delay model for radio techniques.
ViennaThreeModel(double[], double[], double, double) - Constructor for class org.orekit.models.earth.ViennaThreeModel
Build a new instance.
VLBI_DELAY - org.orekit.files.ccsds.Keyword
Data: VLBI delay [s].
VNC - org.orekit.frames.LOFType
Constant for Velocity - Normal - Co-normal frame (X axis aligned with velocity, Y axis aligned with orbital momentum).
VVLH - org.orekit.frames.LOFType
Constant for Vehicle Velocity, Local Horizontal frame (Z axis aligned with opposite of position, Y axis aligned with opposite of orbital momentum).

W

w - Variable in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution
Equinoctial frame w vector.
WEAK - org.orekit.forces.drag.atmosphere.data.MarshallSolarActivityFutureEstimation.StrengthLevel
Weak level of activity.
WeatherModel - Interface in org.orekit.models.earth
Defines a surface meteorology model that can be used to compute the different weather parameters (pressure, temperature, ...).
weatherParameters(double, AbsoluteDate) - Method in class org.orekit.models.earth.GlobalPressureTemperature2Model
 
weatherParameters(double, AbsoluteDate) - Method in class org.orekit.models.earth.GlobalPressureTemperatureModel
 
weatherParameters(double, AbsoluteDate) - Method in interface org.orekit.models.earth.WeatherModel
Calculates the weather parameters of the model.
WGS84_EARTH_ANGULAR_VELOCITY - Static variable in interface org.orekit.utils.Constants
Earth angular velocity from WGS84 model: 7.292115e-5 rad/s.
WGS84_EARTH_C20 - Static variable in interface org.orekit.utils.Constants
Earth un-normalized second zonal coefficient from WGS84 model: .
WGS84_EARTH_EQUATORIAL_RADIUS - Static variable in interface org.orekit.utils.Constants
Earth equatorial radius from WGS84 model: 6378137.0 m.
WGS84_EARTH_FLATTENING - Static variable in interface org.orekit.utils.Constants
Earth flattening from WGS84 model: 1.0 / 298.257223563.
WGS84_EARTH_MU - Static variable in interface org.orekit.utils.Constants
Earth gravitational constant from WGS84 model: 3.986004418e14 m³/s².
withConstantElevation(double) - Method in class org.orekit.propagation.events.ElevationDetector
Setup the minimum elevation for detection.
withConstantElevation(double) - Method in class org.orekit.propagation.events.FieldElevationDetector
Setup the minimum elevation for detection.
withConventions(IERSConventions) - Method in class org.orekit.files.ccsds.ODMParser
Set IERS conventions.
withConventions(IERSConventions) - Method in class org.orekit.files.ccsds.OEMParser
Set IERS conventions.
withConventions(IERSConventions) - Method in class org.orekit.files.ccsds.OMMParser
Set IERS conventions.
withConventions(IERSConventions) - Method in class org.orekit.files.ccsds.OPMParser
Set IERS conventions.
withConventions(IERSConventions) - Method in class org.orekit.files.ccsds.TDMParser
Set IERS conventions.
withDoodson(int, int) - Method in class org.orekit.data.PoissonSeriesParser
Set up columns for Doodson multipliers and Doodson number.
withElevationMask(ElevationMask) - Method in class org.orekit.gnss.DOPComputer
Set the elevation mask.
withElevationMask(ElevationMask) - Method in class org.orekit.propagation.events.ElevationDetector
Setup the elevation mask for detection using the passed in mask object.
withElevationMask(ElevationMask) - Method in class org.orekit.propagation.events.FieldElevationDetector
Setup the elevation mask for detection using the passed in mask object.
withFileFormat(TDMParser.TDMFileFormat) - Method in class org.orekit.files.ccsds.TDMParser
Set file format.
withFirstDelaunay(int) - Method in class org.orekit.data.PoissonSeriesParser
Set up first column of Delaunay multiplier.
withFirstPlanetary(int) - Method in class org.orekit.data.PoissonSeriesParser
Set up first column of planetary multiplier.
withFunction(ToDoubleFunction<SpacecraftState>) - Method in class org.orekit.propagation.events.FunctionalDetector
Create a new event detector with a new g function, keeping all other attributes the same.
withGamma(int) - Method in class org.orekit.data.PoissonSeriesParser
Set up column of GMST tide multiplier.
withGFunction(FunctionalDetector.GFunction) - Method in class org.orekit.propagation.events.FunctionalDetector
Deprecated.
Use FunctionalDetector.withFunction(ToDoubleFunction) instead. Will be removed in next major release.
withHandler(EventHandler<? super T>) - Method in class org.orekit.propagation.events.AbstractDetector
Setup the event handler to call at event occurrences.
withHandler(FieldEventHandler<? super D, T>) - Method in class org.orekit.propagation.events.FieldAbstractDetector
Setup the event handler to call at event occurrences.
withInternationalDesignator(int, int, String) - Method in class org.orekit.files.ccsds.ODMParser
Set international designator.
withInternationalDesignator(int, int, String) - Method in class org.orekit.files.ccsds.OEMParser
Set international designator.
withInternationalDesignator(int, int, String) - Method in class org.orekit.files.ccsds.OMMParser
Set international designator.
withInternationalDesignator(int, int, String) - Method in class org.orekit.files.ccsds.OPMParser
Set international designator.
withMargin(double) - Method in class org.orekit.propagation.events.GeographicZoneDetector
Setup the detector margin.
withMaxCheck(double) - Method in class org.orekit.propagation.events.AbstractDetector
Setup the maximum checking interval.
withMaxCheck(T) - Method in class org.orekit.propagation.events.FieldAbstractDetector
Setup the maximum checking interval.
withMaxIter(int) - Method in class org.orekit.propagation.events.AbstractDetector
Setup the maximum number of iterations in the event time search.
withMaxIter(int) - Method in class org.orekit.propagation.events.FieldAbstractDetector
Setup the maximum number of iterations in the event time search.
withMinElevation(double) - Method in class org.orekit.gnss.DOPComputer
Set the minimum elevation.
withMissionReferenceDate(AbsoluteDate) - Method in class org.orekit.files.ccsds.ODMParser
Set initial date.
withMissionReferenceDate(AbsoluteDate) - Method in class org.orekit.files.ccsds.OEMParser
Set initial date.
withMissionReferenceDate(AbsoluteDate) - Method in class org.orekit.files.ccsds.OMMParser
Set initial date.
withMissionReferenceDate(AbsoluteDate) - Method in class org.orekit.files.ccsds.OPMParser
Set initial date.
withMissionReferenceDate(AbsoluteDate) - Method in class org.orekit.files.ccsds.TDMParser
Set initial date.
withMu(double) - Method in class org.orekit.files.ccsds.ODMParser
Set gravitational coefficient.
withMu(double) - Method in class org.orekit.files.ccsds.OEMParser
Set gravitational coefficient.
withMu(double) - Method in class org.orekit.files.ccsds.OMMParser
Set gravitational coefficient.
withMu(double) - Method in class org.orekit.files.ccsds.OPMParser
Set gravitational coefficient.
withOptionalColumn(int) - Method in class org.orekit.data.PoissonSeriesParser
Set up optional column.
withPenumbra() - Method in class org.orekit.propagation.events.EclipseDetector
Setup the detector to penumbra detection.
withPenumbra() - Method in class org.orekit.propagation.events.FieldEclipseDetector
Setup the detector to penumbra detection.
withPolynomialPart(char, PolynomialParser.Unit) - Method in class org.orekit.data.PoissonSeriesParser
Set up polynomial part parsing.
withReferenceFrame(Frame) - Method in class org.orekit.attitudes.Attitude
Get a similar attitude with a specific reference frame.
withReferenceFrame(Frame) - Method in class org.orekit.attitudes.FieldAttitude
Get a similar attitude with a specific reference frame.
withRefraction(AtmosphericRefractionModel) - Method in class org.orekit.propagation.events.ElevationDetector
Setup the elevation detector to use an atmospheric refraction model in its calculations.
withRefraction(AtmosphericRefractionModel) - Method in class org.orekit.propagation.events.FieldElevationDetector
Setup the elevation detector to use an atmospheric refraction model in its calculations.
withSimpleEOP(boolean) - Method in class org.orekit.files.ccsds.ODMParser
Set EOP interpolation method.
withSimpleEOP(boolean) - Method in class org.orekit.files.ccsds.OEMParser
Set EOP interpolation method.
withSimpleEOP(boolean) - Method in class org.orekit.files.ccsds.OMMParser
Set EOP interpolation method.
withSimpleEOP(boolean) - Method in class org.orekit.files.ccsds.OPMParser
Set EOP interpolation method.
withSimpleEOP(boolean) - Method in class org.orekit.files.ccsds.TDMParser
Set EOP interpolation method.
withSinCos(int, int, double, int, double) - Method in class org.orekit.data.PoissonSeriesParser
Set up columns of the sine and cosine coefficients.
withSwitch(int, int) - Method in class org.orekit.forces.drag.atmosphere.NRLMSISE00
Change a switch.
withThreshold(double) - Method in class org.orekit.propagation.events.AbstractDetector
Setup the convergence threshold.
withThreshold(T) - Method in class org.orekit.propagation.events.FieldAbstractDetector
Setup the convergence threshold.
withUmbra() - Method in class org.orekit.propagation.events.EclipseDetector
Setup the detector to full umbra detection.
withUmbra() - Method in class org.orekit.propagation.events.FieldEclipseDetector
Setup the detector to full umbra detection.
WMM - org.orekit.models.earth.GeoMagneticFieldFactory.FieldModel
World Magnetic Model.
write(Appendable, EphemerisFile) - Method in class org.orekit.files.ccsds.OEMWriter
Write the passed in EphemerisFile using the passed in Appendable.
write(Appendable, EphemerisFile) - Method in interface org.orekit.files.general.EphemerisFileWriter
Write the passed in EphemerisFile using the passed in Appendable.
write(String, EphemerisFile) - Method in interface org.orekit.files.general.EphemerisFileWriter
Write the passed in EphemerisFile to a file at the output path specified.
writeEphemerisLine(TimeStampedPVCoordinates) - Method in class org.orekit.files.ccsds.StreamingOemWriter.Segment
Write a single ephemeris line according to section 5.2.4.
writeHeader() - Method in class org.orekit.files.ccsds.StreamingOemWriter
Writes the standard OEM header for the file.
writeMetadata() - Method in class org.orekit.files.ccsds.StreamingOemWriter.Segment
Write the ephemeris segment metadata.
WRONG_COLUMNS_NUMBER - org.orekit.errors.OrekitMessages
 

X

X - org.orekit.files.ccsds.Keyword
Position vector X-component.
X_DOT - org.orekit.files.ccsds.Keyword
Velocity vector X-component.
xl - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator
L from SPTRCK #3.
xmdot - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator
common parameter for mean anomaly (M) computation.
XML - org.orekit.files.ccsds.TDMParser.TDMFileFormat
XML format.
xn0dp - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator
original recovered mean motion.
xnodcf - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator
common parameter for raan (OMEGA) computation.
xnode - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator
final RAAN.
xnodot - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator
common parameter for raan (OMEGA) computation.

Y

Y - org.orekit.files.ccsds.Keyword
Position vector Y-component.
Y_DOT - org.orekit.files.ccsds.Keyword
Velocity vector Y-component.
YawCompensation - Class in org.orekit.attitudes
This class handles yaw compensation attitude provider.
YawCompensation(Frame, GroundPointing) - Constructor for class org.orekit.attitudes.YawCompensation
Creates a new instance.
YawSteering - Class in org.orekit.attitudes
This class handles yaw steering law.
YawSteering(Frame, GroundPointing, PVCoordinatesProvider, Vector3D) - Constructor for class org.orekit.attitudes.YawSteering
Creates a new instance.
YUMAParser - Class in org.orekit.gnss
This class reads Yuma almanac files and provides GPS almanacs.
YUMAParser(String) - Constructor for class org.orekit.gnss.YUMAParser
Simple constructor.

Z

Z - org.orekit.files.ccsds.Keyword
Position vector Z-component.
Z_DOT - org.orekit.files.ccsds.Keyword
Velocity vector Z-component.
ZERO - Static variable in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenUtilities
0 represented as a polynomial.
ZERO - Static variable in class org.orekit.utils.PVCoordinates
Fixed position/velocity at origin (both p, v and a are zero vectors).
ZERO_TIDE - org.orekit.forces.gravity.potential.TideSystem
Constant for zero-tide gravity fields.
ZIP_ARCHIVE_PATTERN - Static variable in interface org.orekit.data.DataProvider
Pattern for name of zip/jar archives.
ZipJarCrawler - Class in org.orekit.data
Helper class for loading data files from a zip/jar archive.
ZipJarCrawler(File) - Constructor for class org.orekit.data.ZipJarCrawler
Build a zip crawler for an archive file on filesystem.
ZipJarCrawler(ClassLoader, String) - Constructor for class org.orekit.data.ZipJarCrawler
Build a zip crawler for an archive file in classpath.
ZipJarCrawler(String) - Constructor for class org.orekit.data.ZipJarCrawler
Build a zip crawler for an archive file in classpath.
ZipJarCrawler(URL) - Constructor for class org.orekit.data.ZipJarCrawler
Build a zip crawler for an archive file on network.
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