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A

A - Static variable in enum org.orekit.orbits.OrbitType
Name for semi major axis.
a - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator
final semi major axis.
a0dp - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator
original recovered semi major axis.
AbsoluteDate - Class in org.orekit.time
This class represents a specific instant in time.
AbsoluteDate() - Constructor for class org.orekit.time.AbsoluteDate
Create an instance with a default value (AbsoluteDate.J2000_EPOCH).
AbsoluteDate(String, TimeScale) - Constructor for class org.orekit.time.AbsoluteDate
Build an instance from a location (parsed from a string) in a time scale.
AbsoluteDate(DateTimeComponents, TimeScale) - Constructor for class org.orekit.time.AbsoluteDate
Build an instance from a location in a time scale.
AbsoluteDate(DateComponents, TimeComponents, TimeScale) - Constructor for class org.orekit.time.AbsoluteDate
Build an instance from a location in a time scale.
AbsoluteDate(int, int, int, int, int, double, TimeScale) - Constructor for class org.orekit.time.AbsoluteDate
Build an instance from a location in a time scale.
AbsoluteDate(int, Month, int, int, int, double, TimeScale) - Constructor for class org.orekit.time.AbsoluteDate
Build an instance from a location in a time scale.
AbsoluteDate(DateComponents, TimeScale) - Constructor for class org.orekit.time.AbsoluteDate
Build an instance from a location in a time scale.
AbsoluteDate(int, int, int, TimeScale) - Constructor for class org.orekit.time.AbsoluteDate
Build an instance from a location in a time scale.
AbsoluteDate(int, Month, int, TimeScale) - Constructor for class org.orekit.time.AbsoluteDate
Build an instance from a location in a time scale.
AbsoluteDate(Date, TimeScale) - Constructor for class org.orekit.time.AbsoluteDate
Build an instance from a location in a time scale.
AbsoluteDate(AbsoluteDate, double) - Constructor for class org.orekit.time.AbsoluteDate
Build an instance from an elapsed duration since to another instant.
AbsoluteDate(AbsoluteDate, double, TimeScale) - Constructor for class org.orekit.time.AbsoluteDate
Build an instance from an apparent clock offset with respect to another instant in the perspective of a specific time scale.
AbsoluteJacobiansMapper - Class in org.orekit.propagation.numerical
Mapper between two-dimensional Jacobian matrices and one-dimensional additional state arrays.
AbsoluteJacobiansMapper(String, ParameterDriversList) - Constructor for class org.orekit.propagation.numerical.AbsoluteJacobiansMapper
Simple constructor.
AbsolutePartialDerivativesEquations - 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.
AbsolutePartialDerivativesEquations(String, NumericalPropagator) - Constructor for class org.orekit.propagation.numerical.AbsolutePartialDerivativesEquations
Simple constructor.
AbsolutePVCoordinates - Class in org.orekit.utils
Position - Velocity - Acceleration linked to a date and a frame.
AbsolutePVCoordinates(Frame, AbsoluteDate, Vector3D, Vector3D, Vector3D) - Constructor for class org.orekit.utils.AbsolutePVCoordinates
Build from position, velocity, acceleration.
AbsolutePVCoordinates(Frame, AbsoluteDate, Vector3D, Vector3D) - Constructor for class org.orekit.utils.AbsolutePVCoordinates
Build from position and velocity.
AbsolutePVCoordinates(Frame, AbsoluteDate, PVCoordinates) - Constructor for class org.orekit.utils.AbsolutePVCoordinates
Build from frame, date and PVA coordinates.
AbsolutePVCoordinates(Frame, TimeStampedPVCoordinates) - Constructor for class org.orekit.utils.AbsolutePVCoordinates
Build from frame and TimeStampedPVCoordinates.
AbsolutePVCoordinates(AbsoluteDate, double, AbsolutePVCoordinates) - Constructor for class org.orekit.utils.AbsolutePVCoordinates
Multiplicative constructor
AbsolutePVCoordinates(AbsoluteDate, AbsolutePVCoordinates, AbsolutePVCoordinates) - Constructor for class org.orekit.utils.AbsolutePVCoordinates
Subtractive constructor
AbsolutePVCoordinates(AbsoluteDate, double, AbsolutePVCoordinates, double, AbsolutePVCoordinates) - Constructor for class org.orekit.utils.AbsolutePVCoordinates
Linear constructor
AbsolutePVCoordinates(AbsoluteDate, double, AbsolutePVCoordinates, double, AbsolutePVCoordinates, double, AbsolutePVCoordinates) - Constructor for class org.orekit.utils.AbsolutePVCoordinates
Linear constructor
AbsolutePVCoordinates(AbsoluteDate, double, AbsolutePVCoordinates, double, AbsolutePVCoordinates, double, AbsolutePVCoordinates, double, AbsolutePVCoordinates) - Constructor for class org.orekit.utils.AbsolutePVCoordinates
Linear constructor
AbsolutePVCoordinates(Frame, AbsoluteDate, FieldVector3D<DerivativeStructure>) - Constructor for class org.orekit.utils.AbsolutePVCoordinates
Builds a AbsolutePVCoordinates triplet from a FieldVector3D<DerivativeStructure>.
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.
AbstractConstantThrustPropulsionModel - Class in org.orekit.forces.maneuvers.propulsion
This abstract class simply serve as a container for a constant thrust maneuver.
AbstractConstantThrustPropulsionModel(double, double, Vector3D, String) - Constructor for class org.orekit.forces.maneuvers.propulsion.AbstractConstantThrustPropulsionModel
Generic constructor.
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.
AbstractCycleSlipDetector - Class in org.orekit.estimation.measurements.gnss
Base class for cycle-slip detectors.
AbstractDetector<T extends AbstractDetector<T>> - 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.
AbstractDragForceModel - Class in org.orekit.forces.drag
Base class for drag force models.
AbstractDragForceModel(Atmosphere) - Constructor for class org.orekit.forces.drag.AbstractDragForceModel
Constructor.
AbstractDSConverter - Class in org.orekit.propagation.integration
Converter for states and parameters arrays for both numerical and semi-analytical propagators.
AbstractDSConverter(int) - Constructor for class org.orekit.propagation.integration.AbstractDSConverter
Simple constructor.
AbstractDualFrequencyCombination - Class in org.orekit.estimation.measurements.gnss
Base class for dual frequency combination of measurements.
AbstractDualFrequencyCombination(CombinationType, SatelliteSystem) - Constructor for class org.orekit.estimation.measurements.gnss.AbstractDualFrequencyCombination
Constructor.
AbstractEopLoader - Class in org.orekit.frames
Base class for EOP loaders.
AbstractEopLoader(String, DataProvidersManager, Supplier<TimeScale>) - Constructor for class org.orekit.frames.AbstractEopLoader
Simple constructor.
AbstractFieldOfView - Class in org.orekit.geometry.fov
Abstract class representing a spacecraft sensor Field Of View.
AbstractFieldOfView(double) - Constructor for class org.orekit.geometry.fov.AbstractFieldOfView
Build a new instance.
AbstractForceModel - Class in org.orekit.forces
Base class for force models.
AbstractForceModel() - Constructor for class org.orekit.forces.AbstractForceModel
 
AbstractFrames - Class in org.orekit.frames
This class is an implementation of Frames that creates frames when they are first used and uses synchronization to ensure that each frame is only created once.
AbstractFrames(TimeScales, Supplier<Frame>) - Constructor for class org.orekit.frames.AbstractFrames
Simple constructor.
AbstractGaussianContribution - Class in org.orekit.propagation.semianalytical.dsst.forces
Common handling of DSSTForceModel methods for Gaussian contributions to DSST propagation.
AbstractGaussianContribution(String, double, ForceModel, double) - Constructor for class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution
Build a new instance.
AbstractGNSSPropagator - Class in org.orekit.propagation.analytical.gnss
Common handling of AbstractAnalyticalPropagator methods for GNSS propagators.
AbstractGNSSPropagator(GNSSOrbitalElements, AttitudeProvider, Frame, Frame, double, double, double, double) - Constructor for class org.orekit.propagation.analytical.gnss.AbstractGNSSPropagator
Build a new instance.
AbstractGradientConverter - Class in org.orekit.propagation.integration
Converter for states and parameters arrays for both numerical and semi-analytical propagators.
AbstractGradientConverter(int) - Constructor for class org.orekit.propagation.integration.AbstractGradientConverter
Simple constructor.
AbstractIntegratedPropagator - Class in org.orekit.propagation.integration
Common handling of Propagator methods for both numerical and semi-analytical propagators.
AbstractIntegratedPropagator(ODEIntegrator, PropagationType) - 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).
AbstractJacobiansMapper - Class in org.orekit.propagation.integration
Base class for jacobian mapper.
AbstractJacobiansMapper(String, ParameterDriversList) - Constructor for class org.orekit.propagation.integration.AbstractJacobiansMapper
Simple constructor.
AbstractLambdaMethod - Class in org.orekit.estimation.measurements.gnss
Base class for decorrelation/reduction engine for LAMBDA type methods.
AbstractLambdaMethod() - Constructor for class org.orekit.estimation.measurements.gnss.AbstractLambdaMethod
 
AbstractListCrawler<T> - Class in org.orekit.data
Provider for data files defined in a list.
AbstractListCrawler(T...) - Constructor for class org.orekit.data.AbstractListCrawler
Build a data classpath crawler.
AbstractMeasurement<T extends ObservedMeasurement<T>> - Class in org.orekit.estimation.measurements
Abstract class handling measurements boilerplate.
AbstractMeasurement(AbsoluteDate, double, double, double, List<ObservableSatellite>) - Constructor for class org.orekit.estimation.measurements.AbstractMeasurement
Simple constructor for mono-dimensional measurements.
AbstractMeasurement(AbsoluteDate, double[], double[], double[], List<ObservableSatellite>) - Constructor for class org.orekit.estimation.measurements.AbstractMeasurement
Simple constructor, for multi-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.
AbstractMultipleShooting - Class in org.orekit.utils
Multiple shooting method using only constraints on state vectors of patch points (and possibly on epoch and integration time).
AbstractMultipleShooting(List<SpacecraftState>, List<NumericalPropagator>, List<AdditionalEquations>, double, double, String) - Constructor for class org.orekit.utils.AbstractMultipleShooting
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.
AbstractPropagatorBuilder(Orbit, PositionAngle, double, boolean, AttitudeProvider) - 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.
AbstractRadiationForceModel - Class in org.orekit.forces.radiation
Base class for radiation force models.
AbstractRadiationForceModel(ExtendedPVCoordinatesProvider, double) - Constructor for class org.orekit.forces.radiation.AbstractRadiationForceModel
Constructor.
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.
AbstractSelfFeedingLoader - Class in org.orekit.data
Abstract class that combines a DataProvidersManager with a supported names regular expression for DataProvidersManager.feed(String, DataLoader).
AbstractSelfFeedingLoader(String, DataProvidersManager) - Constructor for class org.orekit.data.AbstractSelfFeedingLoader
Create an abstract data loader that can feed itself.
AbstractShapiroBaseModifier - Class in org.orekit.estimation.measurements.modifiers
Class modifying theoretical range measurement with Shapiro time delay.
AbstractShapiroBaseModifier(double) - Constructor for class org.orekit.estimation.measurements.modifiers.AbstractShapiroBaseModifier
Simple constructor.
AbstractSingleFrequencyCombination - Class in org.orekit.estimation.measurements.gnss
Base class for single frequency combination of measurements.
AbstractSingleFrequencyCombination(CombinationType, SatelliteSystem) - Constructor for class org.orekit.estimation.measurements.gnss.AbstractSingleFrequencyCombination
Constructor.
AbstractTimeScales - Class in org.orekit.time
Abstract base class for TimeScales that implements some common functionality.
AbstractTimeScales() - Constructor for class org.orekit.time.AbstractTimeScales
Simple constructor.
acceleration(SpacecraftState, double[]) - Method in class org.orekit.forces.AbstractParametricAcceleration
Compute acceleration.
acceleration(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.AbstractParametricAcceleration
Compute acceleration.
acceleration(SpacecraftState, double[]) - Method in class org.orekit.forces.drag.DragForce
Compute acceleration.
acceleration(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.drag.DragForce
Compute acceleration.
acceleration(SpacecraftState, double[]) - Method in class org.orekit.forces.drag.TimeSpanDragForce
Compute acceleration.
acceleration(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.drag.TimeSpanDragForce
Compute acceleration.
acceleration(SpacecraftState, double[]) - Method in interface org.orekit.forces.ForceModel
Compute acceleration.
acceleration(FieldSpacecraftState<T>, T[]) - Method in interface org.orekit.forces.ForceModel
Compute acceleration.
acceleration(SpacecraftState, double[]) - Method in class org.orekit.forces.gravity.HolmesFeatherstoneAttractionModel
Compute acceleration.
acceleration(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.gravity.HolmesFeatherstoneAttractionModel
Compute acceleration.
acceleration(SpacecraftState, double[]) - Method in class org.orekit.forces.gravity.NewtonianAttraction
Compute acceleration.
acceleration(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.gravity.NewtonianAttraction
Compute acceleration.
acceleration(SpacecraftState, double[]) - Method in class org.orekit.forces.gravity.OceanTides
Compute acceleration.
acceleration(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.gravity.OceanTides
Compute acceleration.
acceleration(SpacecraftState, double[]) - Method in class org.orekit.forces.gravity.Relativity
Compute acceleration.
acceleration(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.gravity.Relativity
Compute acceleration.
acceleration(SpacecraftState, double[]) - Method in class org.orekit.forces.gravity.SingleBodyAbsoluteAttraction
Compute acceleration.
acceleration(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.gravity.SingleBodyAbsoluteAttraction
Compute acceleration.
acceleration(SpacecraftState, double[]) - Method in class org.orekit.forces.gravity.SingleBodyRelativeAttraction
Compute acceleration.
acceleration(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.gravity.SingleBodyRelativeAttraction
Compute acceleration.
acceleration(SpacecraftState, double[]) - Method in class org.orekit.forces.gravity.SolidTides
Compute acceleration.
acceleration(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.gravity.SolidTides
Compute acceleration.
acceleration(SpacecraftState, double[]) - Method in class org.orekit.forces.gravity.ThirdBodyAttraction
Compute acceleration.
acceleration(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.gravity.ThirdBodyAttraction
Compute acceleration.
acceleration(SpacecraftState, double[]) - Method in class org.orekit.forces.inertia.InertialForces
Compute acceleration.
acceleration(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.inertia.InertialForces
Compute acceleration.
acceleration(SpacecraftState, double[]) - Method in class org.orekit.forces.maneuvers.Maneuver
 
acceleration(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.maneuvers.Maneuver
 
acceleration(SpacecraftState, double[]) - Method in class org.orekit.forces.radiation.ECOM2
Compute acceleration.
acceleration(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.radiation.ECOM2
Compute acceleration.
acceleration(SpacecraftState, double[]) - Method in class org.orekit.forces.radiation.SolarRadiationPressure
Compute acceleration.
acceleration(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.radiation.SolarRadiationPressure
Compute acceleration.
acceleration(SpacecraftState, double[]) - Method in class org.orekit.propagation.numerical.cr3bp.CR3BPForceModel
Compute acceleration.
acceleration(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.propagation.numerical.cr3bp.CR3BPForceModel
Compute acceleration.
accept(IntegerLeastSquareSolution[]) - Method in interface org.orekit.estimation.measurements.gnss.AmbiguityAcceptance
Check if one of the candidate solutions can be accepted.
accept(IntegerLeastSquareSolution[]) - Method in class org.orekit.estimation.measurements.gnss.SimpleRatioAmbiguityAcceptance
Check if one of the candidate solutions can be accepted.
acceptStep(OrekitStepInterpolator, AbsoluteDate, double) - Method in class org.orekit.propagation.analytical.AbstractAnalyticalPropagator
Accept a step, triggering events and step handlers.
acceptStep(FieldAbstractAnalyticalPropagator<T>.FieldBasicStepInterpolator, FieldAbsoluteDate<T>, double) - Method in class org.orekit.propagation.analytical.FieldAbstractAnalyticalPropagator
Accept a step, triggering events and step handlers.
AdamsBashforthIntegratorBuilder - Class in org.orekit.propagation.conversion
Builder for AdamsBashforthIntegrator.
AdamsBashforthIntegratorBuilder(int, double, double, double) - Constructor for class org.orekit.propagation.conversion.AdamsBashforthIntegratorBuilder
Build a new instance.
AdamsMoultonIntegratorBuilder - Class in org.orekit.propagation.conversion
Builder for AdamsMoultonIntegrator.
AdamsMoultonIntegratorBuilder(int, double, double, double) - Constructor for class org.orekit.propagation.conversion.AdamsMoultonIntegratorBuilder
Build a new instance.
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(FieldOrekitFixedStepHandler<T>) - Method in class org.orekit.propagation.sampling.FieldOrekitFixedStepHandlerMultiplexer
Add a step handler.
add(FieldOrekitStepHandler<T>) - Method in class org.orekit.propagation.sampling.FieldOrekitStepHandlerMultiplexer
Add a step handler.
add(OrekitFixedStepHandler) - Method in class org.orekit.propagation.sampling.OrekitFixedStepHandlerMultiplexer
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.conversion.AbstractPropagatorBuilder
Add a set of user-specified equations to be integrated along with the orbit propagation (author Shiva Iyer).
addAdditionalEquations(AdditionalEquations) - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
Add a set of user-specified equations to be integrated along with the orbit propagation.
addAdditionalEquations(FieldAdditionalEquations<T>) - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator
Add a set of user-specified equations to be integrated along with the orbit propagation.
addAdditionalState(String, T...) - Method in class org.orekit.propagation.FieldSpacecraftState
Add an additional state.
addAdditionalState(String, double...) - Method in class org.orekit.propagation.SpacecraftState
Add an additional state.
addAdditionalStateProvider(AdditionalStateProvider) - Method in class org.orekit.propagation.AbstractPropagator
Add a set of user-specified state parameters to be computed along with the orbit propagation.
addAdditionalStateProvider(FieldAdditionalStateProvider<T>) - Method in class org.orekit.propagation.FieldAbstractPropagator
Add a set of user-specified state parameters to be computed along with the orbit propagation.
addAdditionalStateProvider(FieldAdditionalStateProvider<T>) - Method in interface org.orekit.propagation.FieldPropagator
Add a set of user-specified state parameters to be computed along with the orbit propagation.
addAdditionalStateProvider(AdditionalStateProvider) - Method in interface org.orekit.propagation.Propagator
Add a set of user-specified state parameters to be computed along with the orbit propagation.
addAttitudeBlock() - Method in class org.orekit.files.ccsds.AEMFile
Add a block to the list of ephemeris blocks.
addCelestialBodyLoader(String, CelestialBodyLoader) - Static method in class org.orekit.bodies.CelestialBodyFactory
Add a loader for celestial bodies.
addCelestialBodyLoader(String, CelestialBodyLoader) - Method in class org.orekit.bodies.LazyLoadedCelestialBodies
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.
addConstraint(int, int, double) - Method in class org.orekit.utils.AbstractMultipleShooting
Add a constraint on one component of one patch point.
addContribution(SpacecraftState, TimeDerivativesEquations) - Method in interface org.orekit.forces.ForceModel
Compute the contribution of the force model to the perturbing acceleration.
addContribution(FieldSpacecraftState<T>, FieldTimeDerivativesEquations<T>) - Method in interface org.orekit.forces.ForceModel
Compute the contribution of the force model to the perturbing acceleration.
addContribution(SpacecraftState, TimeDerivativesEquations) - Method in class org.orekit.forces.gravity.NewtonianAttraction
Compute the contribution of the force model to the perturbing acceleration.
addContribution(FieldSpacecraftState<T>, FieldTimeDerivativesEquations<T>) - Method in class org.orekit.forces.gravity.NewtonianAttraction
Compute the contribution of the force model to the perturbing acceleration.
addContribution(BodiesElements, double[][], double[][]) - Method in class org.orekit.forces.gravity.potential.OceanTidesWave
Add the contribution of the wave to Stokes coefficients.
addContribution(SpacecraftState, TimeDerivativesEquations) - Method in class org.orekit.forces.maneuvers.Maneuver
Compute the contribution of the force model to the perturbing acceleration.
addContribution(FieldSpacecraftState<T>, FieldTimeDerivativesEquations<T>) - Method in class org.orekit.forces.maneuvers.Maneuver
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.
addDefaultCelestialBodyLoader(String) - Method in class org.orekit.bodies.LazyLoadedCelestialBodies
Add the default loaders for all predefined celestial bodies.
addDefaultCelestialBodyLoader(String, String) - Method in class org.orekit.bodies.LazyLoadedCelestialBodies
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).
addDefaultEOP1980HistoryLoaders(String, String, String, String, String, Supplier<TimeScale>) - Method in class org.orekit.frames.LazyLoadedEop
Add the default loaders EOP history (IAU 1980 precession/nutation).
addDefaultEOP1980HistoryLoaders(String, String, String, String, String) - Method in class org.orekit.frames.LazyLoadedFrames
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).
addDefaultEOP2000HistoryLoaders(String, String, String, String, String, Supplier<TimeScale>) - Method in class org.orekit.frames.LazyLoadedEop
Add the default loaders for EOP history (IAU 2000/2006 precession/nutation).
addDefaultEOP2000HistoryLoaders(String, String, String, String, String) - Method in class org.orekit.frames.LazyLoadedFrames
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.
addDefaultOceanTidesReaders() - Method in class org.orekit.forces.gravity.potential.LazyLoadedGravityFields
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.
addDefaultPotentialCoefficientsReaders() - Method in class org.orekit.forces.gravity.potential.LazyLoadedGravityFields
Add the default readers for gravity fields.
addDefaultProviders() - Method in class org.orekit.data.DataProvidersManager
Add the default providers configuration.
addDefaultUTCTAIOffsetsLoaders() - Method in class org.orekit.time.LazyLoadedTimeScales
Add the default loaders for UTC-TAI offsets history files (both IERS and USNO).
addDefaultUTCTAIOffsetsLoaders() - Static method in class org.orekit.time.TimeScalesFactory
Add the default loaders for UTC-TAI offsets history files (both IERS and USNO).
addDragSensitiveValidAfter(DragSensitive, AbsoluteDate) - Method in class org.orekit.forces.drag.TimeSpanDragForce
Add a DragSensitive entry valid after a limit date.
Using addDragSensitiveValidAfter(entry, t) will make entry valid in [t, +∞[ (note the closed bracket).
addDragSensitiveValidBefore(DragSensitive, AbsoluteDate) - Method in class org.orekit.forces.drag.TimeSpanDragForce
Add a DragSensitive entry valid before a limit date.
Using addDragSensitiveValidBefore(entry, t) will make entry valid in ]-∞, t[ (note the open bracket).
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.
addEOPHistoryLoader(IERSConventions, EOPHistoryLoader) - Method in class org.orekit.frames.LazyLoadedEop
Add a loader for Earth Orientation Parameters history.
addEOPHistoryLoader(IERSConventions, EOPHistoryLoader) - Method in class org.orekit.frames.LazyLoadedFrames
Add a loader for Earth Orientation Parameters history.
addEphemeridesBlock() - Method in class org.orekit.files.ccsds.OEMFile
Add a block to the list of ephemeris blocks.
addEventDate(AbsoluteDate) - Method in class org.orekit.propagation.events.DateDetector
Add an event date.
addEventDate(FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.events.FieldDateDetector
Add an event date.
addEventDetector(T) - Method in class org.orekit.propagation.AbstractPropagator
Add an event detector.
addEventDetector(T) - Method in class org.orekit.propagation.analytical.AbstractAnalyticalPropagator
Add an event detector.
addEventDetector(D) - Method in class org.orekit.propagation.analytical.FieldAbstractAnalyticalPropagator
Add an event detector.
addEventDetector(D) - Method in class org.orekit.propagation.FieldAbstractPropagator
Add an event detector.
addEventDetector(D) - Method in interface org.orekit.propagation.FieldPropagator
Add an event detector.
addEventDetector(EventDetector) - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
Add an event detector.
addEventDetector(D) - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator
Add an event detector.
addEventDetector(T) - Method in interface org.orekit.propagation.Propagator
Add an event detector.
addFilter(DataFilter) - Method in class org.orekit.data.DataProvidersManager
Add a data filter.
addForceModel(DSSTForceModel) - Method in class org.orekit.propagation.conversion.DSSTPropagatorBuilder
Add a force model to the global perturbation model.
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.
addForceModel(DSSTForceModel) - Method in class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator
Add a force model to the global perturbation model.
addGridPoint(FieldAbsoluteDate<T>, T[]) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldShortPeriodicsInterpolatedCoefficient
Add a point to the interpolation grid.
addGridPoint(AbsoluteDate, double[]) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.ShortPeriodicsInterpolatedCoefficient
Add a point to the interpolation grid.
addInput(T) - Method in class org.orekit.data.AbstractListCrawler
Add an input to the supported list.
AdditionalEquations - Interface in org.orekit.propagation.integration
This interface allows users to add their own differential equations to a numerical propagator.
AdditionalStateProvider - Interface in org.orekit.propagation
This interface represents providers for additional state data beyond SpacecraftState.
addKeplerContribution(PositionAngle, double, double[]) - Method in class org.orekit.orbits.CartesianOrbit
Add the contribution of the Keplerian motion to parameters derivatives
addKeplerContribution(PositionAngle, double, double[]) - Method in class org.orekit.orbits.CircularOrbit
Add the contribution of the Keplerian motion to parameters derivatives
addKeplerContribution(PositionAngle, double, double[]) - Method in class org.orekit.orbits.EquinoctialOrbit
Add the contribution of the Keplerian motion to parameters derivatives
addKeplerContribution(PositionAngle, T, T[]) - Method in class org.orekit.orbits.FieldCartesianOrbit
Add the contribution of the Keplerian motion to parameters derivatives
addKeplerContribution(PositionAngle, T, T[]) - Method in class org.orekit.orbits.FieldCircularOrbit
Add the contribution of the Keplerian motion to parameters derivatives
addKeplerContribution(PositionAngle, T, T[]) - Method in class org.orekit.orbits.FieldEquinoctialOrbit
Add the contribution of the Keplerian motion to parameters derivatives
addKeplerContribution(PositionAngle, T, T[]) - Method in class org.orekit.orbits.FieldKeplerianOrbit
Add the contribution of the Keplerian motion to parameters derivatives
addKeplerContribution(PositionAngle, T, T[]) - Method in class org.orekit.orbits.FieldOrbit
Add the contribution of the Keplerian motion to parameters derivatives
addKeplerContribution(PositionAngle, double, double[]) - Method in class org.orekit.orbits.KeplerianOrbit
Add the contribution of the Keplerian motion to parameters derivatives
addKeplerContribution(PositionAngle, double, double[]) - Method in class org.orekit.orbits.Orbit
Add the contribution of the Keplerian motion to parameters derivatives
addKeplerContribution(T) - 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.
addManeuver(APMFile.APMManeuver) - Method in class org.orekit.files.ccsds.APMFile
Add a maneuver.
addMassDerivative(T) - Method in interface org.orekit.propagation.numerical.FieldTimeDerivativesEquations
Add the contribution of the flow rate (dm/dt).
addMassDerivative(double) - Method in interface org.orekit.propagation.numerical.TimeDerivativesEquations
Add the contribution of the flow rate (dm/dt).
addMeasurement(ObservedMeasurement<?>) - Method in class org.orekit.estimation.leastsquares.BatchLSEstimator
Add a measurement.
addModifier(EstimationModifier<T>) - Method in class org.orekit.estimation.measurements.AbstractMeasurement
Add a modifier.
addModifier(EstimationModifier<T>) - Method in 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.
addNewSegment(List<SpacecraftState>, CelestialBody, int, TimeScale) - Method in class org.orekit.files.general.OrekitEphemerisFile.OrekitSatelliteEphemeris
Injects pre-computed satellite states into this ephemeris file object, returning the generated OrekitEphemerisFile.OrekitEphemerisSegment that has been stored internally.
addNonKeplerianAcceleration(FieldVector3D<T>) - Method in interface org.orekit.propagation.numerical.FieldTimeDerivativesEquations
Add the contribution of an acceleration expressed in some inertial frame.
addNonKeplerianAcceleration(Vector3D) - Method in interface org.orekit.propagation.numerical.TimeDerivativesEquations
Add the contribution of a non-Keplerian acceleration.
addObservation(TDMFile.Observation) - Method in class org.orekit.files.ccsds.TDMFile.ObservationsBlock
Adds an observation data line.
addObservation(String, AbsoluteDate, double) - Method in class org.orekit.files.ccsds.TDMFile.ObservationsBlock
Adds an observation data line.
addObservationComment(String) - Method in class org.orekit.files.ccsds.TDMFile.ObservationsBlock
Add an observation data line comment.
addObservationsBlock() - Method in class org.orekit.files.ccsds.TDMFile
Add a block to the list of observations blocks.
addObserver(ParameterObserver) - Method in class org.orekit.utils.ParameterDriver
Add an observer for this driver.
addOceanTidesReader(OceanTidesReader) - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory
Add a reader for ocean tides.
addOceanTidesReader(OceanTidesReader) - Method in class org.orekit.forces.gravity.potential.LazyLoadedGravityFields
Add a reader for ocean tides.
addOffset(AngularCoordinates) - Method in class org.orekit.utils.AngularCoordinates
Add an offset from the instance.
addOffset(FieldAngularCoordinates<T>) - Method in class org.orekit.utils.FieldAngularCoordinates
Add an offset from the instance.
addOffset(AngularCoordinates) - Method in class org.orekit.utils.TimeStampedAngularCoordinates
Add an offset from the instance.
addOffset(FieldAngularCoordinates<T>) - Method in class org.orekit.utils.TimeStampedFieldAngularCoordinates
Add an offset from the instance.
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.
addPotentialCoefficientsReader(PotentialCoefficientsReader) - Method in class org.orekit.forces.gravity.potential.LazyLoadedGravityFields
Add a reader for gravity fields.
addPropagationConfiguration(IntegratedPropagatorBuilder, 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.
addSolution(long[], double) - Method in class org.orekit.estimation.measurements.gnss.AbstractLambdaMethod
Add a new solution.
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.
addTroposphericModelValidAfter(EstimatedTroposphericModel, AbsoluteDate) - Method in class org.orekit.models.earth.troposphere.TimeSpanEstimatedTroposphericModel
Add a EstimatedTroposphericModel entry valid after a limit date.
Using addTroposphericModelValidAfter(entry, t) will make entry valid in [t, +∞[ (note the closed bracket).
addTroposphericModelValidBefore(EstimatedTroposphericModel, AbsoluteDate) - Method in class org.orekit.models.earth.troposphere.TimeSpanEstimatedTroposphericModel
Add an EstimatedTroposphericModel entry valid before a limit date.
Using addTroposphericValidBefore(entry, t) will make entry valid in ]-∞, t[ (note the open bracket).
addUTCTAIOffsetsLoader(UTCTAIOffsetsLoader) - Method in class org.orekit.time.LazyLoadedTimeScales
Add a loader for UTC-TAI offsets history files.
addUTCTAIOffsetsLoader(UTCTAIOffsetsLoader) - Static method in class org.orekit.time.TimeScalesFactory
Add a loader for UTC-TAI offsets history files.
addValidAfter(T, FieldAbsoluteDate<D>) - Method in class org.orekit.utils.FieldTimeSpanMap
Add an entry valid after a limit date.
addValidAfter(T, AbsoluteDate) - Method in class org.orekit.utils.TimeSpanMap
Add an entry valid after a limit date.
addValidBefore(T, FieldAbsoluteDate<D>) - Method in class org.orekit.utils.FieldTimeSpanMap
Add an entry valid before a limit date.
addValidBefore(T, AbsoluteDate) - Method in class org.orekit.utils.TimeSpanMap
Add an entry valid before a limit date.
addWaveCoefficients(int, int, int, double, double, double, double, int, String) - Method in class org.orekit.forces.gravity.potential.OceanTidesReader
Add parsed coefficients.
ADMFile - Class in org.orekit.files.ccsds
The ADMFile (Attitude Data Message) class represents any of the two attitude messages used by the CCSDS, (i.e.
ADMFile() - Constructor for class org.orekit.files.ccsds.ADMFile
Constructor.
ADMMetaData - Class in org.orekit.files.ccsds
This class gathers the meta-data present in the Attitude Data Message (ADM).
ADMMetaData(ADMFile) - Constructor for class org.orekit.files.ccsds.ADMMetaData
Create a new meta-data.
ADMParser - Class in org.orekit.files.ccsds
Base class for all CCSDS Attitude Data Message parsers.
ADMParser(AbsoluteDate, double, IERSConventions, boolean, int, int, String, DataContext) - Constructor for class org.orekit.files.ccsds.ADMParser
Complete constructor.
AEMAttitudeType - Enum in org.orekit.files.ccsds
Enumerate for AEM attitude type.
AEMFile - Class in org.orekit.files.ccsds
This class stocks all the information of the Attitude Ephemeris Message (AEM) File parsed by AEMParser.
AEMFile() - Constructor for class org.orekit.files.ccsds.AEMFile
AEMFile constructor.
AEMFile.AemSatelliteEphemeris - Class in org.orekit.files.ccsds
AEM ephemeris blocks for a single satellite.
AEMFile.AttitudeEphemeridesBlock - Class in org.orekit.files.ccsds
The Attitude Ephemerides Blocks class contain metadata and the list of attitude data lines.
AEMParser - Class in org.orekit.files.ccsds
A parser for the CCSDS AEM (Attitude Ephemeris Message).
AEMParser() - Constructor for class org.orekit.files.ccsds.AEMParser
Simple constructor.
AEMParser(DataContext) - Constructor for class org.orekit.files.ccsds.AEMParser
Constructor with data context.
AEMParser.AEMRotationOrder - Enum in org.orekit.files.ccsds
Util class to convert the Euler rotation sequence to RotationOrder.
AemSatelliteEphemeris(List<AEMFile.AttitudeEphemeridesBlock>) - Constructor for class org.orekit.files.ccsds.AEMFile.AemSatelliteEphemeris
Create a container for the set of ephemeris blocks in the file that pertain to a single satellite.
AEMWriter - Class in org.orekit.files.ccsds
A writer for Attitude Ephemeris Messsage (AEM) files.
AEMWriter() - Constructor for class org.orekit.files.ccsds.AEMWriter
Standard default constructor that creates a writer with default configurations.
AEMWriter(String, String, String) - Constructor for class org.orekit.files.ccsds.AEMWriter
Constructor used to create a new AEM writer configured with the necessary parameters to successfully fill in all required fields that aren't part of a standard object.
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.
afterIntegration() - Method in class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator
Method called just after integration.
AggregateBoundedPropagator - Class in org.orekit.propagation.analytical
A BoundedPropagator that covers a larger time span from several constituent propagators that cover shorter time spans.
AggregateBoundedPropagator(Collection<? extends BoundedPropagator>) - Constructor for class org.orekit.propagation.analytical.AggregateBoundedPropagator
Create a propagator by concatenating several BoundedPropagators.
AlignmentDetector - Class in org.orekit.propagation.events
Finder for satellite/body alignment events in orbital plane.
AlignmentDetector(Orbit, PVCoordinatesProvider, double) - Constructor for class org.orekit.propagation.events.AlignmentDetector
Build a new alignment detector.
AlignmentDetector(double, 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.
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 class org.orekit.models.earth.tessellation.DivertedSingularityAiming
Find the along tile direction for tessellation at specified point.
alongTileDirection(Vector3D, GeodeticPoint) - Method in interface org.orekit.models.earth.tessellation.TileAiming
Find the along tile direction for tessellation at specified point.
AlongTrackAiming - Class in org.orekit.models.earth.tessellation
Class used to orient tiles along an orbit track.
AlongTrackAiming(OneAxisEllipsoid, Orbit, boolean) - Constructor for class org.orekit.models.earth.tessellation.AlongTrackAiming
Simple constructor.
AltitudeDetector - Class in org.orekit.propagation.events
Finder for satellite altitude crossing events.
AltitudeDetector(double, BodyShape) - Constructor for class org.orekit.propagation.events.AltitudeDetector
Build a new altitude detector.
AltitudeDetector(double, double, BodyShape) - Constructor for class org.orekit.propagation.events.AltitudeDetector
Build a new altitude detector.
AltitudeDetector(double, double, double, BodyShape) - Constructor for class org.orekit.propagation.events.AltitudeDetector
Build a new altitude detector.
AMBIGUITY_NAME - Static variable in class org.orekit.estimation.measurements.gnss.Phase
Name for ambiguity driver.
AmbiguityAcceptance - Interface in org.orekit.estimation.measurements.gnss
Interface defining ambiguity acceptance tests.
AmbiguitySolver - Class in org.orekit.estimation.measurements.gnss
Class for solving integer ambiguity problems.
AmbiguitySolver(List<ParameterDriver>, IntegerLeastSquareSolver, AmbiguityAcceptance) - Constructor for class org.orekit.estimation.measurements.gnss.AmbiguitySolver
Simple constructor.
andCombine(EventDetector...) - Static method in class org.orekit.propagation.events.BooleanDetector
Create a new event detector that is the logical AND of the given event detectors.
andCombine(Collection<? extends EventDetector>) - Static method in class org.orekit.propagation.events.BooleanDetector
Create a new event detector that is the logical AND of the given event detectors.
AngularAzEl - Class in org.orekit.estimation.measurements
Class modeling an Azimuth-Elevation measurement from a ground station.
AngularAzEl(GroundStation, AbsoluteDate, double[], double[], double[], 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(Rotation, Vector3D) - Constructor for class org.orekit.utils.AngularCoordinates
Builds a rotation/rotation rate pair.
AngularCoordinates(Rotation, Vector3D, Vector3D) - Constructor for class org.orekit.utils.AngularCoordinates
Builds a rotation/rotation rate/rotation acceleration triplet.
AngularCoordinates(PVCoordinates, PVCoordinates, PVCoordinates, PVCoordinates, double) - Constructor for class org.orekit.utils.AngularCoordinates
Build the rotation that transforms a pair of pv coordinates into another one.
AngularCoordinates(PVCoordinates, PVCoordinates) - Constructor for class org.orekit.utils.AngularCoordinates
Build one of the rotations that transform one pv coordinates into another one.
AngularCoordinates(FieldRotation<DerivativeStructure>) - Constructor for class org.orekit.utils.AngularCoordinates
Builds a AngularCoordinates from a FieldRotation<DerivativeStructure>.
AngularDerivativesFilter - Enum in org.orekit.utils
Enumerate for selecting which derivatives to use in TimeStampedAngularCoordinates and TimeStampedFieldAngularCoordinates interpolation.
AngularIonosphericDelayModifier - Class in org.orekit.estimation.measurements.modifiers
Class modifying theoretical angular measurement with ionospheric delay.
AngularIonosphericDelayModifier(IonosphericModel, double) - 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[], 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.
AntexLoader(String, DataProvidersManager, TimeScale) - Constructor for class org.orekit.gnss.antenna.AntexLoader
Construct a loader by specifying the source of ANTEX auxiliary data files.
APMFile - Class in org.orekit.files.ccsds
This class stocks all the information of the Attitude Parameter Message (APM) File parsed by APMParser.
APMFile() - Constructor for class org.orekit.files.ccsds.APMFile
APMFile constructor.
APMFile.APMManeuver - Class in org.orekit.files.ccsds
Maneuver in an APM file.
APMManeuver() - Constructor for class org.orekit.files.ccsds.APMFile.APMManeuver
Simple constructor.
APMParser - Class in org.orekit.files.ccsds
A parser for the CCSDS APM (Attitude Parameter Message).
APMParser() - Constructor for class org.orekit.files.ccsds.APMParser
Simple constructor.
APMParser(DataContext) - Constructor for class org.orekit.files.ccsds.APMParser
Constructor with data context.
appliesTo(String) - Method in class org.orekit.frames.ITRFVersionLoader.ITRFVersionConfiguration
Check if this entry applies to a file name.
apply(Orbit) - Method in class org.orekit.forces.maneuvers.SmallManeuverAnalyticalModel
Compute the effect of the maneuver on an orbit.
apply(SpacecraftState) - Method in class org.orekit.forces.maneuvers.SmallManeuverAnalyticalModel
Compute the effect of the maneuver on a spacecraft state.
apply(SpacecraftState) - Method in interface org.orekit.propagation.analytical.AdapterPropagator.DifferentialEffect
Apply the effect to a spacecraft state.
apply(Orbit) - Method in class org.orekit.propagation.analytical.J2DifferentialEffect
Compute the effect of the maneuver on an orbit.
apply(SpacecraftState) - Method in class org.orekit.propagation.analytical.J2DifferentialEffect
Apply the effect to a spacecraft state.
applyAllFilters(NamedData) - Method in class org.orekit.data.DataProvidersManager
Apply all the relevant data filters, taking care of layers.
applyCorrectionOnPV(CR3BPDifferentialCorrection) - Method in class org.orekit.orbits.HaloOrbit
Apply the differential correction to compute more accurate initial PV.
applyCorrectionOnPV(CR3BPDifferentialCorrection) - Method in class org.orekit.orbits.LibrationOrbit
Apply the differential correction to compute more accurate initial PV.
applyCorrectionOnPV(CR3BPDifferentialCorrection) - Method in class org.orekit.orbits.LyapunovOrbit
Apply the differential correction to compute more accurate initial PV.
applyDifferentialCorrection() - Method in class org.orekit.orbits.LibrationOrbit
Apply differential correction.
applyDifferentialCorrection(AttitudeProvider, TimeScale) - Method in class org.orekit.orbits.LibrationOrbit
Apply differential correction.
applyTo(PVCoordinates) - Method in class org.orekit.utils.AngularCoordinates
Apply the rotation to a pv coordinates.
applyTo(TimeStampedPVCoordinates) - Method in class org.orekit.utils.AngularCoordinates
Apply the rotation to a pv coordinates.
applyTo(FieldPVCoordinates<T>) - Method in class org.orekit.utils.AngularCoordinates
Apply the rotation to a pv coordinates.
applyTo(TimeStampedFieldPVCoordinates<T>) - Method in class org.orekit.utils.AngularCoordinates
Apply the rotation to a pv coordinates.
applyTo(PVCoordinates) - Method in class org.orekit.utils.FieldAngularCoordinates
Apply the rotation to a pv coordinates.
applyTo(TimeStampedPVCoordinates) - Method in class org.orekit.utils.FieldAngularCoordinates
Apply the rotation to a pv coordinates.
applyTo(FieldPVCoordinates<T>) - Method in class org.orekit.utils.FieldAngularCoordinates
Apply the rotation to a pv coordinates.
applyTo(TimeStampedFieldPVCoordinates<T>) - Method in class org.orekit.utils.FieldAngularCoordinates
Apply the rotation to a pv coordinates.
approximateAsPolynomialOnly(int, AbsoluteDate, int, int, AbsoluteDate, AbsoluteDate, double) - Method in class org.orekit.utils.SecularAndHarmonic
Approximate an already fitted model to polynomial only terms.
ApsideDetector - Class in org.orekit.propagation.events
Finder for apside crossing events.
ApsideDetector(Orbit) - Constructor for class org.orekit.propagation.events.ApsideDetector
Build a new instance.
ApsideDetector(double, Orbit) - Constructor for class org.orekit.propagation.events.ApsideDetector
Build a new instance.
ARBITRARY_EPOCH - Static variable in class org.orekit.time.AbsoluteDate
An arbitrary finite date.
ARC_SECONDS_TO_RADIANS - Static variable in interface org.orekit.utils.Constants
Conversion factor from arc seconds to radians: 2*PI/(360*60*60).
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.models.earth.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.models.earth.atmosphere.DTM2000
Identifier for atomic nitrogen.
ATOMIC_OXYGEN - Static variable in class org.orekit.models.earth.atmosphere.DTM2000
Identifier for atomic oxygen.
attachTo(Frame, Transform, boolean) - Method in class org.orekit.frames.OrphanFrame
Attach the instance (and all its children down to leafs) to the main tree.
attachTo(Frame, TransformProvider, boolean) - Method in class org.orekit.frames.OrphanFrame
Attach the instance (and all its children down to leafs) to the main tree.
Attitude - Class in org.orekit.attitudes
This class handles attitude definition at a given date.
Attitude(Frame, TimeStampedAngularCoordinates) - Constructor for class org.orekit.attitudes.Attitude
Creates a new instance.
Attitude(AbsoluteDate, Frame, AngularCoordinates) - Constructor for class org.orekit.attitudes.Attitude
Creates a new instance.
Attitude(AbsoluteDate, Frame, Rotation, Vector3D, Vector3D) - Constructor for class org.orekit.attitudes.Attitude
Creates a new instance.
AttitudeEphemeridesBlock() - Constructor for class org.orekit.files.ccsds.AEMFile.AttitudeEphemeridesBlock
Constructor.
AttitudeProvider - Interface in org.orekit.attitudes
This interface represents an attitude provider model set.
attitudeProvider(AttitudeProvider) - Method in class org.orekit.propagation.analytical.gnss.BeidouPropagator.Builder
Sets the attitude provider.
attitudeProvider(AttitudeProvider) - Method in class org.orekit.propagation.analytical.gnss.GalileoPropagator.Builder
Sets the attitude provider.
attitudeProvider(AttitudeProvider) - Method in class org.orekit.propagation.analytical.gnss.GLONASSAnalyticalPropagator.Builder
Sets the attitude provider.
attitudeProvider(AttitudeProvider) - Method in class org.orekit.propagation.analytical.gnss.GPSPropagator.Builder
Sets the attitude provider.
attitudeProvider(AttitudeProvider) - Method in class org.orekit.propagation.analytical.gnss.IRNSSPropagator.Builder
Sets the attitude provider.
attitudeProvider(AttitudeProvider) - Method in class org.orekit.propagation.analytical.gnss.QZSSPropagator.Builder
Sets the attitude provider.
attitudeProvider(AttitudeProvider) - Method in class org.orekit.propagation.analytical.gnss.SBASPropagator.Builder
Sets the attitude provider.
attitudeProvider(AttitudeProvider) - Method in class org.orekit.propagation.numerical.GLONASSNumericalPropagator.Builder
Sets the attitude provider.
AttitudeProviderModifier - Interface in org.orekit.attitudes
This interface represents an attitude provider that modifies/wraps another underlying provider.
AttitudesSequence - Class in org.orekit.attitudes
This classes manages a sequence of different attitude providers that are activated in turn according to switching events.
AttitudesSequence() - Constructor for class org.orekit.attitudes.AttitudesSequence
Constructor for an initially empty sequence.
AttitudesSequence.SwitchHandler - Interface in org.orekit.attitudes
Interface for attitude switch notifications.
ATTRACTION_COEFFICIENT - Static variable in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBody
Name of the single parameter of this model: the attraction coefficient.
ATTRACTION_COEFFICIENT_SUFFIX - Static variable in class org.orekit.forces.gravity.SingleBodyAbsoluteAttraction
Suffix for parameter name for attraction coefficient enabling Jacobian processing.
ATTRACTION_COEFFICIENT_SUFFIX - Static variable in class org.orekit.forces.gravity.SingleBodyRelativeAttraction
Suffix for parameter name for attraction coefficient enabling Jacobian processing.
ATTRACTION_COEFFICIENT_SUFFIX - Static variable in class org.orekit.forces.gravity.ThirdBodyAttraction
Suffix for parameter name for attraction coefficient enabling Jacobian processing.
AuxiliaryElements - Class in org.orekit.propagation.semianalytical.dsst.utilities
Container class for common parameters used by all DSST forces.
AuxiliaryElements(Orbit, int) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
Simple constructor.

B

B_STAR - Static variable in class org.orekit.propagation.conversion.TLEPropagatorBuilder
Parameter name for B* coefficient.
BasicConstantThrustPropulsionModel - Class in org.orekit.forces.maneuvers.propulsion
Constant thrust propulsion model with: - Constant thrust direction in spacecraft frame - Parameter drivers (for estimation) for the thrust norm or the flow rate.
BasicConstantThrustPropulsionModel(double, double, Vector3D, String) - Constructor for class org.orekit.forces.maneuvers.propulsion.BasicConstantThrustPropulsionModel
Simple constructor.
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.AggregateBoundedPropagator
 
basicPropagate(AbsoluteDate) - Method in class org.orekit.propagation.analytical.Ephemeris
 
basicPropagate(FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.analytical.FieldAbstractAnalyticalPropagator
Propagate an orbit without any fancy features.
basicPropagate(FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.integration.FieldIntegratedEphemeris
Propagate an orbit without any fancy features.
basicPropagate(AbsoluteDate) - Method in class org.orekit.propagation.integration.IntegratedEphemeris
Propagate an orbit without any fancy features.
BatchLSEstimator - Class in org.orekit.estimation.leastsquares
Least squares estimator for orbit determination.
BatchLSEstimator(LeastSquaresOptimizer, IntegratedPropagatorBuilder...) - Constructor for class org.orekit.estimation.leastsquares.BatchLSEstimator
Simple constructor.
BatchLSModel - Class in org.orekit.estimation.leastsquares
BatchLSModel(IntegratedPropagatorBuilder[], List<ObservedMeasurement<?>>, ParameterDriversList, ModelObserver) - Constructor for class org.orekit.estimation.leastsquares.BatchLSModel
Simple constructor.
BatchLSObserver - Interface in org.orekit.estimation.leastsquares
Observer for batch least squares estimator iterations.
BatchLSODModel - Interface in org.orekit.estimation.leastsquares
Interface for models used in the batch least squares orbit determination process.
BDTScale - Class in org.orekit.time
Beidou system time scale.
beforeIntegration(SpacecraftState, AbsoluteDate) - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
Method called just before integration.
beforeIntegration(FieldSpacecraftState<T>, FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator
Method called just before integration.
beforeIntegration(SpacecraftState, AbsoluteDate) - Method in class org.orekit.propagation.numerical.NumericalPropagator
Method called just before integration.
beforeIntegration(SpacecraftState, AbsoluteDate) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator
Method called just before integration.
beforeIntegration(FieldSpacecraftState<T>, FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator
Method called just before integration.
BEIDOU_EPOCH - Static variable in class org.orekit.time.AbsoluteDate
Reference epoch for BeiDou weeks: 2006-01-01T00:00:00 UTC.
BEIDOU_EPOCH - Static variable in class org.orekit.time.DateComponents
Reference epoch for BeiDou weeks: 2006-01-01.
BEIDOU_MU - Static variable in interface org.orekit.propagation.analytical.gnss.BeidouOrbitalElements
Earth's universal gravitational parameter for Beidou user in m³/s².
BEIDOU_PI - Static variable in interface org.orekit.propagation.analytical.gnss.BeidouOrbitalElements
Value of Pi for conversion from semicircles to radian.
BEIDOU_WEEK_IN_SECONDS - Static variable in interface org.orekit.propagation.analytical.gnss.BeidouOrbitalElements
Duration of the Beidou week in seconds.
BEIDOU_WEEK_NB - Static variable in interface org.orekit.propagation.analytical.gnss.BeidouOrbitalElements
Number of weeks in the Beidou cycle.
BeidouAlmanac - Class in org.orekit.gnss
Class for BeiDou almanac.
BeidouAlmanac(int, int, double, double, double, double, double, double, double, double, double, double, double, int) - Constructor for class org.orekit.gnss.BeidouAlmanac
Build a new almanac.
BeidouAlmanac(int, int, double, double, double, double, double, double, double, double, double, double, double, int, AbsoluteDate) - Constructor for class org.orekit.gnss.BeidouAlmanac
Build a new almanac.
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.
BeidouOrbitalElements - Interface in org.orekit.propagation.analytical.gnss
This interface provides the minimal set of orbital elements needed by the BeidouPropagator.
BeidouPropagator - Class in org.orekit.propagation.analytical.gnss
This class aims at propagating a Beidou orbit from BeidouOrbitalElements.
BeidouPropagator.Builder - Class in org.orekit.propagation.analytical.gnss
This nested class aims at building a BeidouPropagator.
BESSELIAN_YEAR - Static variable in interface org.orekit.utils.Constants
Duration of a Besselian year: 365.242198781 Constants.JULIAN_DAY.
beta0 - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator
sqrt (1 - e2).
beta02 - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator
1 - e2.
Bias<T extends ObservedMeasurement<T>> - Class in org.orekit.estimation.measurements.modifiers
Class modeling a measurement bias.
Bias(String[], double[], double[], double[], double[]) - Constructor for class org.orekit.estimation.measurements.modifiers.Bias
Simple constructor.
BodiesElements - Class in org.orekit.data
Elements of the bodies having an effect on nutation.
BodiesElements(AbsoluteDate, double, double, double, double, double, double, double, double, double, double, double, double, double, double, double, double, double, double, double, double, double, double, double, double, double, double, double, double, double, double, double) - Constructor for class org.orekit.data.BodiesElements
Simple constructor.
BodyCenterPointing - Class in org.orekit.attitudes
This class handles body center pointing attitude provider.
BodyCenterPointing(Frame, Ellipsoid) - Constructor for class org.orekit.attitudes.BodyCenterPointing
Creates new instance.
BodyShape - Interface in org.orekit.bodies
Interface representing the rigid surface shape of a natural body.
BooleanDetector - Class in org.orekit.propagation.events
This class provides AND and OR operations for event detectors.
BoundedPropagator - Interface in org.orekit.propagation
This interface is intended for ephemerides valid only during a time range.
BoxAndSolarArraySpacecraft - Class in org.orekit.forces
Class representing the features of a classical satellite with a convex body shape and rotating flat solar arrays.
BoxAndSolarArraySpacecraft(double, double, double, PVCoordinatesProvider, double, Vector3D, double, double, double) - Constructor for class org.orekit.forces.BoxAndSolarArraySpacecraft
Build a spacecraft model with best lighting of solar array.
BoxAndSolarArraySpacecraft(double, double, double, PVCoordinatesProvider, double, Vector3D, double, double, double, double) - Constructor for class org.orekit.forces.BoxAndSolarArraySpacecraft
Build a spacecraft model with best lighting of solar array.
BoxAndSolarArraySpacecraft(BoxAndSolarArraySpacecraft.Facet[], PVCoordinatesProvider, double, Vector3D, double, double, double) - Constructor for class org.orekit.forces.BoxAndSolarArraySpacecraft
Build a spacecraft model with best lighting of solar array.
BoxAndSolarArraySpacecraft(BoxAndSolarArraySpacecraft.Facet[], PVCoordinatesProvider, double, Vector3D, double, double, double, double) - Constructor for class org.orekit.forces.BoxAndSolarArraySpacecraft
Build a spacecraft model with best lighting of solar array.
BoxAndSolarArraySpacecraft(double, double, double, PVCoordinatesProvider, double, Vector3D, AbsoluteDate, Vector3D, double, double, double, double) - Constructor for class org.orekit.forces.BoxAndSolarArraySpacecraft
Build a spacecraft model with linear rotation of solar array.
BoxAndSolarArraySpacecraft(double, double, double, PVCoordinatesProvider, double, Vector3D, AbsoluteDate, Vector3D, double, double, double, double, double) - Constructor for class org.orekit.forces.BoxAndSolarArraySpacecraft
Build a spacecraft model with linear rotation of solar array.
BoxAndSolarArraySpacecraft(BoxAndSolarArraySpacecraft.Facet[], PVCoordinatesProvider, double, Vector3D, AbsoluteDate, Vector3D, double, double, double, double) - Constructor for class org.orekit.forces.BoxAndSolarArraySpacecraft
Build a spacecraft model with linear rotation of solar array.
BoxAndSolarArraySpacecraft(BoxAndSolarArraySpacecraft.Facet[], PVCoordinatesProvider, double, Vector3D, AbsoluteDate, Vector3D, double, double, double, double, double) - Constructor for class org.orekit.forces.BoxAndSolarArraySpacecraft
Build a spacecraft model with linear rotation of solar array.
BoxAndSolarArraySpacecraft.Facet - Class in org.orekit.forces
Class representing a single facet of a convex spacecraft body.
build(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.
build(SpacecraftState[]) - Method in class org.orekit.estimation.measurements.gnss.PhaseBuilder
Generate a single measurement.
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.BeidouPropagator.Builder
Finalizes the build.
build() - Method in class org.orekit.propagation.analytical.gnss.GalileoPropagator.Builder
Finalizes the build.
build() - Method in class org.orekit.propagation.analytical.gnss.GLONASSAnalyticalPropagator.Builder
Finalizes the build.
build() - Method in class org.orekit.propagation.analytical.gnss.GPSPropagator.Builder
Finalizes the build.
build() - Method in class org.orekit.propagation.analytical.gnss.IRNSSPropagator.Builder
Finalizes the build.
build() - Method in class org.orekit.propagation.analytical.gnss.QZSSPropagator.Builder
Finalizes the build.
build() - Method in class org.orekit.propagation.analytical.gnss.SBASPropagator.Builder
Finalizes the build.
build() - Method in class org.orekit.propagation.numerical.GLONASSNumericalPropagator.Builder
Finalizes the build.
buildAttitudeProvider(AbsoluteDate, AbsoluteDate, ExtendedPVCoordinatesProvider, Frame, int) - Method in enum org.orekit.gnss.antenna.SatelliteType
Build an attitude provider suitable for this satellite type.
Builder(BeidouOrbitalElements) - Constructor for class org.orekit.propagation.analytical.gnss.BeidouPropagator.Builder
Initializes the builder.
Builder(BeidouOrbitalElements, Frames) - Constructor for class org.orekit.propagation.analytical.gnss.BeidouPropagator.Builder
Initializes the builder.
Builder(GalileoOrbitalElements) - Constructor for class org.orekit.propagation.analytical.gnss.GalileoPropagator.Builder
Initializes the builder.
Builder(GalileoOrbitalElements, Frames) - Constructor for class org.orekit.propagation.analytical.gnss.GalileoPropagator.Builder
Initializes the builder.
Builder(GLONASSOrbitalElements) - Constructor for class org.orekit.propagation.analytical.gnss.GLONASSAnalyticalPropagator.Builder
Initializes the builder.
Builder(GLONASSOrbitalElements, DataContext) - Constructor for class org.orekit.propagation.analytical.gnss.GLONASSAnalyticalPropagator.Builder
Initializes the builder.
Builder(GPSOrbitalElements) - Constructor for class org.orekit.propagation.analytical.gnss.GPSPropagator.Builder
Initializes the builder.
Builder(GPSOrbitalElements, Frames) - Constructor for class org.orekit.propagation.analytical.gnss.GPSPropagator.Builder
Initializes the builder.
Builder(IRNSSOrbitalElements, Frames) - Constructor for class org.orekit.propagation.analytical.gnss.IRNSSPropagator.Builder
Initializes the builder.
Builder(QZSSOrbitalElements) - Constructor for class org.orekit.propagation.analytical.gnss.QZSSPropagator.Builder
Initializes the builder.
Builder(QZSSOrbitalElements, Frames) - Constructor for class org.orekit.propagation.analytical.gnss.QZSSPropagator.Builder
Initializes the builder.
Builder(SBASOrbitalElements, Frames) - Constructor for class org.orekit.propagation.analytical.gnss.SBASPropagator.Builder
Initializes the builder.
Builder(ClassicalRungeKuttaIntegrator, GLONASSEphemeris, boolean) - Constructor for class org.orekit.propagation.numerical.GLONASSNumericalPropagator.Builder
Initializes the builder.
buildFromCustomAttitude(AttitudeProvider, Vector3D) - Static method in class org.orekit.forces.maneuvers.propulsion.ThrustDirectionAndAttitudeProvider
Build a ThrustDirectionAndAttitudeProvider where the attitude is provided by an external.
buildFromDirectionInFrame(Frame, ThrustDirectionProvider, Vector3D) - Static method in class org.orekit.forces.maneuvers.propulsion.ThrustDirectionAndAttitudeProvider
Build a ThrustDirectionAndAttitudeProvider by a variable direction in a custom frame.
buildFromDirectionInLOF(LOFType, ThrustDirectionProvider, Vector3D) - Static method in class org.orekit.forces.maneuvers.propulsion.ThrustDirectionAndAttitudeProvider
Build a ThrustDirectionAndAttitudeProvider by a variable direction in a Local Orbital Frame.
buildFromFixedDirectionInSatelliteFrame(Vector3D) - Static method in class org.orekit.forces.maneuvers.propulsion.ThrustDirectionAndAttitudeProvider
Build a ThrustDirectionAndAttitudeProvider from a fixed direction in the satellite frame.
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.
buildKalmanModel(List<IntegratedPropagatorBuilder>, List<CovarianceMatrixProvider>, ParameterDriversList) - Method in class org.orekit.propagation.conversion.DSSTPropagatorBuilder
Build a new KalmanODModel.
buildKalmanModel(List<IntegratedPropagatorBuilder>, List<CovarianceMatrixProvider>, ParameterDriversList) - Method in interface org.orekit.propagation.conversion.IntegratedPropagatorBuilder
Build a new KalmanODModel.
buildKalmanModel(List<IntegratedPropagatorBuilder>, List<CovarianceMatrixProvider>, ParameterDriversList) - Method in class org.orekit.propagation.conversion.NumericalPropagatorBuilder
Build a new KalmanODModel.
buildLSModel(IntegratedPropagatorBuilder[], List<ObservedMeasurement<?>>, ParameterDriversList, ModelObserver) - Method in class org.orekit.propagation.conversion.DSSTPropagatorBuilder
Build a new BatchLSODModel.
buildLSModel(IntegratedPropagatorBuilder[], List<ObservedMeasurement<?>>, ParameterDriversList, ModelObserver) - Method in interface org.orekit.propagation.conversion.IntegratedPropagatorBuilder
Build a new BatchLSODModel.
buildLSModel(IntegratedPropagatorBuilder[], List<ObservedMeasurement<?>>, ParameterDriversList, ModelObserver) - Method in class org.orekit.propagation.conversion.NumericalPropagatorBuilder
Build a new BatchLSODModel.
buildPropagator(double[]) - Method in class org.orekit.propagation.conversion.DSSTPropagatorBuilder
Build a propagator.
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

c1 - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator
C1 from SPTRCK #3.
c2 - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator
C2 from SPTRCK #3.
c4 - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator
C4 from SPTRCK #3.
CachedNormalizedSphericalHarmonicsProvider - Class in org.orekit.forces.gravity.potential
CachedNormalizedSphericalHarmonicsProvider(NormalizedSphericalHarmonicsProvider, double, int, int, double, double) - Constructor for class org.orekit.forces.gravity.potential.CachedNormalizedSphericalHarmonicsProvider
Simple constructor.
calculateField(double, double, double) - Method in class org.orekit.models.earth.GeoMagneticField
Calculate the magnetic field at the specified geodetic point identified by latitude, longitude and altitude.
canAdd(int, int) - Method in class org.orekit.forces.gravity.potential.OceanTidesReader
Check if coefficients can be added.
CartesianDerivativesFilter - Enum in org.orekit.utils
Enumerate for selecting which derivatives to use in TimeStampedPVCoordinates and TimeStampedFieldPVCoordinates interpolation.
CartesianOrbit - Class in org.orekit.orbits
This class holds Cartesian orbital parameters.
CartesianOrbit(TimeStampedPVCoordinates, Frame, double) - Constructor for class org.orekit.orbits.CartesianOrbit
Constructor from Cartesian parameters.
CartesianOrbit(PVCoordinates, Frame, AbsoluteDate, double) - Constructor for class org.orekit.orbits.CartesianOrbit
Constructor from Cartesian parameters.
CartesianOrbit(Orbit) - Constructor for class org.orekit.orbits.CartesianOrbit
Constructor from any kind of orbital parameters.
CCSDS_AEM_VERS - Static variable in class org.orekit.files.ccsds.StreamingAemWriter
Version number implemented.
CCSDS_EPOCH - Static variable in class org.orekit.time.AbsoluteDate
Reference epoch for CCSDS Time Code Format (CCSDS 301.0-B-4): 1958-01-01T00:00:00 International Atomic Time (not UTC).
CCSDS_EPOCH - Static variable in class org.orekit.time.DateComponents
Reference epoch for CCSDS Time Code Format (CCSDS 301.0-B-4): 1958-01-01.
CCSDS_OEM_VERS - Static variable in class org.orekit.files.ccsds.OEMWriter
Version number implemented.
CCSDS_OEM_VERS - Static variable in class org.orekit.files.ccsds.StreamingOemWriter
Version number implemented.
CCSDSFrame - Enum in org.orekit.files.ccsds
Frames used in CCSDS Orbit Data Messages.
CcsdsModifiedFrame - Class in org.orekit.files.ccsds
A reference frame created from the REF_FRAME and CENTER_NAME is a CCSDS OPM, OMM, or OEM file.
CcsdsTimeScale - Enum in org.orekit.files.ccsds
The set of time scales defined in Annex A of the ODM CCSDS standard 502.0-B-2.
CelestialBodies - Interface in org.orekit.bodies
Commonly used celestial bodies.
CelestialBody - Interface in org.orekit.bodies
Interface for celestial bodies like Sun, Moon or solar system planets.
CelestialBodyFactory - Class in org.orekit.bodies
Factory class for bodies of the solar system.
CelestialBodyLoader - Interface in org.orekit.bodies
Interface for loading celestial bodies.
CelestialBodyPointed - Class in org.orekit.attitudes
This class handles a celestial body pointed attitude provider.
CelestialBodyPointed(Frame, PVCoordinatesProvider, Vector3D, Vector3D, Vector3D) - Constructor for class org.orekit.attitudes.CelestialBodyPointed
Creates new instance.
CenterName - Enum in org.orekit.files.ccsds
Orbit central bodies for which a Celestial body can be created.
CENTRAL_ATTRACTION_COEFFICIENT - Static variable in class org.orekit.forces.gravity.NewtonianAttraction
Name of the single parameter of this model: the central attraction coefficient.
CENTRAL_ATTRACTION_COEFFICIENT - Static variable in class org.orekit.propagation.semianalytical.dsst.forces.DSSTNewtonianAttraction
Name of the single parameter of this model: the central attraction coefficient.
CENTURY - Static variable in interface org.orekit.propagation.numerical.cr3bp.CR3BPConstants
Moon semi-major axis = 384 400 000 m.
checkEOPContinuity(double) - Method in class org.orekit.frames.EOPHistory
Check Earth orientation parameters continuity.
checkInitialFiringState(SpacecraftState) - Method in class org.orekit.forces.maneuvers.trigger.EventBasedManeuverTriggers
Method to set the firing state on initialization.
checkTimeSystems() - Method in class org.orekit.files.ccsds.AEMFile
Check that, according to the CCSDS standard, every AEMBlock has the same time system.
checkTimeSystems() - Method in class org.orekit.files.ccsds.OEMFile
Check that, according to the CCSDS standard, every OEMBlock has the same time system.
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.
CircularFieldOfView - Class in org.orekit.geometry.fov
Class representing a spacecraft sensor Field Of View with circular shape.
CircularFieldOfView(Vector3D, double, double) - Constructor for class org.orekit.geometry.fov.CircularFieldOfView
Build a new instance.
CircularFieldOfViewDetector - Class in org.orekit.propagation.events
Deprecated.
CircularFieldOfViewDetector(double, PVCoordinatesProvider, Vector3D, double) - Constructor for class org.orekit.propagation.events.CircularFieldOfViewDetector
Deprecated.
Build a new instance.
CircularFieldOfViewDetector(double, PVCoordinatesProvider, double, VisibilityTrigger, Vector3D, double) - Constructor for class org.orekit.propagation.events.CircularFieldOfViewDetector
Deprecated.
Build a new instance.
CircularOrbit - Class in org.orekit.orbits
This class handles circular orbital parameters.
CircularOrbit(double, double, double, double, double, double, PositionAngle, Frame, AbsoluteDate, double) - Constructor for class org.orekit.orbits.CircularOrbit
Creates a new instance.
CircularOrbit(double, double, double, double, double, double, double, double, double, double, double, double, PositionAngle, Frame, AbsoluteDate, double) - Constructor for class org.orekit.orbits.CircularOrbit
Creates a new instance.
CircularOrbit(TimeStampedPVCoordinates, Frame, double) - Constructor for class org.orekit.orbits.CircularOrbit
Constructor from Cartesian parameters.
CircularOrbit(PVCoordinates, Frame, AbsoluteDate, double) - Constructor for class org.orekit.orbits.CircularOrbit
Constructor from Cartesian parameters.
CircularOrbit(Orbit) - Constructor for class org.orekit.orbits.CircularOrbit
Constructor from any kind of orbital parameters.
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.
ClasspathCrawler - Class in org.orekit.data
Provider for data files stored as resources in the classpath.
ClasspathCrawler(String...) - Constructor for class org.orekit.data.ClasspathCrawler
Build a data classpath crawler.
ClasspathCrawler(ClassLoader, String...) - Constructor for class org.orekit.data.ClasspathCrawler
Build a data classpath crawler.
clear() - Method in class org.orekit.propagation.events.handlers.FieldRecordAndContinue
Clear all stored events.
clear() - Method in class org.orekit.propagation.events.handlers.RecordAndContinue
Clear all stored events.
clearCelestialBodyCache(String) - Static method in class org.orekit.bodies.CelestialBodyFactory
Clear the specified celestial body from the internal cache.
clearCelestialBodyCache() - Static method in class org.orekit.bodies.CelestialBodyFactory
Clear all loaded celestial bodies.
clearCelestialBodyCache(String) - Method in class org.orekit.bodies.LazyLoadedCelestialBodies
Clear the specified celestial body from the internal cache.
clearCelestialBodyCache() - Method in class org.orekit.bodies.LazyLoadedCelestialBodies
Clear all loaded celestial bodies.
clearCelestialBodyLoaders(String) - Static method in class org.orekit.bodies.CelestialBodyFactory
Clear loaders for one celestial body.
clearCelestialBodyLoaders() - Static method in class org.orekit.bodies.CelestialBodyFactory
Clear loaders for all celestial bodies.
clearCelestialBodyLoaders(String) - Method in class org.orekit.bodies.LazyLoadedCelestialBodies
Clear loaders for one celestial body.
clearCelestialBodyLoaders() - Method in class org.orekit.bodies.LazyLoadedCelestialBodies
Clear loaders for all celestial bodies.
clearEOPHistoryLoaders() - Static method in class org.orekit.frames.FramesFactory
Clear loaders for Earth Orientation Parameters history.
clearEOPHistoryLoaders() - Method in class org.orekit.frames.LazyLoadedEop
Clear loaders for Earth Orientation Parameters history.
clearEOPHistoryLoaders() - Method in class org.orekit.frames.LazyLoadedFrames
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.FieldShortPeriodicsInterpolatedCoefficient
Clear the recorded values from the interpolation grid.
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.
clearOceanTidesReaders() - Method in class org.orekit.forces.gravity.potential.LazyLoadedGravityFields
Clear ocean tides readers.
clearPotentialCoefficientsReaders() - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory
Clear gravity field readers.
clearPotentialCoefficientsReaders() - Method in class org.orekit.forces.gravity.potential.LazyLoadedGravityFields
Clear gravity field readers.
clearProviders() - Method in class org.orekit.data.DataProvidersManager
Remove all data providers.
clearUTCTAIOffsetsLoaders() - Method in class org.orekit.time.LazyLoadedTimeScales
Clear loaders for UTC-TAI offsets history files.
clearUTCTAIOffsetsLoaders() - Static method in class org.orekit.time.TimeScalesFactory
Clear loaders for UTC-TAI offsets history files.
CLOCK_CORRECTIONS - Static variable in class org.orekit.propagation.analytical.gnss.ClockCorrectionsProvider
Name of the additional state for satellite clock corrections.
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.
CM_COEFFICIENTS - Static variable in class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseral
Identifier for cMm coefficients.
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.
CombinationType - Enum in org.orekit.estimation.measurements.gnss
Enumerate for combination of measurements types.
combine(ObservationData, ObservationData) - Method in class org.orekit.estimation.measurements.gnss.AbstractDualFrequencyCombination
Combines observation data using a dual frequency combination of measurements.
combine(ObservationDataSet) - Method in class org.orekit.estimation.measurements.gnss.AbstractDualFrequencyCombination
Combines observation data using a combination of measurements.
combine(ObservationDataSet) - Method in class org.orekit.estimation.measurements.gnss.AbstractSingleFrequencyCombination
Combines observation data using a combination of measurements.
combine(ObservationData, ObservationData) - Method in class org.orekit.estimation.measurements.gnss.AbstractSingleFrequencyCombination
Combines observation data using a single frequency combination of measurements.
combine(ObservationDataSet) - Method in interface org.orekit.estimation.measurements.gnss.MeasurementCombination
Combines observation data using a combination of measurements.
combine(ObservationDataSet) - Method in class org.orekit.estimation.measurements.gnss.MelbourneWubbenaCombination
Combines observation data using a combination of measurements.
CombinedObservationData - Class in org.orekit.gnss
Combined observation data.
CombinedObservationData(CombinationType, MeasurementType, double, double, List<ObservationData>) - Constructor for class org.orekit.gnss.CombinedObservationData
Constructor.
CombinedObservationDataSet - Class in org.orekit.gnss
Combined observation data set.
CombinedObservationDataSet(RinexHeader, SatelliteSystem, int, AbsoluteDate, double, List<CombinedObservationData>) - Constructor for class org.orekit.gnss.CombinedObservationDataSet
Simple constructor.
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(IntegerLeastSquareSolution) - Method in class org.orekit.estimation.measurements.gnss.IntegerLeastSquareSolution
compareTo(CoefficientsFactory.NSKey) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.CoefficientsFactory.NSKey
compareTo(AbsoluteDate) - Method in class org.orekit.time.AbsoluteDate
Compare the instance with another date.
compareTo(DateComponents) - Method in class org.orekit.time.DateComponents
compareTo(DateTimeComponents) - Method in class org.orekit.time.DateTimeComponents
compareTo(FieldAbsoluteDate<T>) - Method in class org.orekit.time.FieldAbsoluteDate
Compare the instance with another date.
compareTo(TimeComponents) - Method in class org.orekit.time.TimeComponents
compile(PoissonSeries...) - Static method in class org.orekit.data.PoissonSeries
Join several nutation series, for fast simultaneous evaluation.
complainIfNotSupported(String) - Method in class org.orekit.forces.AbstractForceModel
Complain if a parameter is not supported.
CompositeDataContext - Class in org.orekit.data
A simple implementation of DataContext that composes the constituent factories into a data context.
CompositeDataContext(TimeScales, Frames, CelestialBodies, GravityFields, GeoMagneticFields) - Constructor for class org.orekit.data.CompositeDataContext
Simple constructor.
compute(AbsoluteDate, List<Propagator>) - Method in class org.orekit.gnss.DOPComputer
Compute the DOP at a given date for a set of GNSS spacecrafts.
compute(LibrationOrbitType) - Method in class org.orekit.orbits.CR3BPDifferentialCorrection
Return the real starting PVCoordinates on the Libration orbit type after differential correction from a first guess.
compute() - Method in class org.orekit.utils.AbstractMultipleShooting
Return the list of corrected patch points.
compute() - Method in interface org.orekit.utils.MultipleShooting
Return the list of corrected patch points.
computeAdditionalConstraints(List<SpacecraftState>) - Method in class org.orekit.propagation.numerical.cr3bp.CR3BPMultipleShooter
Compute the additional constraints.
computeAdditionalConstraints(List<SpacecraftState>) - Method in class org.orekit.utils.AbstractMultipleShooting
Compute the additional constraints.
computeAdditionalConstraints(List<SpacecraftState>) - Method in class org.orekit.utils.MultipleShooter
Compute the additional constraints.
computeAdditionalJacobianMatrix(List<SpacecraftState>) - Method in class org.orekit.propagation.numerical.cr3bp.CR3BPMultipleShooter
Compute a part of the Jacobian matrix from additional constraints.
computeAdditionalJacobianMatrix(List<SpacecraftState>) - Method in class org.orekit.utils.AbstractMultipleShooting
Compute a part of the Jacobian matrix from additional constraints.
computeAdditionalJacobianMatrix(List<SpacecraftState>) - Method in class org.orekit.utils.MultipleShooter
Compute a part of the Jacobian matrix from additional constraints.
computeDerivatives(SpacecraftState) - Method in interface org.orekit.propagation.integration.AbstractIntegratedPropagator.MainStateEquations
Compute differential equations for main state.
computeDerivatives(SpacecraftState, double[]) - Method in interface org.orekit.propagation.integration.AdditionalEquations
Compute the derivatives related to the additional state parameters.
computeDerivatives(FieldSpacecraftState<T>) - Method in interface org.orekit.propagation.integration.FieldAbstractIntegratedPropagator.MainStateEquations
Compute differential equations for main state.
computeDerivatives(FieldSpacecraftState<T>, T[]) - Method in interface org.orekit.propagation.integration.FieldAdditionalEquations
Compute the derivatives related to the additional state parameters.
computeDerivatives(SpacecraftState, double[]) - Method in class org.orekit.propagation.numerical.cr3bp.STMEquations
Compute the derivatives related to the additional state parameters.
computeDerivatives(SpacecraftState, double[]) - Method in class org.orekit.propagation.numerical.EpochDerivativesEquations
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.
computeDerivatives(SpacecraftState, double[]) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPartialDerivativesEquations
Compute the derivatives related to the additional state parameters.
computeEpochJacobianMatrix(List<SpacecraftState>) - Method in class org.orekit.propagation.numerical.cr3bp.CR3BPMultipleShooter
Compute a part of the Jacobian matrix with derivatives from epoch.
computeEpochJacobianMatrix(List<SpacecraftState>) - Method in class org.orekit.utils.AbstractMultipleShooting
Compute a part of the Jacobian matrix with derivatives from epoch.
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).
computeGsHs(T, T, T, T, int, Field<T>) - Static method in class org.orekit.propagation.semianalytical.dsst.utilities.CoefficientsFactory
Compute recursively Gs and Hs polynomials from equation 3.1-(5).
computeHaloFirstGuess(double, LibrationOrbitFamily, double, double) - Method in class org.orekit.orbits.RichardsonExpansion
Calculate first Guess.
computeInitValues(T, T, T) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.FieldHansenTesseralLinear
Compute the values for the first four coefficients and their derivatives by means of series.
computeInitValues(T, T, T) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.FieldHansenThirdBodyLinear
Compute the initial values (see Collins, 4-255, 4-256 and 4.259)
computeInitValues(T) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.FieldHansenZonalLinear
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)
computeInitValues(double) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenZonalLinear
Compute the roots for the Hansen coefficients and their derivatives.
computeJacobianEccentricWrtCartesian() - Method in class org.orekit.orbits.CartesianOrbit
 
computeJacobianEccentricWrtCartesian() - Method in class org.orekit.orbits.CircularOrbit
Compute the Jacobian of the orbital parameters with eccentric angle with respect to the Cartesian parameters.
computeJacobianEccentricWrtCartesian() - Method in class org.orekit.orbits.EquinoctialOrbit
Compute the Jacobian of the orbital parameters with eccentric angle with respect to the Cartesian parameters.
computeJacobianEccentricWrtCartesian() - Method in class org.orekit.orbits.FieldCartesianOrbit
 
computeJacobianEccentricWrtCartesian() - Method in class org.orekit.orbits.FieldCircularOrbit
Compute the Jacobian of the orbital parameters with eccentric angle with respect to the Cartesian parameters.
computeJacobianEccentricWrtCartesian() - Method in class org.orekit.orbits.FieldEquinoctialOrbit
Compute the Jacobian of the orbital parameters with eccentric angle with respect to the Cartesian parameters.
computeJacobianEccentricWrtCartesian() - Method in class org.orekit.orbits.FieldKeplerianOrbit
Compute the Jacobian of the orbital parameters with eccentric angle with respect to the Cartesian parameters.
computeJacobianEccentricWrtCartesian() - Method in class org.orekit.orbits.FieldOrbit
Compute the Jacobian of the orbital parameters with eccentric angle with respect to the Cartesian parameters.
computeJacobianEccentricWrtCartesian() - Method in class org.orekit.orbits.KeplerianOrbit
Compute the Jacobian of the orbital parameters with eccentric angle with respect to the Cartesian parameters.
computeJacobianEccentricWrtCartesian() - Method in class org.orekit.orbits.Orbit
Compute the Jacobian of the orbital parameters with eccentric angle with respect to the Cartesian parameters.
computeJacobianMeanWrtCartesian() - Method in class org.orekit.orbits.CartesianOrbit
 
computeJacobianMeanWrtCartesian() - Method in class org.orekit.orbits.CircularOrbit
Compute the Jacobian of the orbital parameters with mean angle with respect to the Cartesian parameters.
computeJacobianMeanWrtCartesian() - Method in class org.orekit.orbits.EquinoctialOrbit
Compute the Jacobian of the orbital parameters with mean angle with respect to the Cartesian parameters.
computeJacobianMeanWrtCartesian() - Method in class org.orekit.orbits.FieldCartesianOrbit
 
computeJacobianMeanWrtCartesian() - Method in class org.orekit.orbits.FieldCircularOrbit
Compute the Jacobian of the orbital parameters with mean angle with respect to the Cartesian parameters.
computeJacobianMeanWrtCartesian() - Method in class org.orekit.orbits.FieldEquinoctialOrbit
Compute the Jacobian of the orbital parameters with mean angle with respect to the Cartesian parameters.
computeJacobianMeanWrtCartesian() - Method in class org.orekit.orbits.FieldKeplerianOrbit
Compute the Jacobian of the orbital parameters with mean angle with respect to the Cartesian parameters.
computeJacobianMeanWrtCartesian() - Method in class org.orekit.orbits.FieldOrbit
Compute the Jacobian of the orbital parameters with mean angle with respect to the Cartesian parameters.
computeJacobianMeanWrtCartesian() - Method in class org.orekit.orbits.KeplerianOrbit
Compute the Jacobian of the orbital parameters with mean angle with respect to the Cartesian parameters.
computeJacobianMeanWrtCartesian() - Method in class org.orekit.orbits.Orbit
Compute the Jacobian of the orbital parameters with mean angle with respect to the Cartesian parameters.
computeJacobianTrueWrtCartesian() - Method in class org.orekit.orbits.CartesianOrbit
 
computeJacobianTrueWrtCartesian() - Method in class org.orekit.orbits.CircularOrbit
Compute the Jacobian of the orbital parameters with true angle with respect to the Cartesian parameters.
computeJacobianTrueWrtCartesian() - Method in class org.orekit.orbits.EquinoctialOrbit
Compute the Jacobian of the orbital parameters with true angle with respect to the Cartesian parameters.
computeJacobianTrueWrtCartesian() - Method in class org.orekit.orbits.FieldCartesianOrbit
 
computeJacobianTrueWrtCartesian() - Method in class org.orekit.orbits.FieldCircularOrbit
Compute the Jacobian of the orbital parameters with true angle with respect to the Cartesian parameters.
computeJacobianTrueWrtCartesian() - Method in class org.orekit.orbits.FieldEquinoctialOrbit
Compute the Jacobian of the orbital parameters with true angle with respect to the Cartesian parameters.
computeJacobianTrueWrtCartesian() - Method in class org.orekit.orbits.FieldKeplerianOrbit
Compute the Jacobian of the orbital parameters with true angle with respect to the Cartesian parameters.
computeJacobianTrueWrtCartesian() - Method in class org.orekit.orbits.FieldOrbit
Compute the Jacobian of the orbital parameters with true angle with respect to the Cartesian parameters.
computeJacobianTrueWrtCartesian() - Method in class org.orekit.orbits.KeplerianOrbit
Compute the Jacobian of the orbital parameters with true angle with respect to the Cartesian parameters.
computeJacobianTrueWrtCartesian() - Method in class org.orekit.orbits.Orbit
Compute the Jacobian of the orbital parameters with true angle with respect to the Cartesian parameters.
computeLimitVisibilityPoint(double, double, double) - Method in class org.orekit.frames.TopocentricFrame
Compute the limit visibility point for a satellite in a given direction.
computeLyapunov(STMEquations) - Method in class org.orekit.orbits.CR3BPDifferentialCorrection
Return the real starting PVCoordinates on the Lyapunov orbit after differential correction from a first guess.
computeLyapunovFirstGuess(double, double, double) - Method in class org.orekit.orbits.RichardsonExpansion
Calculate first Guess.
computeMeanState(SpacecraftState, AttitudeProvider, Collection<DSSTForceModel>) - Static method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator
Conversion from osculating to mean orbit.
computeMeanState(SpacecraftState, AttitudeProvider, Collection<DSSTForceModel>, double, int) - Static method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator
Conversion from osculating to mean orbit.
computeMeanState(FieldSpacecraftState<T>, AttitudeProvider, Collection<DSSTForceModel>) - Method in class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator
Conversion from osculating to mean orbit.
computeMeanState(FieldSpacecraftState<T>, AttitudeProvider, Collection<DSSTForceModel>, double, int) - Method in class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator
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.
computeOsculatingState(FieldSpacecraftState<T>, AttitudeProvider, Collection<DSSTForceModel>) - Method in class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator
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).
computeQns(T, 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).
computeThrustDirection(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.forces.maneuvers.propulsion.ConstantThrustDirectionProvider
 
computeThrustDirection(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in interface org.orekit.forces.maneuvers.propulsion.ThrustDirectionProvider
Compute the thrust direction corresponding to an orbital state.
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.troposphere.DiscreteTroposphericModel
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.troposphere.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.troposphere.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.troposphere.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.troposphere.FixedTroposphericDelay
 
computeZenithDelay(T, T[], FieldAbsoluteDate<T>) - Method in class org.orekit.models.earth.troposphere.FixedTroposphericDelay
 
computeZenithDelay(double, double[], AbsoluteDate) - Method in class org.orekit.models.earth.troposphere.MariniMurrayModel
 
computeZenithDelay(T, T[], FieldAbsoluteDate<T>) - Method in class org.orekit.models.earth.troposphere.MariniMurrayModel
 
computeZenithDelay(double, double[], AbsoluteDate) - Method in class org.orekit.models.earth.troposphere.MendesPavlisModel
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.troposphere.MendesPavlisModel
This method allows the computation of the zenith hydrostatic and zenith wet delay.
computeZenithDelay(double, double[], AbsoluteDate) - Method in class org.orekit.models.earth.troposphere.SaastamoinenModel
 
computeZenithDelay(T, T[], FieldAbsoluteDate<T>) - Method in class org.orekit.models.earth.troposphere.SaastamoinenModel
 
computeZenithDelay(double, double[], AbsoluteDate) - Method in class org.orekit.models.earth.troposphere.TimeSpanEstimatedTroposphericModel
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.troposphere.TimeSpanEstimatedTroposphericModel
This method allows the computation of the zenith hydrostatic and zenith wet delay.
computeZenithDelay(double, double[], AbsoluteDate) - Method in class org.orekit.models.earth.troposphere.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.troposphere.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.troposphere.ViennaThreeModel
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.troposphere.ViennaThreeModel
This method allows the computation of the zenith hydrostatic and zenith wet delay.
ConfigurableLowThrustManeuver - Class in org.orekit.forces.maneuvers
This class implements a configurable low thrust maneuver.
ConfigurableLowThrustManeuver(ThrustDirectionAndAttitudeProvider, AbstractDetector<? extends EventDetector>, AbstractDetector<? extends EventDetector>, double, double) - Constructor for class org.orekit.forces.maneuvers.ConfigurableLowThrustManeuver
Constructor.
configureOceanLoadDeformationCoefficients(OceanLoadDeformationCoefficients) - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory
Configure ocean load deformation coefficients.
configureOceanLoadDeformationCoefficients(OceanLoadDeformationCoefficients) - Method in class org.orekit.forces.gravity.potential.LazyLoadedGravityFields
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.
ConstantThrustDirectionProvider - Class in org.orekit.forces.maneuvers.propulsion
Simple implementation of VariableThrustDirectionVector, providing a constant direction.
ConstantThrustDirectionProvider(Vector3D) - Constructor for class org.orekit.forces.maneuvers.propulsion.ConstantThrustDirectionProvider
Constructor.
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, AttitudeProvider, 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, String) - Constructor for class org.orekit.forces.maneuvers.ConstantThrustManeuver
Simple constructor for a constant direction and constant thrust.
ConstantThrustManeuver(AbsoluteDate, double, AttitudeProvider, AbstractConstantThrustPropulsionModel) - Constructor for class org.orekit.forces.maneuvers.ConstantThrustManeuver
Simple constructor for a constant direction and constant thrust.
ConstantThrustManeuver(AttitudeProvider, DateBasedManeuverTriggers, AbstractConstantThrustPropulsionModel) - Constructor for class org.orekit.forces.maneuvers.ConstantThrustManeuver
Simple constructor for a constant direction and constant thrust.
contains(String) - Static method in enum org.orekit.files.ccsds.CcsdsTimeScale
Check if timeScale is one of the values supported by this enum.
containsSatellite(String) - Method in class org.orekit.files.sp3.SP3File
Tests whether a satellite with the given id is contained in this orbit file.
ContinueOnEvent<T extends EventDetector> - Class in org.orekit.propagation.events.handlers
Event handler which will always return continue as a state.
ContinueOnEvent() - Constructor for class org.orekit.propagation.events.handlers.ContinueOnEvent
 
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(double[]) - Method in interface org.orekit.data.SimpleTimeStampedTableParser.RowConverter
Convert a row.
convert(Propagator, double, int, List<String>) - Method in class org.orekit.propagation.conversion.AbstractPropagatorConverter
Convert a propagator to another.
convert(Propagator, double, int, String...) - Method in class org.orekit.propagation.conversion.AbstractPropagatorConverter
Convert a propagator to another.
convert(List<SpacecraftState>, boolean, List<String>) - Method in class org.orekit.propagation.conversion.AbstractPropagatorConverter
Find the propagator that minimize the mean square error for a sample of states.
convert(List<SpacecraftState>, boolean, String...) - Method in class org.orekit.propagation.conversion.AbstractPropagatorConverter
Find the propagator that minimize the mean square error for a sample of states.
convert() - Method in class org.orekit.propagation.conversion.OsculatingToMeanElementsConverter
Convert an osculating orbit into a mean orbit, in DSST sense.
convert(Propagator, double, int, List<String>) - Method in interface org.orekit.propagation.conversion.PropagatorConverter
Convert a propagator into another one.
convert(Propagator, double, int, String...) - Method in interface org.orekit.propagation.conversion.PropagatorConverter
Convert a propagator into another one.
convert(List<SpacecraftState>, boolean, List<String>) - Method in interface org.orekit.propagation.conversion.PropagatorConverter
Find the propagator that minimize the mean square error for a sample of states.
convert(List<SpacecraftState>, boolean, String...) - Method in interface org.orekit.propagation.conversion.PropagatorConverter
Find the propagator that minimize the mean square error for a sample of states.
convertType(Orbit) - Method in enum org.orekit.orbits.OrbitType
Convert an orbit to the instance type.
convertType(FieldOrbit<T>) - Method in enum org.orekit.orbits.OrbitType
Convert an orbit to the instance type.
copy() - Method in class org.orekit.propagation.conversion.DSSTPropagatorBuilder
Create a copy of a DSSTPropagatorBuilder object.
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.BeidouGeo
Select the /** 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(GNSSAttitudeContext) - Method in class org.orekit.gnss.attitude.BeidouMeo
Select the /** 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(GNSSAttitudeContext) - Method in class org.orekit.gnss.attitude.Galileo
Select the /** 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(GNSSAttitudeContext) - Method in class org.orekit.gnss.attitude.GenericGNSS
Select the /** 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(GNSSAttitudeContext) - Method in class org.orekit.gnss.attitude.Glonass
Select the /** 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(GNSSAttitudeContext) - Method in class org.orekit.gnss.attitude.GPSBlockIIA
Select the /** 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(GNSSAttitudeContext) - Method in class org.orekit.gnss.attitude.GPSBlockIIF
Select the /** 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(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.GPSBlockIIR
Compute GNSS attitude with midnight/noon yaw turn correction.
cosi0 - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator
cosinus original inclination.
CovarianceMatrix(AbsoluteDate, LOFType, Frame, RealMatrix) - Constructor for class org.orekit.files.ccsds.OEMFile.CovarianceMatrix
Covariance Matrix constructor.
CovarianceMatrixProvider - Interface in org.orekit.estimation.sequential
Provider for process noise matrices.
CR3BPConstants - Interface in org.orekit.propagation.numerical.cr3bp
Set of useful physical CR3BP constants using JPL data.
CR3BPDifferentialCorrection - Class in org.orekit.orbits
Class implementing the differential correction method for Halo or Lyapunov Orbits.
CR3BPDifferentialCorrection(PVCoordinates, CR3BPSystem, double) - Constructor for class org.orekit.orbits.CR3BPDifferentialCorrection
Simple Constructor.
CR3BPDifferentialCorrection(PVCoordinates, CR3BPSystem, double, AttitudeProvider, TimeScale) - Constructor for class org.orekit.orbits.CR3BPDifferentialCorrection
Simple Constructor.
CR3BPFactory - Class in org.orekit.bodies
Factory class creating predefined CR3BP system using CR3BPSystem class.
CR3BPForceModel - Class in org.orekit.propagation.numerical.cr3bp
Class calculating the acceleration induced by CR3BP model.
CR3BPForceModel(CR3BPSystem) - Constructor for class org.orekit.propagation.numerical.cr3bp.CR3BPForceModel
Simple constructor.
CR3BPMultipleShooter - Class in org.orekit.propagation.numerical.cr3bp
Multiple shooting method applicable for orbits, either propagation in CR3BP, or in an ephemeris model.
CR3BPMultipleShooter(List<SpacecraftState>, List<NumericalPropagator>, List<AdditionalEquations>, double, double) - Constructor for class org.orekit.propagation.numerical.cr3bp.CR3BPMultipleShooter
Simple Constructor.
CR3BPRotatingFrame - Class in org.orekit.frames
Class creating the rotating frame centered on the barycenter of the CR3BP System.
CR3BPRotatingFrame(double, CelestialBody, CelestialBody) - Constructor for class org.orekit.frames.CR3BPRotatingFrame
Simple constructor.
CR3BPSystem - Class in org.orekit.bodies
Class creating, from two different celestial bodies, the corresponding system with respect to the Circular Restricted Three Body problem hypotheses.
CR3BPSystem(CelestialBody, CelestialBody, double) - Constructor for class org.orekit.bodies.CR3BPSystem
Simple constructor.
CR3BPSystem(CelestialBody, CelestialBody, double, double) - Constructor for class org.orekit.bodies.CR3BPSystem
Simple constructor.
create(double, double, int, EventHandler<? super ImpulseManeuver<T>>) - Method in class org.orekit.forces.maneuvers.ImpulseManeuver
Build a new instance.
create(OneAxisEllipsoid, GeodeticPoint) - Static method in class org.orekit.gnss.DOPComputer
Creates a DOP computer for one location.
create(double, double, int, EventHandler<? super T>) - Method in class org.orekit.propagation.events.AbstractDetector
Build a new instance.
create(double, double, int, EventHandler<? super AlignmentDetector>) - Method in class org.orekit.propagation.events.AlignmentDetector
Build a new instance.
create(double, double, int, EventHandler<? super AltitudeDetector>) - Method in class org.orekit.propagation.events.AltitudeDetector
Build a new instance.
create(double, double, int, EventHandler<? super AngularSeparationDetector>) - Method in class org.orekit.propagation.events.AngularSeparationDetector
Build a new instance.
create(double, double, int, EventHandler<? super ApsideDetector>) - Method in class org.orekit.propagation.events.ApsideDetector
Build a new instance.
create(double, double, int, EventHandler<? super BooleanDetector>) - Method in class org.orekit.propagation.events.BooleanDetector
 
create(double, double, int, EventHandler<? super CircularFieldOfViewDetector>) - Method in class org.orekit.propagation.events.CircularFieldOfViewDetector
Deprecated.
Build a new instance.
create(double, double, int, EventHandler<? super DateDetector>) - Method in class org.orekit.propagation.events.DateDetector
Build a new instance.
create(double, double, int, EventHandler<? super EclipseDetector>) - Method in class org.orekit.propagation.events.EclipseDetector
Build a new instance.
create(double, double, int, EventHandler<? super ElevationDetector>) - Method in class org.orekit.propagation.events.ElevationDetector
Build a new instance.
create(double, double, int, EventHandler<? super ElevationExtremumDetector>) - Method in class org.orekit.propagation.events.ElevationExtremumDetector
Build a new instance.
create(double, double, int, EventHandler<? super EventEnablingPredicateFilter<T>>) - Method in class org.orekit.propagation.events.EventEnablingPredicateFilter
Build a new instance.
create(double, double, int, EventHandler<? super EventShifter<T>>) - Method in class org.orekit.propagation.events.EventShifter
Build a new instance.
create(double, double, int, EventHandler<? super EventSlopeFilter<T>>) - Method in class org.orekit.propagation.events.EventSlopeFilter
Build a new instance.
create(T, T, int, FieldEventHandler<? super D, T>) - Method in class org.orekit.propagation.events.FieldAbstractDetector
Build a new instance.
create(T, T, int, FieldEventHandler<? super FieldAltitudeDetector<T>, T>) - Method in class org.orekit.propagation.events.FieldAltitudeDetector
Build a new instance.
create(T, T, int, FieldEventHandler<? super FieldApsideDetector<T>, T>) - Method in class org.orekit.propagation.events.FieldApsideDetector
Build a new instance.
create(T, T, int, FieldEventHandler<? super FieldDateDetector<T>, T>) - Method in class org.orekit.propagation.events.FieldDateDetector
Build a new instance.
create(T, T, int, FieldEventHandler<? super FieldEclipseDetector<T>, T>) - Method in class org.orekit.propagation.events.FieldEclipseDetector
Build a new instance.
create(T, T, int, FieldEventHandler<? super FieldElevationDetector<T>, T>) - Method in class org.orekit.propagation.events.FieldElevationDetector
Build a new instance.
create(T, T, int, FieldEventHandler<? super FieldFunctionalDetector<T>, T>) - Method in class org.orekit.propagation.events.FieldFunctionalDetector
 
create(T, T, int, FieldEventHandler<? super FieldLatitudeCrossingDetector<T>, T>) - Method in class org.orekit.propagation.events.FieldLatitudeCrossingDetector
Build a new instance.
create(T, T, int, FieldEventHandler<? super FieldNodeDetector<T>, T>) - Method in class org.orekit.propagation.events.FieldNodeDetector
Build a new instance.
create(double, double, int, EventHandler<? super FieldOfViewDetector>) - Method in class org.orekit.propagation.events.FieldOfViewDetector
Build a new instance.
create(double, double, int, EventHandler<? super FootprintOverlapDetector>) - Method in class org.orekit.propagation.events.FootprintOverlapDetector
Build a new instance.
create(double, double, int, EventHandler<? super 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 HaloXZPlaneCrossingDetector>) - Method in class org.orekit.propagation.events.HaloXZPlaneCrossingDetector
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 MagneticFieldDetector>) - Method in class org.orekit.propagation.events.MagneticFieldDetector
Build a new instance.
create(double, double, int, EventHandler<? super NegateDetector>) - Method in class org.orekit.propagation.events.NegateDetector
 
create(double, double, int, EventHandler<? super NodeDetector>) - Method in class org.orekit.propagation.events.NodeDetector
Build a new instance.
create(double, double, int, EventHandler<? super PositionAngleDetector>) - Method in class org.orekit.propagation.events.PositionAngleDetector
Build a new instance.
createBesselianEpoch(double) - Static method in class org.orekit.time.AbsoluteDate
Build an instance corresponding to a Besselian Epoch (BE).
createBesselianEpoch(double) - Method in class org.orekit.time.AbstractTimeScales
 
createBesselianEpoch(T) - Static method in class org.orekit.time.FieldAbsoluteDate
Build an instance corresponding to a Besselian Epoch (BE).
createBesselianEpoch(T, TimeScales) - Static method in class org.orekit.time.FieldAbsoluteDate
Build an instance corresponding to a Besselian Epoch (BE).
createBesselianEpoch(double) - Method in interface org.orekit.time.TimeScales
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, T) - Static method in class org.orekit.time.FieldAbsoluteDate
Build an instance corresponding to a GPS date.
createGPSDate(int, T, TimeScale) - 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(double) - Method in class org.orekit.time.AbstractTimeScales
 
createJulianEpoch(T) - Static method in class org.orekit.time.FieldAbsoluteDate
Build an instance corresponding to a Julian Epoch (JE).
createJulianEpoch(T, TimeScales) - Static method in class org.orekit.time.FieldAbsoluteDate
Build an instance corresponding to a Julian Epoch (JE).
createJulianEpoch(double) - Method in interface org.orekit.time.TimeScales
Build an instance corresponding to a Julian Epoch (JE).
createMapper(AbsoluteDate, double, OrbitType, PositionAngle, AttitudeProvider, Frame) - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
Create a mapper between raw double components and spacecraft state.
createMapper(FieldAbsoluteDate<T>, T, 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>, T, OrbitType, PositionAngle, AttitudeProvider, Frame) - Method in class org.orekit.propagation.numerical.FieldNumericalPropagator
Create a mapper between raw double components and spacecraft state.
createMapper(AbsoluteDate, double, OrbitType, PositionAngle, AttitudeProvider, Frame) - Method in class org.orekit.propagation.numerical.GLONASSNumericalPropagator
 
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>, T, OrbitType, PositionAngle, AttitudeProvider, Frame) - Method in class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator
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.
createPropagators(RealVector) - Method in class org.orekit.estimation.leastsquares.BatchLSModel
Create the propagators and parameters corresponding to an evaluation point.
createPropagators(RealVector) - Method in interface org.orekit.estimation.leastsquares.BatchLSODModel
Create the propagators and parameters corresponding to an evaluation point.
createPropagators(RealVector) - Method in class org.orekit.estimation.leastsquares.DSSTBatchLSModel
Create the propagators and parameters corresponding to an evaluation point.
createTransformedITRF(Frame, String) - Method in enum org.orekit.frames.HelmertTransformation.Predefined
Create an ITRF frame by transforming another ITRF frame.
createTransformedITRF(Frame, String, TimeScale) - Method in enum org.orekit.frames.HelmertTransformation.Predefined
Create an ITRF frame by transforming another ITRF frame.
createVertex(Vector3D, Vector3D, double, int) - Method in enum org.orekit.geometry.fov.PolygonalFieldOfView.DefiningConeType
Create a vertex.
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.
CssiSpaceWeatherData - Class in org.orekit.models.earth.atmosphere.data
This class provides three-hourly and daily solar activity data needed by atmospheric models: F107 solar flux, Ap and Kp indexes.
CssiSpaceWeatherData(String) - Constructor for class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherData
Simple constructor.
CssiSpaceWeatherData(String, DataProvidersManager, TimeScale) - Constructor for class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherData
Constructor that allows specifying the source of the CSSI space weather file.
CssiSpaceWeatherDataLoader - Class in org.orekit.models.earth.atmosphere.data
This class reads solar activity data from CSSI Space Weather files for the class CssiSpaceWeatherData.
CssiSpaceWeatherDataLoader(TimeScale) - Constructor for class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherDataLoader
Constructor.
CssiSpaceWeatherDataLoader.LineParameters - Class in org.orekit.models.earth.atmosphere.data
Container class for Solar activity indexes.
CssiSpaceWeatherDataLoader.LineReader - Class in org.orekit.models.earth.atmosphere.data
Helper class to parse line data and to raise exceptions if needed.
cycleSlipDataSet(String, AbsoluteDate, double, Frequency) - Method in class org.orekit.estimation.measurements.gnss.AbstractCycleSlipDetector
Set the data: collect data at the current Date, at the current frequency, for a given satellite, add it within the attributes data and stuff.
CycleSlipDetectorResults - Class in org.orekit.estimation.measurements.gnss
This class is used to contains all the data computed within cycle-slip detector.
CycleSlipDetectors - Interface in org.orekit.estimation.measurements.gnss
Interface for phase measurement cycle-slip detection.

D

DataContext - Interface in org.orekit.data
Provides auxiliary data for portions of the application.
dataContext(DataContext) - Method in class org.orekit.propagation.analytical.gnss.GLONASSAnalyticalPropagator.Builder
Sets the data context used by the propagator.
dataContext(DataContext) - Method in class org.orekit.propagation.numerical.GLONASSNumericalPropagator.Builder
Sets the data context used by the propagator.
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
This class manages supported data providers.
DataProvidersManager() - Constructor for class org.orekit.data.DataProvidersManager
Build an instance with default configuration.
DATE_AFTER - Static variable in class org.orekit.forces.drag.TimeSpanDragForce
Prefix for dates after in the parameter drivers' name.
DATE_AFTER - Static variable in class org.orekit.models.earth.troposphere.TimeSpanEstimatedTroposphericModel
Prefix for dates after in the tropospheric parameter drivers' name.
DATE_BEFORE - Static variable in class org.orekit.forces.drag.TimeSpanDragForce
Prefix for dates before in the parameter drivers' name.
DATE_BEFORE - Static variable in class org.orekit.models.earth.troposphere.TimeSpanEstimatedTroposphericModel
Prefix for dates before in the tropospheric parameter drivers' name.
DateBasedManeuverTriggers - Class in org.orekit.forces.maneuvers.trigger
Maneuver triggers based on a start and end date, with no parameter drivers.
DateBasedManeuverTriggers(AbsoluteDate, double) - Constructor for class org.orekit.forces.maneuvers.trigger.DateBasedManeuverTriggers
 
DateComponents - Class in org.orekit.time
Class representing a date broken up as year, month and day components.
DateComponents(int, int, int) - Constructor for class org.orekit.time.DateComponents
Build a date from its components.
DateComponents(int, Month, int) - Constructor for class org.orekit.time.DateComponents
Build a date from its components.
DateComponents(int, int) - Constructor for class org.orekit.time.DateComponents
Build a date from a year and day number.
DateComponents(int) - Constructor for class org.orekit.time.DateComponents
Build a date from its offset with respect to a DateComponents.J2000_EPOCH.
DateComponents(DateComponents, int) - Constructor for class org.orekit.time.DateComponents
Build a date from its offset with respect to a reference epoch.
DateDetector - Class in org.orekit.propagation.events
Finder for date events.
DateDetector(double, double, TimeStamped...) - Constructor for class org.orekit.propagation.events.DateDetector
Build a new instance.
DateDetector(AbsoluteDate) - Constructor for class org.orekit.propagation.events.DateDetector
Build a new instance.
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(DateComponents, TimeComponents) - Constructor for class org.orekit.time.DateTimeComponents
Build a new instance from its components.
DateTimeComponents(int, int, int, int, int, double) - Constructor for class org.orekit.time.DateTimeComponents
Build an instance from raw level components.
DateTimeComponents(int, Month, int, int, int, double) - Constructor for class org.orekit.time.DateTimeComponents
Build an instance from raw level components.
DateTimeComponents(int, int, int) - Constructor for class org.orekit.time.DateTimeComponents
Build an instance from raw level components.
DateTimeComponents(int, Month, int) - Constructor for class org.orekit.time.DateTimeComponents
Build an instance from raw level components.
DateTimeComponents(DateTimeComponents, double) - Constructor for class org.orekit.time.DateTimeComponents
Build an instance from a seconds offset with respect to another one.
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.
DeepSDP4(TLE, AttitudeProvider, double, Frame) - 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_LOW_ELEVATION_THRESHOLD - Static variable in class org.orekit.models.earth.troposphere.SaastamoinenModel
Default lowest acceptable elevation angle [rad].
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 maximum 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.StreamingAemWriter
Default value for Keyword.ORIGINATOR.
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.atmosphere.data.MarshallSolarActivityFutureEstimation
Default regular expression for the supported name that work with all officially published files.
DEFAULT_SUPPORTED_NAMES - Static variable in class org.orekit.models.earth.ionosphere.KlobucharIonoCoefficientsLoader
Default supported files name pattern.
DEFAULT_SUPPORTED_NAMES - Static variable in class org.orekit.models.earth.troposphere.ViennaModelCoefficientsLoader
Default supported files name pattern.
DEFAULT_SUPPORTED_NAMES - Static variable in class org.orekit.models.earth.weather.GlobalPressureTemperature2Model
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.
DefaultDataContext - Annotation Type in org.orekit.annotation
Indicates that the annotated method, field, or constructor uses the default data context.
DefaultDataContextPlugin - Class in org.orekit.compiler.plugin
Processes DefaultDataContext to issue warnings at compile time.
DefaultDataContextPlugin() - Constructor for class org.orekit.compiler.plugin.DefaultDataContextPlugin
 
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.troposphere.SaastamoinenModel
Default file name for δR correction term table.
dependsOnPositionOnly() - Method in class org.orekit.forces.drag.AbstractDragForceModel
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.SingleBodyAbsoluteAttraction
Check if force models depends on position only.
dependsOnPositionOnly() - Method in class org.orekit.forces.gravity.SingleBodyRelativeAttraction
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.inertia.InertialForces
Check if force models depends on position only.
dependsOnPositionOnly() - Method in class org.orekit.forces.maneuvers.Maneuver
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.AbstractRadiationForceModel
Check if force models depends on position only.
dependsOnPositionOnly() - Method in class org.orekit.propagation.numerical.cr3bp.CR3BPForceModel
Check if force models depends on position only.
derivative(BodiesElements) - Method in interface org.orekit.data.PoissonSeries.CompiledSeries
Evaluate time derivative of a set of Poisson series.
derivative(FieldBodiesElements<S>) - Method in interface org.orekit.data.PoissonSeries.CompiledSeries
Evaluate time derivative of a set of Poisson series.
derivative(double) - Method in class org.orekit.data.PolynomialNutation
Evaluate the time derivative of the polynomial.
derivative(T) - Method in class org.orekit.data.PolynomialNutation
Evaluate the time derivative of the polynomial.
detect(List<ObservationDataSet>) - Method in class org.orekit.estimation.measurements.gnss.AbstractCycleSlipDetector
Detects if a cycle-slip occurs for a given list of observation data set.
detect(List<ObservationDataSet>) - Method in interface org.orekit.estimation.measurements.gnss.CycleSlipDetectors
Detects if a cycle-slip occurs for a given list of observation data set.
differentiate(ParameterFunction, int, double) - Static method in class org.orekit.utils.Differentiation
Differentiate a scalar function using finite differences.
differentiate(StateFunction, int, AttitudeProvider, OrbitType, PositionAngle, double, int) - Static method in class org.orekit.utils.Differentiation
Differentiate a vector function using finite differences.
Differentiation - Class in org.orekit.utils
Utility class for differentiating various kinds of functions.
directionAt(double) - Method in class org.orekit.geometry.fov.CircularFieldOfView
Get boundary direction at angle.
directionAt(double) - Method in class org.orekit.geometry.fov.EllipticalFieldOfView
Get boundary direction at angle.
directionAt(double) - Method in class org.orekit.geometry.fov.SmoothFieldOfView
Get boundary direction at angle.
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.
discreteSearch() - Method in class org.orekit.estimation.measurements.gnss.AbstractLambdaMethod
Find the best solutions to the Integer Least Square problem.
discreteSearch() - Method in class org.orekit.estimation.measurements.gnss.IntegerBootstrapping
Compute the solution by the bootstrap method from equation (13) in P.J.G.
discreteSearch() - Method in class org.orekit.estimation.measurements.gnss.LambdaMethod
Find the best solutions to the Integer Least Square problem.
discreteSearch() - Method in class org.orekit.estimation.measurements.gnss.ModifiedLambdaMethod
Find the best solutions to the Integer Least Square problem.
DiscreteTroposphericModel - Interface in org.orekit.models.earth.troposphere
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.
DivertedSingularityAiming - Class in org.orekit.models.earth.tessellation
Class used to orient tiles such that there are no singularities within the zone of interest.
DivertedSingularityAiming(SphericalPolygonsSet) - Constructor for class org.orekit.models.earth.tessellation.DivertedSingularityAiming
Simple constructor.
doEvent(SpacecraftState) - Method in class org.orekit.propagation.events.EventState
Notify the user's listener of the event.
doEvent(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.events.FieldEventState
Notify the user's listener of the event.
doModify(EstimatedMeasurement<?>) - Method in class org.orekit.estimation.measurements.modifiers.AbstractShapiroBaseModifier
Modify measurement.
DOP - Class in org.orekit.gnss
This class is a container for the result of a single DOP computation.
DOP(GeodeticPoint, AbsoluteDate, int, double, double, double, double, double) - Constructor for class org.orekit.gnss.DOP
Constructor.
DOP_MIN_ELEVATION - Static variable in class org.orekit.gnss.DOPComputer
Minimum elevation : 0°.
DOPComputer - Class in org.orekit.gnss
This class aims at computing the dilution of precision.
DormandPrince54IntegratorBuilder - Class in org.orekit.propagation.conversion
Builder for DormandPrince54Integrator.
DormandPrince54IntegratorBuilder(double, double, double) - Constructor for class org.orekit.propagation.conversion.DormandPrince54IntegratorBuilder
Build a new instance.
DormandPrince853IntegratorBuilder - Class in org.orekit.propagation.conversion
Builder for DormandPrince853Integrator.
DormandPrince853IntegratorBuilder(double, double, double) - Constructor for class org.orekit.propagation.conversion.DormandPrince853IntegratorBuilder
Build a new instance.
DoubleDihedraFieldOfView - Class in org.orekit.geometry.fov
Class representing a spacecraft sensor Field Of View with dihedral shape (i.e.
DoubleDihedraFieldOfView(Vector3D, Vector3D, double, Vector3D, double, double) - Constructor for class org.orekit.geometry.fov.DoubleDihedraFieldOfView
Build a Field Of View with dihedral shape (i.e.
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(FieldAbsoluteDate<T>, Frame, FieldVector3D<T>, FieldRotation<T>, T, T, FieldVector3D<T>, T[]) - Method in class org.orekit.forces.BoxAndSolarArraySpacecraft
Compute the acceleration due to drag.
dragAcceleration(AbsoluteDate, Frame, Vector3D, Rotation, double, double, Vector3D, double[]) - Method in interface org.orekit.forces.drag.DragSensitive
Compute the acceleration due to drag.
dragAcceleration(FieldAbsoluteDate<T>, Frame, FieldVector3D<T>, FieldRotation<T>, T, T, FieldVector3D<T>, T[]) - Method in interface org.orekit.forces.drag.DragSensitive
Compute the acceleration due to drag.
dragAcceleration(AbsoluteDate, Frame, Vector3D, Rotation, double, double, Vector3D, double[]) - Method in class org.orekit.forces.drag.IsotropicDrag
Compute the acceleration due to drag.
dragAcceleration(FieldAbsoluteDate<T>, Frame, FieldVector3D<T>, FieldRotation<T>, T, T, FieldVector3D<T>, T[]) - Method in class org.orekit.forces.drag.IsotropicDrag
Compute the acceleration due to drag.
DragForce - Class in org.orekit.forces.drag
Atmospheric drag force model.
DragForce(Atmosphere, DragSensitive) - Constructor for class org.orekit.forces.drag.DragForce
Simple constructor.
DragSensitive - Interface in org.orekit.forces.drag
Interface for spacecraft that are sensitive to atmospheric drag forces.
DSSTAtmosphericDrag - Class in org.orekit.propagation.semianalytical.dsst.forces
Atmospheric drag contribution to the DSSTPropagator.
DSSTAtmosphericDrag(DragForce, double) - Constructor for class org.orekit.propagation.semianalytical.dsst.forces.DSSTAtmosphericDrag
Simple constructor with custom force.
DSSTAtmosphericDrag(Atmosphere, double, double, double) - Constructor for class org.orekit.propagation.semianalytical.dsst.forces.DSSTAtmosphericDrag
Simple constructor assuming spherical spacecraft.
DSSTAtmosphericDrag(Atmosphere, DragSensitive, double) - Constructor for class org.orekit.propagation.semianalytical.dsst.forces.DSSTAtmosphericDrag
Simple constructor with custom spacecraft.
DSSTBatchLSModel - Class in org.orekit.estimation.leastsquares
DSSTBatchLSModel(IntegratedPropagatorBuilder[], List<ObservedMeasurement<?>>, ParameterDriversList, ModelObserver, PropagationType, PropagationType) - Constructor for class org.orekit.estimation.leastsquares.DSSTBatchLSModel
Simple constructor.
DSSTForceModel - Interface in org.orekit.propagation.semianalytical.dsst.forces
This interface represents a force modifying spacecraft motion for a DSSTPropagator.
DSSTJacobiansMapper - Class in org.orekit.propagation.semianalytical.dsst
Mapper between two-dimensional Jacobian matrices and one-dimensional additional state arrays.
DSSTKalmanModel - Class in org.orekit.estimation.sequential
Class defining the process model dynamics to use with a KalmanEstimator.
DSSTKalmanModel(List<IntegratedPropagatorBuilder>, List<CovarianceMatrixProvider>, ParameterDriversList, PropagationType, PropagationType) - Constructor for class org.orekit.estimation.sequential.DSSTKalmanModel
Kalman process model constructor (package private).
DSSTNewtonianAttraction - Class in org.orekit.propagation.semianalytical.dsst.forces
Force model for Newtonian central body attraction for the DSST propagator.
DSSTNewtonianAttraction(double) - Constructor for class org.orekit.propagation.semianalytical.dsst.forces.DSSTNewtonianAttraction
Simple constructor.
DSSTPartialDerivativesEquations - Class in org.orekit.propagation.semianalytical.dsst
Set of additional equations computing the partial derivatives of the state (orbit) with respect to initial state and force models parameters.
DSSTPartialDerivativesEquations(String, DSSTPropagator, PropagationType) - Constructor for class org.orekit.propagation.semianalytical.dsst.DSSTPartialDerivativesEquations
Simple constructor.
DSSTPropagator - Class in org.orekit.propagation.semianalytical.dsst
This class propagates orbits using the DSST theory.
DSSTPropagator(ODEIntegrator, PropagationType) - Constructor for class org.orekit.propagation.semianalytical.dsst.DSSTPropagator
Create a new instance of DSSTPropagator.
DSSTPropagator(ODEIntegrator, PropagationType, AttitudeProvider) - Constructor for class org.orekit.propagation.semianalytical.dsst.DSSTPropagator
Create a new instance of DSSTPropagator.
DSSTPropagator(ODEIntegrator) - Constructor for class org.orekit.propagation.semianalytical.dsst.DSSTPropagator
Create a new instance of DSSTPropagator.
DSSTPropagatorBuilder - Class in org.orekit.propagation.conversion
Builder for DSST propagator.
DSSTPropagatorBuilder(Orbit, ODEIntegratorBuilder, double, PropagationType, PropagationType) - Constructor for class org.orekit.propagation.conversion.DSSTPropagatorBuilder
Build a new instance.
DSSTPropagatorBuilder(Orbit, ODEIntegratorBuilder, double, PropagationType, PropagationType, AttitudeProvider) - Constructor for class org.orekit.propagation.conversion.DSSTPropagatorBuilder
Build a new instance.
DSSTSolarRadiationPressure - Class in org.orekit.propagation.semianalytical.dsst.forces
Solar radiation pressure contribution to the DSSTPropagator.
DSSTSolarRadiationPressure(double, double, ExtendedPVCoordinatesProvider, double, double) - Constructor for class org.orekit.propagation.semianalytical.dsst.forces.DSSTSolarRadiationPressure
Simple constructor with default reference values and spherical spacecraft.
DSSTSolarRadiationPressure(ExtendedPVCoordinatesProvider, double, RadiationSensitive, double) - Constructor for class org.orekit.propagation.semianalytical.dsst.forces.DSSTSolarRadiationPressure
Simple constructor with default reference values, but custom spacecraft.
DSSTSolarRadiationPressure(double, double, double, double, ExtendedPVCoordinatesProvider, double, double) - Constructor for class org.orekit.propagation.semianalytical.dsst.forces.DSSTSolarRadiationPressure
Constructor with customizable reference values but spherical spacecraft.
DSSTSolarRadiationPressure(double, double, ExtendedPVCoordinatesProvider, double, RadiationSensitive, double) - Constructor for class org.orekit.propagation.semianalytical.dsst.forces.DSSTSolarRadiationPressure
Complete constructor.
DSSTTesseral - Class in org.orekit.propagation.semianalytical.dsst.forces
Tesseral contribution to the central body gravitational perturbation.
DSSTTesseral(Frame, double, UnnormalizedSphericalHarmonicsProvider) - Constructor for class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseral
Simple constructor with default reference values.
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, double) - 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) - Constructor for class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonal
Constructor with default reference values.
DSSTZonal(UnnormalizedSphericalHarmonicsProvider, int, int, int) - Constructor for class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonal
Simple constructor.
DTM2000 - Class in org.orekit.models.earth.atmosphere
This atmosphere model is the realization of the DTM-2000 model.
DTM2000(DTM2000InputParameters, PVCoordinatesProvider, BodyShape) - Constructor for class org.orekit.models.earth.atmosphere.DTM2000
Simple constructor for independent computation.
DTM2000(DTM2000InputParameters, PVCoordinatesProvider, BodyShape, TimeScale) - Constructor for class org.orekit.models.earth.atmosphere.DTM2000
Simple constructor for independent computation.
DTM2000InputParameters - Interface in org.orekit.models.earth.atmosphere
Container for solar activity data, compatible with DTM2000 Atmosphere model.
durationFrom(AbsoluteDate) - Method in class org.orekit.time.AbsoluteDate
Compute the physically elapsed duration between two instants.
durationFrom(FieldAbsoluteDate<T>) - Method in class org.orekit.time.FieldAbsoluteDate
Compute the physically elapsed duration between two instants.
durationFrom(AbsoluteDate) - Method in class org.orekit.time.FieldAbsoluteDate
Compute the physically elapsed duration between two instants.
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.
e0sq - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator
original eccentricity squared.
E_X - Static variable in enum org.orekit.orbits.OrbitType
Name for eccentricity vector first component.
E_Y - Static variable in enum org.orekit.orbits.OrbitType
Name for eccentricity vector second component.
EARTH - Static variable in class org.orekit.bodies.CelestialBodyFactory
Predefined name for Earth.
EARTH_ANGULAR_VELOCITY - Static variable in class org.orekit.estimation.measurements.EstimatedEarthFrameProvider
Earth Angular Velocity, in rad/s, from TIRF model.
EARTH_MOON - Static variable in class org.orekit.bodies.CelestialBodyFactory
Predefined name for Earth-Moon barycenter.
EARTH_MOON_BARYCENTER_SEMI_MAJOR_AXIS - Static variable in interface org.orekit.propagation.numerical.cr3bp.CR3BPConstants
Earth-Moon barycenter semi-major axis in meters.
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 - Static variable in enum org.orekit.orbits.OrbitType
Name for eccentricity.
ECC_ANOM - Static variable in enum org.orekit.orbits.OrbitType
Name for eccentric anomaly.
ECC_LAT_ARG - Static variable in enum org.orekit.orbits.OrbitType
Name for eccentric argument of latitude.
ECC_LON_ARG - Static variable in enum org.orekit.orbits.OrbitType
Name for eccentric argument of longitude.
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.BeidouPropagator.Builder
Sets the Earth Centered Earth Fixed frame.
ecef(Frame) - Method in class org.orekit.propagation.analytical.gnss.GalileoPropagator.Builder
Sets the Earth Centered Earth Fixed frame.
ecef(Frame) - Method in class org.orekit.propagation.analytical.gnss.GLONASSAnalyticalPropagator.Builder
Sets the Earth Centered Earth Fixed frame assimilated to the WGS84 ECEF.
ecef(Frame) - Method in class org.orekit.propagation.analytical.gnss.GPSPropagator.Builder
Sets the Earth Centered Earth Fixed frame assimilated to the WGS84 ECEF.
ecef(Frame) - Method in class org.orekit.propagation.analytical.gnss.IRNSSPropagator.Builder
Sets the Earth Centered Earth Fixed frame assimilated to the WGS84 ECEF.
ecef(Frame) - Method in class org.orekit.propagation.analytical.gnss.QZSSPropagator.Builder
Sets the Earth Centered Earth Fixed frame assimilated to the WGS84 ECEF.
ecef(Frame) - Method in class org.orekit.propagation.analytical.gnss.SBASPropagator.Builder
Sets the Earth Centered Earth Fixed frame assimilated to the WGS84 ECEF.
eci(Frame) - Method in class org.orekit.propagation.analytical.gnss.BeidouPropagator.Builder
Sets the Earth Centered Inertial frame used for propagation.
eci(Frame) - Method in class org.orekit.propagation.analytical.gnss.GalileoPropagator.Builder
Sets the Earth Centered Inertial frame used for propagation.
eci(Frame) - Method in class org.orekit.propagation.analytical.gnss.GLONASSAnalyticalPropagator.Builder
Sets the Earth Centered Inertial frame used for propagation.
eci(Frame) - Method in class org.orekit.propagation.analytical.gnss.GPSPropagator.Builder
Sets the Earth Centered Inertial frame used for propagation.
eci(Frame) - Method in class org.orekit.propagation.analytical.gnss.IRNSSPropagator.Builder
Sets the Earth Centered Inertial frame used for propagation.
eci(Frame) - Method in class org.orekit.propagation.analytical.gnss.QZSSPropagator.Builder
Sets the Earth Centered Inertial frame used for propagation.
eci(Frame) - Method in class org.orekit.propagation.analytical.gnss.SBASPropagator.Builder
Sets the Earth Centered Inertial frame used for propagation.
eci(Frame) - Method in class org.orekit.propagation.numerical.GLONASSNumericalPropagator.Builder
Sets the Earth Centered Inertial frame used for propagation.
EcksteinHechlerPropagator - Class in org.orekit.propagation.analytical
This class propagates a SpacecraftState using the analytical Eckstein-Hechler model.
EcksteinHechlerPropagator(Orbit, UnnormalizedSphericalHarmonicsProvider) - Constructor for class org.orekit.propagation.analytical.EcksteinHechlerPropagator
Build a propagator from orbit and potential provider.
EcksteinHechlerPropagator(Orbit, AttitudeProvider, double, UnnormalizedSphericalHarmonicsProvider, UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics) - Constructor for class org.orekit.propagation.analytical.EcksteinHechlerPropagator
Private helper constructor.
EcksteinHechlerPropagator(Orbit, double, double, double, double, double, double, double) - Constructor for class org.orekit.propagation.analytical.EcksteinHechlerPropagator
Build a propagator from orbit and potential.
EcksteinHechlerPropagator(Orbit, double, UnnormalizedSphericalHarmonicsProvider) - Constructor for class org.orekit.propagation.analytical.EcksteinHechlerPropagator
Build a propagator from orbit, mass and potential provider.
EcksteinHechlerPropagator(Orbit, double, double, double, double, double, double, double, double) - Constructor for class org.orekit.propagation.analytical.EcksteinHechlerPropagator
Build a propagator from orbit, mass and potential.
EcksteinHechlerPropagator(Orbit, AttitudeProvider, UnnormalizedSphericalHarmonicsProvider) - Constructor for class org.orekit.propagation.analytical.EcksteinHechlerPropagator
Build a propagator from orbit, attitude provider and potential provider.
EcksteinHechlerPropagator(Orbit, AttitudeProvider, double, double, double, double, double, double, double) - Constructor for class org.orekit.propagation.analytical.EcksteinHechlerPropagator
Build a propagator from orbit, attitude provider and potential.
EcksteinHechlerPropagator(Orbit, AttitudeProvider, double, UnnormalizedSphericalHarmonicsProvider) - Constructor for class org.orekit.propagation.analytical.EcksteinHechlerPropagator
Build a propagator from orbit, attitude provider, mass and potential provider.
EcksteinHechlerPropagator(Orbit, AttitudeProvider, double, double, double, double, double, double, double, double) - Constructor for class org.orekit.propagation.analytical.EcksteinHechlerPropagator
Build a propagator from orbit, attitude provider, mass and potential.
EcksteinHechlerPropagator(Orbit, UnnormalizedSphericalHarmonicsProvider, PropagationType) - Constructor for class org.orekit.propagation.analytical.EcksteinHechlerPropagator
Build a propagator from orbit and potential provider.
EcksteinHechlerPropagator(Orbit, AttitudeProvider, double, UnnormalizedSphericalHarmonicsProvider, PropagationType) - 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, PropagationType) - Constructor for class org.orekit.propagation.analytical.EcksteinHechlerPropagator
Private helper constructor.
EcksteinHechlerPropagator(Orbit, AttitudeProvider, double, double, double, double, double, double, double, double, PropagationType) - Constructor for class org.orekit.propagation.analytical.EcksteinHechlerPropagator
Build a propagator from orbit, attitude provider, mass and potential.
EcksteinHechlerPropagatorBuilder - Class in org.orekit.propagation.conversion
Builder for Eckstein-Hechler propagator.
EcksteinHechlerPropagatorBuilder(Orbit, UnnormalizedSphericalHarmonicsProvider, PositionAngle, double) - Constructor for class org.orekit.propagation.conversion.EcksteinHechlerPropagatorBuilder
Build a new instance.
EcksteinHechlerPropagatorBuilder(Orbit, UnnormalizedSphericalHarmonicsProvider, PositionAngle, double, AttitudeProvider) - Constructor for class org.orekit.propagation.conversion.EcksteinHechlerPropagatorBuilder
Build a new instance.
EcksteinHechlerPropagatorBuilder(Orbit, double, double, TideSystem, double, double, double, double, double, OrbitType, PositionAngle, double) - Constructor for class org.orekit.propagation.conversion.EcksteinHechlerPropagatorBuilder
Build a new instance.
EclipseDetector - Class in org.orekit.propagation.events
Finder for satellite eclipse related events.
EclipseDetector(PVCoordinatesProvider, double, OneAxisEllipsoid) - Constructor for class org.orekit.propagation.events.EclipseDetector
Build a new eclipse detector.
EclipticProvider - Class in org.orekit.frames
An inertial frame aligned with the ecliptic.
EclipticProvider(IERSConventions) - Constructor for class org.orekit.frames.EclipticProvider
Create a transform provider from MOD to an ecliptically aligned frame.
EclipticProvider(IERSConventions, TimeScales) - Constructor for class org.orekit.frames.EclipticProvider
Create a transform provider from MOD to an ecliptically aligned frame.
ECOM2 - Class in org.orekit.forces.radiation
The Empirical CODE Orbit Model 2 (ECOM2) of the Center for Orbit Determination in Europe (CODE).
ECOM2(int, int, double, ExtendedPVCoordinatesProvider, double) - Constructor for class org.orekit.forces.radiation.ECOM2
Constructor.
ECOM_COEFFICIENT - Static variable in class org.orekit.forces.radiation.ECOM2
Parameter name for ECOM model coefficients enabling Jacobian processing.
eeta - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator
original eccentricity * eta.
EGM96_EARTH_C20 - Static variable in interface org.orekit.utils.Constants
Earth un-normalized second zonal coefficient from EGM96 model: -1.08262668355315e-3.
EGM96_EARTH_C30 - Static variable in interface org.orekit.utils.Constants
Earth un-normalized third zonal coefficient from EGM96 model: 2.53265648533224e-6.
EGM96_EARTH_C40 - Static variable in interface org.orekit.utils.Constants
Earth un-normalized fourth zonal coefficient from EGM96 model: 1.619621591367e-6.
EGM96_EARTH_C50 - Static variable in interface org.orekit.utils.Constants
Earth un-normalized fifth zonal coefficient from EGM96 model: 2.27296082868698e-7.
EGM96_EARTH_C60 - Static variable in interface org.orekit.utils.Constants
Earth un-normalized sixth zonal coefficient from EGM96 model: -5.40681239107085e-7.
EGM96_EARTH_EQUATORIAL_RADIUS - Static variable in interface org.orekit.utils.Constants
Earth equatorial radius from EGM96 model: 6378136.3 m.
EGM96_EARTH_MU - Static variable in interface org.orekit.utils.Constants
Earth gravitational constant from EGM96 model: 3.986004415e14 m³/s².
EGM_FILENAME - Static variable in class org.orekit.forces.gravity.potential.GravityFieldFactory
Default regular expression for EGM files.
EGMFormatReader - Class in org.orekit.forces.gravity.potential
This reader is adapted to the EGM Format.
EGMFormatReader(String, boolean) - Constructor for class org.orekit.forces.gravity.potential.EGMFormatReader
Simple constructor.
EGMFormatReader(String, boolean, boolean) - Constructor for class org.orekit.forces.gravity.potential.EGMFormatReader
Simple constructor that allows overriding 'standard' EGM96 ae and mu with WGS84 variants.
EIGEN5C_EARTH_C20 - Static variable in interface org.orekit.utils.Constants
Earth un-normalized second zonal coefficient from EIGEN5C model: -1.082626457231767e-3.
EIGEN5C_EARTH_C30 - Static variable in interface org.orekit.utils.Constants
Earth un-normalized third zonal coefficient from EIGEN5C model: 2.532547231862799e-6.
EIGEN5C_EARTH_C40 - Static variable in interface org.orekit.utils.Constants
Earth un-normalized fourth zonal coefficient from EIGEN5C model: 1.619964434136e-6.
EIGEN5C_EARTH_C50 - Static variable in interface org.orekit.utils.Constants
Earth un-normalized fifth zonal coefficient from EIGEN5C model: 2.277928487005437e-7.
EIGEN5C_EARTH_C60 - Static variable in interface org.orekit.utils.Constants
Earth un-normalized sixth zonal coefficient from EIGEN5C model: -5.406653715879098e-7.
EIGEN5C_EARTH_EQUATORIAL_RADIUS - Static variable in interface org.orekit.utils.Constants
Earth equatorial radius from EIGEN5C model: 6378136.46 m.
EIGEN5C_EARTH_MU - Static variable in interface org.orekit.utils.Constants
Earth gravitational constant from EIGEN5C model: 3.986004415e14 m³/s².
ElevationDetector - Class in org.orekit.propagation.events
Finder for satellite raising/setting events that allows for the setting of azimuth and/or elevation bounds or a ground azimuth/elevation mask input.
ElevationDetector(TopocentricFrame) - Constructor for class org.orekit.propagation.events.ElevationDetector
Creates an instance of Elevation detector based on passed in topocentric frame and the minimum elevation angle.
ElevationDetector(double, double, TopocentricFrame) - Constructor for class org.orekit.propagation.events.ElevationDetector
Creates an instance of Elevation detector based on passed in topocentric frame and overrides of default maximal checking interval and convergence threshold values.
ElevationExtremumDetector - Class in org.orekit.propagation.events
Detector for elevation extremum with respect to a ground point.
ElevationExtremumDetector(TopocentricFrame) - Constructor for class org.orekit.propagation.events.ElevationExtremumDetector
Build a new detector.
ElevationExtremumDetector(double, double, TopocentricFrame) - Constructor for class org.orekit.propagation.events.ElevationExtremumDetector
Build a detector.
ElevationFilter<T extends ObservedMeasurement<T>> - Class in org.orekit.estimation.measurements.filtering
Elevation pre-processing filter.
ElevationFilter(GroundStation, double) - Constructor for class org.orekit.estimation.measurements.filtering.ElevationFilter
Constructor.
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.
EllipticalFieldOfView - Class in org.orekit.geometry.fov
Class representing a spacecraft sensor Field Of View with elliptical shape.
EllipticalFieldOfView(Vector3D, Vector3D, double, double, double) - Constructor for class org.orekit.geometry.fov.EllipticalFieldOfView
Build a new instance.
ellipticEccentricToMean(T, T) - Static method in class org.orekit.orbits.FieldKeplerianOrbit
Computes the mean anomaly from the elliptic eccentric anomaly.
ellipticEccentricToMean(double, double) - Static method in class org.orekit.orbits.KeplerianOrbit
Computes the mean anomaly from the elliptic eccentric anomaly.
ellipticEccentricToTrue(T, T) - Static method in class org.orekit.orbits.FieldKeplerianOrbit
Computes the true anomaly from the elliptic eccentric anomaly.
ellipticEccentricToTrue(double, double) - Static method in class org.orekit.orbits.KeplerianOrbit
Computes the true anomaly from the elliptic eccentric anomaly.
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, ITRFVersion) - Constructor for class org.orekit.frames.EOPEntry
EOPEntry(int, double, double, double, double, double, double, double, double, ITRFVersion, AbsoluteDate) - 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<? extends EOPEntry>, boolean) - Constructor for class org.orekit.frames.EOPHistory
Simple constructor.
EOPHistory(IERSConventions, Collection<? extends EOPEntry>, boolean, TimeScales) - Constructor for class org.orekit.frames.EOPHistory
Simple constructor.
EOPHistoryLoader - Interface in org.orekit.frames
Interface for loading Earth Orientation Parameters history.
EOPHistoryLoader.Parser - Interface in org.orekit.frames
Interface for parsing EOP data files.
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(List<SpacecraftState>, int, double, AttitudeProvider) - Constructor for class org.orekit.propagation.analytical.Ephemeris
Constructor with tabulated states.
EPHEMERIS_GENERATION_MODE - Static variable in interface org.orekit.propagation.FieldPropagator
Indicator for ephemeris generation mode.
EPHEMERIS_GENERATION_MODE - Static variable in interface org.orekit.propagation.Propagator
Indicator for ephemeris generation mode.
EphemerisFile - Interface in org.orekit.files.general
An interface for accessing the data stored in an ephemeris file and using the data to create a working Propagator.
EphemerisFile.EphemerisSegment - Interface in org.orekit.files.general
A segment of an ephemeris for a satellite.
EphemerisFile.SatelliteEphemeris - Interface in org.orekit.files.general
Contains the information about a single satellite from an EphemerisFile.
EphemerisFileParser - Interface in org.orekit.files.general
Parse an ephemeris file.
EphemerisFileWriter - Interface in org.orekit.files.general
An interface for writing out ephemeris files to disk.
EpochDerivativesEquations - Class in org.orekit.propagation.numerical
This class is a copy of AbsolutePartialDerivativesEquations The computation of the derivatives of the acceleration due to a ThirdBodyAttraction has been added.
EpochDerivativesEquations(String, NumericalPropagator) - Constructor for class org.orekit.propagation.numerical.EpochDerivativesEquations
Simple constructor.
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.estimation.measurements.gnss.IntegerLeastSquareSolution
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 represents 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 represents the same time as another instance.
equals(Object) - Method in class org.orekit.time.TimeComponents
EquinoctialOrbit - Class in org.orekit.orbits
This class handles equinoctial orbital parameters, which can support both circular and equatorial orbits.
EquinoctialOrbit(double, double, double, double, double, double, PositionAngle, Frame, AbsoluteDate, double) - Constructor for class org.orekit.orbits.EquinoctialOrbit
Creates a new instance.
EquinoctialOrbit(double, double, double, double, double, double, double, double, double, double, double, double, PositionAngle, Frame, AbsoluteDate, double) - Constructor for class org.orekit.orbits.EquinoctialOrbit
Creates a new instance.
EquinoctialOrbit(TimeStampedPVCoordinates, Frame, double) - Constructor for class org.orekit.orbits.EquinoctialOrbit
Constructor from Cartesian parameters.
EquinoctialOrbit(PVCoordinates, Frame, AbsoluteDate, double) - Constructor for class org.orekit.orbits.EquinoctialOrbit
Constructor from Cartesian parameters.
EquinoctialOrbit(Orbit) - Constructor for class org.orekit.orbits.EquinoctialOrbit
Constructor from any kind of orbital parameters.
estimate(Frame, PV, PV, PV) - Method in class org.orekit.estimation.iod.IodGibbs
Give an initial orbit estimation, assuming Keplerian motion.
estimate(Frame, Vector3D, AbsoluteDate, Vector3D, AbsoluteDate, Vector3D, AbsoluteDate) - Method in class org.orekit.estimation.iod.IodGibbs
Give an initial orbit estimation, assuming Keplerian motion.
estimate(Vector3D, Vector3D, Vector3D, Vector3D, AbsoluteDate, Vector3D, AbsoluteDate, Vector3D, AbsoluteDate, double, double, int, boolean) - Method in class org.orekit.estimation.iod.IodGooding
Orbit got from Observed Three Lines of Sight (angles only).
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, PVCoordinates, AbsoluteDate, Vector3D, AbsoluteDate, Vector3D, AbsoluteDate, Vector3D) - Method in class org.orekit.estimation.iod.IodLaplace
Estimate orbit from three line of sight angles from the same location.
estimate() - Method in class org.orekit.estimation.leastsquares.BatchLSEstimator
Estimate the orbital, propagation and measurements parameters.
estimate(int, int, SpacecraftState[]) - Method in class org.orekit.estimation.measurements.AbstractMeasurement
Estimate the theoretical value of the measurement.
estimate(int, int, SpacecraftState[]) - Method in interface org.orekit.estimation.measurements.ObservedMeasurement
Estimate the theoretical value of the measurement.
EstimatedEarthFrameProvider - Class in org.orekit.estimation.measurements
Class modeling an Earth frame whose Earth Orientation Parameters can be estimated.
EstimatedEarthFrameProvider(UT1Scale) - Constructor for class org.orekit.estimation.measurements.EstimatedEarthFrameProvider
Build an estimated Earth frame.
EstimatedIonosphericModel - Class in org.orekit.models.earth.ionosphere
An estimated ionospheric model.
EstimatedIonosphericModel(IonosphericMappingFunction, double) - Constructor for class org.orekit.models.earth.ionosphere.EstimatedIonosphericModel
Build a new instance.
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.troposphere
An estimated tropospheric model.
EstimatedTroposphericModel(double, double, MappingFunction, double) - Constructor for class org.orekit.models.earth.troposphere.EstimatedTroposphericModel
Build a new instance using the given environmental conditions.
EstimatedTroposphericModel(MappingFunction, double) - Constructor for class org.orekit.models.earth.troposphere.EstimatedTroposphericModel
Build a new instance using a standard atmosphere model.
estimateRate(Rotation, Rotation, double) - Static method in class org.orekit.utils.AngularCoordinates
Estimate rotation rate between two orientations.
estimateRate(FieldRotation<T>, FieldRotation<T>, double) - Static method in class org.orekit.utils.FieldAngularCoordinates
Estimate rotation rate between two orientations.
estimateRate(FieldRotation<T>, FieldRotation<T>, T) - Static method in class org.orekit.utils.FieldAngularCoordinates
Estimate rotation rate between two orientations.
estimateVelocity(FieldVector3D<T>, FieldVector3D<T>, double) - Static method in class org.orekit.utils.FieldPVCoordinates
Estimate velocity between two positions.
estimateVelocity(Vector3D, Vector3D, double) - Static method in class org.orekit.utils.PVCoordinates
Estimate velocity between two positions.
EstimationModifier<T extends ObservedMeasurement<T>> - Interface in org.orekit.estimation.measurements
Interface for estimated measurements modifiers used for orbit determination.
EstimationsProvider - Interface in org.orekit.estimation.measurements
Interface for retrieving estimated measurements during orbit determination.
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(OrekitStepInterpolator) - Method in class org.orekit.propagation.events.EventState
Evaluate the impact of the proposed step on the event detector.
evaluateStep(FieldOrekitStepInterpolator<T>) - Method in class org.orekit.propagation.events.FieldEventState
Evaluate the impact of the proposed step on the event detector.
evaluateTC(AbsoluteDate) - Method in enum org.orekit.utils.IERSConventions
Evaluate the date offset between the current date and the reference date.
evaluateTC(AbsoluteDate, TimeScales) - 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.
evaluateTC(FieldAbsoluteDate<T>, TimeScales) - 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.
EventBasedManeuverTriggers - Class in org.orekit.forces.maneuvers.trigger
Maneuver triggers based on start and stop detectors.
EventBasedManeuverTriggers(AbstractDetector<? extends EventDetector>, AbstractDetector<? extends EventDetector>) - Constructor for class org.orekit.forces.maneuvers.trigger.EventBasedManeuverTriggers
Constructor.
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.
eventIsEnabled(SpacecraftState, S, double) - Method in interface org.orekit.propagation.events.EnablingPredicate
Compute an event enabling function of state.
eventOccurred(SpacecraftState, EventDetector, boolean) - Method in class org.orekit.forces.maneuvers.trigger.EventBasedManeuverTriggers
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, 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(FieldSpacecraftState<T>, boolean) - Method in class org.orekit.propagation.events.FieldAbstractDetector
Handle the event.
eventOccurred(FieldSpacecraftState<T>, boolean) - Method in interface org.orekit.propagation.events.FieldEventDetector
Handle the event.
eventOccurred(SpacecraftState, T, boolean) - Method in class org.orekit.propagation.events.handlers.ContinueOnEvent
Specific implementation of the eventOccurred interface.
eventOccurred(SpacecraftState, T, boolean) - Method in interface org.orekit.propagation.events.handlers.EventHandler
eventOccurred method mirrors the same interface method as in EventDetector and its subclasses, but with an additional parameter that allows the calling method to pass in an object from the detector which would have potential additional data to allow the implementing class to determine the correct return state.
eventOccurred(FieldSpacecraftState<T>, KK, boolean) - Method in class org.orekit.propagation.events.handlers.FieldContinueOnEvent
Specific implementation of the eventOccurred interface.
eventOccurred(FieldSpacecraftState<T>, KK, boolean) - Method in interface org.orekit.propagation.events.handlers.FieldEventHandler
eventOccurred method mirrors the same interface method as in EventDetector and its subclasses, but with an additional parameter that allows the calling method to pass in an object from the detector which would have potential additional data to allow the implementing class to determine the correct return state.
eventOccurred(FieldSpacecraftState<E>, T, boolean) - Method in class org.orekit.propagation.events.handlers.FieldRecordAndContinue
 
eventOccurred(FieldSpacecraftState<T>, KK, boolean) - Method in class org.orekit.propagation.events.handlers.FieldStopOnDecreasing
Handle a detection event and choose what to do next.
eventOccurred(FieldSpacecraftState<T>, KK, boolean) - Method in class org.orekit.propagation.events.handlers.FieldStopOnEvent
Specific implementation of the eventOccurred interface.
eventOccurred(FieldSpacecraftState<T>, KK, boolean) - Method in class org.orekit.propagation.events.handlers.FieldStopOnIncreasing
Handle a detection event and choose what to do next.
eventOccurred(SpacecraftState, T, boolean) - Method in class org.orekit.propagation.events.handlers.RecordAndContinue
 
eventOccurred(SpacecraftState, T, boolean) - Method in class org.orekit.propagation.events.handlers.StopOnDecreasing
Handle a detection event and choose what to do next.
eventOccurred(SpacecraftState, T, boolean) - Method in class org.orekit.propagation.events.handlers.StopOnEvent
Specific implementation of the eventOccurred interface.
eventOccurred(SpacecraftState, T, boolean) - Method in class org.orekit.propagation.events.handlers.StopOnIncreasing
Handle a detection event and choose what to do next.
EventShifter<T extends EventDetector> - Class in org.orekit.propagation.events
Wrapper shifting events occurrences times.
EventShifter(T, boolean, double, double) - Constructor for class org.orekit.propagation.events.EventShifter
Build a new instance.
EventsLogger - Class in org.orekit.propagation.events
This class logs events detectors events during propagation.
EventsLogger() - Constructor for class org.orekit.propagation.events.EventsLogger
Simple constructor.
EventsLogger.LoggedEvent - Class in org.orekit.propagation.events
Class for logged events entries.
EventSlopeFilter<T extends EventDetector> - Class in org.orekit.propagation.events
Wrapper used to detect only increasing or decreasing events.
EventSlopeFilter(T, FilterType) - Constructor for class org.orekit.propagation.events.EventSlopeFilter
EventState<T extends EventDetector> - Class in org.orekit.propagation.events
This class handles the state for one event detector during integration steps.
EventState(T) - Constructor for class org.orekit.propagation.events.EventState
Simple constructor.
EventState.EventOccurrence - Class in org.orekit.propagation.events
Class to hold the data related to an event occurrence that is needed to decide how to modify integration.
ExceptionalDataContext - Class in org.orekit.data
A data context that always throws a runtime exception when it's methods are used.
ExceptionalDataContext() - Constructor for class org.orekit.data.ExceptionalDataContext
 
extend(DerivativeStructure, DSFactory) - Method in class org.orekit.propagation.integration.AbstractDSConverter
Add zero derivatives.
extend(FieldVector3D<DerivativeStructure>, DSFactory) - Method in class org.orekit.propagation.integration.AbstractDSConverter
Add zero derivatives.
extend(FieldRotation<DerivativeStructure>, DSFactory) - Method in class org.orekit.propagation.integration.AbstractDSConverter
Add zero derivatives.
extend(Gradient, int) - Method in class org.orekit.propagation.integration.AbstractGradientConverter
Add zero derivatives.
extend(FieldVector3D<Gradient>, int) - Method in class org.orekit.propagation.integration.AbstractGradientConverter
Add zero derivatives.
extend(FieldRotation<Gradient>, int) - Method in class org.orekit.propagation.integration.AbstractGradientConverter
Add zero derivatives.
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.
extractDragSensitiveRange(AbsoluteDate, AbsoluteDate) - Method in class org.orekit.forces.drag.TimeSpanDragForce
Extract a range of the DragSensitive map.
extractParameters(double[], AbsoluteDate) - Method in class org.orekit.forces.drag.TimeSpanDragForce
Extract the proper parameter drivers' values from the array in input of the acceleration method.
extractParameters(T[], FieldAbsoluteDate<T>) - Method in class org.orekit.forces.drag.TimeSpanDragForce
Extract the proper parameter drivers' values from the array in input of the acceleration method.
extractParameters(double[], AbsoluteDate) - Method in class org.orekit.models.earth.troposphere.TimeSpanEstimatedTroposphericModel
Extract the proper parameter drivers' values from the array in input of the pathDelay method.
extractParameters(T[], FieldAbsoluteDate<T>) - Method in class org.orekit.models.earth.troposphere.TimeSpanEstimatedTroposphericModel
Extract the proper parameter drivers' values from the array in input of the pathDelay method.
extractRange(AbsoluteDate, AbsoluteDate) - Method in class org.orekit.utils.TimeSpanMap
Extract a range of the map.

F

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 Frames.
FactoryManagedFrame(Frame, TransformProvider, boolean, Predefined) - Constructor for class org.orekit.frames.FactoryManagedFrame
Simple constructor.
feed(Pattern, DataLoader) - Method in class org.orekit.data.AbstractListCrawler
Deprecated.
feed(Pattern, DataLoader, DataProvidersManager) - Method in class org.orekit.data.AbstractListCrawler
Feed a data file loader by browsing the data collection.
feed(DataLoader) - Method in class org.orekit.data.AbstractSelfFeedingLoader
feed(Pattern, DataLoader) - Method in class org.orekit.data.ClasspathCrawler
Deprecated.
feed(Pattern, DataLoader, DataProvidersManager) - 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
Deprecated.
Use DataProvider.feed(Pattern, DataLoader, DataProvidersManager) instead which allows specifying the DataProvidersManager to use for filtering resources. This method uses the default instance: DataProvidersManager.getInstance().
feed(Pattern, DataLoader, DataProvidersManager) - Method in interface org.orekit.data.DataProvider
Feed a data file loader by browsing the data collection.
feed(String, DataLoader) - Method in class org.orekit.data.DataProvidersManager
Feed a data file loader by browsing all data providers.
feed(Pattern, DataLoader) - Method in class org.orekit.data.DirectoryCrawler
Deprecated.
feed(Pattern, DataLoader, DataProvidersManager) - 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.ZipJarCrawler
Deprecated.
feed(Pattern, DataLoader, DataProvidersManager) - 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.
fetchEvaluatedMeasurement(int, EstimatedMeasurement<?>) - Method in class org.orekit.estimation.leastsquares.BatchLSModel
Fetch a measurement that was evaluated during propagation.
fetchEvaluatedMeasurement(int, EstimatedMeasurement<?>) - Method in interface org.orekit.estimation.leastsquares.BatchLSODModel
Fetch a measurement that was evaluated during propagation.
fetchEvaluatedMeasurement(int, EstimatedMeasurement<?>) - Method in class org.orekit.estimation.leastsquares.DSSTBatchLSModel
Fetch a measurement that was evaluated during propagation.
FieldAbsoluteDate<T extends RealFieldElement<T>> - Class in org.orekit.time
This class represents a specific instant in time.
FieldAbsoluteDate(Field<T>, AbsoluteDate) - Constructor for class org.orekit.time.FieldAbsoluteDate
Build an instance from an AbsoluteDate.
FieldAbsoluteDate(Field<T>) - Constructor for class org.orekit.time.FieldAbsoluteDate
Create an instance with a default value (FieldAbsoluteDate.getJ2000Epoch(Field)).
FieldAbsoluteDate(FieldAbsoluteDate<T>, T) - Constructor for class org.orekit.time.FieldAbsoluteDate
Build an instance from an elapsed duration since to another instant.
FieldAbsoluteDate(Field<T>, String, TimeScale) - Constructor for class org.orekit.time.FieldAbsoluteDate
Build an instance from a location (parsed from a string) in a time scale.
FieldAbsoluteDate(Field<T>, DateTimeComponents, TimeScale) - Constructor for class org.orekit.time.FieldAbsoluteDate
Build an instance from a location in a time scale.
FieldAbsoluteDate(Field<T>, DateComponents, TimeComponents, TimeScale) - Constructor for class org.orekit.time.FieldAbsoluteDate
Build an instance from a location in a time scale.
FieldAbsoluteDate(Field<T>, int, int, int, int, int, double, TimeScale) - Constructor for class org.orekit.time.FieldAbsoluteDate
Build an instance from a location in a time scale.
FieldAbsoluteDate(Field<T>, int, Month, int, int, int, double, TimeScale) - Constructor for class org.orekit.time.FieldAbsoluteDate
Build an instance from a location in a time scale.
FieldAbsoluteDate(Field<T>, DateComponents, TimeScale) - Constructor for class org.orekit.time.FieldAbsoluteDate
Build an instance from a location in a time scale.
FieldAbsoluteDate(Field<T>, int, int, int, TimeScale) - Constructor for class org.orekit.time.FieldAbsoluteDate
Build an instance from a location in a time scale.
FieldAbsoluteDate(Field<T>, int, Month, int, TimeScale) - Constructor for class org.orekit.time.FieldAbsoluteDate
Build an instance from a location in a time scale.
FieldAbsoluteDate(Field<T>, Date, TimeScale) - Constructor for class org.orekit.time.FieldAbsoluteDate
Build an instance from a location in a time scale.
FieldAbsoluteDate(FieldAbsoluteDate<T>, double) - Constructor for class org.orekit.time.FieldAbsoluteDate
Build an instance from an elapsed duration since to another instant.
FieldAbsoluteDate(AbsoluteDate, T) - Constructor for class org.orekit.time.FieldAbsoluteDate
Build an instance from an elapsed duration since to another instant.
FieldAbsoluteDate(FieldAbsoluteDate<T>, double, TimeScale) - Constructor for class org.orekit.time.FieldAbsoluteDate
Build an instance from an apparent clock offset with respect to another instant in the perspective of a specific time scale.
FieldAbsolutePVCoordinates<T extends RealFieldElement<T>> - Class in org.orekit.utils
Field implementation of AbsolutePVCoordinates.
FieldAbsolutePVCoordinates(Frame, FieldAbsoluteDate<T>, FieldVector3D<T>, FieldVector3D<T>, FieldVector3D<T>) - Constructor for class org.orekit.utils.FieldAbsolutePVCoordinates
Build from position, velocity, acceleration.
FieldAbsolutePVCoordinates(Frame, FieldAbsoluteDate<T>, FieldVector3D<T>, FieldVector3D<T>) - Constructor for class org.orekit.utils.FieldAbsolutePVCoordinates
Build from position and velocity.
FieldAbsolutePVCoordinates(Frame, FieldAbsoluteDate<T>, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.FieldAbsolutePVCoordinates
Build from frame, date and FieldPVA coordinates.
FieldAbsolutePVCoordinates(Frame, TimeStampedFieldPVCoordinates<T>) - Constructor for class org.orekit.utils.FieldAbsolutePVCoordinates
Build from frame and TimeStampedFieldPVCoordinates.
FieldAbsolutePVCoordinates(FieldAbsoluteDate<T>, T, FieldAbsolutePVCoordinates<T>) - Constructor for class org.orekit.utils.FieldAbsolutePVCoordinates
Multiplicative constructor
FieldAbsolutePVCoordinates(FieldAbsoluteDate<T>, FieldAbsolutePVCoordinates<T>, FieldAbsolutePVCoordinates<T>) - Constructor for class org.orekit.utils.FieldAbsolutePVCoordinates
Subtractive constructor
FieldAbsolutePVCoordinates(FieldAbsoluteDate<T>, T, FieldAbsolutePVCoordinates<T>, T, FieldAbsolutePVCoordinates<T>) - Constructor for class org.orekit.utils.FieldAbsolutePVCoordinates
Linear constructor
FieldAbsolutePVCoordinates(FieldAbsoluteDate<T>, T, FieldAbsolutePVCoordinates<T>, T, FieldAbsolutePVCoordinates<T>, T, FieldAbsolutePVCoordinates<T>) - Constructor for class org.orekit.utils.FieldAbsolutePVCoordinates
Linear constructor
FieldAbsolutePVCoordinates(FieldAbsoluteDate<T>, T, FieldAbsolutePVCoordinates<T>, T, FieldAbsolutePVCoordinates<T>, T, FieldAbsolutePVCoordinates<T>, T, FieldAbsolutePVCoordinates<T>) - Constructor for class org.orekit.utils.FieldAbsolutePVCoordinates
Linear constructor
FieldAbsolutePVCoordinates(Frame, FieldAbsoluteDate<T>, FieldVector3D<FieldDerivativeStructure<T>>) - Constructor for class org.orekit.utils.FieldAbsolutePVCoordinates
Builds a FieldAbsolutePVCoordinates triplet from a FieldVector3D<DerivativeStructure>.
FieldAbstractAnalyticalPropagator<T extends RealFieldElement<T>> - Class in org.orekit.propagation.analytical
Common handling of FieldPropagator methods for analytical propagators.
FieldAbstractAnalyticalPropagator(Field<T>, AttitudeProvider) - Constructor for class org.orekit.propagation.analytical.FieldAbstractAnalyticalPropagator
Build a new instance.
FieldAbstractDetector<D extends FieldEventDetector<T>,T extends RealFieldElement<T>> - Class in org.orekit.propagation.events
Common parts shared by several orbital events finders.
FieldAbstractDetector(T, T, int, FieldEventHandler<? super D, T>) - Constructor for class org.orekit.propagation.events.FieldAbstractDetector
Build a new instance.
FieldAbstractIntegratedPropagator<T extends RealFieldElement<T>> - Class in org.orekit.propagation.integration
Common handling of FieldPropagator methods for both numerical and semi-analytical propagators.
FieldAbstractIntegratedPropagator(Field<T>, FieldODEIntegrator<T>, PropagationType) - Constructor for class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator
Build a new instance.
FieldAbstractIntegratedPropagator.MainStateEquations<T extends RealFieldElement<T>> - Interface in org.orekit.propagation.integration
Differential equations for the main state (orbit, attitude and mass).
FieldAbstractPropagator<T extends RealFieldElement<T>> - Class in org.orekit.propagation
Common handling of Propagator methods for analytical propagators.
FieldAbstractPropagator(Field<T>) - Constructor for class org.orekit.propagation.FieldAbstractPropagator
Build a new instance.
FieldAdditionalEquations<T extends RealFieldElement<T>> - Interface in org.orekit.propagation.integration
This interface allows users to add their own differential equations to a numerical propagator.
FieldAdditionalStateProvider<T extends RealFieldElement<T>> - Interface in org.orekit.propagation
This interface represents providers for additional state data beyond SpacecraftState.
FieldAltitudeDetector<T extends RealFieldElement<T>> - Class in org.orekit.propagation.events
Finder for satellite altitude crossing events.
FieldAltitudeDetector(T, BodyShape) - Constructor for class org.orekit.propagation.events.FieldAltitudeDetector
Build a new altitude detector.
FieldAltitudeDetector(T, T, BodyShape) - Constructor for class org.orekit.propagation.events.FieldAltitudeDetector
Build a new altitude detector.
FieldAltitudeDetector(T, T, T, BodyShape) - Constructor for class org.orekit.propagation.events.FieldAltitudeDetector
Build a new altitude detector.
FieldAngularCoordinates<T extends RealFieldElement<T>> - Class in org.orekit.utils
Simple container for rotation / rotation rate pairs, using RealFieldElement.
FieldAngularCoordinates(FieldRotation<T>, FieldVector3D<T>) - Constructor for class org.orekit.utils.FieldAngularCoordinates
Builds a rotation/rotation rate pair.
FieldAngularCoordinates(FieldRotation<T>, FieldVector3D<T>, FieldVector3D<T>) - Constructor for class org.orekit.utils.FieldAngularCoordinates
Builds a rotation / rotation rate / rotation acceleration triplet.
FieldAngularCoordinates(FieldPVCoordinates<T>, FieldPVCoordinates<T>, FieldPVCoordinates<T>, FieldPVCoordinates<T>, double) - Constructor for class org.orekit.utils.FieldAngularCoordinates
Build the rotation that transforms a pair of pv coordinates into another one.
FieldAngularCoordinates(Field<T>, AngularCoordinates) - Constructor for class org.orekit.utils.FieldAngularCoordinates
Builds a FieldAngularCoordinates from a field and a regular AngularCoordinates.
FieldAngularCoordinates(FieldRotation<FieldDerivativeStructure<T>>) - Constructor for class org.orekit.utils.FieldAngularCoordinates
Builds a FieldAngularCoordinates from a FieldRotation<FieldDerivativeStructure>.
FieldApsideDetector<T extends RealFieldElement<T>> - Class in org.orekit.propagation.events
Finder for apside crossing events.
FieldApsideDetector(FieldOrbit<T>) - Constructor for class org.orekit.propagation.events.FieldApsideDetector
Build a new instance.
FieldApsideDetector(T, FieldOrbit<T>) - Constructor for class org.orekit.propagation.events.FieldApsideDetector
Build a new instance.
FieldAttitude<T extends RealFieldElement<T>> - Class in org.orekit.attitudes
This class handles attitude definition at a given date.
FieldAttitude(Frame, TimeStampedFieldAngularCoordinates<T>) - Constructor for class org.orekit.attitudes.FieldAttitude
Creates a new instance.
FieldAttitude(FieldAbsoluteDate<T>, Frame, FieldAngularCoordinates<T>) - Constructor for class org.orekit.attitudes.FieldAttitude
Creates a new instance.
FieldAttitude(FieldAbsoluteDate<T>, Frame, FieldRotation<T>, FieldVector3D<T>, FieldVector3D<T>) - Constructor for class org.orekit.attitudes.FieldAttitude
Creates a new instance.
FieldAttitude(FieldAbsoluteDate<T>, Frame, Rotation, Vector3D, Vector3D, Field<T>) - Constructor for class org.orekit.attitudes.FieldAttitude
Creates a new instance.
FieldAttitude(Field<T>, Attitude) - Constructor for class org.orekit.attitudes.FieldAttitude
Builds an instance for a regular Attitude.
FieldAuxiliaryElements<T extends RealFieldElement<T>> - Class in org.orekit.propagation.semianalytical.dsst.utilities
Container class for common parameters used by all DSST forces.
FieldAuxiliaryElements(FieldOrbit<T>, int) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.FieldAuxiliaryElements
Simple constructor.
FieldBodiesElements<T extends RealFieldElement<T>> - Class in org.orekit.data
Elements of the bodies having an effect on nutation.
FieldBodiesElements(FieldAbsoluteDate<T>, T, T, T, T, T, T, T, T, T, T, T, T, T, T, T, T, T, T, T, T, T, T, T, T, T, T, T, T, T, T, T) - Constructor for class org.orekit.data.FieldBodiesElements
Simple constructor.
FieldBoundedPropagator<T extends RealFieldElement<T>> - Interface in org.orekit.propagation
This interface is intended for ephemerides valid only during a time range.
FieldCartesianOrbit<T extends RealFieldElement<T>> - Class in org.orekit.orbits
This class holds Cartesian orbital parameters.
FieldCartesianOrbit(TimeStampedFieldPVCoordinates<T>, Frame, T) - Constructor for class org.orekit.orbits.FieldCartesianOrbit
Constructor from Cartesian parameters.
FieldCartesianOrbit(FieldPVCoordinates<T>, Frame, FieldAbsoluteDate<T>, T) - Constructor for class org.orekit.orbits.FieldCartesianOrbit
Constructor from Cartesian parameters.
FieldCartesianOrbit(FieldOrbit<T>) - Constructor for class org.orekit.orbits.FieldCartesianOrbit
Constructor from any kind of orbital parameters.
FieldCircularOrbit<T extends RealFieldElement<T>> - Class in org.orekit.orbits
This class handles circular orbital parameters.
FieldCircularOrbit(T, T, T, T, T, T, PositionAngle, Frame, FieldAbsoluteDate<T>, T) - 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>, T) - Constructor for class org.orekit.orbits.FieldCircularOrbit
Creates a new instance.
FieldCircularOrbit(TimeStampedFieldPVCoordinates<T>, Frame, T) - Constructor for class org.orekit.orbits.FieldCircularOrbit
Constructor from Cartesian parameters.
FieldCircularOrbit(FieldPVCoordinates<T>, Frame, FieldAbsoluteDate<T>, T) - Constructor for class org.orekit.orbits.FieldCircularOrbit
Constructor from Cartesian parameters.
FieldCircularOrbit(FieldOrbit<T>) - Constructor for class org.orekit.orbits.FieldCircularOrbit
Constructor from any kind of orbital parameters.
FieldCjSjCoefficient<T extends RealFieldElement<T>> - 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.
FieldCjSjCoefficient(T, T, Field<T>) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.FieldCjSjCoefficient
Cj(k, h) and Sj(k, h) constructor.
FieldContinueOnEvent<KK extends FieldEventDetector<T>,T extends RealFieldElement<T>> - Class in org.orekit.propagation.events.handlers
Event handler which will always return continue as a state.
FieldContinueOnEvent() - Constructor for class org.orekit.propagation.events.handlers.FieldContinueOnEvent
 
FieldDateDetector<T extends RealFieldElement<T>> - Class in org.orekit.propagation.events
Finder for date events.
FieldDateDetector(T, T, FieldTimeStamped<T>...) - Constructor for class org.orekit.propagation.events.FieldDateDetector
Build a new instance.
FieldDateDetector(FieldAbsoluteDate<T>) - Constructor for class org.orekit.propagation.events.FieldDateDetector
Build a new instance.
FieldDelaunayArguments<T extends RealFieldElement<T>> - Class in org.orekit.data
Delaunay arguments used for nutation or tides.
FieldDelaunayArguments(FieldAbsoluteDate<T>, T, T, T, T, T, T, T, T, T, T, T, T, T) - Constructor for class org.orekit.data.FieldDelaunayArguments
Simple constructor.
FieldDSSTPropagator<T extends RealFieldElement<T>> - Class in org.orekit.propagation.semianalytical.dsst
This class propagates orbits using the DSST theory.
FieldDSSTPropagator(Field<T>, FieldODEIntegrator<T>, PropagationType) - Constructor for class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator
Create a new instance of DSSTPropagator.
FieldDSSTPropagator(Field<T>, FieldODEIntegrator<T>, PropagationType, AttitudeProvider) - Constructor for class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator
Create a new instance of DSSTPropagator.
FieldDSSTPropagator(Field<T>, FieldODEIntegrator<T>) - Constructor for class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator
Create a new instance of DSSTPropagator.
FieldDSSTPropagator(Field<T>, FieldODEIntegrator<T>, AttitudeProvider) - Constructor for class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator
Create a new instance of DSSTPropagator.
FieldEcksteinHechlerPropagator<T extends RealFieldElement<T>> - Class in org.orekit.propagation.analytical
This class propagates a FieldSpacecraftState using the analytical Eckstein-Hechler model.
FieldEcksteinHechlerPropagator(FieldOrbit<T>, UnnormalizedSphericalHarmonicsProvider) - Constructor for class org.orekit.propagation.analytical.FieldEcksteinHechlerPropagator
Build a propagator from FieldOrbit and potential provider.
FieldEcksteinHechlerPropagator(FieldOrbit<T>, AttitudeProvider, T, UnnormalizedSphericalHarmonicsProvider, UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics) - Constructor for class org.orekit.propagation.analytical.FieldEcksteinHechlerPropagator
Private helper constructor.
FieldEcksteinHechlerPropagator(FieldOrbit<T>, double, T, double, double, double, double, double) - Constructor for class org.orekit.propagation.analytical.FieldEcksteinHechlerPropagator
Build a propagator from FieldOrbit and potential.
FieldEcksteinHechlerPropagator(FieldOrbit<T>, T, UnnormalizedSphericalHarmonicsProvider) - Constructor for class org.orekit.propagation.analytical.FieldEcksteinHechlerPropagator
Build a propagator from FieldOrbit, mass and potential provider.
FieldEcksteinHechlerPropagator(FieldOrbit<T>, T, double, T, double, double, double, double, double) - Constructor for class org.orekit.propagation.analytical.FieldEcksteinHechlerPropagator
Build a propagator from FieldOrbit, mass and potential.
FieldEcksteinHechlerPropagator(FieldOrbit<T>, AttitudeProvider, UnnormalizedSphericalHarmonicsProvider) - Constructor for class org.orekit.propagation.analytical.FieldEcksteinHechlerPropagator
Build a propagator from FieldOrbit, attitude provider and potential provider.
FieldEcksteinHechlerPropagator(FieldOrbit<T>, AttitudeProvider, double, T, double, double, double, double, double) - Constructor for class org.orekit.propagation.analytical.FieldEcksteinHechlerPropagator
Build a propagator from FieldOrbit, attitude provider and potential.
FieldEcksteinHechlerPropagator(FieldOrbit<T>, AttitudeProvider, T, UnnormalizedSphericalHarmonicsProvider) - Constructor for class org.orekit.propagation.analytical.FieldEcksteinHechlerPropagator
Build a propagator from FieldOrbit, attitude provider, mass and potential provider.
FieldEcksteinHechlerPropagator(FieldOrbit<T>, AttitudeProvider, T, double, T, 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>, UnnormalizedSphericalHarmonicsProvider, PropagationType) - Constructor for class org.orekit.propagation.analytical.FieldEcksteinHechlerPropagator
Build a propagator from orbit and potential provider.
FieldEcksteinHechlerPropagator(FieldOrbit<T>, AttitudeProvider, T, UnnormalizedSphericalHarmonicsProvider, PropagationType) - Constructor for class org.orekit.propagation.analytical.FieldEcksteinHechlerPropagator
Build a propagator from orbit, attitude provider, mass and potential provider.
FieldEcksteinHechlerPropagator(FieldOrbit<T>, AttitudeProvider, T, UnnormalizedSphericalHarmonicsProvider, UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics, PropagationType) - Constructor for class org.orekit.propagation.analytical.FieldEcksteinHechlerPropagator
Private helper constructor.
FieldEcksteinHechlerPropagator(FieldOrbit<T>, AttitudeProvider, T, double, T, double, double, double, double, double, PropagationType) - Constructor for class org.orekit.propagation.analytical.FieldEcksteinHechlerPropagator
Build a propagator from FieldOrbit, attitude provider, mass and potential.
FieldEclipseDetector<T extends RealFieldElement<T>> - Class in org.orekit.propagation.events
Finder for satellite eclipse related events.
FieldEclipseDetector(PVCoordinatesProvider, double, PVCoordinatesProvider, double, Field<T>) - Constructor for class org.orekit.propagation.events.FieldEclipseDetector
Build a new eclipse detector.
FieldEclipseDetector(T, PVCoordinatesProvider, double, PVCoordinatesProvider, double) - Constructor for class org.orekit.propagation.events.FieldEclipseDetector
Build a new eclipse detector.
FieldEclipseDetector(T, T, PVCoordinatesProvider, double, PVCoordinatesProvider, double) - Constructor for class org.orekit.propagation.events.FieldEclipseDetector
Build a new eclipse detector.
FieldElevationDetector<T extends RealFieldElement<T>> - Class in org.orekit.propagation.events
Finder for satellite raising/setting events that allows for the setting of azimuth and/or elevation bounds or a ground azimuth/elevation mask input.
FieldElevationDetector(Field<T>, TopocentricFrame) - Constructor for class org.orekit.propagation.events.FieldElevationDetector
Creates an instance of Elevation detector based on passed in topocentric frame and the minimum elevation angle.
FieldElevationDetector(T, T, TopocentricFrame) - Constructor for class org.orekit.propagation.events.FieldElevationDetector
Creates an instance of Elevation detector based on passed in topocentric frame and overrides of default maximal checking interval and convergence threshold values.
FieldEquinoctialOrbit<T extends RealFieldElement<T>> - Class in org.orekit.orbits
This class handles equinoctial orbital parameters, which can support both circular and equatorial orbits.
FieldEquinoctialOrbit(T, T, T, T, T, T, PositionAngle, Frame, FieldAbsoluteDate<T>, T) - 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>, T) - Constructor for class org.orekit.orbits.FieldEquinoctialOrbit
Creates a new instance.
FieldEquinoctialOrbit(TimeStampedFieldPVCoordinates<T>, Frame, T) - Constructor for class org.orekit.orbits.FieldEquinoctialOrbit
Constructor from Cartesian parameters.
FieldEquinoctialOrbit(FieldPVCoordinates<T>, Frame, FieldAbsoluteDate<T>, T) - Constructor for class org.orekit.orbits.FieldEquinoctialOrbit
Constructor from Cartesian parameters.
FieldEquinoctialOrbit(FieldOrbit<T>) - Constructor for class org.orekit.orbits.FieldEquinoctialOrbit
Constructor from any kind of orbital parameters.
FieldEventDetector<T extends RealFieldElement<T>> - Interface in org.orekit.propagation.events
This interface represents space-dynamics aware events detectors.
FieldEventHandler<KK extends FieldEventDetector<T>,T extends RealFieldElement<T>> - Interface in org.orekit.propagation.events.handlers
An interface defining how to override event handling behavior in the standard propagator eventing classes without requiring subclassing.
FieldEventsLogger<T extends RealFieldElement<T>> - Class in org.orekit.propagation.events
This class logs events detectors events during propagation.
FieldEventsLogger() - Constructor for class org.orekit.propagation.events.FieldEventsLogger
Simple constructor.
FieldEventsLogger.FieldLoggedEvent<T extends RealFieldElement<T>> - Class in org.orekit.propagation.events
Class for logged events entries.
FieldEventState<D extends FieldEventDetector<T>,T extends RealFieldElement<T>> - Class in org.orekit.propagation.events
This class handles the state for one event detector during integration steps.
FieldEventState(D) - Constructor for class org.orekit.propagation.events.FieldEventState
Simple constructor.
FieldEventState.EventOccurrence<T extends RealFieldElement<T>> - Class in org.orekit.propagation.events
Class to hold the data related to an event occurrence that is needed to decide how to modify integration.
FieldFixedNumberInterpolationGrid<T extends RealFieldElement<T>> - 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.
FieldFixedNumberInterpolationGrid(Field<T>, int) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.FieldFixedNumberInterpolationGrid
Constructor.
FieldFunctionalDetector<T extends RealFieldElement<T>> - Class in org.orekit.propagation.events
A detector that implements the FieldFunctionalDetector.g(FieldSpacecraftState) function using a lambda that can be set using FieldFunctionalDetector.withFunction(Function).
FieldFunctionalDetector(Field<T>) - Constructor for class org.orekit.propagation.events.FieldFunctionalDetector
Create an event detector with the default values.
FieldGammaMnsFunction<T extends RealFieldElement<T>> - Class in org.orekit.propagation.semianalytical.dsst.utilities
Compute the Γmn,s(γ) function from equation 2.7.1-(13).
FieldGammaMnsFunction(int, T, int, Field<T>) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.FieldGammaMnsFunction
Simple constructor.
FieldGeodeticPoint<T extends RealFieldElement<T>> - Class in org.orekit.bodies
Point location relative to a 2D body surface, using RealFieldElement.
FieldGeodeticPoint(T, T, T) - Constructor for class org.orekit.bodies.FieldGeodeticPoint
Build a new instance.
FieldGHIJjsPolynomials<T extends RealFieldElement<T>> - 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.
FieldGHIJjsPolynomials(T, T, T, T) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHIJjsPolynomials
Create a set of Gjs, Hjs, Ijs and Jjs polynomials.
FieldGHmsjPolynomials<T extends RealFieldElement<T>> - 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.
FieldGHmsjPolynomials(T, T, T, T, int, Field<T>) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHmsjPolynomials
Create a set of Gmsj and Hmsj polynomials.
FieldHansenTesseralLinear<T extends RealFieldElement<T>> - Class in org.orekit.propagation.semianalytical.dsst.utilities.hansen
Hansen coefficients K(t,n,s) for t!=0 and n < 0.
FieldHansenTesseralLinear(int, int, int, int, int, Field<T>) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.hansen.FieldHansenTesseralLinear
Constructor.
FieldHansenThirdBodyLinear<T extends RealFieldElement<T>> - Class in org.orekit.propagation.semianalytical.dsst.utilities.hansen
Hansen coefficients K(t,n,s) for t=0 and n > 0.
FieldHansenThirdBodyLinear(int, int, Field<T>) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.hansen.FieldHansenThirdBodyLinear
Constructor.
FieldHansenZonalLinear<T extends RealFieldElement<T>> - Class in org.orekit.propagation.semianalytical.dsst.utilities.hansen
Hansen coefficients K(t,n,s) for t=0 and n < 0.
FieldHansenZonalLinear(int, int, Field<T>) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.hansen.FieldHansenZonalLinear
Constructor.
FieldIntegratedEphemeris<T extends RealFieldElement<T>> - Class in org.orekit.propagation.integration
This class stores sequentially generated orbital parameters for later retrieval.
FieldIntegratedEphemeris(FieldAbsoluteDate<T>, FieldAbsoluteDate<T>, FieldAbsoluteDate<T>, FieldStateMapper<T>, PropagationType, FieldDenseOutputModel<T>, Map<String, T[]>, List<FieldAdditionalStateProvider<T>>, String[]) - Constructor for class org.orekit.propagation.integration.FieldIntegratedEphemeris
Creates a new instance of IntegratedEphemeris.
FieldInterpolationGrid<T extends RealFieldElement<T>> - Interface in org.orekit.propagation.semianalytical.dsst.utilities
Interface for interpolation grids.
FieldKeplerianOrbit<T extends RealFieldElement<T>> - Class in org.orekit.orbits
This class handles traditional Keplerian orbital parameters.
FieldKeplerianOrbit(T, T, T, T, T, T, PositionAngle, Frame, FieldAbsoluteDate<T>, T) - 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>, T) - Constructor for class org.orekit.orbits.FieldKeplerianOrbit
Creates a new instance.
FieldKeplerianOrbit(TimeStampedFieldPVCoordinates<T>, Frame, T) - Constructor for class org.orekit.orbits.FieldKeplerianOrbit
Constructor from Cartesian parameters.
FieldKeplerianOrbit(FieldPVCoordinates<T>, Frame, FieldAbsoluteDate<T>, T) - Constructor for class org.orekit.orbits.FieldKeplerianOrbit
Constructor from Cartesian parameters.
FieldKeplerianOrbit(FieldOrbit<T>) - Constructor for class org.orekit.orbits.FieldKeplerianOrbit
Constructor from any kind of orbital parameters.
FieldKeplerianPropagator<T extends RealFieldElement<T>> - Class in org.orekit.propagation.analytical
Simple Keplerian orbit propagator.
FieldKeplerianPropagator(FieldOrbit<T>) - Constructor for class org.orekit.propagation.analytical.FieldKeplerianPropagator
Build a propagator from orbit only.
FieldKeplerianPropagator(FieldOrbit<T>, T) - 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, T) - Constructor for class org.orekit.propagation.analytical.FieldKeplerianPropagator
Build a propagator from orbit, attitude provider and central attraction coefficient μ.
FieldKeplerianPropagator(FieldOrbit<T>, AttitudeProvider, T, T) - Constructor for class org.orekit.propagation.analytical.FieldKeplerianPropagator
Build propagator from orbit, attitude provider, central attraction coefficient μ and mass.
FieldLatitudeCrossingDetector<T extends RealFieldElement<T>> - Class in org.orekit.propagation.events
Detector for geographic latitude crossing.
FieldLatitudeCrossingDetector(Field<T>, OneAxisEllipsoid, double) - Constructor for class org.orekit.propagation.events.FieldLatitudeCrossingDetector
Build a new detector.
FieldLatitudeCrossingDetector(T, T, OneAxisEllipsoid, double) - Constructor for class org.orekit.propagation.events.FieldLatitudeCrossingDetector
Build a detector.
FieldLnsCoefficients<T extends RealFieldElement<T>> - Class in org.orekit.propagation.semianalytical.dsst.utilities
Compute the Lns(γ).
FieldLnsCoefficients(int, int, T[][], TreeMap<CoefficientsFactory.NSKey, Double>, T, Field<T>) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.FieldLnsCoefficients
Create a set of Lns(γ) coefficients.
FieldMaxGapInterpolationGrid<T extends RealFieldElement<T>> - Class in org.orekit.propagation.semianalytical.dsst.utilities
Interpolation grid where points obey a maximum time gap.
FieldMaxGapInterpolationGrid(Field<T>, T) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.FieldMaxGapInterpolationGrid
Constructor.
FieldModeHandler<T extends RealFieldElement<T>> - Interface in org.orekit.propagation.integration
Common interface for all propagator mode handlers initialization.
FieldNodeDetector<T extends RealFieldElement<T>> - Class in org.orekit.propagation.events
Finder for node crossing events.
FieldNodeDetector(FieldOrbit<T>, Frame) - Constructor for class org.orekit.propagation.events.FieldNodeDetector
Build a new instance.
FieldNodeDetector(T, FieldOrbit<T>, Frame) - Constructor for class org.orekit.propagation.events.FieldNodeDetector
Build a new instance.
FieldNumericalPropagator<T extends RealFieldElement<T>> - Class in org.orekit.propagation.numerical
This class propagates orbits using numerical integration.
FieldNumericalPropagator(Field<T>, FieldODEIntegrator<T>) - Constructor for class org.orekit.propagation.numerical.FieldNumericalPropagator
Create a new instance of NumericalPropagator, based on orbit definition mu.
FieldNumericalPropagator(Field<T>, FieldODEIntegrator<T>, AttitudeProvider) - Constructor for class org.orekit.propagation.numerical.FieldNumericalPropagator
Create a new instance of NumericalPropagator, based on orbit definition mu.
FieldOfView - Interface in org.orekit.geometry.fov
Interface representing a spacecraft sensor Field Of View.
FieldOfView - Class in org.orekit.propagation.events
Deprecated.
as of 10.1, replaced by PolygonalFieldOfView
FieldOfView(SphericalPolygonsSet, double) - Constructor for class org.orekit.propagation.events.FieldOfView
Deprecated.
Build a new instance.
FieldOfView(Vector3D, Vector3D, double, Vector3D, double, double) - Constructor for class org.orekit.propagation.events.FieldOfView
Deprecated.
Build a Field Of View with dihedral shape (i.e.
FieldOfView(Vector3D, Vector3D, double, int, double) - Constructor for class org.orekit.propagation.events.FieldOfView
Deprecated.
Build Field Of View with a regular polygon shape.
FieldOfViewDetector - Class in org.orekit.propagation.events
Finder for target entry/exit events with respect to a satellite sensor Field Of View.
FieldOfViewDetector(PVCoordinatesProvider, FieldOfView) - Constructor for class org.orekit.propagation.events.FieldOfViewDetector
FieldOfViewDetector(PVCoordinatesProvider, FieldOfView) - Constructor for class org.orekit.propagation.events.FieldOfViewDetector
Build a new instance.
FieldOfViewDetector(PVCoordinatesProvider, double, VisibilityTrigger, FieldOfView) - Constructor for class org.orekit.propagation.events.FieldOfViewDetector
Build a new instance.
FieldOfViewDetector(PVCoordinatesProvider, double, VisibilityTrigger, FieldOfView) - Constructor for class org.orekit.propagation.events.FieldOfViewDetector
FieldOrbit<T extends RealFieldElement<T>> - Class in org.orekit.orbits
This class handles orbital parameters.
FieldOrbit(Frame, FieldAbsoluteDate<T>, T) - Constructor for class org.orekit.orbits.FieldOrbit
Default constructor.
FieldOrbit(TimeStampedFieldPVCoordinates<T>, Frame, T) - Constructor for class org.orekit.orbits.FieldOrbit
Set the orbit from Cartesian parameters.
FieldOrekitFixedStepHandler<T extends RealFieldElement<T>> - Interface in org.orekit.propagation.sampling
This interface is a space-dynamics aware fixed size step handler.
FieldOrekitFixedStepHandlerMultiplexer<T extends RealFieldElement<T>> - Class in org.orekit.propagation.sampling
This class gathers several FieldOrekitFixedStepHandler instances into one.
FieldOrekitFixedStepHandlerMultiplexer() - Constructor for class org.orekit.propagation.sampling.FieldOrekitFixedStepHandlerMultiplexer
Simple constructor.
FieldOrekitStepHandler<T extends RealFieldElement<T>> - Interface in org.orekit.propagation.sampling
This interface is a space-dynamics aware step handler.
FieldOrekitStepHandlerMultiplexer<T extends RealFieldElement<T>> - Class in org.orekit.propagation.sampling
This class gathers several OrekitStepHandler instances into one.
FieldOrekitStepHandlerMultiplexer() - Constructor for class org.orekit.propagation.sampling.FieldOrekitStepHandlerMultiplexer
Simple constructor.
FieldOrekitStepInterpolator<T extends RealFieldElement<T>> - Interface in org.orekit.propagation.sampling
This interface is a space-dynamics aware step interpolator.
FieldOrekitStepNormalizer<T extends RealFieldElement<T>> - Class in org.orekit.propagation.sampling
This class wraps an object implementing OrekitFixedStepHandler into a OrekitStepHandler.
FieldOrekitStepNormalizer(T, FieldOrekitFixedStepHandler<T>) - Constructor for class org.orekit.propagation.sampling.FieldOrekitStepNormalizer
Simple constructor.
FieldPoleCorrection<T extends RealFieldElement<T>> - Class in org.orekit.frames
Simple container class for pole correction parameters.
FieldPoleCorrection(T, T) - Constructor for class org.orekit.frames.FieldPoleCorrection
Simple constructor.
FieldPropagator<T extends RealFieldElement<T>> - Interface in org.orekit.propagation
This interface provides a way to propagate an orbit at any time.
FieldPVCoordinates<T extends RealFieldElement<T>> - Class in org.orekit.utils
Simple container for Position/Velocity pairs, using RealFieldElement.
FieldPVCoordinates(FieldVector3D<T>, FieldVector3D<T>) - Constructor for class org.orekit.utils.FieldPVCoordinates
Builds a FieldPVCoordinates triplet with zero acceleration.
FieldPVCoordinates(FieldVector3D<T>, FieldVector3D<T>, FieldVector3D<T>) - Constructor for class org.orekit.utils.FieldPVCoordinates
Builds a FieldPVCoordinates triplet.
FieldPVCoordinates(Field<T>, PVCoordinates) - Constructor for class org.orekit.utils.FieldPVCoordinates
Builds a FieldPVCoordinates from a field and a regular PVCoordinates.
FieldPVCoordinates(double, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.FieldPVCoordinates
Multiplicative constructor.
FieldPVCoordinates(T, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.FieldPVCoordinates
Multiplicative constructor.
FieldPVCoordinates(T, PVCoordinates) - Constructor for class org.orekit.utils.FieldPVCoordinates
Multiplicative constructor.
FieldPVCoordinates(FieldPVCoordinates<T>, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.FieldPVCoordinates
Subtractive constructor.
FieldPVCoordinates(double, FieldPVCoordinates<T>, double, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.FieldPVCoordinates
Linear constructor.
FieldPVCoordinates(T, FieldPVCoordinates<T>, T, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.FieldPVCoordinates
Linear constructor.
FieldPVCoordinates(T, PVCoordinates, T, PVCoordinates) - Constructor for class org.orekit.utils.FieldPVCoordinates
Linear constructor.
FieldPVCoordinates(double, FieldPVCoordinates<T>, double, FieldPVCoordinates<T>, double, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.FieldPVCoordinates
Linear constructor.
FieldPVCoordinates(T, FieldPVCoordinates<T>, T, FieldPVCoordinates<T>, T, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.FieldPVCoordinates
Linear constructor.
FieldPVCoordinates(T, PVCoordinates, T, PVCoordinates, T, PVCoordinates) - Constructor for class org.orekit.utils.FieldPVCoordinates
Linear constructor.
FieldPVCoordinates(double, FieldPVCoordinates<T>, double, FieldPVCoordinates<T>, double, FieldPVCoordinates<T>, double, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.FieldPVCoordinates
Linear constructor.
FieldPVCoordinates(T, FieldPVCoordinates<T>, T, FieldPVCoordinates<T>, T, FieldPVCoordinates<T>, T, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.FieldPVCoordinates
Linear constructor.
FieldPVCoordinates(T, PVCoordinates, T, PVCoordinates, T, PVCoordinates, T, PVCoordinates) - Constructor for class org.orekit.utils.FieldPVCoordinates
Linear constructor.
FieldPVCoordinates(FieldVector3D<FieldDerivativeStructure<T>>) - Constructor for class org.orekit.utils.FieldPVCoordinates
Builds a FieldPVCoordinates triplet from a FieldVector3D<FieldDerivativeStructure>.
FieldPVCoordinatesProvider<T extends RealFieldElement<T>> - Interface in org.orekit.utils
Interface for PV coordinates providers.
FieldRecordAndContinue<T extends FieldEventDetector<E>,E extends RealFieldElement<E>> - Class in org.orekit.propagation.events.handlers
Handler that will record every time an event occurs and always return Action.CONTINUE.
FieldRecordAndContinue() - Constructor for class org.orekit.propagation.events.handlers.FieldRecordAndContinue
Create a new handler using an ArrayList to store events.
FieldRecordAndContinue(List<FieldRecordAndContinue.Event<T, E>>) - Constructor for class org.orekit.propagation.events.handlers.FieldRecordAndContinue
Create a handler using the given collection to store events.
FieldRecordAndContinue.Event<T,F extends RealFieldElement<F>> - Class in org.orekit.propagation.events.handlers
A single event detected during propagation.
FieldShortPeriodicsInterpolatedCoefficient<T extends RealFieldElement<T>> - Class in org.orekit.propagation.semianalytical.dsst.utilities
Interpolated short periodics coefficients.
FieldShortPeriodicsInterpolatedCoefficient(int) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.FieldShortPeriodicsInterpolatedCoefficient
Simple constructor.
FieldShortPeriodTerms<T extends RealFieldElement<T>> - Interface in org.orekit.propagation.semianalytical.dsst.forces
Additive short period terms contributing to the mean to osculating orbit mapping.
FieldSpacecraftState<T extends RealFieldElement<T>> - Class in org.orekit.propagation
This class is the representation of a complete state holding orbit, attitude and mass information at a given date.
FieldSpacecraftState(FieldOrbit<T>) - Constructor for class org.orekit.propagation.FieldSpacecraftState
Build a spacecraft state from orbit only.
FieldSpacecraftState(FieldOrbit<T>, FieldAttitude<T>) - Constructor for class org.orekit.propagation.FieldSpacecraftState
Build a spacecraft state from orbit and attitude provider.
FieldSpacecraftState(FieldOrbit<T>, T) - Constructor for class org.orekit.propagation.FieldSpacecraftState
Create a new instance from orbit and mass.
FieldSpacecraftState(FieldOrbit<T>, FieldAttitude<T>, T) - Constructor for class org.orekit.propagation.FieldSpacecraftState
Build a spacecraft state from orbit, attitude provider and mass.
FieldSpacecraftState(FieldOrbit<T>, Map<String, T[]>) - Constructor for class org.orekit.propagation.FieldSpacecraftState
Build a spacecraft state from orbit only.
FieldSpacecraftState(FieldOrbit<T>, FieldAttitude<T>, Map<String, T[]>) - Constructor for class org.orekit.propagation.FieldSpacecraftState
Build a spacecraft state from orbit and attitude provider.
FieldSpacecraftState(FieldOrbit<T>, T, Map<String, T[]>) - Constructor for class org.orekit.propagation.FieldSpacecraftState
Create a new instance from orbit and mass.
FieldSpacecraftState(FieldOrbit<T>, FieldAttitude<T>, T, Map<String, T[]>) - Constructor for class org.orekit.propagation.FieldSpacecraftState
Build a spacecraft state from orbit, attitude provider and mass.
FieldSpacecraftState(Field<T>, SpacecraftState) - Constructor for class org.orekit.propagation.FieldSpacecraftState
FieldSpacecraftState(FieldAbsolutePVCoordinates<T>) - Constructor for class org.orekit.propagation.FieldSpacecraftState
Build a spacecraft state from orbit only.
FieldSpacecraftState(FieldAbsolutePVCoordinates<T>, FieldAttitude<T>) - Constructor for class org.orekit.propagation.FieldSpacecraftState
Build a spacecraft state from orbit and attitude provider.
FieldSpacecraftState(FieldAbsolutePVCoordinates<T>, T) - Constructor for class org.orekit.propagation.FieldSpacecraftState
Create a new instance from orbit and mass.
FieldSpacecraftState(FieldAbsolutePVCoordinates<T>, FieldAttitude<T>, T) - Constructor for class org.orekit.propagation.FieldSpacecraftState
Build a spacecraft state from orbit, attitude provider and mass.
FieldSpacecraftState(FieldAbsolutePVCoordinates<T>, Map<String, T[]>) - Constructor for class org.orekit.propagation.FieldSpacecraftState
Build a spacecraft state from orbit only.
FieldSpacecraftState(FieldAbsolutePVCoordinates<T>, FieldAttitude<T>, Map<String, T[]>) - Constructor for class org.orekit.propagation.FieldSpacecraftState
Build a spacecraft state from orbit and attitude provider.
FieldSpacecraftState(FieldAbsolutePVCoordinates<T>, T, Map<String, T[]>) - Constructor for class org.orekit.propagation.FieldSpacecraftState
Create a new instance from orbit and mass.
FieldSpacecraftState(FieldAbsolutePVCoordinates<T>, FieldAttitude<T>, T, Map<String, T[]>) - Constructor for class org.orekit.propagation.FieldSpacecraftState
Build a spacecraft state from orbit, attitude provider and mass.
FieldStateMapper<T extends RealFieldElement<T>> - Class in org.orekit.propagation.integration
This class maps between raw double elements and FieldSpacecraftState instances.
FieldStateMapper(FieldAbsoluteDate<T>, T, OrbitType, PositionAngle, AttitudeProvider, Frame) - Constructor for class org.orekit.propagation.integration.FieldStateMapper
Simple constructor.
FieldStopOnDecreasing<KK extends FieldEventDetector<T>,T extends RealFieldElement<T>> - Class in org.orekit.propagation.events.handlers
Handle a detection event and choose what to do next.
FieldStopOnDecreasing() - Constructor for class org.orekit.propagation.events.handlers.FieldStopOnDecreasing
 
FieldStopOnEvent<KK extends FieldEventDetector<T>,T extends RealFieldElement<T>> - Class in org.orekit.propagation.events.handlers
Event handler which will always return continue as a state.
FieldStopOnEvent() - Constructor for class org.orekit.propagation.events.handlers.FieldStopOnEvent
 
FieldStopOnIncreasing<KK extends FieldEventDetector<T>,T extends RealFieldElement<T>> - Class in org.orekit.propagation.events.handlers
Handle a detection event and choose what to do next.
FieldStopOnIncreasing() - Constructor for class org.orekit.propagation.events.handlers.FieldStopOnIncreasing
 
FieldTimeDerivativesEquations<T extends RealFieldElement<T>> - Interface in org.orekit.propagation.numerical
Interface summing up the contribution of several forces into orbit and mass derivatives.
FieldTimeInterpolable<T extends FieldTimeInterpolable<T,KK>,KK extends RealFieldElement<KK>> - Interface in org.orekit.time
This interface represents objects that can be interpolated in time.
FieldTimeShiftable<T extends FieldTimeInterpolable<T,KK>,KK extends RealFieldElement<KK>> - Interface in org.orekit.time
This interface represents objects that can be shifted in time.
FieldTimeSpanMap<T,D extends RealFieldElement<D>> - Class in org.orekit.utils
Container for objects that apply to spans of time.
FieldTimeSpanMap(T, Field<D>) - Constructor for class org.orekit.utils.FieldTimeSpanMap
Create a map containing a single object, initially valid throughout the timeline.
FieldTimeSpanMap.Transition<S,D extends RealFieldElement<D>> - Class in org.orekit.utils
Local class holding transition times.
FieldTimeStamped<T extends RealFieldElement<T>> - Interface in org.orekit.time
This interface represents objects that have a AbsoluteDate date attached to them.
FieldTransform<T extends RealFieldElement<T>> - Class in org.orekit.frames
Transformation class in three dimensional space.
FieldTransform(Field<T>, Transform) - Constructor for class org.orekit.frames.FieldTransform
Build a transform from a regular transform.
FieldTransform(FieldAbsoluteDate<T>, FieldVector3D<T>) - Constructor for class org.orekit.frames.FieldTransform
Build a translation transform.
FieldTransform(FieldAbsoluteDate<T>, FieldRotation<T>) - Constructor for class org.orekit.frames.FieldTransform
Build a rotation transform.
FieldTransform(FieldAbsoluteDate<T>, FieldVector3D<T>, FieldVector3D<T>) - Constructor for class org.orekit.frames.FieldTransform
Build a translation transform, with its first time derivative.
FieldTransform(FieldAbsoluteDate<T>, FieldVector3D<T>, FieldVector3D<T>, FieldVector3D<T>) - Constructor for class org.orekit.frames.FieldTransform
Build a translation transform, with its first and second time derivatives.
FieldTransform(FieldAbsoluteDate<T>, FieldPVCoordinates<T>) - Constructor for class org.orekit.frames.FieldTransform
Build a translation transform, with its first time derivative.
FieldTransform(FieldAbsoluteDate<T>, FieldRotation<T>, FieldVector3D<T>) - Constructor for class org.orekit.frames.FieldTransform
Build a rotation transform.
FieldTransform(FieldAbsoluteDate<T>, FieldRotation<T>, FieldVector3D<T>, FieldVector3D<T>) - Constructor for class org.orekit.frames.FieldTransform
Build a rotation transform.
FieldTransform(FieldAbsoluteDate<T>, FieldAngularCoordinates<T>) - Constructor for class org.orekit.frames.FieldTransform
Build a rotation transform.
FieldTransform(FieldAbsoluteDate<T>, FieldTransform<T>, FieldTransform<T>) - Constructor for class org.orekit.frames.FieldTransform
Build a transform by combining two existing ones.
FieldTransformGenerator<T extends RealFieldElement<T>> - Class in org.orekit.frames
Generator to use field transforms in GenericTimeStampedCache.
FieldTransformGenerator(Field<T>, int, TransformProvider, double) - Constructor for class org.orekit.frames.FieldTransformGenerator
simple constructor.
FIFTIES_EPOCH - Static variable in class org.orekit.time.AbsoluteDate
Reference epoch for 1950 dates: 1950-01-01T00:00:00 Terrestrial Time.
FIFTIES_EPOCH - Static variable in class org.orekit.time.DateComponents
Reference epoch for 1950 dates: 1950-01-01.
FilesListCrawler - Class in org.orekit.data
Provider for data files in an explicit list.
FilesListCrawler(File...) - Constructor for class org.orekit.data.FilesListCrawler
Build a data classpath crawler.
fillHalfRow(T, FieldVector3D<T>, T[], int) - Method in class org.orekit.orbits.FieldOrbit
Fill a Jacobian half row with a single vector.
fillHalfRow(T, FieldVector3D<T>, T, FieldVector3D<T>, T[], int) - Method in class org.orekit.orbits.FieldOrbit
Fill a Jacobian half row with a linear combination of vectors.
fillHalfRow(T, FieldVector3D<T>, T, FieldVector3D<T>, T, FieldVector3D<T>, T[], int) - Method in class org.orekit.orbits.FieldOrbit
Fill a Jacobian half row with a linear combination of vectors.
fillHalfRow(T, FieldVector3D<T>, T, FieldVector3D<T>, T, FieldVector3D<T>, T, FieldVector3D<T>, T[], int) - Method in class org.orekit.orbits.FieldOrbit
Fill a Jacobian half row with a linear combination of vectors.
fillHalfRow(T, FieldVector3D<T>, T, FieldVector3D<T>, T, FieldVector3D<T>, T, FieldVector3D<T>, T, FieldVector3D<T>, T[], int) - Method in class org.orekit.orbits.FieldOrbit
Fill a Jacobian half row with a linear combination of vectors.
fillHalfRow(T, FieldVector3D<T>, T, FieldVector3D<T>, T, FieldVector3D<T>, T, FieldVector3D<T>, T, FieldVector3D<T>, T, FieldVector3D<T>, T[], int) - Method in class org.orekit.orbits.FieldOrbit
Fill a Jacobian half row with a linear combination of vectors.
fillHalfRow(double, Vector3D, double[], int) - Static method in class org.orekit.orbits.Orbit
Fill a Jacobian half row with a single vector.
fillHalfRow(double, Vector3D, double, Vector3D, double[], int) - Static method in class org.orekit.orbits.Orbit
Fill a Jacobian half row with a linear combination of vectors.
fillHalfRow(double, Vector3D, double, Vector3D, double, Vector3D, double[], int) - Static method in class org.orekit.orbits.Orbit
Fill a Jacobian half row with a linear combination of vectors.
fillHalfRow(double, Vector3D, double, Vector3D, double, Vector3D, double, Vector3D, double[], int) - Static method in class org.orekit.orbits.Orbit
Fill a Jacobian half row with a linear combination of vectors.
fillHalfRow(double, Vector3D, double, Vector3D, double, Vector3D, double, Vector3D, double, Vector3D, double[], int) - Static method in class org.orekit.orbits.Orbit
Fill a Jacobian half row with a linear combination of vectors.
fillHalfRow(double, Vector3D, double, Vector3D, double, Vector3D, double, Vector3D, double, Vector3D, double, Vector3D, double[], int) - Static method in class org.orekit.orbits.Orbit
Fill a Jacobian half row with a linear combination of vectors.
fillHistory(IERSConventions.NutationCorrectionConverter, SortedSet<EOPEntry>) - Method in interface org.orekit.frames.EOPHistoryLoader
Load celestial body.
filter(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.
filter(ObservedMeasurement<T>, SpacecraftState) - Method in class org.orekit.estimation.measurements.filtering.ElevationFilter
Apply a filter to an observed measurement.
filter(ObservedMeasurement<T>, SpacecraftState) - Method in interface org.orekit.estimation.measurements.filtering.MeasurementFilter
Apply a filter to an observed measurement.
filter(ObservedMeasurement<T>, SpacecraftState) - Method in class org.orekit.estimation.measurements.filtering.ResidualFilter
Apply a filter to an observed measurement.
filter(NamedData) - Method in class org.orekit.gnss.HatanakaCompressFilter
Filter the named data.
filter(boolean) - Method in class org.orekit.utils.ParameterDriversList
Filter parameters to keep only one type of selection status.
FilterType - Enum in org.orekit.propagation.events
Enumerate for filtering events.
finalizeEstimation(ObservedMeasurement<?>, ProcessEstimate) - Method in class org.orekit.estimation.sequential.DSSTKalmanModel
Finalize estimation.
finalizeEstimation(ObservedMeasurement<?>, ProcessEstimate) - Method in class org.orekit.estimation.sequential.KalmanModel
Finalize estimation.
finalizeEstimation(ObservedMeasurement<?>, ProcessEstimate) - Method in interface org.orekit.estimation.sequential.KalmanODModel
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.
finished(TaskEvent) - Method in class org.orekit.compiler.plugin.DefaultDataContextPlugin
 
FiniteDifferencePropagatorConverter - Class in org.orekit.propagation.conversion
Propagator converter using finite differences to compute the Jacobian.
FiniteDifferencePropagatorConverter(PropagatorBuilder, double, int) - Constructor for class org.orekit.propagation.conversion.FiniteDifferencePropagatorConverter
Simple constructor.
fit() - Method in class org.orekit.utils.SecularAndHarmonic
Fit parameters.
FixedNumberInterpolationGrid - Class in org.orekit.propagation.semianalytical.dsst.utilities
Interpolation grid where a fixed number of points are evenly spaced between the start and the end of the integration step.
FixedNumberInterpolationGrid(int) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.FixedNumberInterpolationGrid
Constructor.
FixedRate - Class in org.orekit.attitudes
This class handles a simple attitude provider at constant rate around a fixed axis.
FixedRate(Attitude) - Constructor for class org.orekit.attitudes.FixedRate
Creates a new instance.
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.troposphere
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.troposphere.FixedTroposphericDelay
Creates a new FixedTroposphericDelay instance.
FixedTroposphericDelay(String) - Constructor for class org.orekit.models.earth.troposphere.FixedTroposphericDelay
Creates a new FixedTroposphericDelay instance, and loads the delay values from the given resource via the default data context.
FixedTroposphericDelay(String, DataProvidersManager) - Constructor for class org.orekit.models.earth.troposphere.FixedTroposphericDelay
Creates a new FixedTroposphericDelay instance, and loads the delay values from the given resource via the specified data manager.
fixIntegerAmbiguities(int, List<ParameterDriver>, RealMatrix) - Method in class org.orekit.estimation.measurements.gnss.AmbiguitySolver
Fix integer ambiguities.
FLOW_RATE - Static variable in class org.orekit.forces.maneuvers.ConstantThrustManeuver
Deprecated.
FLOW_RATE - Static variable in class org.orekit.forces.maneuvers.propulsion.BasicConstantThrustPropulsionModel
Parameter name for flow rate.
FLOW_RATE_SCALE - Static variable in class org.orekit.forces.maneuvers.propulsion.BasicConstantThrustPropulsionModel
Flow rate scaling factor.
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
FootprintOverlapDetector(FieldOfView, OneAxisEllipsoid, SphericalPolygonsSet, double) - Constructor for class org.orekit.propagation.events.FootprintOverlapDetector
Build a new instance.
ForceModel - Interface in org.orekit.forces
This interface represents a force modifying spacecraft motion.
Frame - Class in org.orekit.frames
Tridimensional references frames class.
Frame(Frame, Transform, String) - Constructor for class org.orekit.frames.Frame
Build a non-inertial frame from its transform with respect to its parent.
Frame(Frame, TransformProvider, String) - Constructor for class org.orekit.frames.Frame
Build a non-inertial frame from its transform with respect to its parent.
Frame(Frame, Transform, String, boolean) - Constructor for class org.orekit.frames.Frame
Build a frame from its transform with respect to its parent.
Frame(Frame, TransformProvider, String, boolean) - Constructor for class org.orekit.frames.Frame
Build a frame from its transform with respect to its parent.
FrameAncestorException - Exception in org.orekit.errors
This class is the base class for exception thrown by the UpdatableFrame.updateTransform method.
FrameAncestorException(Localizable, Object...) - Constructor for exception org.orekit.errors.FrameAncestorException
Simple constructor.
Frames - Interface in org.orekit.frames
A collection of commonly used Frames.
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.
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.
fromSeconds(int, double, double, int) - Static method in class org.orekit.time.TimeComponents
Build a time from the second number within the day.
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.
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, InputStream, String, TimeScales) - 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.
FundamentalNutationArguments(IERSConventions, TimeScale, List<double[]>, TimeScales) - Constructor for class org.orekit.data.FundamentalNutationArguments
Build a model of fundamental arguments from an IERS table file.
FUTURE_INFINITY - Static variable in class org.orekit.time.AbsoluteDate
Dummy date at infinity in the future direction.

G

g(SpacecraftState) - Method in class org.orekit.forces.maneuvers.ImpulseManeuver
Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.AbstractDetector
Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.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
Deprecated.
Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.DateDetector
Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.EclipseDetector
Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.ElevationDetector
Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.ElevationExtremumDetector
Compute the value of the detection function.
g(SpacecraftState) - Method in interface org.orekit.propagation.events.EventDetector
Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.EventEnablingPredicateFilter
Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.EventShifter
Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.EventSlopeFilter
Compute the value of the switching function.
g(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.events.FieldAbstractDetector
Compute the value of the switching function.
g(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.events.FieldAltitudeDetector
Compute the value of the switching function.
g(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.events.FieldApsideDetector
Compute the value of the switching function.
g(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.events.FieldDateDetector
Compute the value of the switching function.
g(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.events.FieldEclipseDetector
Compute the value of the switching function.
g(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.events.FieldElevationDetector
Compute the value of the switching function.
g(FieldSpacecraftState<T>) - Method in interface org.orekit.propagation.events.FieldEventDetector
Compute the value of the switching function.
g(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.events.FieldFunctionalDetector
 
g(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.events.FieldLatitudeCrossingDetector
Compute the value of the detection function.
g(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.events.FieldNodeDetector
Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.FieldOfViewDetector
Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.FootprintOverlapDetector
Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.FunctionalDetector
 
g(SpacecraftState) - Method in class org.orekit.propagation.events.GeographicZoneDetector
Compute the value of the detection function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.GroundAtNightDetector
Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.GroundFieldOfViewDetector
Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.HaloXZPlaneCrossingDetector
Compute the value of the detection function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.InterSatDirectViewDetector
Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.LatitudeCrossingDetector
Compute the value of the detection function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.LatitudeExtremumDetector
Compute the value of the detection function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.LongitudeCrossingDetector
Compute the value of the detection function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.LongitudeExtremumDetector
Compute the value of the detection function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.MagneticFieldDetector
Compute the value of the detection function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.NegateDetector
 
g(SpacecraftState) - Method in class org.orekit.propagation.events.NodeDetector
Compute the value of the switching function.
g(SpacecraftState) - Method in class org.orekit.propagation.events.PositionAngleDetector
Compute the value of the detection function.
G0_STANDARD_GRAVITY - Static variable in interface org.orekit.utils.Constants
Standard gravity constant, used in maneuvers definition: 9.80665 m/s².
Galileo - Class in org.orekit.gnss.attitude
Attitude providers for Galileo navigation satellites.
Galileo(double, AbsoluteDate, AbsoluteDate, ExtendedPVCoordinatesProvider, Frame) - Constructor for class org.orekit.gnss.attitude.Galileo
Simple constructor.
GALILEO_EPOCH - Static variable in class org.orekit.time.AbsoluteDate
Reference epoch for Galileo System Time: 1999-08-22T00:00:00 GST.
GALILEO_EPOCH - Static variable in class org.orekit.time.DateComponents
Reference epoch for Galileo System Time: 1999-08-22.
GALILEO_MU - Static variable in interface org.orekit.propagation.analytical.gnss.GalileoOrbitalElements
Earth's universal gravitational parameter for Galileo user in m³/s².
GALILEO_PI - Static variable in interface org.orekit.propagation.analytical.gnss.GalileoOrbitalElements
Value of Pi for conversion from semicircles to radian.
GALILEO_WEEK_IN_SECONDS - Static variable in interface org.orekit.propagation.analytical.gnss.GalileoOrbitalElements
Duration of the Galileo week in seconds.
GALILEO_WEEK_NB - Static variable in interface org.orekit.propagation.analytical.gnss.GalileoOrbitalElements
Number of weeks in the Galileo cycle.
GalileoAlmanac - Class in org.orekit.gnss
Class for Galileo almanac.
GalileoAlmanac(int, int, double, double, double, double, int, double, double, double, double, double, double, int, int, int) - Constructor for class org.orekit.gnss.GalileoAlmanac
Build a new almanac.
GalileoAlmanac(int, int, double, double, double, double, int, double, double, double, double, double, double, int, int, int, AbsoluteDate) - Constructor for class org.orekit.gnss.GalileoAlmanac
Build a new almanac.
GalileoOrbitalElements - Interface in org.orekit.propagation.analytical.gnss
This interface provides the minimal set of orbital elements needed by the GalileoPropagator.
GalileoPropagator - Class in org.orekit.propagation.analytical.gnss
This class aims at propagating a Galileo orbit from GalileoOrbitalElements.
GalileoPropagator.Builder - Class in org.orekit.propagation.analytical.gnss
This nested class aims at building a GalileoPropagator.
GalileoScale - Class in org.orekit.time
Galileo system time scale.
GammaMnsFunction - Class in org.orekit.propagation.semianalytical.dsst.utilities
Compute the Γmn,s(γ) function from equation 2.7.1-(13).
GammaMnsFunction(int, double, int) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.GammaMnsFunction
Simple constructor.
generate(List<OrekitStepInterpolator>) - Method in class org.orekit.estimation.measurements.generation.ContinuousScheduler
Generate a sequence of measurements.
generate(List<OrekitStepInterpolator>) - Method in class org.orekit.estimation.measurements.generation.EventBasedScheduler
Generate a sequence of measurements.
generate(AbsoluteDate, AbsoluteDate) - Method in class org.orekit.estimation.measurements.generation.Generator
Generate measurements.
generate(List<OrekitStepInterpolator>) - Method in interface org.orekit.estimation.measurements.generation.Scheduler
Generate a sequence of measurements.
generate(AbsoluteDate, AbsoluteDate) - Method in class org.orekit.frames.FieldTransformGenerator
Generate a chronologically sorted list of entries to be cached.
generate(AbsoluteDate, AbsoluteDate) - Method in class org.orekit.frames.TransformGenerator
Generate a chronologically sorted list of entries to be cached.
generate(AbsoluteDate, AbsoluteDate) - Method in interface org.orekit.utils.TimeStampedGenerator
Generate a chronologically sorted list of entries to be cached.
generateCartesianOrbit() - Method in class org.orekit.files.ccsds.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(BodyShape, SphericalPolygonsSet, double) - Constructor for class org.orekit.propagation.events.GeographicZoneDetector
Build a new detector.
GeographicZoneDetector(double, double, BodyShape, SphericalPolygonsSet, double) - Constructor for class org.orekit.propagation.events.GeographicZoneDetector
Build a detector.
Geoid - Class in org.orekit.models.earth
A geoid is a level surface of the gravity potential of a body.
Geoid(NormalizedSphericalHarmonicsProvider, ReferenceEllipsoid) - Constructor for class org.orekit.models.earth.Geoid
Creates a geoid from the given geopotential, reference ellipsoid and the assumptions in the comment for Geoid.
GeoMagneticElements - Class in org.orekit.models.earth
Contains the elements to represent a magnetic field at a single point.
GeoMagneticElements(Vector3D) - Constructor for class org.orekit.models.earth.GeoMagneticElements
Construct a new element with the given field vector.
GeoMagneticField - Class in org.orekit.models.earth
Used to calculate the geomagnetic field at a given geodetic point on earth.
GeoMagneticField(String, double, int, int, double, double) - Constructor for class org.orekit.models.earth.GeoMagneticField
Create a new geomagnetic field model with the given parameters.
GeoMagneticFieldFactory - Class in org.orekit.models.earth
Factory for different GeoMagneticField models.
GeoMagneticFieldFactory.FieldModel - Enum in org.orekit.models.earth
The currently supported geomagnetic field models.
GeoMagneticFields - Interface in org.orekit.models.earth
Methods for obtaining geomagnetic fields.
GeoMagneticModelLoader - Class in org.orekit.models.earth
Loads geomagnetic field models from a given input stream.
GeoMagneticModelLoader() - Constructor for class org.orekit.models.earth.GeoMagneticModelLoader
 
GeometryFreeCombination - Class in org.orekit.estimation.measurements.gnss
Geometry-free combination.
GeometryFreeCycleSlipDetector - Class in org.orekit.estimation.measurements.gnss
Geometry free cycle slip detectors.
GeometryFreeCycleSlipDetector(double, double, int) - Constructor for class org.orekit.estimation.measurements.gnss.GeometryFreeCycleSlipDetector
Constructor.
get(FieldAbsoluteDate<D>) - Method in class org.orekit.utils.FieldTimeSpanMap
Get the entry valid at a specified date.
get(AbsoluteDate) - Method in class org.orekit.utils.TimeSpanMap
Get the entry valid at a specified date.
get24HoursKp(AbsoluteDate) - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherData
Get the last 24H mean geomagnetic index.
get24HoursKp(AbsoluteDate) - Method in class org.orekit.models.earth.atmosphere.data.MarshallSolarActivityFutureEstimation
The Kp index is derived from the Ap index.
get24HoursKp(AbsoluteDate) - Method in interface org.orekit.models.earth.atmosphere.DTM2000InputParameters
Get the last 24H mean geomagnetic index.
getA() - Method in class org.orekit.bodies.Ellipse
Get the semi major axis.
getA() - Method in class org.orekit.bodies.Ellipsoid
Get the length of the first semi-axis.
getA() - Method in class org.orekit.files.ccsds.OGMFile
Get the orbit semi-major axis.
getA() - Method in class org.orekit.models.earth.troposphere.ViennaModelCoefficientsLoader
Returns the a coefficients array.
getA() - Method in class org.orekit.models.earth.weather.GlobalPressureTemperature2Model
Returns the a coefficients array.
getA() - Method in class org.orekit.orbits.CartesianOrbit
Get the semi-major axis.
getA() - Method in class org.orekit.orbits.CircularOrbit
Get the semi-major axis.
getA() - Method in class org.orekit.orbits.EquinoctialOrbit
Get the semi-major axis.
getA() - Method in class org.orekit.orbits.FieldCartesianOrbit
Get the semi-major axis.
getA() - Method in class org.orekit.orbits.FieldCircularOrbit
Get the semi-major axis.
getA() - Method in class org.orekit.orbits.FieldEquinoctialOrbit
Get the semi-major axis.
getA() - Method in class org.orekit.orbits.FieldKeplerianOrbit
Get the semi-major axis.
getA() - Method in class org.orekit.orbits.FieldOrbit
Get the semi-major axis.
getA() - Method in class org.orekit.orbits.KeplerianOrbit
Get the semi-major axis.
getA() - Method in class org.orekit.orbits.Orbit
Get the semi-major axis.
getA() - Method in class org.orekit.propagation.FieldSpacecraftState
Get the semi-major axis.
getA() - Method in class org.orekit.propagation.SpacecraftState
Get the semi-major axis.
getAbscissaGrid() - Method in class org.orekit.utils.InterpolationTableLoader
Returns a copy of the abscissa grid for the interpolation function.
getAbsoluteDate() - Method in class org.orekit.utils.FieldTimeSpanMap.Transition
Get the transition field absolute date.
getAbsPVA() - Method in class org.orekit.propagation.FieldSpacecraftState
Get the absolute position-velocity-acceleration.
getAbsPVA() - Method in class org.orekit.propagation.SpacecraftState
Get the absolute position-velocity-acceleration.
getAcceleration(SpacecraftState, Attitude, double[]) - Method in interface org.orekit.forces.maneuvers.propulsion.PropulsionModel
Get the acceleration of the spacecraft during maneuver and in maneuver frame.
getAcceleration(FieldSpacecraftState<T>, FieldAttitude<T>, T[]) - Method in interface org.orekit.forces.maneuvers.propulsion.PropulsionModel
Get the acceleration of the spacecraft during maneuver and in maneuver frame.
getAcceleration(SpacecraftState, Attitude, double[]) - Method in interface org.orekit.forces.maneuvers.propulsion.ThrustPropulsionModel
Get the acceleration of the spacecraft during maneuver and in maneuver frame.
getAcceleration(FieldSpacecraftState<T>, FieldAttitude<T>, T[]) - Method in interface org.orekit.forces.maneuvers.propulsion.ThrustPropulsionModel
Get the acceleration of the spacecraft during maneuver and in maneuver frame.
getAcceleration() - Method in class org.orekit.frames.FieldTransform
Get the second time derivative of the translation.
getAcceleration() - Method in class org.orekit.frames.Transform
Get the second time derivative of the translation.
getAcceleration() - Method in class org.orekit.utils.FieldPVCoordinates
Gets the acceleration.
getAcceleration() - Method in class org.orekit.utils.PVCoordinates
Gets the acceleration.
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.
getAdditionalEquations() - Method in class org.orekit.propagation.conversion.AbstractPropagatorBuilder
Get the list of additional equations.
getAdditionalState(SpacecraftState) - Method in interface org.orekit.propagation.AdditionalStateProvider
Get the additional state.
getAdditionalState(SpacecraftState) - Method in class org.orekit.propagation.analytical.gnss.ClockCorrectionsProvider
Get the additional state.
getAdditionalState(FieldSpacecraftState<T>) - Method in interface org.orekit.propagation.FieldAdditionalStateProvider
Get the additional state.
getAdditionalState(String) - Method in class org.orekit.propagation.FieldSpacecraftState
Get an additional state.
getAdditionalState(String) - Method in class org.orekit.propagation.SpacecraftState
Get an additional state.
getAdditionalStateDimension() - Method in class org.orekit.propagation.integration.AbstractJacobiansMapper
Compute the length of the one-dimensional additional state array needed.
getAdditionalStateDimension() - Method in class org.orekit.propagation.numerical.JacobiansMapper
Compute the length of the one-dimensional additional state array needed.
getAdditionalStateDimension() - Method in class org.orekit.propagation.semianalytical.dsst.DSSTJacobiansMapper
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.
getADMFile() - Method in class org.orekit.files.ccsds.ADMMetaData
Get the ADM file to which these meta-data belong.
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.BeidouAlmanac
 
getAf0() - Method in class org.orekit.gnss.GalileoAlmanac
 
getAf0() - Method in class org.orekit.gnss.GPSAlmanac
 
getAf0() - Method in class org.orekit.gnss.IRNSSAlmanac
 
getAf0() - Method in class org.orekit.gnss.QZSSAlmanac
 
getAf0() - Method in interface org.orekit.propagation.analytical.gnss.GNSSOrbitalElements
Gets the Zeroth Order Clock Correction.
getAf1() - Method in class org.orekit.gnss.BeidouAlmanac
 
getAf1() - Method in class org.orekit.gnss.GalileoAlmanac
 
getAf1() - Method in class org.orekit.gnss.GPSAlmanac
 
getAf1() - Method in class org.orekit.gnss.IRNSSAlmanac
 
getAf1() - Method in class org.orekit.gnss.QZSSAlmanac
 
getAf1() - Method in interface org.orekit.propagation.analytical.gnss.GNSSOrbitalElements
Gets the First Order Clock Correction.
getAf2() - Method in interface org.orekit.propagation.analytical.gnss.GNSSOrbitalElements
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.
getAGf0() - Method in interface org.orekit.propagation.analytical.gnss.SBASOrbitalElements
Gets the Zeroth Order Clock Correction.
getAGf1() - Method in interface org.orekit.propagation.analytical.gnss.SBASOrbitalElements
Gets the First Order Clock Correction.
getAlignAngle() - Method in class org.orekit.propagation.events.AlignmentDetector
Get the alignment angle (rad).
getAll() - Method in class org.orekit.utils.ImmutableTimeStampedCache
Get all of the data in this cache.
getAllAmbiguityDrivers() - Method in class org.orekit.estimation.measurements.gnss.AmbiguitySolver
Get all the ambiguity parameters drivers.
getAllForceModels() - Method in class org.orekit.propagation.conversion.DSSTPropagatorBuilder
Get the list of all force models.
getAllForceModels() - Method in class org.orekit.propagation.conversion.NumericalPropagatorBuilder
Get the list of all force models.
getAllForceModels() - Method in class org.orekit.propagation.numerical.FieldNumericalPropagator
Get all the force models, perturbing forces and Newtonian attraction included.
getAllForceModels() - Method in class org.orekit.propagation.numerical.NumericalPropagator
Get all the force models, perturbing forces and Newtonian attraction included.
getAllForceModels() - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator
Get all the force models, perturbing forces and Newtonian attraction included.
getAllForceModels() - Method in class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator
Get all the force models, perturbing forces and Newtonian attraction included.
getAlmanacs() - Method in class org.orekit.gnss.SEMParser
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.ionosphere.KlobucharIonoCoefficientsLoader
Returns the alpha coefficients array.
getAlpha(PositionAngle) - Method in class org.orekit.orbits.CircularOrbit
Get the latitude argument.
getAlpha(PositionAngle) - Method in class org.orekit.orbits.FieldCircularOrbit
Get the latitude argument.
getAlpha() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
Get direction cosine α for central body.
getAlpha() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldAuxiliaryElements
Get direction cosine α for central body.
getAlphaDot(PositionAngle) - Method in class org.orekit.orbits.CircularOrbit
Get the latitude argument derivative.
getAlphaDot(PositionAngle) - Method in class org.orekit.orbits.FieldCircularOrbit
Get the latitude argument derivative.
getAlphaE() - Method in class org.orekit.orbits.CircularOrbit
Get the eccentric latitude argument.
getAlphaE() - Method in class org.orekit.orbits.FieldCircularOrbit
Get the eccentric latitude argument.
getAlphaEDot() - Method in class org.orekit.orbits.CircularOrbit
Get the eccentric latitude argument derivative.
getAlphaEDot() - Method in class org.orekit.orbits.FieldCircularOrbit
Get the eccentric latitude argument derivative.
getAlphaM() - Method in class org.orekit.orbits.CircularOrbit
Get the mean latitude argument.
getAlphaM() - Method in class org.orekit.orbits.FieldCircularOrbit
Get the mean latitude argument.
getAlphaMDot() - Method in class org.orekit.orbits.CircularOrbit
Get the mean latitude argument derivative.
getAlphaMDot() - Method in class org.orekit.orbits.FieldCircularOrbit
Get the mean latitude argument derivative.
getAlphaV() - Method in class org.orekit.orbits.CircularOrbit
Get the true latitude argument.
getAlphaV() - Method in class org.orekit.orbits.FieldCircularOrbit
Get the true latitude argument.
getAlphaVDot() - Method in class org.orekit.orbits.CircularOrbit
Get the true latitude argument derivative.
getAlphaVDot() - Method in class org.orekit.orbits.FieldCircularOrbit
Get the true latitude argument derivative.
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.
getAngularCoordinates(AbsoluteDate, double[], boolean, RotationOrder) - Method in enum org.orekit.files.ccsds.AEMAttitudeType
Get the angular coordinates corresponding to the attitude data.
getAngularCoordinates() - Method in class org.orekit.files.ccsds.AEMFile.AttitudeEphemeridesBlock
Get an unmodifiable list of attitude data lines.
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.
getAODC() - Method in interface org.orekit.propagation.analytical.gnss.BeidouOrbitalElements
Gets the Age Of Data Clock (AODC).
getAODE() - Method in interface org.orekit.propagation.analytical.gnss.BeidouOrbitalElements
Gets the Age Of Data Ephemeris (AODE).
getAp(AbsoluteDate) - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherData
Get the Ap geomagnetic indices.
getAp(AbsoluteDate) - Method in class org.orekit.models.earth.atmosphere.data.MarshallSolarActivityFutureEstimation
Get the Ap geomagnetic indices.
getAp(AbsoluteDate) - Method in interface org.orekit.models.earth.atmosphere.NRLMSISE00InputParameters
Get the Ap geomagnetic indices.
getApAvg() - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherDataLoader.LineParameters
Gets the arithmetic average of all eight Ap indices for the current entry.
getApproxPos() - Method in class org.orekit.gnss.RinexHeader
Get the Approximate Marker Position.
getArbitraryEpoch(Field<T>) - Static method in class org.orekit.time.FieldAbsoluteDate
Get an arbitrary date.
getArea() - Method in class org.orekit.forces.BoxAndSolarArraySpacecraft.Facet
Get facet area.
getAstronomicalAmplitudesMap() - Method in class org.orekit.forces.gravity.potential.AstronomicalAmplitudeReader
Get astronomical amplitudes map.
getAtmosphere() - Method in class org.orekit.forces.drag.DragForce
Get the atmospheric model.
getAtmosphere() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTAtmosphericDrag
Get the atmospheric model.
getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in interface org.orekit.attitudes.AttitudeProvider
Compute the attitude corresponding to an orbital state.
getAttitude(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in interface org.orekit.attitudes.AttitudeProvider
Compute the attitude corresponding to an orbital state.
getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.AttitudesSequence
Compute the attitude corresponding to an orbital state.
getAttitude(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.AttitudesSequence
Compute the attitude corresponding to an orbital state.
getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.CelestialBodyPointed
Compute the attitude corresponding to an orbital state.
getAttitude(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.CelestialBodyPointed
Compute the attitude corresponding to an orbital state.
getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.FixedRate
Compute the attitude corresponding to an orbital state.
getAttitude(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.FixedRate
Compute the attitude corresponding to an orbital state.
getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.GroundPointing
Compute the attitude corresponding to an orbital state.
getAttitude(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.GroundPointing
Compute the attitude corresponding to an orbital state.
getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.InertialProvider
Compute the attitude corresponding to an orbital state.
getAttitude(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.InertialProvider
Compute the attitude corresponding to an orbital state.
getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.LofOffset
Compute the attitude corresponding to an orbital state.
getAttitude(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.LofOffset
Compute the attitude corresponding to an orbital state.
getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.LofOffsetPointing
Compute the attitude corresponding to an orbital state.
getAttitude(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.LofOffsetPointing
Compute the attitude corresponding to an orbital state.
getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.SpinStabilized
Compute the attitude corresponding to an orbital state.
getAttitude(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.SpinStabilized
Compute the attitude corresponding to an orbital state.
getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.TabulatedLofOffset
Compute the attitude corresponding to an orbital state.
getAttitude(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.TabulatedLofOffset
Compute the attitude corresponding to an orbital state.
getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.TabulatedProvider
Compute the attitude corresponding to an orbital state.
getAttitude(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.TabulatedProvider
Compute the attitude corresponding to an orbital state.
getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.YawCompensation
Compute the attitude corresponding to an orbital state.
getAttitude(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.YawCompensation
Compute the attitude corresponding to an orbital state.
getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.YawSteering
Compute the attitude corresponding to an orbital state.
getAttitude(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.YawSteering
Compute the attitude corresponding to an orbital state.
getAttitude(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.forces.maneuvers.propulsion.ThrustDirectionAndAttitudeProvider
Compute the attitude corresponding to an orbital state.
getAttitude(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.forces.maneuvers.propulsion.ThrustDirectionAndAttitudeProvider
Compute the attitude corresponding to an orbital state.
getAttitude() - Method in class org.orekit.propagation.FieldSpacecraftState
Get the attitude.
getAttitude() - Method in class org.orekit.propagation.SpacecraftState
Get the attitude.
getAttitudeBlocks() - Method in class org.orekit.files.ccsds.AEMFile
Get the list of attitude ephemerides blocks as an unmodifiable list.
getAttitudeData(TimeStampedAngularCoordinates, boolean, RotationOrder) - Method in enum org.orekit.files.ccsds.AEMAttitudeType
Get the attitude data corresponding to the attitude type.
getAttitudeDataLines() - Method in class org.orekit.files.ccsds.AEMFile.AttitudeEphemeridesBlock
Get the list of attitude data lines.
getAttitudeDataLinesComment() - Method in class org.orekit.files.ccsds.AEMFile.AttitudeEphemeridesBlock
Get the attitude data lines comment.
getAttitudeDirection() - Method in class org.orekit.files.ccsds.AEMFile.AttitudeEphemeridesBlock
Get the rotation direction of the attitude.
getAttitudeFromFrame(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.forces.maneuvers.propulsion.ThrustDirectionAndAttitudeProvider
Compute the attitude for DIRECTION_IN_FRAME or DIRECTION_IN_LOF types.
getAttitudeOverride() - Method in class org.orekit.forces.maneuvers.ImpulseManeuver
Get the Attitude Provider to use during maneuver.
getAttitudeOverride() - Method in class org.orekit.forces.maneuvers.Maneuver
Get the attitude override used for the maneuver.
getAttitudeProvider() - Method in class org.orekit.propagation.AbstractPropagator
Get attitude provider.
getAttitudeProvider() - Method in class org.orekit.propagation.conversion.AbstractPropagatorBuilder
Get the attitude provider.
getAttitudeProvider() - Method in class org.orekit.propagation.FieldAbstractPropagator
Get attitude provider.
getAttitudeProvider() - Method in interface org.orekit.propagation.FieldPropagator
Get attitude provider.
getAttitudeProvider() - Method in class org.orekit.propagation.integration.FieldStateMapper
Get the attitude provider.
getAttitudeProvider() - Method in class org.orekit.propagation.integration.StateMapper
Get the attitude provider.
getAttitudeProvider() - Method in interface org.orekit.propagation.Propagator
Get attitude provider.
getAttitudeQuaternionDirection() - Method in class org.orekit.files.ccsds.APMFile
Get the rotation direction of the attitude quaternion.
getAttitudeType(String) - Static method in enum org.orekit.files.ccsds.AEMAttitudeType
Get the attitude type corresponding to the given name.
getAttitudeType() - Method in class org.orekit.files.ccsds.AEMFile.AttitudeEphemeridesBlock
Get the format of the data lines in the message.
getAugmentedInitialState(SpacecraftState, AdditionalEquations) - Method in class org.orekit.propagation.numerical.cr3bp.CR3BPMultipleShooter
Compute the additional state from the additionalEquations.
getAugmentedInitialState(SpacecraftState, AdditionalEquations) - Method in class org.orekit.utils.AbstractMultipleShooting
Compute the additional state from the additionalEquations.
getAugmentedInitialState(SpacecraftState, AdditionalEquations) - Method in class org.orekit.utils.MultipleShooter
Compute the additional state from the additionalEquations.
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
 
getAverageFlux(AbsoluteDate) - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherData
Get the value of the 81 day average of F10.7 solar flux centered on current day.
getAverageFlux(AbsoluteDate) - Method in class org.orekit.models.earth.atmosphere.data.MarshallSolarActivityFutureEstimation
Get the value of the 81 day average of F10.7 solar flux centered on current day.
getAverageFlux(AbsoluteDate) - Method in interface org.orekit.models.earth.atmosphere.NRLMSISE00InputParameters
Get the value of the 81 day average of F10.7 solar flux centered on current day.
getAzimuth(Vector3D, Frame, AbsoluteDate) - Method in class org.orekit.frames.TopocentricFrame
Get the azimuth of a point with regards to the topocentric frame center point.
getAzimuth(FieldVector3D<T>, Frame, FieldAbsoluteDate<T>) - Method in class org.orekit.frames.TopocentricFrame
Get the azimuth of a point with regards to the topocentric frame center point.
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).
getB() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldAuxiliaryElements
Get B = sqrt(1 - e²).
getBaseFrame() - Method in class org.orekit.estimation.measurements.GroundStation
Get the base frame associated with the station.
getBaseName(T) - Method in class org.orekit.data.AbstractListCrawler
Get the base name of an input.
getBaseName(File) - Method in class org.orekit.data.FilesListCrawler
Get the base name of an input.
getBaseName(URL) - Method in class org.orekit.data.NetworkCrawler
Get the base name of an input.
getBaseState(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.YawCompensation
Compute the base system state at given date, without compensation.
getBaseState(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.YawCompensation
Compute the base system state at given date, without compensation.
getBaseState(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.YawSteering
Compute the base system state at given date, without compensation.
getBaseState(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.YawSteering
Compute the base system state at given date, without compensation.
getBaseWeight() - Method in class org.orekit.estimation.measurements.AbstractMeasurement
Get the base weight associated with the measurement
getBaseWeight() - Method in class org.orekit.estimation.measurements.generation.AbstractMeasurementBuilder
Get the base weight associated with the measurement
getBaseWeight() - Method in interface org.orekit.estimation.measurements.ObservedMeasurement
Get the base weight associated with the measurement
getBasicDimension() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
Get state vector dimension without additional parameters.
getBasicDimension() - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator
Get state vector dimension without additional parameters.
getBDT() - Method in class org.orekit.time.LazyLoadedTimeScales
 
getBDT() - Method in interface org.orekit.time.TimeScales
Get the BeiDou Navigation Satellite System time scale.
getBDT() - Static method in class org.orekit.time.TimeScalesFactory
Get the BeiDou Navigation Satellite System time scale.
getBeacon() - Method in class org.orekit.propagation.events.AngularSeparationDetector
Get the beacon at the center of the proximity zone.
getBefore() - Method in class org.orekit.utils.FieldTimeSpanMap.Transition
Get the entry valid before transition.
getBefore() - Method in class org.orekit.utils.TimeSpanMap.Transition
Get the entry valid before transition.
getBeginDate(Frequency) - Method in class org.orekit.estimation.measurements.gnss.CycleSlipDetectorResults
Return the date of validity beginning of the detector.
getBeidouEpoch() - Method in class org.orekit.time.AbstractTimeScales
 
getBeidouEpoch() - Method in interface org.orekit.time.TimeScales
Reference epoch for BeiDou weeks: 2006-01-01T00:00:00 UTC.
getBeidouOrbitalElements() - Method in class org.orekit.propagation.analytical.gnss.BeidouPropagator
Get the underlying Beidou orbital elements.
getBeta() - Method in class org.orekit.models.earth.ionosphere.KlobucharIonoCoefficientsLoader
Returns the beta coefficients array.
getBeta() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
Get direction cosine β for central body.
getBeta() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldAuxiliaryElements
Get direction cosine β for central body.
getBGD() - Method in interface org.orekit.propagation.analytical.gnss.GalileoOrbitalElements
Gets the estimated broadcast group delay differential.
getBGDE1E5a() - Method in interface org.orekit.propagation.analytical.gnss.GalileoOrbitalElements
Gets the E1/E5a broadcast group delay.
getBGDE5bE1() - Method in interface org.orekit.propagation.analytical.gnss.GalileoOrbitalElements
Gets the Broadcast Group Delay E5b/E1.
getBody(String) - Method in interface org.orekit.bodies.CelestialBodies
Get a celestial body.
getBody(String) - Static method in class org.orekit.bodies.CelestialBodyFactory
Get a celestial body.
getBody(String) - Method in class org.orekit.bodies.LazyLoadedCelestialBodies
Get a celestial body.
getBody() - Method in class org.orekit.propagation.events.FieldLatitudeCrossingDetector
Get the body on which the geographic zone is defined.
getBody() - Method in class org.orekit.propagation.events.FootprintOverlapDetector
Get the body on which the geographic zone is defined.
getBody() - Method in class org.orekit.propagation.events.GeographicZoneDetector
Get the body on which the geographic zone is defined.
getBody() - Method in class org.orekit.propagation.events.LatitudeCrossingDetector
Get the body on which the geographic zone is defined.
getBody() - Method in class org.orekit.propagation.events.LatitudeExtremumDetector
Get the body on which the geographic zone is defined.
getBody() - Method in class org.orekit.propagation.events.LongitudeCrossingDetector
Get the body on which the geographic zone is defined.
getBody() - Method in class org.orekit.propagation.events.LongitudeExtremumDetector
Get the body on which the geographic zone is defined.
getBody() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBody
Get third body.
getBodyFrame() - Method in class org.orekit.attitudes.GroundPointing
Get the body frame.
getBodyFrame() - Method in interface org.orekit.bodies.BodyShape
Get body frame related to body shape.
getBodyFrame() - Method in class org.orekit.bodies.OneAxisEllipsoid
Get body frame related to body shape.
getBodyFrame() - Method in class org.orekit.models.earth.Geoid
 
getBodyOrientedFrame() - Method in interface org.orekit.bodies.CelestialBody
Get a body oriented, body centered frame.
getBodyShape() - Method in class org.orekit.propagation.events.AltitudeDetector
Get the body shape.
getBodyShape() - Method in class org.orekit.propagation.events.FieldAltitudeDetector
Get the body shape.
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.
getC() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldAuxiliaryElements
Get C = 1 + p² + q².
getC2n0(int) - Method in class org.orekit.models.earth.ReferenceEllipsoid
Get the fully normalized coefficient C2n,0 for the normal gravity potential.
getCacheSlotsNumber() - Static method in class org.orekit.utils.OrekitConfiguration
Get the number of slots to use in caches.
getCalendarWeek() - Method in class org.orekit.time.DateComponents
Get the calendar week number.
getCalls() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
Get the number of calls to the differential equations computation method.
getCalls() - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator
Get the number of calls to the differential equations computation method.
getCapitalizedAbbreviation() - Method in enum org.orekit.time.Month
Get the capitalized three letters abbreviation.
getCapitalizedName() - Method in enum org.orekit.time.Month
Get the capitalized full name.
getCartesian() - Method in class org.orekit.frames.FieldTransform
Get the underlying elementary Cartesian part.
getCartesian() - Method in class org.orekit.frames.Transform
Get the underlying elementary Cartesian part.
getCartesianIntersectionPoint(Line, Vector3D, Frame, AbsoluteDate) - Method in class org.orekit.bodies.OneAxisEllipsoid
Get the intersection point of a line with the surface of the body.
getCartesianIntersectionPoint(FieldLine<T>, FieldVector3D<T>, Frame, FieldAbsoluteDate<T>) - Method in class org.orekit.bodies.OneAxisEllipsoid
Get the intersection point of a line with the surface of the body.
getCcsdsEpoch() - Method in class org.orekit.time.AbstractTimeScales
 
getCCSDSEpoch(Field<T>) - Static method in class org.orekit.time.FieldAbsoluteDate
Reference epoch for CCSDS Time Code Format (CCSDS 301.0-B-4):
getCcsdsEpoch() - Method in interface org.orekit.time.TimeScales
Reference epoch for CCSDS Time Code Format (CCSDS 301.0-B-4): 1958-01-01T00:00:00 International Atomic Time (not UTC).
getCelestialBodies() - Static method in class org.orekit.bodies.CelestialBodyFactory
Get the instance of CelestialBodies that is called by the static methods in this class.
getCelestialBodies() - Method in class org.orekit.data.CompositeDataContext
 
getCelestialBodies() - Method in interface org.orekit.data.DataContext
Get a factory constructing CelestialBodys based on the auxiliary data in this context.
getCelestialBodies() - Method in class org.orekit.data.ExceptionalDataContext
 
getCelestialBodies() - Method in class org.orekit.data.LazyLoadedDataContext
 
getCelestialBody() - Method in enum org.orekit.files.ccsds.CenterName
Get the celestial body corresponding to the CCSDS constant.
getCelestialBody(CelestialBodies) - 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.geometry.fov.SmoothFieldOfView
Get the direction of the FOV center, in spacecraft frame.
getCenter() - Method in class org.orekit.models.earth.tessellation.Tile
Get the center point.
getCenter() - Method in class org.orekit.propagation.events.CircularFieldOfViewDetector
Deprecated.
Get the direction of FOV center.
getCenterBody() - Method in class org.orekit.files.ccsds.ADMMetaData
Get the CelestialBody corresponding to the center name.
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.ADMMetaData
Get the origin of reference frame.
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.BeidouAlmanac
 
getCic() - Method in class org.orekit.gnss.GalileoAlmanac
 
getCic() - Method in class org.orekit.gnss.GPSAlmanac
 
getCic() - Method in class org.orekit.gnss.IRNSSAlmanac
 
getCic() - Method in class org.orekit.gnss.QZSSAlmanac
 
getCic() - Method in interface org.orekit.propagation.analytical.gnss.GNSSOrbitalElements
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) - Method in class org.orekit.frames.AbstractFrames
 
getCIRF(IERSConventions, boolean) - Method in interface org.orekit.frames.Frames
Get the CIRF2000 reference frame.
getCIRF(IERSConventions, boolean) - Static method in class org.orekit.frames.FramesFactory
Get the CIRF2000 reference frame.
getCis() - Method in class org.orekit.gnss.BeidouAlmanac
 
getCis() - Method in class org.orekit.gnss.GalileoAlmanac
 
getCis() - Method in class org.orekit.gnss.GPSAlmanac
 
getCis() - Method in class org.orekit.gnss.IRNSSAlmanac
 
getCis() - Method in class org.orekit.gnss.QZSSAlmanac
 
getCis() - Method in interface org.orekit.propagation.analytical.gnss.GNSSOrbitalElements
Gets the Amplitude of the Sine Harmonic Correction Term to the Angle of Inclination.
getCj(int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.CjSjCoefficient
Get the Cj coefficient.
getCj(int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldCjSjCoefficient
Get the Cj coefficient.
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.
getCoefficients() - Method in enum org.orekit.forces.gravity.potential.OceanLoadDeformationCoefficients
Get the load deformation coefficients for ocean tides.
getCoefficients(String) - Method in class org.orekit.models.earth.displacement.OceanLoadingCoefficientsBLQFactory
Get the coefficients for a given site.
getCoefficients(FieldAbsoluteDate<T>, Set<String>) - Method in interface org.orekit.propagation.semianalytical.dsst.forces.FieldShortPeriodTerms
Computes the coefficients involved in the contributions.
getCoefficients(AbsoluteDate, Set<String>) - Method in interface org.orekit.propagation.semianalytical.dsst.forces.ShortPeriodTerms
Computes the coefficients involved in the contributions.
getCoefficientsKeyPrefix() - Method in interface org.orekit.propagation.semianalytical.dsst.forces.FieldShortPeriodTerms
Get the prefix for short period coefficients keys.
getCoefficientsKeyPrefix() - Method in interface org.orekit.propagation.semianalytical.dsst.forces.ShortPeriodTerms
Get the prefix for short period coefficients keys.
getCombinationType() - Method in class org.orekit.gnss.CombinedObservationData
Get the type of the combination of measurements used to build the instance.
getCombinedFrequency(Frequency, Frequency) - Method in class org.orekit.estimation.measurements.gnss.AbstractDualFrequencyCombination
Get the combined frequency of two measurements.
getCombinedFrequency(Frequency, Frequency) - Method in class org.orekit.estimation.measurements.gnss.GeometryFreeCombination
Get the combined frequency of two measurements.
getCombinedFrequency(Frequency, Frequency) - Method in class org.orekit.estimation.measurements.gnss.IonosphereFreeCombination
Get the combined frequency of two measurements.
getCombinedFrequency(Frequency, Frequency) - Method in class org.orekit.estimation.measurements.gnss.NarrowLaneCombination
Get the combined frequency of two measurements.
getCombinedFrequency(Frequency, Frequency) - Method in class org.orekit.estimation.measurements.gnss.WideLaneCombination
Get the combined frequency of two measurements.
getCombinedMHzFrequency() - Method in class org.orekit.gnss.CombinedObservationData
Get the value of the combined frequency in MHz.
getCombinedProvider(TransformProvider, TransformProvider) - Static method in class org.orekit.frames.TransformProviderUtils
Combine two transform providers.
getCombinedValue(double, Frequency, double, Frequency) - Method in class org.orekit.estimation.measurements.gnss.AbstractDualFrequencyCombination
Get the combined observed value of two measurements.
getCombinedValue(double, double) - Method in class org.orekit.estimation.measurements.gnss.AbstractSingleFrequencyCombination
Get the combined observed value of two measurements.
getCombinedValue(double, Frequency, double, Frequency) - Method in class org.orekit.estimation.measurements.gnss.GeometryFreeCombination
Get the combined observed value of two measurements.
getCombinedValue(double, double) - Method in class org.orekit.estimation.measurements.gnss.GRAPHICCombination
Get the combined observed value of two measurements.
getCombinedValue(double, Frequency, double, Frequency) - Method in class org.orekit.estimation.measurements.gnss.IonosphereFreeCombination
Get the combined observed value of two measurements.
getCombinedValue(double, Frequency, double, Frequency) - Method in class org.orekit.estimation.measurements.gnss.NarrowLaneCombination
Get the combined observed value of two measurements.
getCombinedValue(double, double) - Method in class org.orekit.estimation.measurements.gnss.PhaseMinusCodeCombination
Get the combined observed value of two measurements.
getCombinedValue(double, Frequency, double, Frequency) - Method in class org.orekit.estimation.measurements.gnss.WideLaneCombination
Get the combined observed value of two measurements.
getComment() - Method in class org.orekit.files.ccsds.ADMMetaData
Get the meta-data comment.
getComment() - Method in class org.orekit.files.ccsds.APMFile.APMManeuver
Get the maneuvers data comment, each string in the list corresponds to one line of comment.
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.
getCompleteName(T) - Method in class org.orekit.data.AbstractListCrawler
Get the complete name of a input.
getCompleteName(File) - Method in class org.orekit.data.FilesListCrawler
Get the complete name of a input.
getCompleteName(URL) - Method in class org.orekit.data.NetworkCrawler
Get the complete name of a input.
getComponents(TimeScale) - Method in class org.orekit.time.AbsoluteDate
Split the instance into date/time components.
getComponents(int) - Method in class org.orekit.time.AbsoluteDate
Split the instance into date/time components for a local time.
getComponents(int, TimeScale) - Method in class org.orekit.time.AbsoluteDate
Split the instance into date/time components for a local time.
getComponents(TimeZone) - Method in class org.orekit.time.AbsoluteDate
Split the instance into date/time components for a time zone.
getComponents(TimeZone, TimeScale) - Method in class org.orekit.time.AbsoluteDate
Split the instance into date/time components for a time zone.
getComponents(TimeScale) - Method in class org.orekit.time.FieldAbsoluteDate
Split the instance into date/time components.
getComponents(int) - Method in class org.orekit.time.FieldAbsoluteDate
Split the instance into date/time components for a local time.
getComponents(int, TimeScale) - Method in class org.orekit.time.FieldAbsoluteDate
Split the instance into date/time components for a local time.
getComponents(TimeZone) - Method in class org.orekit.time.FieldAbsoluteDate
Split the instance into date/time components for a time zone.
getComponents(TimeZone, TimeScale) - Method in class org.orekit.time.FieldAbsoluteDate
Split the instance into date/time components for a time zone.
getConfiguration(String, int) - Method in class org.orekit.frames.ITRFVersionLoader
 
getConfiguration(String, int) - Method in interface org.orekit.frames.ItrfVersionProvider
Get the ITRF version configuration defined by a given file at specified date.
getConstantNormalizedProvider(int, int) - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory
Get the constant gravity field coefficients provider from the first supported file.
getConstantNormalizedProvider(int, int) - Method in interface org.orekit.forces.gravity.potential.GravityFields
Get a constant gravity field normalized coefficients provider.
getConstantNormalizedProvider(int, int) - Method in class org.orekit.forces.gravity.potential.LazyLoadedGravityFields
Get a constant gravity field normalized coefficients provider.
getConstantProvider(boolean, int, int) - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
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.
getConstantUnnormalizedProvider(int, int) - Method in interface org.orekit.forces.gravity.potential.GravityFields
Get a constant gravity field unnormalized coefficients provider.
getConstantUnnormalizedProvider(int, int) - Method in class org.orekit.forces.gravity.potential.LazyLoadedGravityFields
Get a constant gravity field unnormalized coefficients provider.
getConstraintsMap() - Method in class org.orekit.utils.AbstractMultipleShooting
Get the map of patch points components which are constrained.
getConventions() - Method in class org.orekit.files.ccsds.ADMParser
Get IERS conventions.
getConventions() - Method in class org.orekit.files.ccsds.NDMFile
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.
getConversionJacobian(SpacecraftState) - Method in class org.orekit.propagation.integration.AbstractJacobiansMapper
Get the conversion Jacobian between state parameters and parameters used for derivatives.
getConversionJacobian(SpacecraftState) - Method in class org.orekit.propagation.numerical.AbsoluteJacobiansMapper
Get the conversion Jacobian between state parameters and parameters used for derivatives.
getConversionJacobian(SpacecraftState) - Method in class org.orekit.propagation.numerical.JacobiansMapper
Get the conversion Jacobian between state parameters and parameters used for derivatives.
getConversionJacobian(SpacecraftState) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTJacobiansMapper
Get the conversion Jacobian between state parameters and parameters used for derivatives.
getConverter(ITRFVersion, ITRFVersion) - Static method in enum org.orekit.frames.ITRFVersion
Find a converter between specified ITRF frames.
getConverter(ITRFVersion, ITRFVersion, TimeScale) - Static method in enum org.orekit.frames.ITRFVersion
Find a converter between specified ITRF frames.
getCoordinates(SpacecraftState, int, DSFactory) - Static method in class org.orekit.estimation.measurements.AbstractMeasurement
getCoordinates(SpacecraftState, int, int) - Static method in class org.orekit.estimation.measurements.AbstractMeasurement
Get Cartesian coordinates as derivatives.
getCoordinates() - Method in class org.orekit.files.ccsds.OEMFile.EphemeridesBlock
 
getCoordinates() - Method in interface org.orekit.files.general.EphemerisFile.EphemerisSegment
Get the coordinates for this ephemeris segment in EphemerisFile.EphemerisSegment.getFrame().
getCoordinates() - Method in class org.orekit.files.general.OrekitEphemerisFile.OrekitEphemerisSegment
 
getCoordinates() - Method in class org.orekit.files.sp3.SP3File.SP3Ephemeris
 
getCoordinateSystem() - Method in class org.orekit.files.sp3.SP3File
Returns the coordinate system of the entries in this orbit file.
getCorrectedMeasurement() - Method in class org.orekit.estimation.sequential.DSSTKalmanModel
Get the estimated measurement.
getCorrectedMeasurement() - Method in interface org.orekit.estimation.sequential.KalmanEstimation
Get the estimated measurement.
getCorrectedMeasurement() - Method in class org.orekit.estimation.sequential.KalmanModel
Get the estimated measurement.
getCorrectedSpacecraftStates() - Method in class org.orekit.estimation.sequential.DSSTKalmanModel
Get the corrected spacecraft states.
getCorrectedSpacecraftStates() - Method in interface org.orekit.estimation.sequential.KalmanEstimation
Get the corrected spacecraft states.
getCorrectedSpacecraftStates() - Method in class org.orekit.estimation.sequential.KalmanModel
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.
getCr3bpSystem() - Method in class org.orekit.orbits.RichardsonExpansion
Get the considered CR3BP system.
getCrc() - Method in class org.orekit.gnss.BeidouAlmanac
 
getCrc() - Method in class org.orekit.gnss.GalileoAlmanac
 
getCrc() - Method in class org.orekit.gnss.GPSAlmanac
 
getCrc() - Method in class org.orekit.gnss.IRNSSAlmanac
 
getCrc() - Method in class org.orekit.gnss.QZSSAlmanac
 
getCrc() - Method in interface org.orekit.propagation.analytical.gnss.GNSSOrbitalElements
Gets the Amplitude of the Cosine Harmonic Correction Term to the Orbit Radius.
getCreationDate() - Method in class org.orekit.files.ccsds.NDMFile
Get the file creation date and time in UTC.
getCrs() - Method in class org.orekit.gnss.BeidouAlmanac
 
getCrs() - Method in class org.orekit.gnss.GalileoAlmanac
 
getCrs() - Method in class org.orekit.gnss.GPSAlmanac
 
getCrs() - Method in class org.orekit.gnss.IRNSSAlmanac
 
getCrs() - Method in class org.orekit.gnss.QZSSAlmanac
 
getCrs() - Method in interface org.orekit.propagation.analytical.gnss.GNSSOrbitalElements
Gets the Amplitude of the Sine Harmonic Correction Term to the Orbit Radius.
getCtr81Adj() - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherDataLoader.LineParameters
Gets the centered 81-day arithmetic average of F10.7 (adjusted).
getCtr81Obs() - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherDataLoader.LineParameters
Gets the centered 81-day arithmetic average of F10.7 (observed).
getCuc() - Method in class org.orekit.gnss.BeidouAlmanac
 
getCuc() - Method in class org.orekit.gnss.GalileoAlmanac
 
getCuc() - Method in class org.orekit.gnss.GPSAlmanac
 
getCuc() - Method in class org.orekit.gnss.IRNSSAlmanac
 
getCuc() - Method in class org.orekit.gnss.QZSSAlmanac
 
getCuc() - Method in interface org.orekit.propagation.analytical.gnss.GNSSOrbitalElements
Gets the Amplitude of the Cosine Harmonic Correction Term to the Argument of Latitude.
getCurrentDate() - Method in class org.orekit.estimation.sequential.DSSTKalmanModel
Get the current date.
getCurrentDate() - Method in interface org.orekit.estimation.sequential.KalmanEstimation
Get the current date.
getCurrentDate() - Method in class org.orekit.estimation.sequential.KalmanEstimator
Get the current date.
getCurrentDate() - Method in class org.orekit.estimation.sequential.KalmanModel
Get the current date.
getCurrentMeasurementNumber() - Method in class org.orekit.estimation.sequential.DSSTKalmanModel
Get the current measurement number.
getCurrentMeasurementNumber() - Method in interface org.orekit.estimation.sequential.KalmanEstimation
Get the current measurement number.
getCurrentMeasurementNumber() - Method in class org.orekit.estimation.sequential.KalmanEstimator
Get the current measurement number.
getCurrentMeasurementNumber() - Method in class org.orekit.estimation.sequential.KalmanModel
Get the current measurement number.
getCurrentState() - Method in interface org.orekit.propagation.sampling.FieldOrekitStepInterpolator
Get the state at previous grid point date.
getCurrentState() - Method in interface org.orekit.propagation.sampling.OrekitStepInterpolator
Get the state at current grid point date.
getCus() - Method in class org.orekit.gnss.BeidouAlmanac
 
getCus() - Method in class org.orekit.gnss.GalileoAlmanac
 
getCus() - Method in class org.orekit.gnss.GPSAlmanac
 
getCus() - Method in class org.orekit.gnss.IRNSSAlmanac
 
getCus() - Method in class org.orekit.gnss.QZSSAlmanac
 
getCus() - Method in interface org.orekit.propagation.analytical.gnss.GNSSOrbitalElements
Gets the Amplitude of the Sine Harmonic Correction Term to the Argument of Latitude.
getCycleSlipMap() - Method in class org.orekit.estimation.measurements.gnss.CycleSlipDetectorResults
Get the cycle slip Map with contains the results.
getD() - Method in class org.orekit.data.DelaunayArguments
Get the mean elongation of the Moon from the Sun.
getD() - Method in class org.orekit.data.FieldDelaunayArguments
Get the mean elongation of the Moon from the Sun.
getDailyFlux(AbsoluteDate) - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherData
Get the value of the daily F10.7 solar flux for previous day.
getDailyFlux(AbsoluteDate) - Method in class org.orekit.models.earth.atmosphere.data.MarshallSolarActivityFutureEstimation
Get the value of the daily F10.7 solar flux for previous day.
getDailyFlux(AbsoluteDate) - Method in interface org.orekit.models.earth.atmosphere.NRLMSISE00InputParameters
Get the value of the daily F10.7 solar flux for previous day.
getData() - Method in class org.orekit.utils.TimeSpanMap.Span
Get the data valid during this time span.
getDataContext() - Method in class org.orekit.files.ccsds.ADMParser
Get the data context used for getting frames, time scales, and celestial bodies.
getDataContext() - Method in class org.orekit.files.ccsds.NDMFile
Get the data context.
getDataContext() - Method in class org.orekit.files.ccsds.ODMParser
Get the data context used for getting frames, time scales, and celestial bodies.
getDataContext() - Method in class org.orekit.files.ccsds.TDMParser
Get the data context.
getDataProvidersManager() - Method in class org.orekit.data.AbstractSelfFeedingLoader
Get the data provider manager.
getDataProvidersManager() - Method in class org.orekit.data.LazyLoadedDataContext
Get the provider of auxiliary data for this data context.
getDataProvidersManager() - Method in class org.orekit.frames.LazyLoadedEop
Get the data providers manager for this instance.
getDataQuality() - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData
Getter for the dataQuality.
getDataSet() - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherDataLoader
Getter for the data set.
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.BeidouAlmanac
 
getDate() - Method in class org.orekit.gnss.CombinedObservationDataSet
Get the date.
getDate() - Method in class org.orekit.gnss.DOP
Gets the calculation date of the DOP.
getDate() - Method in class org.orekit.gnss.GalileoAlmanac
 
getDate() - Method in class org.orekit.gnss.GLONASSAlmanac
 
getDate() - Method in class org.orekit.gnss.GLONASSEphemeris
 
getDate() - Method in class org.orekit.gnss.GPSAlmanac
 
getDate() - Method in class org.orekit.gnss.IRNSSAlmanac
 
getDate() - Method in class org.orekit.gnss.ObservationDataSet
Get the date.
getDate() - Method in class org.orekit.gnss.QZSSAlmanac
 
getDate() - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherDataLoader.LineParameters
 
getDate() - Method in class org.orekit.orbits.FieldOrbit
Get the date of orbital parameters.
getDate() - Method in class org.orekit.orbits.Orbit
Get the date of orbital parameters.
getDate() - Method in class org.orekit.propagation.analytical.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.semianalytical.dsst.utilities.FieldAuxiliaryElements
Get the date of the orbit.
getDate() - Method in class org.orekit.propagation.SpacecraftState
Get the date.
getDate() - Method in class org.orekit.time.AbsoluteDate
Get the date.
getDate() - Method in class org.orekit.time.DateTimeComponents
Get the date component.
getDate() - Method in class org.orekit.time.FieldAbsoluteDate
Get the date.
getDate() - Method in interface org.orekit.time.FieldTimeStamped
Get the date.
getDate() - Method in class org.orekit.time.GLONASSDate
 
getDate() - Method in class org.orekit.time.GNSSDate
Get the date.
getDate() - Method in interface org.orekit.time.TimeStamped
Get the date.
getDate() - Method in class org.orekit.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.
getDayNumber() - Method in class org.orekit.time.GLONASSDate
Get the number of the current day in a four year interval.
getDayOfWeek() - Method in class org.orekit.time.DateComponents
Get the day of week.
getDayOfYear() - Method in class org.orekit.time.DateComponents
Get the day number in year.
getDcjDh(int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.CjSjCoefficient
Get the dCj / dh coefficient.
getDcjDh(int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldCjSjCoefficient
Get the dCj / dh coefficient.
getDcjDk(int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.CjSjCoefficient
Get the dCj / dk coefficient.
getDcjDk(int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldCjSjCoefficient
Get the dCj / dk coefficient.
getDdEps() - Method in class org.orekit.frames.EOPEntry
Get the correction for nutation in obliquity δΔε.
getDdim() - Method in class org.orekit.bodies.CR3BPSystem
Get the CR3BP distance between the two bodies.
getDDot() - Method in class org.orekit.data.DelaunayArguments
Get the mean elongation of the Moon from the Sun time derivative.
getDDot() - Method in class org.orekit.data.FieldDelaunayArguments
Get the mean elongation of the Moon from the Sun time derivative.
getDdPsi() - Method in class org.orekit.frames.EOPEntry
Get the correction for nutation in longitude δΔΨ.
getDecimalYear(int, int, int) - Static method in class org.orekit.models.earth.GeoMagneticField
Utility function to get a decimal year for a given day.
getDeclination() - Method in class org.orekit.models.earth.GeoMagneticElements
Returns the declination of the magnetic field in radians.
getDecorrelatedReference() - Method in class org.orekit.estimation.measurements.gnss.AbstractLambdaMethod
Get the reference decorrelated ambiguities.
getDecreasingTimeShift() - Method in class org.orekit.propagation.events.EventShifter
Get the decreasing events time shift.
getDefault() - Static method in interface org.orekit.data.DataContext
Get the default data context that is used to implement the static factories (TimeScalesFactory, FramesFactory, etc) and loaders that feed themselves (e.g.
getDefaultLaw(Frames) - Static method in interface org.orekit.propagation.Propagator
Get a default law using the given frames.
getDefaultModel() - Static method in class org.orekit.models.earth.troposphere.FixedTroposphericDelay
Returns the default model, loading delay values from the file "tropospheric-delay.txt" via the default data context.
getDefaultYawRate(int) - Static method in class org.orekit.gnss.attitude.GPSBlockIIA
Get the default yaw rate for a satellite.
getDelaunayMultipliers() - Method in class org.orekit.models.earth.displacement.Tide
Get the multipliers for Delaunay arguments (l, l', F, D, Ω).
getDeltaI() - Method in class org.orekit.gnss.GLONASSAlmanac
 
getDeltaI() - Method in interface org.orekit.propagation.analytical.gnss.GLONASSOrbitalElements
Get the correction to the mean value of inlination.
getDeltaMass() - Method in class org.orekit.files.ccsds.OPMFile.Maneuver
Get mass change during maneuver (value is < 0).
getDeltaT() - Method in class org.orekit.gnss.GLONASSAlmanac
 
getDeltaT() - Method in interface org.orekit.propagation.analytical.gnss.GLONASSOrbitalElements
Get the correction to the mean value of Draconian period.
getDeltaTDot() - Method in class org.orekit.gnss.GLONASSAlmanac
 
getDeltaTDot() - Method in interface org.orekit.propagation.analytical.gnss.GLONASSOrbitalElements
Get the rate of change of Draconian period.
getDeltaVSat() - Method in class org.orekit.forces.maneuvers.ImpulseManeuver
Get the velocity increment in satellite frame.
getDensity(AbsoluteDate, Vector3D, Frame) - Method in interface org.orekit.models.earth.atmosphere.Atmosphere
Get the local density.
getDensity(FieldAbsoluteDate<T>, FieldVector3D<T>, Frame) - Method in interface org.orekit.models.earth.atmosphere.Atmosphere
Get the local density.
getDensity(int, double, double, double, double, double, double, double, double) - Method in class org.orekit.models.earth.atmosphere.DTM2000
Get the local density with initial entries.
getDensity(int, T, T, T, T, double, double, double, double) - Method in class org.orekit.models.earth.atmosphere.DTM2000
Get the local density with initial entries.
getDensity(AbsoluteDate, Vector3D, Frame) - Method in class org.orekit.models.earth.atmosphere.DTM2000
Get the local density.
getDensity(FieldAbsoluteDate<T>, FieldVector3D<T>, Frame) - Method in class org.orekit.models.earth.atmosphere.DTM2000
Get the local density.
getDensity(Vector3D, Vector3D) - Method in class org.orekit.models.earth.atmosphere.HarrisPriester
Get the local density.
getDensity(Vector3D, FieldVector3D<T>) - Method in class org.orekit.models.earth.atmosphere.HarrisPriester
Get the local density.
getDensity(AbsoluteDate, Vector3D, Frame) - Method in class org.orekit.models.earth.atmosphere.HarrisPriester
Get the local density at some position.
getDensity(FieldAbsoluteDate<T>, FieldVector3D<T>, Frame) - Method in class org.orekit.models.earth.atmosphere.HarrisPriester
Get the local density at some position.
getDensity(double, double, double, double, double, double, double, double, double, double, double, double, double, double, double) - Method in class org.orekit.models.earth.atmosphere.JB2008
Get the local density with initial entries.
getDensity(T, T, T, T, T, T, double, double, double, double, double, double, double, double, double) - Method in class org.orekit.models.earth.atmosphere.JB2008
Get the local density with initial entries.
getDensity(AbsoluteDate, Vector3D, Frame) - Method in class org.orekit.models.earth.atmosphere.JB2008
Get the local density.
getDensity(FieldAbsoluteDate<T>, FieldVector3D<T>, Frame) - Method in class org.orekit.models.earth.atmosphere.JB2008
Get the local density.
getDensity(int) - Method in class org.orekit.models.earth.atmosphere.NRLMSISE00.FieldOutput
Get one of the stored densities.
getDensity(AbsoluteDate, Vector3D, Frame) - Method in class org.orekit.models.earth.atmosphere.NRLMSISE00
Get the local density.
getDensity(FieldAbsoluteDate<T>, FieldVector3D<T>, Frame) - Method in class org.orekit.models.earth.atmosphere.NRLMSISE00
Get the local density.
getDensity(AbsoluteDate, Vector3D, Frame) - Method in class org.orekit.models.earth.atmosphere.SimpleExponentialAtmosphere
Get the local density.
getDensity(FieldAbsoluteDate<T>, FieldVector3D<T>, Frame) - Method in class org.orekit.models.earth.atmosphere.SimpleExponentialAtmosphere
 
getDepth() - Method in class org.orekit.frames.Frame
Get the depth of the frame.
getDerivative(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGammaMnsFunction
Get Γ function derivative.
getDerivative(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GammaMnsFunction
Get Γ function derivative.
getDerivative(int, T) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.FieldHansenTesseralLinear
Compute the value of the derivative dKj-n-1, s / de².
getDerivative(int, T) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.FieldHansenThirdBodyLinear
Compute the value of the Hansen coefficient dK₀n, s / dΧ.
getDerivative(int, T) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.FieldHansenZonalLinear
Get the dK₀-n-1,s / dΧ coefficient derivative.
getDerivative(int, double) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenTesseralLinear
Compute the value of the derivative dKj-n-1, s / de².
getDerivative(int, double) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenThirdBodyLinear
Compute the value of the Hansen coefficient dK₀n, s / dΧ.
getDerivative(int, double) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenZonalLinear
Get the dK₀-n-1,s / dΧ coefficient derivative.
getDerivativesDrivers() - Method in class org.orekit.estimation.measurements.EstimatedMeasurement
Get all the drivers with set derivatives.
getDerivativesToEpoch(SpacecraftState, double[]) - Method in class org.orekit.forces.gravity.ThirdBodyAttractionEpoch
Compute derivatives of the state w.r.t epoch.
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.FieldRecordAndContinue.Event
Get the detector.
getDetector() - Method in class org.orekit.propagation.events.handlers.RecordAndContinue.Event
Get the detector.
getDetectors() - Method in class org.orekit.propagation.events.BooleanDetector
Get the list of original detectors.
getdGjsdAlpha(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHIJjsPolynomials
Get the dGjs / dα coefficient.
getdGjsdAlpha(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
Get the dGjs / dα coefficient.
getdGjsdBeta(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHIJjsPolynomials
Get the dGjs / dβ coefficient.
getdGjsdBeta(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
Get the dGjs / dβ coefficient.
getdGjsdh(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHIJjsPolynomials
Get the dGjs / dh coefficient.
getdGjsdh(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
Get the dGjs / dh coefficient.
getdGjsdk(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHIJjsPolynomials
Get the dGjs / dk coefficient.
getdGjsdk(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
Get the dGjs / dk coefficient.
getdGmsdAlpha(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHmsjPolynomials
Get the dGmsj / dα coefficient.
getdGmsdAlpha(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHmsjPolynomials
Get the dGmsj / dα coefficient.
getdGmsdBeta(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHmsjPolynomials
Get the dGmsj / dβ coefficient.
getdGmsdBeta(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHmsjPolynomials
Get the dGmsj / dβ coefficient.
getdGmsdh(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHmsjPolynomials
Get the dGmsj / dh coefficient.
getdGmsdh(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHmsjPolynomials
Get the dGmsj / dh coefficient.
getdGmsdk(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHmsjPolynomials
Get the dGmsj / dk coefficient.
getdGmsdk(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHmsjPolynomials
Get the dGmsj / dk coefficient.
getdHjsdAlpha(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHIJjsPolynomials
Get the dHjs / dα coefficient.
getdHjsdAlpha(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
Get the dHjs / dα coefficient.
getdHjsdBeta(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHIJjsPolynomials
Get the dHjs / dβ coefficient.
getdHjsdBeta(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
Get the dHjs / dβ coefficient.
getdHjsdh(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHIJjsPolynomials
Get the dHjs / dh coefficient.
getdHjsdh(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
Get the dHjs / dh coefficient.
getdHjsdk(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHIJjsPolynomials
Get the dHjs / dk coefficient.
getdHjsdk(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
Get the dHjs / dk coefficient.
getdHmsdAlpha(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHmsjPolynomials
Get the dHmsj / dα coefficient.
getdHmsdAlpha(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHmsjPolynomials
Get the dHmsj / dα coefficient.
getdHmsdBeta(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHmsjPolynomials
Get the dHmsj / dβ coefficient.
getdHmsdBeta(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHmsjPolynomials
Get the dHmsj / dβ coefficient.
getdHmsdh(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHmsjPolynomials
Get the dHmsj / dh coefficient.
getdHmsdh(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHmsjPolynomials
Get the dHmsj / dh coefficient.
getdHmsdk(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHmsjPolynomials
Get the dHmsj / dk coefficient.
getdHmsdk(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHmsjPolynomials
Get the dHmsj / dk coefficient.
getDiagReference() - Method in class org.orekit.estimation.measurements.gnss.AbstractLambdaMethod
Get a reference to the diagonal matrix of the decomposition.
getdIjsdAlpha(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHIJjsPolynomials
Get the dIjs / dα coefficient.
getdIjsdAlpha(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
Get the dIjs / dα coefficient.
getdIjsdBeta(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHIJjsPolynomials
Get the dIjs / dβ coefficient.
getdIjsdBeta(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
Get the dIjs / dβ coefficient.
getdIjsdh(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHIJjsPolynomials
Get the dIjs / dh coefficient.
getdIjsdh(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
Get the dIjs / dh coefficient.
getdIjsdk(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHIJjsPolynomials
Get the dIjs / dk coefficient.
getdIjsdk(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
Get the dIjs / dk coefficient.
getDimension() - Method in class org.orekit.estimation.measurements.AbstractMeasurement
Get the dimension of the measurement.
getDimension() - Method in interface org.orekit.estimation.measurements.ObservedMeasurement
Get the dimension of the measurement.
getDirection() - Method in class org.orekit.forces.maneuvers.ConstantThrustManeuver
Get the direction.
getDirection() - Method in class org.orekit.forces.maneuvers.propulsion.AbstractConstantThrustPropulsionModel
Get the thrust direction in S/C frame.
getDirection(SpacecraftState) - Method in interface org.orekit.forces.maneuvers.propulsion.ThrustPropulsionModel
Get the thrust direction in spacecraft frame.
getDisplacements() - Method in class org.orekit.estimation.measurements.GroundStation
Get the displacement models.
getdJjsdAlpha(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHIJjsPolynomials
Get the dJjs / dα coefficient.
getdJjsdAlpha(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
Get the dJjs / dα coefficient.
getdJjsdBeta(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHIJjsPolynomials
Get the dJjs / dβ coefficient.
getdJjsdBeta(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
Get the dJjs / dβ coefficient.
getdJjsdh(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHIJjsPolynomials
Get the dJjs / dh coefficient.
getdJjsdh(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
Get the dJjs / dh coefficient.
getdJjsdk(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHIJjsPolynomials
Get the dJjs / dk coefficient.
getdJjsdk(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
Get the dJjs / dk coefficient.
getdLnsdGamma(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldLnsCoefficients
Get the value of dLns / dγ (γ).
getdLnsdGamma(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.LnsCoefficients
Get the value of dLns / dγ (γ).
getDnl(double, double, int, int) - Static method in class org.orekit.propagation.semianalytical.dsst.utilities.UpperBounds
Get the upper bound value Dnl(Χ).
getDnl(T, T, int, int) - Static method in class org.orekit.propagation.semianalytical.dsst.utilities.UpperBounds
Get the upper bound value Dnl(Χ).
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.
getDrag() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTAtmosphericDrag
Get drag force.
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.
getDragSensitive(AbsoluteDate) - Method in class org.orekit.forces.drag.TimeSpanDragForce
Get the DragSensitive model valid at a date.
getDragSensitiveSpan(AbsoluteDate) - Method in class org.orekit.forces.drag.TimeSpanDragForce
Get the DragSensitive TimeSpanMap.Span containing a specified date.
getDrivers(double, Orbit, PositionAngle) - Method in enum org.orekit.orbits.OrbitType
Get parameters drivers initialized from a reference orbit.
getDrivers() - Method in class org.orekit.utils.ParameterDriversList
Get delegating drivers for all parameters.
getDSDensityWrtStateUsingFiniteDifferences(AbsoluteDate, Frame, FieldVector3D<DerivativeStructure>) - Method in class org.orekit.forces.drag.AbstractDragForceModel
Compute density and its derivatives.
getDsjDh(int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.CjSjCoefficient
Get the dSj / dh coefficient.
getDsjDh(int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldCjSjCoefficient
Get the dSj / dh coefficient.
getDsjDk(int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.CjSjCoefficient
Get the dSj / dk coefficient.
getDsjDk(int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldCjSjCoefficient
Get the dSj / dk coefficient.
getDSTDTC(AbsoluteDate) - Method in interface org.orekit.models.earth.atmosphere.JB2008InputParameters
Get the temperature change computed from Dst index.
getDuration() - Method in class org.orekit.files.ccsds.APMFile.APMManeuver
Get duration (value is 0 for impulsive maneuver).
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).
getDuration() - Method in class org.orekit.forces.maneuvers.trigger.DateBasedManeuverTriggers
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.BeidouAlmanac
 
getE() - Method in class org.orekit.gnss.GalileoAlmanac
 
getE() - Method in class org.orekit.gnss.GLONASSAlmanac
 
getE() - Method in class org.orekit.gnss.GPSAlmanac
 
getE() - Method in class org.orekit.gnss.IRNSSAlmanac
 
getE() - Method in class org.orekit.gnss.QZSSAlmanac
 
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.GLONASSOrbitalElements
Get the Eccentricity.
getE() - Method in interface org.orekit.propagation.analytical.gnss.GNSSOrbitalElements
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
Get the earliest entry in this cache.
getEarliest() - Method in interface org.orekit.utils.TimeStampedCache
Get the earliest entry in this cache.
getEarth() - Method in interface org.orekit.bodies.CelestialBodies
Get the Earth singleton body.
getEarth() - Static method in class org.orekit.bodies.CelestialBodyFactory
Get the Earth singleton body.
getEarth() - Method in class org.orekit.bodies.LazyLoadedCelestialBodies
 
getEarthMoonBarycenter() - Method in interface org.orekit.bodies.CelestialBodies
Get the Earth-Moon barycenter singleton bodies pair.
getEarthMoonBarycenter() - Static method in class org.orekit.bodies.CelestialBodyFactory
Get the Earth-Moon barycenter singleton bodies pair.
getEarthMoonBarycenter() - Method in class org.orekit.bodies.LazyLoadedCelestialBodies
 
getEarthMoonCR3BP() - Static method in class org.orekit.bodies.CR3BPFactory
Get the Earth-Moon CR3BP singleton bodies pair.
getEarthOrientationAngleFunction(TimeScale) - Method in enum org.orekit.utils.IERSConventions
Get the function computing the raw Earth Orientation Angle.
getEarthOrientationAngleFunction(TimeScale, TimeScale) - Method in enum org.orekit.utils.IERSConventions
Get the function computing the raw Earth Orientation Angle.
getEast() - Method in class org.orekit.bodies.FieldGeodeticPoint
Get the direction to the east of point, expressed in parent shape frame.
getEast() - Method in class org.orekit.bodies.GeodeticPoint
Get the direction to the east of point, expressed in parent shape frame.
getEast() - Method in class org.orekit.frames.TopocentricFrame
Get the east direction of topocentric frame, expressed in parent shape frame.
getEastOffsetDriver() - Method in class org.orekit.estimation.measurements.GroundStation
Get a driver allowing to change station position along East axis.
getEcc() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
Get the eccentricity.
getEcc() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldAuxiliaryElements
Get the eccentricity.
getEccentricAnomaly() - Method in class org.orekit.orbits.FieldKeplerianOrbit
Get the eccentric anomaly.
getEccentricAnomaly() - Method in class org.orekit.orbits.KeplerianOrbit
Get the eccentric anomaly.
getEccentricAnomalyDot() - Method in class org.orekit.orbits.FieldKeplerianOrbit
Get the eccentric anomaly derivative.
getEccentricAnomalyDot() - Method in class org.orekit.orbits.KeplerianOrbit
Get the eccentric anomaly derivative.
getEccentricities(Frequency) - Method in class org.orekit.gnss.antenna.Antenna
Get the phase center eccentricities.
getEccentricities() - Method in class org.orekit.gnss.antenna.FrequencyPattern
Get the phase center eccentricities.
getEccentricities() - Method in class org.orekit.gnss.RinexHeader
Get the eccentricities of antenna center.
getECEF() - Method in class org.orekit.propagation.analytical.gnss.AbstractGNSSPropagator
Gets the Earth Centered Earth Fixed frame used to propagate GNSS orbits according to the Interface Control Document.
getECEF() - Method in class org.orekit.propagation.analytical.gnss.GLONASSAnalyticalPropagator
Gets the Earth Centered Earth Fixed frame used to propagate GLONASS orbits.
getECEF() - Method in class org.orekit.propagation.analytical.gnss.SBASPropagator
Gets the Earth Centered Earth Fixed frame used to propagate GNSS orbits.
getECI() - Method in class org.orekit.propagation.analytical.gnss.AbstractGNSSPropagator
Gets the Earth Centered Inertial frame used to propagate the orbit.
getECI() - Method in class org.orekit.propagation.analytical.gnss.GLONASSAnalyticalPropagator
Gets the Earth Centered Inertial frame used to propagate the orbit.
getECI() - Method in class org.orekit.propagation.analytical.gnss.SBASPropagator
Gets the Earth Centered Inertial frame used to propagate the orbit.
getEclipseAngles(Vector3D, Vector3D) - Method in class org.orekit.forces.radiation.AbstractRadiationForceModel
Get the useful angles for eclipse computation.
getEclipseAngles(FieldVector3D<T>, FieldVector3D<T>) - Method in class org.orekit.forces.radiation.AbstractRadiationForceModel
Get the useful angles for eclipse computation.
getEcliptic(IERSConventions) - Method in class org.orekit.frames.AbstractFrames
 
getEcliptic(IERSConventions) - Method in interface org.orekit.frames.Frames
Get the ecliptic frame.
getEcliptic(IERSConventions) - Static method in class org.orekit.frames.FramesFactory
Get the ecliptic frame.
getEDot() - Method in class org.orekit.orbits.CartesianOrbit
Get the eccentricity derivative.
getEDot() - Method in class org.orekit.orbits.CircularOrbit
Get the eccentricity derivative.
getEDot() - Method in class org.orekit.orbits.EquinoctialOrbit
Get the eccentricity derivative.
getEDot() - Method in class org.orekit.orbits.FieldCartesianOrbit
Get the eccentricity derivative.
getEDot() - Method in class org.orekit.orbits.FieldCircularOrbit
Get the eccentricity derivative.
getEDot() - Method in class org.orekit.orbits.FieldEquinoctialOrbit
Get the eccentricity derivative.
getEDot() - Method in class org.orekit.orbits.FieldKeplerianOrbit
Get the eccentricity derivative.
getEDot() - Method in class org.orekit.orbits.FieldOrbit
Get the eccentricity derivative.
getEDot() - Method in class org.orekit.orbits.KeplerianOrbit
Get the eccentricity derivative.
getEDot() - Method in class org.orekit.orbits.Orbit
Get the eccentricity derivative.
getEffects() - Method in class org.orekit.propagation.analytical.AdapterPropagator
Get the differential effects.
getElem(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.PolynomialFunctionMatrix
Get the value of an element.
getElementNumber() - Method in class org.orekit.propagation.analytical.tle.TLE
Get the element number.
getElementSetNumber() - Method in class org.orekit.files.ccsds.OMMFile
Get the element set number for this satellite.
getElevation(Vector3D, Frame, AbsoluteDate) - Method in class org.orekit.frames.TopocentricFrame
Get the elevation of a point with regards to the local point.
getElevation(FieldVector3D<T>, Frame, FieldAbsoluteDate<T>) - Method in class org.orekit.frames.TopocentricFrame
Get the elevation of a point with regards to the local point.
getElevation(SpacecraftState) - Method in class org.orekit.propagation.events.ElevationExtremumDetector
Get the elevation value.
getElevation(double) - Method in class org.orekit.utils.ElevationMask
Get the interpolated elevation for a given azimuth according to the mask.
getElevationMask() - Method in class org.orekit.gnss.DOPComputer
Get the elevation mask.
getElevationMask() - Method in class org.orekit.propagation.events.ElevationDetector
Returns the currently configured elevation mask.
getElevationMask() - Method in class org.orekit.propagation.events.FieldElevationDetector
Returns the currently configured elevation mask.
getEllipsoid() - Method in interface org.orekit.models.earth.EarthShape
Get the underlying ellipsoid model that defines latitude and longitude.
getEllipsoid() - Method in class org.orekit.models.earth.Geoid
 
getEllipsoid() - Method in class org.orekit.models.earth.ReferenceEllipsoid
 
getEME2000() - Method in class org.orekit.frames.AbstractFrames
 
getEME2000() - Method in interface org.orekit.frames.Frames
Get the unique EME2000 frame.
getEME2000() - Static method in class org.orekit.frames.FramesFactory
Get the unique EME2000 frame.
getEnd() - Method in class org.orekit.estimation.measurements.generation.AbstractMeasurementBuilder
Get the end of the measurements time span.
getEnd() - Method in class org.orekit.utils.TimeSpanMap.Span
Get the end of this time span.
getEndDate(Frequency) - Method in class org.orekit.estimation.measurements.gnss.CycleSlipDetectorResults
Return the end date at the given frequency.
getEndDate() - Method in class org.orekit.forces.maneuvers.ConstantThrustManeuver
Get the end date.
getEndDate() - Method in class org.orekit.forces.maneuvers.trigger.DateBasedManeuverTriggers
Get the end date.
getEndDate() - Method in class org.orekit.frames.EOPHistory
Get the date of the last available Earth Orientation Parameters.
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(IERSConventions, boolean) - Method in interface org.orekit.frames.Frames
Get Earth Orientation Parameters history.
getEOPHistory(IERSConventions, boolean) - Static method in class org.orekit.frames.FramesFactory
Get Earth Orientation Parameters history.
getEOPHistory() - Method in class org.orekit.frames.GTODProvider
Get the EOP history.
getEOPHistory(IERSConventions, boolean, TimeScales) - Method in class org.orekit.frames.LazyLoadedEop
Get Earth Orientation Parameters history.
getEOPHistory(IERSConventions, boolean) - Method in class org.orekit.frames.LazyLoadedFrames
Get Earth Orientation Parameters history.
getEopHistory(IERSConventions, boolean) - Method in class org.orekit.time.AbstractTimeScales
Get the EOP history for the given conventions.
getEopHistory(IERSConventions, boolean) - Method in class org.orekit.time.LazyLoadedTimeScales
 
getEOPHistory() - Method in class org.orekit.time.UT1Scale
Get the EOP history.
getEOPTidalCorrection() - Method in enum org.orekit.utils.IERSConventions
Get the function computing tidal corrections for Earth Orientation Parameters.
getEOPTidalCorrection(TimeScales) - Method in enum org.orekit.utils.IERSConventions
Get the function computing tidal corrections for Earth Orientation Parameters.
getEphemeridesBlocks() - Method in class org.orekit.files.ccsds.OEMFile
Get the list of ephemerides blocks as an unmodifiable list.
getEphemeridesDataLines() - Method in class org.orekit.files.ccsds.OEMFile.EphemeridesBlock
Get the list of Ephemerides data lines.
getEphemeridesDataLinesComment() - Method in class org.orekit.files.ccsds.OEMFile.EphemeridesBlock
Get the ephemerides data lines comment.
getEphemerisType() - Method in class org.orekit.files.ccsds.OMMFile
Get the ephemeris type.
getEphemerisType() - Method in class org.orekit.propagation.analytical.tle.TLE
Get the type of ephemeris.
getEpoch() - Method in class org.orekit.files.ccsds.APMFile
Get the epoch of the data.
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.APMFile
Get the comment for epoch.
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).
getEpochStart() - Method in class org.orekit.files.ccsds.APMFile.APMManeuver
Get epoch start.
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.DSSTKalmanModel
Get the current corrected estimate.
getEstimate() - Method in class org.orekit.estimation.sequential.KalmanModel
Get the current corrected estimate.
getEstimate() - Method in interface org.orekit.estimation.sequential.KalmanODModel
Get the current corrected estimate.
getEstimatedEarthFrame() - Method in class org.orekit.estimation.measurements.GroundStation
Get the estimated Earth frame, including the estimated linear models for pole and prime meridian.
getEstimatedMeasurement(int) - Method in interface org.orekit.estimation.measurements.EstimationsProvider
Get one estimated measurement.
getEstimatedMeasurements() - Method in class org.orekit.estimation.measurements.MultiplexedMeasurement
Get the underlying estimated measurements.
getEstimatedMeasurementsParameters() - Method in class org.orekit.estimation.sequential.DSSTKalmanModel
Get the list of estimated measurements parameters.
getEstimatedMeasurementsParameters() - Method in interface org.orekit.estimation.sequential.KalmanEstimation
Get the list of estimated measurements parameters.
getEstimatedMeasurementsParameters() - Method in class org.orekit.estimation.sequential.KalmanEstimator
Get the list of estimated measurements parameters.
getEstimatedMeasurementsParameters() - Method in class org.orekit.estimation.sequential.KalmanModel
Get the list of estimated measurements parameters.
getEstimatedOrbitalParameters() - Method in class org.orekit.estimation.sequential.DSSTKalmanModel
Get the list of estimated orbital parameters.
getEstimatedOrbitalParameters() - Method in interface org.orekit.estimation.sequential.KalmanEstimation
Get the list of estimated orbital parameters.
getEstimatedOrbitalParameters() - Method in class org.orekit.estimation.sequential.KalmanModel
Get the list of estimated orbital parameters.
getEstimatedPropagationParameters() - Method in class org.orekit.estimation.sequential.DSSTKalmanModel
Get the list of estimated propagation parameters.
getEstimatedPropagationParameters() - Method in interface org.orekit.estimation.sequential.KalmanEstimation
Get the list of estimated propagation parameters.
getEstimatedPropagationParameters() - Method in class org.orekit.estimation.sequential.KalmanModel
Get the list of estimated propagation parameters.
getEstimatedPropagators() - Method in class org.orekit.estimation.sequential.DSSTKalmanModel
Get the propagators estimated with the values set in the propagators builders.
getEstimatedPropagators() - Method in class org.orekit.estimation.sequential.KalmanModel
Get the propagators estimated with the values set in the propagators builders.
getEstimatedPropagators() - Method in interface org.orekit.estimation.sequential.KalmanODModel
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.
getEulerComment() - Method in class org.orekit.files.ccsds.APMFile
Get the comment for Euler angles.
getEulerDirection() - Method in class org.orekit.files.ccsds.APMFile
Get the rotation direction of the attitude Euler angles (A2B or B2A).
getEulerFrameAString() - Method in class org.orekit.files.ccsds.APMFile
Get the reference frame specifying one frame of the transformation.
getEulerFrameBString() - Method in class org.orekit.files.ccsds.APMFile
Get the reference frame specifying the second portion of the transformation.
getEulerRotSeq() - Method in class org.orekit.files.ccsds.AEMFile.AttitudeEphemeridesBlock
Get the rotation sequence of the Euler angles (e.g., 312, where X=1, Y=2, Z=3).
getEulerRotSeq() - Method in class org.orekit.files.ccsds.APMFile
Get the rotation order of Euler angles (X=1, Y=2, Z=3).
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.
getEvaluationsCount() - Method in class org.orekit.estimation.leastsquares.BatchLSModel
Get the evaluations count.
getEvaluationsCount() - Method in interface org.orekit.estimation.leastsquares.BatchLSODModel
Get the evaluations count.
getEvaluationsCount() - Method in class org.orekit.estimation.leastsquares.DSSTBatchLSModel
Get the evaluations count.
getEventDate() - Method in class org.orekit.propagation.events.EventState
Get the occurrence time of the event triggered in the current step.
getEventDate() - Method in class org.orekit.propagation.events.FieldEventState
Get the occurrence time of the event triggered in the current step.
getEventDetector() - Method in class org.orekit.propagation.events.EventsLogger.LoggedEvent
Get the event detector triggered.
getEventDetector() - Method in class org.orekit.propagation.events.EventState
Get the underlying event detector.
getEventDetector() - Method in class org.orekit.propagation.events.FieldEventsLogger.FieldLoggedEvent
Get the event detector triggered.
getEventDetector() - Method in class org.orekit.propagation.events.FieldEventState
Get the underlying event detector.
getEvents() - Method in class org.orekit.propagation.events.handlers.FieldRecordAndContinue
Get the events passed to this handler.
getEvents() - Method in class org.orekit.propagation.events.handlers.RecordAndContinue
Get the events passed to this handler.
getEventsDetectors() - Method in class org.orekit.forces.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 class org.orekit.forces.drag.TimeSpanDragForce
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.SingleBodyAbsoluteAttraction
Get the discrete events related to the model.
getEventsDetectors() - Method in class org.orekit.forces.gravity.SingleBodyRelativeAttraction
Get the discrete events related to the model.
getEventsDetectors() - Method in class org.orekit.forces.gravity.SolidTides
Get the discrete events related to the model.
getEventsDetectors() - Method in class org.orekit.forces.gravity.ThirdBodyAttraction
Get the discrete events related to the model.
getEventsDetectors() - Method in class org.orekit.forces.inertia.InertialForces
Get the discrete events related to the model.
getEventsDetectors() - Method in class org.orekit.forces.maneuvers.Maneuver
Get the discrete events related to the model.
getEventsDetectors() - Method in class org.orekit.forces.maneuvers.trigger.DateBasedManeuverTriggers
Get the event detectors associated with the triggers.
getEventsDetectors() - Method in class org.orekit.forces.maneuvers.trigger.EventBasedManeuverTriggers
Get the event detectors associated with the triggers.
getEventsDetectors() - Method in interface org.orekit.forces.maneuvers.trigger.ManeuverTriggers
Get the event detectors associated with the triggers.
getEventsDetectors() - Method in class org.orekit.forces.radiation.AbstractRadiationForceModel
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 class org.orekit.propagation.numerical.cr3bp.CR3BPForceModel
Get the discrete events related to the model.
getEventsDetectors() - Method in interface org.orekit.propagation.Propagator
Get all the events detectors that have been added.
getEventsDetectors() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTAtmosphericDrag
Get the discrete events related to the model.
getEventsDetectors() - Method in interface org.orekit.propagation.semianalytical.dsst.forces.DSSTForceModel
Get the discrete events related to the model.
getEventsDetectors() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTNewtonianAttraction
Get the discrete events related to the model.
getEventsDetectors() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTSolarRadiationPressure
Get the discrete events related to the model.
getEventsDetectors() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseral
Get the discrete events related to the model.
getEventsDetectors() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBody
Get the discrete events related to the model.
getEventsDetectors() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonal
Get the discrete events related to the model.
getEvolution(double, RealVector, MeasurementDecorator) - Method in class org.orekit.estimation.sequential.DSSTKalmanModel
getEvolution(double, RealVector, MeasurementDecorator) - Method in class org.orekit.estimation.sequential.KalmanModel
getExtrapolationThreshold() - Method in class org.orekit.propagation.analytical.Ephemeris
Get the maximum timespan outside of the stored ephemeris that is allowed for extrapolation.
getF() - Method in class org.orekit.data.DelaunayArguments
Get L - Ω where L is the mean longitude of the Moon.
getF() - Method in class org.orekit.data.FieldDelaunayArguments
Get L - Ω where L is the mean longitude of the Moon.
getF10(AbsoluteDate) - Method in interface org.orekit.models.earth.atmosphere.JB2008InputParameters
Get the value of the instantaneous solar flux index (1e-22*Watt/(m²*Hertz)).
getF107Adj() - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherDataLoader.LineParameters
Gets the 10.7-cm Solar Radio Flux (F10.7) Adjusted to 1 AU.
getF107Obs() - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherDataLoader.LineParameters
Gets the observed (unadjusted) value of F10.7.
getF10B(AbsoluteDate) - Method in interface org.orekit.models.earth.atmosphere.JB2008InputParameters
Get the value of the mean solar flux.
getFactoryKey() - Method in class org.orekit.frames.FactoryManagedFrame
Get the key of the frame within the factory.
getFDot() - Method in class org.orekit.data.DelaunayArguments
Get L - Ω where L is the mean longitude of the Moon time derivative.
getFDot() - Method in class org.orekit.data.FieldDelaunayArguments
Get L - Ω where L is the mean longitude of the Moon time derivative.
getField(GeoMagneticFieldFactory.FieldModel, double) - Static method in class org.orekit.models.earth.GeoMagneticFieldFactory
Get the GeoMagneticField for the given model type and year.
getField(GeoMagneticFieldFactory.FieldModel, double) - Method in interface org.orekit.models.earth.GeoMagneticFields
Get the GeoMagneticField for the given model type and year.
getField(GeoMagneticFieldFactory.FieldModel, double) - Method in class org.orekit.models.earth.LazyLoadedGeoMagneticFields
 
getField() - Method in class org.orekit.propagation.FieldAbstractPropagator
Field getter.
getField() - Method in class org.orekit.time.FieldAbsoluteDate
Get the field.
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 class org.orekit.forces.drag.TimeSpanDragForce
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.SingleBodyAbsoluteAttraction
 
getFieldEventsDetectors(Field<T>) - Method in class org.orekit.forces.gravity.SingleBodyRelativeAttraction
 
getFieldEventsDetectors(Field<T>) - Method in class org.orekit.forces.gravity.SolidTides
Get the discrete events related to the model.
getFieldEventsDetectors(Field<T>) - Method in class org.orekit.forces.gravity.ThirdBodyAttraction
Get the discrete events related to the model.
getFieldEventsDetectors(Field<T>) - Method in class org.orekit.forces.inertia.InertialForces
Get the discrete events related to the model.
getFieldEventsDetectors(Field<T>) - Method in class org.orekit.forces.maneuvers.Maneuver
Get the discrete events related to the model.
getFieldEventsDetectors(Field<T>) - Method in class org.orekit.forces.maneuvers.trigger.DateBasedManeuverTriggers
Get the event detectors associated with the triggers.
getFieldEventsDetectors(Field<T>) - Method in class org.orekit.forces.maneuvers.trigger.EventBasedManeuverTriggers
Get the event detectors associated with the triggers.
getFieldEventsDetectors(Field<T>) - Method in interface org.orekit.forces.maneuvers.trigger.ManeuverTriggers
Get the event detectors associated with the triggers.
getFieldEventsDetectors(Field<T>) - Method in class org.orekit.forces.radiation.AbstractRadiationForceModel
Get the discrete events related to the model.
getFieldEventsDetectors(Field<T>) - Method in class org.orekit.propagation.numerical.cr3bp.CR3BPForceModel
 
getFieldEventsDetectors(Field<T>) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTAtmosphericDrag
Get the discrete events related to the model.
getFieldEventsDetectors(Field<T>) - Method in interface org.orekit.propagation.semianalytical.dsst.forces.DSSTForceModel
Get the discrete events related to the model.
getFieldEventsDetectors(Field<T>) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTNewtonianAttraction
Get the discrete events related to the model.
getFieldEventsDetectors(Field<T>) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTSolarRadiationPressure
Get the discrete events related to the model.
getFieldEventsDetectors(Field<T>) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseral
Get the discrete events related to the model.
getFieldEventsDetectors(Field<T>) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBody
Get the discrete events related to the model.
getFieldEventsDetectors(Field<T>) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonal
Get the discrete events related to the model.
getFieldOfView() - Method in class org.orekit.propagation.events.FieldOfViewDetector
Deprecated.
as of 10.1, replaced by FieldOfViewDetector.getFOV()
getFieldOfView() - Method in class org.orekit.propagation.events.FootprintOverlapDetector
Deprecated.
as of 10.1, replaced by FootprintOverlapDetector.getFOV()
getFieldOfView() - Method in class org.orekit.propagation.events.GroundFieldOfViewDetector
Deprecated.
as of 10.1, replaced by GroundFieldOfViewDetector.getFOV()
getFieldVector() - Method in class org.orekit.models.earth.GeoMagneticElements
Returns the magnetic field vector in nTesla.
getFiftiesEpoch() - Method in class org.orekit.time.AbstractTimeScales
 
getFiftiesEpoch(Field<T>) - Static method in class org.orekit.time.FieldAbsoluteDate
Reference epoch for 1950 dates: 1950-01-01T00:00:00 Terrestrial Time.
getFiftiesEpoch() - Method in interface org.orekit.time.TimeScales
Reference epoch for 1950 dates: 1950-01-01T00:00:00 Terrestrial Time.
getFileDate(AbsoluteDate) - Method in class org.orekit.models.earth.atmosphere.data.MarshallSolarActivityFutureEstimation
Get the date of the file from which data at the specified date comes from.
getFileFormat() - Method in class org.orekit.files.ccsds.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.
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.
getFlowRate(SpacecraftState) - Method in class org.orekit.forces.maneuvers.propulsion.AbstractConstantThrustPropulsionModel
Get the flow rate (kg/s).
getFlowRate(SpacecraftState, double[]) - Method in class org.orekit.forces.maneuvers.propulsion.AbstractConstantThrustPropulsionModel
Get the flow rate (kg/s).
getFlowRate(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.maneuvers.propulsion.AbstractConstantThrustPropulsionModel
Get the flow rate (kg/s).
getFlowRate() - Method in class org.orekit.forces.maneuvers.propulsion.AbstractConstantThrustPropulsionModel
Get the flow rate (kg/s).
getFlowRate(double[]) - Method in class org.orekit.forces.maneuvers.propulsion.AbstractConstantThrustPropulsionModel
Get the flow rate (kg/s).
getFlowRate(T[]) - Method in class org.orekit.forces.maneuvers.propulsion.AbstractConstantThrustPropulsionModel
Get the flow rate (kg/s).
getFlowRate() - Method in class org.orekit.forces.maneuvers.propulsion.BasicConstantThrustPropulsionModel
Get the flow rate (kg/s).
getFlowRate(double[]) - Method in class org.orekit.forces.maneuvers.propulsion.BasicConstantThrustPropulsionModel
Get the flow rate (kg/s).
getFlowRate(T[]) - Method in class org.orekit.forces.maneuvers.propulsion.BasicConstantThrustPropulsionModel
Get the flow rate (kg/s).
getFlowRate() - Method in class org.orekit.forces.maneuvers.propulsion.ScaledConstantThrustPropulsionModel
Get the flow rate (kg/s).
getFlowRate(double[]) - Method in class org.orekit.forces.maneuvers.propulsion.ScaledConstantThrustPropulsionModel
Get the flow rate (kg/s).
getFlowRate(T[]) - Method in class org.orekit.forces.maneuvers.propulsion.ScaledConstantThrustPropulsionModel
Get the flow rate (kg/s).
getFlowRate(SpacecraftState) - Method in interface org.orekit.forces.maneuvers.propulsion.ThrustPropulsionModel
Get the flow rate (kg/s).
getFlowRate(SpacecraftState, double[]) - Method in interface org.orekit.forces.maneuvers.propulsion.ThrustPropulsionModel
Get the flow rate (kg/s).
getFlowRate(FieldSpacecraftState<T>, T[]) - Method in interface org.orekit.forces.maneuvers.propulsion.ThrustPropulsionModel
Get the flow rate (kg/s).
getFluxQualifier() - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherDataLoader.LineParameters
Gets the Flux Qualifier.
getFocus1() - Method in class org.orekit.geometry.fov.EllipticalFieldOfView
Get first focus in spacecraft frame.
getFocus2() - Method in class org.orekit.geometry.fov.EllipticalFieldOfView
Get second focus in spacecraft frame.
getFootprint(Transform, OneAxisEllipsoid, double) - Method in interface org.orekit.geometry.fov.FieldOfView
Get the footprint of the Field Of View on ground.
getFootprint(Transform, OneAxisEllipsoid, double) - Method in class org.orekit.geometry.fov.PolygonalFieldOfView
Get the footprint of the Field Of View on ground.
getFootprint(Transform, OneAxisEllipsoid, double) - Method in class org.orekit.geometry.fov.SmoothFieldOfView
Get the footprint of the Field Of View on ground.
getFormatVersion() - Method in class org.orekit.files.ccsds.NDMFile
Get the CCSDS NDM (ADM or ODM) format version.
getFOV() - Method in class org.orekit.propagation.events.FieldOfViewDetector
Get the Field Of View.
getFOV() - Method in class org.orekit.propagation.events.FootprintOverlapDetector
Get the Field Of View.
getFOV() - Method in class org.orekit.propagation.events.GroundFieldOfViewDetector
Get the Field Of View.
getFrame() - Method in class org.orekit.bodies.Ellipse
Get the defining frame.
getFrame() - Method in class org.orekit.bodies.Ellipsoid
Get the ellipsoid central frame.
getFrame(IERSConventions, boolean) - Method in enum org.orekit.files.ccsds.CCSDSFrame
Get the frame corresponding to the CCSDS constant.
getFrame(IERSConventions, boolean, DataContext) - Method in enum org.orekit.files.ccsds.CCSDSFrame
Get the frame corresponding to the CCSDS constant.
getFrame() - Method in class org.orekit.files.ccsds.ODMMetaData
Get the reference frame in which data are given: used for state vector and Keplerian elements data (and for the covariance reference frame if none is given).
getFrame() - Method in class org.orekit.files.ccsds.OEMFile.CovarianceMatrix
Get coordinate system for covariance matrix, for absolute frames.
getFrame() - Method in class org.orekit.files.ccsds.OEMFile.EphemeridesBlock
 
getFrame() - Method in interface org.orekit.files.general.EphemerisFile.EphemerisSegment
Get the reference frame for this ephemeris segment.
getFrame() - Method in class org.orekit.files.general.OrekitEphemerisFile.OrekitEphemerisSegment
 
getFrame() - Method in class org.orekit.files.sp3.SP3File.SP3Ephemeris
 
getFrame(Predefined) - Method in class org.orekit.frames.AbstractFrames
 
getFrame(Predefined) - Method in interface org.orekit.frames.Frames
Get one of the predefined frames.
getFrame(Predefined) - Static method in class org.orekit.frames.FramesFactory
Get one of the predefined frames.
getFrame() - Method in class org.orekit.frames.OrphanFrame
Get the associated frame.
getFrame() - Method in interface org.orekit.models.earth.atmosphere.Atmosphere
Get the frame of the central body.
getFrame() - Method in class org.orekit.models.earth.atmosphere.DTM2000
Get the frame of the central body.
getFrame() - Method in class org.orekit.models.earth.atmosphere.HarrisPriester
Get the frame of the central body.
getFrame() - Method in class org.orekit.models.earth.atmosphere.JB2008
Get the frame of the central body.
getFrame() - Method in class org.orekit.models.earth.atmosphere.NRLMSISE00
Get the frame of the central body.
getFrame() - Method in class org.orekit.models.earth.atmosphere.SimpleExponentialAtmosphere
Get the frame of the central body.
getFrame() - Method in class org.orekit.orbits.FieldOrbit
Get the frame in which the orbital parameters are defined.
getFrame() - Method in class org.orekit.orbits.Orbit
Get the frame in which the orbital parameters are defined.
getFrame() - Method in class org.orekit.propagation.AbstractPropagator
Get the frame in which the orbit is propagated.
getFrame() - Method in class org.orekit.propagation.analytical.Ephemeris
 
getFrame() - Method in class org.orekit.propagation.analytical.gnss.AbstractGNSSPropagator
Get the frame in which the orbit is propagated.
getFrame() - Method in class org.orekit.propagation.analytical.gnss.GLONASSAnalyticalPropagator
Get the frame in which the orbit is propagated.
getFrame() - Method in class org.orekit.propagation.analytical.gnss.SBASPropagator
Get the frame in which the orbit is propagated.
getFrame() - Method in class org.orekit.propagation.analytical.tle.TLEPropagator
Get the frame in which the orbit is propagated.
getFrame() - Method in class org.orekit.propagation.conversion.AbstractPropagatorBuilder
Get the frame in which the orbit is propagated.
getFrame() - Method in class org.orekit.propagation.conversion.AbstractPropagatorConverter
Get the frame of the initial state.
getFrame() - Method in interface org.orekit.propagation.conversion.PropagatorBuilder
Get the frame in which the orbit is propagated.
getFrame() - Method in class org.orekit.propagation.events.FieldNodeDetector
Get the frame in which the equator is defined.
getFrame() - Method in class org.orekit.propagation.events.GroundFieldOfViewDetector
Get the sensor reference frame.
getFrame() - Method in class org.orekit.propagation.events.NodeDetector
Get the frame in which the equator is defined.
getFrame() - Method in class org.orekit.propagation.FieldAbstractPropagator
Get the frame in which the orbit is propagated.
getFrame() - Method in interface org.orekit.propagation.FieldPropagator
Get the frame in which the orbit is propagated.
getFrame() - Method in class org.orekit.propagation.FieldSpacecraftState
Get the defining frame.
getFrame() - Method in class org.orekit.propagation.integration.FieldIntegratedEphemeris
 
getFrame() - Method in class org.orekit.propagation.integration.FieldStateMapper
Get the inertial frame.
getFrame() - Method in class org.orekit.propagation.integration.IntegratedEphemeris
 
getFrame() - Method in class org.orekit.propagation.integration.StateMapper
Get the inertial frame.
getFrame() - Method in interface org.orekit.propagation.Propagator
Get the frame in which the orbit is propagated.
getFrame() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
Get the definition frame of the orbit.
getFrame() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldAuxiliaryElements
Get the definition frame of the orbit.
getFrame() - Method in class org.orekit.propagation.SpacecraftState
Get the defining frame.
getFrame() - Method in class org.orekit.utils.AbsolutePVCoordinates
Get the frame in which the coordinates are defined.
getFrame() - Method in class org.orekit.utils.FieldAbsolutePVCoordinates
Get the frame in which the coordinates are defined.
getFrameCenterString() - Method in class org.orekit.files.ccsds.AEMFile.AttitudeEphemeridesBlock
Get the name of the center of the coordinate system the ephemeris is provided in.
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.
getFrames() - Method in class org.orekit.data.CompositeDataContext
 
getFrames() - Method in interface org.orekit.data.DataContext
Get a factory constructing Frames based on the auxiliary data in this context.
getFrames() - Method in class org.orekit.data.ExceptionalDataContext
 
getFrames() - Method in class org.orekit.data.LazyLoadedDataContext
 
getFrames() - Static method in class org.orekit.frames.FramesFactory
Get the instance of Frames that is called by the static methods in this class.
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
 
getFreeAmbiguityDrivers() - Method in class org.orekit.estimation.measurements.gnss.AmbiguitySolver
Get the ambiguity parameters drivers that have not been fixed yet.
getFreeAmbiguityIndirection(int, List<ParameterDriver>) - Method in class org.orekit.estimation.measurements.gnss.AmbiguitySolver
Get ambiguity indirection array for ambiguity parameters drivers that have not been fixed yet.
getFreeEpochMap() - Method in class org.orekit.utils.AbstractMultipleShooting
Get the flags representing the free epoch of patch points.
getFreePatchPointMap() - Method in class org.orekit.utils.AbstractMultipleShooting
Get the flags representing the free components of patch points.
getFreeStateParameters() - Method in class org.orekit.estimation.measurements.modifiers.IonosphericDSConverter
Deprecated.
Get the number of free state parameters.
getFreeStateParameters() - Method in class org.orekit.estimation.measurements.modifiers.IonosphericGradientConverter
Get the number of free state parameters.
getFreeStateParameters() - Method in class org.orekit.estimation.measurements.modifiers.TroposphericDSConverter
Deprecated.
Get the number of free state parameters.
getFreeStateParameters() - Method in class org.orekit.estimation.measurements.modifiers.TroposphericGradientConverter
Get the number of free state parameters.
getFreeStateParameters() - Method in class org.orekit.propagation.integration.AbstractDSConverter
Get the number of free state parameters.
getFreeStateParameters() - Method in class org.orekit.propagation.integration.AbstractGradientConverter
Get the number of free state parameters.
getFreqOffset() - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData
Getter for the freqOffset.
getFrequencies() - Method in class org.orekit.gnss.antenna.Antenna
Get supported frequencies.
getFrequency(SatelliteSystem) - Method in enum org.orekit.gnss.ObservationType
Get the frequency for a specified satellite system.
getFrequencyChannel() - Method in class org.orekit.gnss.GLONASSAlmanac
Get the frequency channel.
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.FieldFunctionalDetector
Get the switching function.
getFunction() - Method in class org.orekit.propagation.events.FunctionalDetector
Get the switching function.
getFutureInfinity() - Method in class org.orekit.time.AbstractTimeScales
 
getFutureInfinity(Field<T>) - Static method in class org.orekit.time.FieldAbsoluteDate
Dummy date at infinity in the future direction.
getFutureInfinity() - Method in interface org.orekit.time.TimeScales
Dummy date at infinity in the future direction.
getGalileoEpoch() - Method in class org.orekit.time.AbstractTimeScales
 
getGalileoEpoch(Field<T>) - Static method in class org.orekit.time.FieldAbsoluteDate
Reference epoch for Galileo System Time: 1999-08-22T00:00:00 UTC.
getGalileoEpoch() - Method in interface org.orekit.time.TimeScales
Reference epoch for Galileo System Time: 1999-08-22T00:00:00 GST.
getGalileoOrbitalElements() - Method in class org.orekit.propagation.analytical.gnss.GalileoPropagator
Get the underlying Galileo orbital elements.
getGamma(LagrangianPoints) - Method in class org.orekit.bodies.CR3BPSystem
Get the position of the Lagrangian point in the CR3BP Rotating frame.
getGamma() - Method in class org.orekit.data.DelaunayArguments
Get the tide parameter γ = GMST + π.
getGamma() - Method in class org.orekit.data.FieldDelaunayArguments
Get the tide parameter γ = GMST + π.
getGamma() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
Get direction cosine γ for central body.
getGamma() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldAuxiliaryElements
Get direction cosine γ for central body.
getGammaDot() - Method in class org.orekit.data.DelaunayArguments
Get the tide parameter γ = GMST + π time derivative.
getGammaDot() - Method in class org.orekit.data.FieldDelaunayArguments
Get the tide parameter γ = GMST + π time derivative.
getGammaN() - Method in interface org.orekit.propagation.analytical.gnss.GLONASSOrbitalElements
Get the relative deviation of predicted satellite carrier frequency from nominal value.
getGASTFunction(TimeScale, EOPHistory) - Method in enum org.orekit.utils.IERSConventions
Get the function computing Greenwich apparent sidereal time, in radians.
getGASTFunction(TimeScale, EOPHistory, TimeScales) - Method in enum org.orekit.utils.IERSConventions
Get the function computing Greenwich apparent sidereal time, in radians.
getGCRF() - Method in class org.orekit.frames.AbstractFrames
 
getGCRF() - Method in interface org.orekit.frames.Frames
Get the unique GCRF frame.
getGCRF() - Static method in class org.orekit.frames.FramesFactory
Get the unique GCRF frame.
getGdop() - Method in class org.orekit.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.
getGeoMagneticFields() - Method in class org.orekit.data.CompositeDataContext
 
getGeoMagneticFields() - Method in interface org.orekit.data.DataContext
Get a factory constructing GeoMagneticFields based on the auxiliary data in this context.
getGeoMagneticFields() - Method in class org.orekit.data.ExceptionalDataContext
 
getGeoMagneticFields() - Method in class org.orekit.data.LazyLoadedDataContext
 
getGeoMagneticFields() - Static method in class org.orekit.models.earth.GeoMagneticFieldFactory
Get the instance of GeoMagneticFields that is called by methods in this class.
getGeometryFreeCombination(SatelliteSystem) - Static method in class org.orekit.estimation.measurements.gnss.MeasurementCombinationFactory
Get the Geometry-Free combination of measurements.
getGetNeighborsCalls() - Method in class org.orekit.utils.GenericTimeStampedCache
Get the number of calls to the GenericTimeStampedCache.getNeighbors(AbsoluteDate) method.
getGjs(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHIJjsPolynomials
Get the Gjs coefficient.
getGjs(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
Get the Gjs coefficient.
getGlo2UTC() - Method in class org.orekit.gnss.GLONASSAlmanac
Get the correction from GLONASS to UTC.
getGLONASS() - Method in class org.orekit.time.LazyLoadedTimeScales
 
getGLONASS() - Method in interface org.orekit.time.TimeScales
Get the GLObal NAvigation Satellite System time scale.
getGLONASS() - Static method in class org.orekit.time.TimeScalesFactory
Get the GLObal NAvigation Satellite System time scale.
getGlonassEpoch() - Method in class org.orekit.time.AbstractTimeScales
 
getGlonassEpoch() - Method in interface org.orekit.time.TimeScales
Reference epoch for GLONASS four-year interval number: 1996-01-01T00:00:00 GLONASS time.
getGLONASSOrbitalElements() - Method in class org.orekit.propagation.analytical.gnss.GLONASSAnalyticalPropagator
Gets the underlying GLONASS orbital elements.
getGLONASSOrbitalElements() - Method in class org.orekit.propagation.numerical.GLONASSNumericalPropagator
Gets the underlying GLONASS orbital elements.
getGloOffset() - Method in class org.orekit.gnss.GLONASSAlmanac
Get the correction of time relative to GLONASS system time.
getGM() - Method in interface org.orekit.bodies.CelestialBody
Get the attraction coefficient of the body.
getGM() - Method in class org.orekit.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.FieldGHmsjPolynomials
Get the Gmsj coefficient.
getGmsj(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHmsjPolynomials
Get the Gmsj coefficient.
getGMST(IERSConventions, boolean) - Method in class org.orekit.time.AbstractTimeScales
 
getGMST() - Method in class org.orekit.time.GLONASSDate
Get the Greenwich Mean Sidereal Time.
getGMST(IERSConventions, boolean) - Method in class org.orekit.time.LazyLoadedTimeScales
 
getGMST(IERSConventions, boolean) - Method in interface org.orekit.time.TimeScales
Get the Greenwich Mean Sidereal Time scale.
getGMST(IERSConventions, boolean) - Static method in class org.orekit.time.TimeScalesFactory
Get the Greenwich Mean Sidereal Time scale.
getGMSTFunction(TimeScale) - Method in enum org.orekit.utils.IERSConventions
Get the function computing Greenwich mean sidereal time, in radians.
getGMSTFunction(TimeScale, TimeScales) - Method in enum org.orekit.utils.IERSConventions
Get the function computing Greenwich mean sidereal time, in radians.
getGMSTRateFunction(TimeScale) - Method in enum org.orekit.utils.IERSConventions
Get the function computing Greenwich mean sidereal time rate, in radians per second.
getGMSTRateFunction(TimeScale, TimeScales) - Method in enum org.orekit.utils.IERSConventions
Get the function computing Greenwich mean sidereal time rate, in radians per second.
getGnssNb() - Method in class org.orekit.gnss.DOP
Gets the number of GNSS satellites taken into account for DOP computation.
getGPS() - Method in class org.orekit.time.LazyLoadedTimeScales
 
getGPS() - Method in interface org.orekit.time.TimeScales
Get the Global Positioning System scale.
getGPS() - Static method in class org.orekit.time.TimeScalesFactory
Get the Global Positioning System scale.
getGPS2Glo() - Method in class org.orekit.gnss.GLONASSAlmanac
Get the correction to GPS time relative GLONASS.
getGpsEpoch() - Method in class org.orekit.time.AbstractTimeScales
 
getGPSEpoch(Field<T>) - Static method in class org.orekit.time.FieldAbsoluteDate
Reference epoch for GPS weeks: 1980-01-06T00:00:00 GPS time.
getGpsEpoch() - Method in interface org.orekit.time.TimeScales
Reference epoch for GPS weeks: 1980-01-06T00:00:00 GPS time.
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.
getGradientDensityWrtStateUsingFiniteDifferences(AbsoluteDate, Frame, FieldVector3D<Gradient>) - Method in class org.orekit.forces.drag.AbstractDragForceModel
Compute density and its derivatives.
getGRAPHICCombination(SatelliteSystem) - Static method in class org.orekit.estimation.measurements.gnss.MeasurementCombinationFactory
Get the GRAPHIC combination of measurements.
getGravityFields() - Method in class org.orekit.data.CompositeDataContext
 
getGravityFields() - Method in interface org.orekit.data.DataContext
Get a factory constructing gravity fields based on the auxiliary data in this context.
getGravityFields() - Method in class org.orekit.data.ExceptionalDataContext
 
getGravityFields() - Method in class org.orekit.data.LazyLoadedDataContext
 
getGravityFields() - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory
Get the instance of GravityFields that is called by the static methods of this class.
getGridPoints() - Method in class org.orekit.frames.InterpolatingTransformProvider
Get the number of interpolation grid points.
getGridPoints() - Method in class org.orekit.frames.ShiftingTransformProvider
Get the number of interpolation grid points.
getGridPoints(T, T) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldFixedNumberInterpolationGrid
Get grid points that are within the current step.
getGridPoints(T, T) - Method in interface org.orekit.propagation.semianalytical.dsst.utilities.FieldInterpolationGrid
Get grid points that are within the current step.
getGridPoints(T, T) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldMaxGapInterpolationGrid
Get grid points that are within the current step.
getGridPoints(double, double) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FixedNumberInterpolationGrid
Get grid points that are within the current step.
getGridPoints(double, double) - Method in interface org.orekit.propagation.semianalytical.dsst.utilities.InterpolationGrid
Get grid points that are within the current step.
getGridPoints(double, double) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.MaxGapInterpolationGrid
Get grid points that are within the current step.
getGrs80(Frame) - Static method in class org.orekit.models.earth.ReferenceEllipsoid
Get the GRS80 ellipsoid, attached to the given body frame.
getGST() - Method in class org.orekit.time.LazyLoadedTimeScales
 
getGST() - Method in interface org.orekit.time.TimeScales
Get the Galileo System Time scale.
getGST() - Static method in class org.orekit.time.TimeScalesFactory
Get the Galileo System Time scale.
getGTOD(boolean) - Method in class org.orekit.frames.AbstractFrames
 
getGTOD(IERSConventions, boolean) - Method in class org.orekit.frames.AbstractFrames
 
getGTOD(boolean) - Method in interface org.orekit.frames.Frames
Get the GTOD reference frame.
getGTOD(IERSConventions, boolean) - Method in interface org.orekit.frames.Frames
Get the GTOD reference frame.
getGTOD(boolean) - Static method in class org.orekit.frames.FramesFactory
Get the GTOD reference frame.
getGTOD(IERSConventions, boolean) - Static method in class org.orekit.frames.FramesFactory
Get the GTOD reference frame.
getH() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
Get the y component of eccentricity vector.
getH() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldAuxiliaryElements
Get the y component of eccentricity vector.
getHalfAperture() - Method in class org.orekit.geometry.fov.CircularFieldOfView
get the FOV half aperture angle.
getHalfAperture() - Method in class org.orekit.propagation.events.CircularFieldOfViewDetector
Deprecated.
Get FOV half aperture angle.
getHalfApertureAlongX() - Method in class org.orekit.geometry.fov.EllipticalFieldOfView
get the FOV half aperture angle for spreading along Xell (i.e.
getHalfApertureAlongY() - Method in class org.orekit.geometry.fov.EllipticalFieldOfView
get the FOV half aperture angle for spreading along Yell (i.e.
getHaloOrbitalPeriod(double) - Method in class org.orekit.orbits.RichardsonExpansion
Return the orbital period of the Halo Orbit.
getHandler() - Method in class org.orekit.propagation.events.AbstractDetector
Get the handler.
getHandler() - Method in class org.orekit.propagation.events.FieldAbstractDetector
Get the handler.
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.ADMMetaData
Get boolean testing whether the body corresponding to the centerName attribute can be created through the CelestialBodies.
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 CelestialBodies.
getHasManeuver() - Method in class org.orekit.files.ccsds.APMFile
Get boolean testing whether the APM contains at least one maneuver.
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.CombinedObservationDataSet
Get the Rinex header associated with this data set.
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.NDMFile
Get the header comment.
getHealth() - Method in class org.orekit.gnss.BeidouAlmanac
Gets the Health status.
getHealth() - Method in class org.orekit.gnss.GLONASSAlmanac
Get the Health status.
getHealth() - Method in class org.orekit.gnss.GPSAlmanac
Gets the Health status.
getHealth() - Method in class org.orekit.gnss.QZSSAlmanac
Gets the Health status.
getHealthE1() - Method in class org.orekit.gnss.GalileoAlmanac
Gets the E1-B/C signal health status.
getHealthE5a() - Method in class org.orekit.gnss.GalileoAlmanac
Gets the E5a signal health status.
getHealthE5b() - Method in class org.orekit.gnss.GalileoAlmanac
Gets the E5b signal health status.
getHjs(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHIJjsPolynomials
Get the Hjs coefficient.
getHjs(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
Get the Hjs coefficient.
getHmsj(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHmsjPolynomials
Get the Hmsj coefficient.
getHmsj(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHmsjPolynomials
Get the Hmsj coefficient.
getHorizontalIntensity() - Method in class org.orekit.models.earth.GeoMagneticElements
Returns the horizontal intensity of the magnetic field (= norm of the vector in the plane spanned by the x/y components of the field vector).
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.BeidouAlmanac
 
getI0() - Method in class org.orekit.gnss.GalileoAlmanac
 
getI0() - Method in class org.orekit.gnss.GPSAlmanac
 
getI0() - Method in class org.orekit.gnss.IRNSSAlmanac
 
getI0() - Method in class org.orekit.gnss.QZSSAlmanac
 
getI0() - Method in interface org.orekit.propagation.analytical.gnss.GNSSOrbitalElements
Gets the Inclination Angle at Reference Time.
getI11() - Method in class org.orekit.files.ccsds.APMFile
Get the moment of Inertia about the 1-axis (N.m²).
getI12() - Method in class org.orekit.files.ccsds.APMFile
Get the moment of Inertia about the 1 and 2 axes (N.m²).
getI13() - Method in class org.orekit.files.ccsds.APMFile
Get the moment of Inertia about the 1 and 3 axes (N.m²).
getI22() - Method in class org.orekit.files.ccsds.APMFile
Get the moment of Inertia about the 2-axis (N.m²).
getI23() - Method in class org.orekit.files.ccsds.APMFile
Get the moment of Inertia about the 2 and 3 axes (N.m²).
getI33() - Method in class org.orekit.files.ccsds.APMFile
Get the moment of Inertia about the 3-axis (N.m²).
getICRF() - Method in class org.orekit.frames.AbstractFrames
 
getICRF() - Method in interface org.orekit.frames.Frames
Get the unique ICRF frame.
getICRF() - Static method in class org.orekit.frames.FramesFactory
Get the unique ICRF frame.
getId() - Method in class org.orekit.files.ccsds.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.BeidouAlmanac
 
getIDot() - Method in class org.orekit.gnss.GalileoAlmanac
 
getIDot() - Method in class org.orekit.gnss.GPSAlmanac
 
getIDot() - Method in class org.orekit.gnss.IRNSSAlmanac
 
getIDot() - Method in class org.orekit.gnss.QZSSAlmanac
 
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.GNSSOrbitalElements
Gets the Rate of Inclination Angle.
getIers2003(Frame) - Static method in class org.orekit.models.earth.ReferenceEllipsoid
Get the IERS2003 ellipsoid, attached to the given body frame.
getIers2010(Frame) - Static method in class org.orekit.models.earth.ReferenceEllipsoid
Get the IERS2010 ellipsoid, attached to the given body frame.
getIers96(Frame) - Static method in class org.orekit.models.earth.ReferenceEllipsoid
Get the IERS96 ellipsoid, attached to the given body frame.
getIGRF(double) - Static method in class org.orekit.models.earth.GeoMagneticFieldFactory
Get the IGRF model for the given year.
getIGRF(double) - Method in interface org.orekit.models.earth.GeoMagneticFields
Get the IGRF model for the given year.
getIGRF(double) - Method in class org.orekit.models.earth.LazyLoadedGeoMagneticFields
 
getIjs(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHIJjsPolynomials
Get the Ijs coefficient.
getIjs(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
Get the Ijs coefficient.
getImaginary(int, int) - Method in class org.orekit.utils.LoveNumbers
Get the imaginary part of a nominal Love numbers.
getInclination() - Method in class org.orekit.models.earth.GeoMagneticElements
Returns the inclination of the magnetic field in radians.
getIncreasingTimeShift() - Method in class org.orekit.propagation.events.EventShifter
Get the increasing events time shift.
getInertialDV() - Method in class org.orekit.forces.maneuvers.SmallManeuverAnalyticalModel
Get the inertial velocity increment of the maneuver.
getInertialFrame() - Method in class org.orekit.files.ccsds.OEMFile.EphemeridesBlock
 
getInertialFrame() - Method in interface org.orekit.files.general.EphemerisFile.EphemerisSegment
Get the inertial reference frame for this ephemeris segment.
getInertialFrame() - Method in class org.orekit.files.general.OrekitEphemerisFile.OrekitEphemerisSegment
 
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.
getInertiaRefFrameString() - Method in class org.orekit.files.ccsds.APMFile
Get the coordinate system for the inertia tensor.
getInitialCovarianceMatrix(SpacecraftState) - Method in class org.orekit.estimation.sequential.AbstractCovarianceMatrixProvider
Get the initial covariance matrix.
getInitialCovarianceMatrix(SpacecraftState) - Method in interface org.orekit.estimation.sequential.CovarianceMatrixProvider
Get the initial covariance matrix.
getInitialFlowrate() - Method in class org.orekit.forces.maneuvers.propulsion.AbstractConstantThrustPropulsionModel
 
getInitialIntegrationState() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
Get the initial state for integration.
getInitialIntegrationState() - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator
Get the initial state for integration.
getInitialIntegrationState() - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator
Get the initial state for integration.
getInitialIntegrationState() - Method in class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator
Get the initial state for integration.
getInitialOrbitDate() - Method in class org.orekit.propagation.conversion.AbstractPropagatorBuilder
Get the date of the initial orbit.
getInitialOrbitDate() - Method in interface org.orekit.propagation.conversion.PropagatorBuilder
Get the date of the initial orbit.
getInitialPV() - Method in class org.orekit.orbits.LibrationOrbit
Return the initialPV on the libration orbit.
getInitialState() - Method in class org.orekit.propagation.AbstractPropagator
Get the propagator initial state.
getInitialState() - Method in class org.orekit.propagation.analytical.AdapterPropagator
Get the propagator initial state.
getInitialState() - Method in class org.orekit.propagation.analytical.AggregateBoundedPropagator
 
getInitialState() - Method in class org.orekit.propagation.analytical.Ephemeris
Get the propagator initial state.
getInitialState() - Method in class org.orekit.propagation.FieldAbstractPropagator
Get the propagator initial state.
getInitialState() - Method in interface org.orekit.propagation.FieldPropagator
Get the propagator initial state.
getInitialState() - Method in class org.orekit.propagation.integration.FieldIntegratedEphemeris
Get the propagator initial state.
getInitialState() - Method in class org.orekit.propagation.integration.IntegratedEphemeris
Get the propagator initial state.
getInitialState() - Method in interface org.orekit.propagation.Propagator
Get the propagator initial state.
getInitialThrustVector() - Method in class org.orekit.forces.maneuvers.propulsion.AbstractConstantThrustPropulsionModel
 
getInnovation(MeasurementDecorator, NonLinearEvolution, RealMatrix) - Method in class org.orekit.estimation.sequential.DSSTKalmanModel
getInnovation(MeasurementDecorator, NonLinearEvolution, RealMatrix) - Method in class org.orekit.estimation.sequential.KalmanModel
getInputs() - Method in class org.orekit.data.AbstractListCrawler
Get the list of inputs supported by the instance.
getInstance() - Static method in class org.orekit.data.DataProvidersManager
Deprecated.
This class is no longer a singleton. In order to support loading multiple data sets code should be updated to accept an instance of this class. If you need to maintain compatibility with Orekit 10.0's behavior use the default data context: DataContext.getDefault().getDataProvidersManager().
getInstantFlux(AbsoluteDate) - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherData
Get the value of the instantaneous solar flux.
getInstantFlux(AbsoluteDate) - Method in class org.orekit.models.earth.atmosphere.data.MarshallSolarActivityFutureEstimation
Get the value of the instantaneous solar flux.
getInstantFlux(AbsoluteDate) - Method in interface org.orekit.models.earth.atmosphere.DTM2000InputParameters
Get the value of the instantaneous solar flux.
getIntegrationInterval() - Method in class org.orekit.files.ccsds.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.DSSTPropagatorBuilder
Get the integrator builder.
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(FieldAbsoluteDate<T>) - Method in interface org.orekit.propagation.sampling.FieldOrekitStepInterpolator
Get the state at interpolated date.
getInterpolatedState(AbsoluteDate) - Method in interface org.orekit.propagation.sampling.OrekitStepInterpolator
Get the state at interpolated date.
getInterpolationDegree() - Method in class org.orekit.files.ccsds.AEMFile.AttitudeEphemeridesBlock
Get the interpolation degree.
getInterpolationDegree() - Method in class org.orekit.files.ccsds.OEMFile.EphemeridesBlock
Get the interpolation degree.
getInterpolationMethod() - Method in class org.orekit.files.ccsds.AEMFile.AttitudeEphemeridesBlock
Get the interpolation method to be used.
getInterpolationMethod() - Method in class org.orekit.files.ccsds.OEMFile.EphemeridesBlock
Get the interpolation method to be used.
getInterpolationSamples() - Method in class org.orekit.files.ccsds.OEMFile.EphemeridesBlock
 
getInterpolationSamples() - Method in interface org.orekit.files.general.EphemerisFile.EphemerisSegment
Get the number of samples to use in interpolation.
getInterpolationSamples() - Method in class org.orekit.files.general.OrekitEphemerisFile.OrekitEphemerisSegment
 
getInterpolationSamples() - Method in class org.orekit.files.sp3.SP3File.SP3Ephemeris
 
getIntersectionPoint(Line, Vector3D, Frame, AbsoluteDate) - Method in interface org.orekit.bodies.BodyShape
Get the intersection point of a line with the surface of the body.
getIntersectionPoint(FieldLine<T>, FieldVector3D<T>, Frame, FieldAbsoluteDate<T>) - Method in interface org.orekit.bodies.BodyShape
Get the intersection point of a line with the surface of the body.
getIntersectionPoint(Line, Vector3D, Frame, AbsoluteDate) - Method in class org.orekit.bodies.OneAxisEllipsoid
Get the intersection point of a line with the surface of the body.
getIntersectionPoint(FieldLine<T>, FieldVector3D<T>, Frame, FieldAbsoluteDate<T>) - Method in class org.orekit.bodies.OneAxisEllipsoid
Get the intersection point of a line with the surface of the body.
getIntersectionPoint(Line, Vector3D, Frame, AbsoluteDate) - Method in class org.orekit.models.earth.Geoid
Get the intersection point of a line with the surface of the body.
getIntersectionPoint(FieldLine<T>, FieldVector3D<T>, Frame, FieldAbsoluteDate<T>) - Method in class org.orekit.models.earth.Geoid
Get the intersection point of a line with the surface of the body.
getInterval() - Method in class org.orekit.gnss.RinexHeader
Get the observation interval in seconds.
getIntervalNumber() - Method in class org.orekit.time.GLONASSDate
Get the number of the current four year interval.
getInverse() - Method in class org.orekit.frames.FieldTransform
Get the inverse transform of the instance.
getInverse() - Method in class org.orekit.frames.Transform
Get the inverse transform of the instance.
getIOD() - Method in class org.orekit.gnss.GalileoAlmanac
Get the Issue of Data (IOD).
getIOD() - Method in interface org.orekit.propagation.analytical.gnss.BeidouOrbitalElements
Gets the BeiDou Issue Of Data (IOD).
getIOD() - Method in interface org.orekit.propagation.analytical.gnss.GLONASSOrbitalElements
Gets the GLONASS Issue Of Data (IOD).
getIODC() - Method in interface org.orekit.propagation.analytical.gnss.GPSOrbitalElements
Gets the Issue Of Data Clock (IODC).
getIODC() - Method in interface org.orekit.propagation.analytical.gnss.QZSSOrbitalElements
Gets the Issue Of Data Clock (IODC).
getIODE() - Method in interface org.orekit.propagation.analytical.gnss.GPSOrbitalElements
Gets the Issue Of Data Ephemeris (IODE).
getIODE() - Method in interface org.orekit.propagation.analytical.gnss.QZSSOrbitalElements
Gets the Issue Of Data Ephemeris (IODE).
getIODEC() - Method in interface org.orekit.propagation.analytical.gnss.IRNSSOrbitalElements
Gets the Issue Of Data Ephemeris and Clock (IODEC).
getIODN() - Method in interface org.orekit.propagation.analytical.gnss.SBASOrbitalElements
Gets the Issue Of Data Navigation (IODN).
getIODNav() - Method in interface org.orekit.propagation.analytical.gnss.GalileoOrbitalElements
Gets the Issue Of Data (IOD).
getIonosphereFreeCombination(SatelliteSystem) - Static method in class org.orekit.estimation.measurements.gnss.MeasurementCombinationFactory
Get the Ionosphere-Free combination of measurements.
getIRNSS() - Method in class org.orekit.time.LazyLoadedTimeScales
 
getIRNSS() - Method in interface org.orekit.time.TimeScales
Get the Indian Regional Navigation Satellite System time scale.
getIRNSS() - Static method in class org.orekit.time.TimeScalesFactory
Get the Indian Regional Navigation Satellite System time scale.
getIrnssEpoch() - Method in class org.orekit.time.AbstractTimeScales
 
getIrnssEpoch() - Method in interface org.orekit.time.TimeScales
Reference epoch for IRNSS weeks: 1999-08-22T00:00:00 IRNSS time.
getIRNSSOrbitalElements() - Method in class org.orekit.propagation.analytical.gnss.IRNSSPropagator
Gets the underlying IRNSS orbital elements.
getISP() - Method in class org.orekit.forces.maneuvers.ConfigurableLowThrustManeuver
Get the specific impulse.
getISP() - Method in class org.orekit.forces.maneuvers.ConstantThrustManeuver
Get the specific impulse.
getIsp() - Method in class org.orekit.forces.maneuvers.ImpulseManeuver
Get the specific impulse.
getIsp() - Method in class org.orekit.forces.maneuvers.propulsion.AbstractConstantThrustPropulsionModel
Get the specific impulse.
getIsp(SpacecraftState) - Method in interface org.orekit.forces.maneuvers.propulsion.ThrustPropulsionModel
Get the specific impulse (s).
getIteration() - Method in class org.orekit.estimation.measurements.EstimatedMeasurement
Get the iteration number.
getIterationsCount() - Method in class org.orekit.estimation.leastsquares.BatchLSEstimator
Get the number of iterations used for last estimation.
getIterationsCount() - Method in class org.orekit.estimation.leastsquares.BatchLSModel
Get the iterations count.
getIterationsCount() - Method in interface org.orekit.estimation.leastsquares.BatchLSODModel
Get the iterations count.
getIterationsCount() - Method in class org.orekit.estimation.leastsquares.DSSTBatchLSModel
Get the iterations count.
getITRF(IERSConventions, boolean) - Method in class org.orekit.frames.AbstractFrames
 
getITRF(ITRFVersion, IERSConventions, boolean) - Method in class org.orekit.frames.AbstractFrames
 
getITRF(IERSConventions, boolean) - Method in interface org.orekit.frames.Frames
Get an unspecified International Terrestrial Reference Frame.
getITRF(ITRFVersion, IERSConventions, boolean) - Method in interface org.orekit.frames.Frames
Get an specific International Terrestrial Reference Frame.
getITRF(IERSConventions, boolean) - Static method in class org.orekit.frames.FramesFactory
Get an unspecified International Terrestrial Reference Frame.
getITRF(ITRFVersion, IERSConventions, boolean) - Static method in class org.orekit.frames.FramesFactory
Get an specific International Terrestrial Reference Frame.
getITRFEquinox(IERSConventions, boolean) - Method in class org.orekit.frames.AbstractFrames
 
getITRFEquinox(IERSConventions, boolean) - Method in interface org.orekit.frames.Frames
Get the equinox-based ITRF reference frame.
getITRFEquinox(IERSConventions, boolean) - Static method in class org.orekit.frames.FramesFactory
Get the equinox-based ITRF reference frame.
getITRFType() - Method in class org.orekit.frames.EOPEntry
Get the ITRF version this entry defines.
getITRFVersion(AbsoluteDate) - Method in class org.orekit.frames.EOPHistory
Get the ITRF version.
getITRFVersion(int) - Static method in enum org.orekit.frames.ITRFVersion
Find an ITRF version from its reference year.
getITRFVersion(String) - Static method in enum org.orekit.frames.ITRFVersion
Find an ITRF version from its name.
getITRFVersion() - Method in class org.orekit.frames.VersionedITRF
Get the ITRF version.
getJ2000Day() - Method in class org.orekit.time.DateComponents
Get the day number with respect to J2000 epoch.
getJ2000Epoch() - Method in class org.orekit.time.AbstractTimeScales
 
getJ2000Epoch(Field<T>) - Static method in class org.orekit.time.FieldAbsoluteDate
J2000.0 Reference epoch: 2000-01-01T12:00:00 Terrestrial Time (not UTC).
getJ2000Epoch() - Method in interface org.orekit.time.TimeScales
J2000.0 Reference epoch: 2000-01-01T12:00:00 Terrestrial Time (not UTC).
getJacobian(Orbit, PositionAngle, double[][]) - Method in class org.orekit.forces.maneuvers.SmallManeuverAnalyticalModel
Compute the Jacobian of the orbit with respect to maneuver parameters.
getJacobian(CartesianDerivativesFilter, T[][]) - Method in class org.orekit.frames.FieldTransform
Compute the Jacobian of the FieldTransform.transformPVCoordinates(FieldPVCoordinates) method of the transform.
getJacobian(CartesianDerivativesFilter, double[][]) - Method in class org.orekit.frames.Transform
Compute the Jacobian of the Transform.transformPVCoordinates(PVCoordinates) method of the transform.
getJacobianWrtCartesian(PositionAngle, T[][]) - Method in class org.orekit.orbits.FieldOrbit
Compute the Jacobian of the orbital parameters with respect to the Cartesian parameters.
getJacobianWrtCartesian(PositionAngle, double[][]) - Method in class org.orekit.orbits.Orbit
Compute the Jacobian of the orbital parameters with respect to the Cartesian parameters.
getJacobianWrtParameters(PositionAngle, T[][]) - Method in class org.orekit.orbits.FieldOrbit
Compute the Jacobian of the Cartesian parameters with respect to the orbital parameters.
getJacobianWrtParameters(PositionAngle, double[][]) - Method in class org.orekit.orbits.Orbit
Compute the Jacobian of the Cartesian parameters with respect to the orbital parameters.
getJavaEpoch() - Method in class org.orekit.time.AbstractTimeScales
 
getJavaEpoch(Field<T>) - Static method in class org.orekit.time.FieldAbsoluteDate
Java Reference epoch: 1970-01-01T00:00:00 Universal Time Coordinate.
getJavaEpoch() - Method in interface org.orekit.time.TimeScales
Java Reference epoch: 1970-01-01T00:00:00 Universal Time Coordinate.
getJD0() - Method in class org.orekit.time.GLONASSDate
Get the current Julian date JD0.
getJjs(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGHIJjsPolynomials
Get the Jjs coefficient.
getJjs(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
Get the Jjs coefficient.
getJulianDay() - Method in class org.orekit.files.sp3.SP3File
Returns the julian day for this SP3 file.
getJulianEpoch() - Method in class org.orekit.time.AbstractTimeScales
 
getJulianEpoch(Field<T>) - Static method in class org.orekit.time.FieldAbsoluteDate
Reference epoch for julian dates: -4712-01-01T12:00:00 Terrestrial Time.
getJulianEpoch() - Method in interface org.orekit.time.TimeScales
Reference epoch for julian dates: -4712-01-01T12:00:00 Terrestrial Time.
getJupiter() - Method in interface org.orekit.bodies.CelestialBodies
Get the Jupiter singleton body.
getJupiter() - Static method in class org.orekit.bodies.CelestialBodyFactory
Get the Jupiter singleton body.
getJupiter() - Method in class org.orekit.bodies.LazyLoadedCelestialBodies
 
getK() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
Get the x component of eccentricity vector.
getK() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldAuxiliaryElements
Get the x component of eccentricity vector.
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.semianalytical.dsst.utilities.FieldAuxiliaryElements
Get the Keplerian period.
getKeplerianPeriod() - Method in class org.orekit.propagation.SpacecraftState
Get the Keplerian period.
getKey() - Method in enum org.orekit.gnss.SatelliteSystem
Get the key for the system.
getKeyword() - Method in class org.orekit.files.ccsds.TDMFile.Observation
Getter for the keyword.
getKpSum() - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherDataLoader.LineParameters
Gets the sum of all eight Kp indices for the current entry.
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.
getLagrangianPoint() - Method in class org.orekit.orbits.RichardsonExpansion
Get the considered lagrangian point.
getLambda() - Method in class org.orekit.gnss.GLONASSAlmanac
 
getLambda() - Method in interface org.orekit.propagation.analytical.gnss.GLONASSOrbitalElements
Get the longitude of ascending node of orbit.
getLastDailyPredictedDate() - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherDataLoader
Gets the day (at data start) of the last daily data entry.
getLastEstimations() - Method in class org.orekit.estimation.leastsquares.BatchLSEstimator
Get the last estimations performed.
getLastKnownLeapSecond() - Method in class org.orekit.time.UTCScale
Get the date of the last known leap second.
getLastObservedDate() - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherDataLoader
Gets the day (at data start) of the last observed data entry.
getLatest() - Method in class org.orekit.utils.GenericTimeStampedCache
Get the latest cached entry.
getLatest() - Method in class org.orekit.utils.ImmutableTimeStampedCache
Get the latest entry in this cache.
getLatest() - Method in interface org.orekit.utils.TimeStampedCache
Get the latest entry in this cache.
getLatitude() - Method in class org.orekit.bodies.FieldGeodeticPoint
Get the latitude.
getLatitude() - Method in class org.orekit.bodies.GeodeticPoint
Get the latitude.
getLatitude() - Method in class org.orekit.propagation.events.FieldLatitudeCrossingDetector
Get the fixed latitude to be crossed (radians).
getLatitude() - Method in class org.orekit.propagation.events.LatitudeCrossingDetector
Get the fixed latitude to be crossed (radians).
getLaunchNumber() - Method in class org.orekit.files.ccsds.ADMMetaData
Get the launch number.
getLaunchNumber() - Method in class org.orekit.files.ccsds.ADMParser
Get the launch number.
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.ADMMetaData
Get the piece of launch.
getLaunchPiece() - Method in class org.orekit.files.ccsds.ADMParser
Get the piece of launch.
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.ADMMetaData
Get the launch year.
getLaunchYear() - Method in class org.orekit.files.ccsds.ADMParser
Get the launch year.
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.semianalytical.dsst.utilities.FieldAuxiliaryElements
Get the eccentric longitude.
getLE() - Method in class org.orekit.propagation.SpacecraftState
Get the eccentric latitude argument (as per equinoctial parameters).
getLeap(AbsoluteDate) - Method in class org.orekit.time.GLONASSScale
Get the value of the previous leap.
getLeap(FieldAbsoluteDate<T>) - Method in class org.orekit.time.GLONASSScale
Get the value of the previous leap.
getLeap(AbsoluteDate) - Method in interface org.orekit.time.TimeScale
Get the value of the previous leap.
getLeap(FieldAbsoluteDate<T>) - Method in interface org.orekit.time.TimeScale
Get the value of the previous leap.
getLeap(AbsoluteDate) - Method in class org.orekit.time.UTCScale
Get the value of the previous leap.
getLeap(FieldAbsoluteDate<T>) - Method in class org.orekit.time.UTCScale
Get the value of the previous leap.
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(Vector3D, Frame, AbsoluteDate) - Method in class org.orekit.forces.radiation.SolarRadiationPressure
Get the lighting ratio ([0-1]).
getLightingRatio(FieldVector3D<T>, Frame, FieldAbsoluteDate<T>) - Method in class org.orekit.forces.radiation.SolarRadiationPressure
Get the lighting ratio ([0-1]).
getLine() - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherDataLoader.LineReader
Get the last line read from the stream.
getLine1() - Method in class org.orekit.propagation.analytical.tle.TLE
Get the first line.
getLine2() - Method in class org.orekit.propagation.analytical.tle.TLE
Get the second line.
getLineNumber() - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherDataLoader.LineReader
Get the line number of the last line read from the file.
getListAppliedDCBS() - Method in class org.orekit.gnss.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, AuxiliaryElements) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution
Compute the limits in L, the true longitude, for integration.
getLLimits(FieldSpacecraftState<T>, FieldAuxiliaryElements<T>) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution
Compute the limits in L, the true longitude, for integration.
getLLimits(SpacecraftState, AuxiliaryElements) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTAtmosphericDrag
Compute the limits in L, the true longitude, for integration.
getLLimits(FieldSpacecraftState<T>, FieldAuxiliaryElements<T>) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTAtmosphericDrag
Compute the limits in L, the true longitude, for integration.
getLLimits(SpacecraftState, AuxiliaryElements) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTSolarRadiationPressure
Compute the limits in L, the true longitude, for integration.
getLLimits(FieldSpacecraftState<T>, FieldAuxiliaryElements<T>) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTSolarRadiationPressure
Compute the limits in L, the true longitude, for integration.
getLM() - Method in class org.orekit.orbits.CartesianOrbit
Get the mean longitude argument.
getLM() - Method in class org.orekit.orbits.CircularOrbit
Get the mean longitude argument.
getLM() - Method in class org.orekit.orbits.EquinoctialOrbit
Get the mean longitude argument.
getLM() - Method in class org.orekit.orbits.FieldCartesianOrbit
Get the mean longitude argument.
getLM() - Method in class org.orekit.orbits.FieldCircularOrbit
Get the mean longitude argument.
getLM() - Method in class org.orekit.orbits.FieldEquinoctialOrbit
Get the mean longitude argument.
getLM() - Method in class org.orekit.orbits.FieldKeplerianOrbit
Get the mean longitude argument.
getLM() - Method in class org.orekit.orbits.FieldOrbit
Get the mean longitude argument.
getLM() - Method in class org.orekit.orbits.KeplerianOrbit
Get the mean longitude argument.
getLM() - Method in class org.orekit.orbits.Orbit
Get the mean longitude argument.
getLM() - Method in class org.orekit.propagation.FieldSpacecraftState
Get the mean longitude argument (as per equinoctial parameters).
getLM() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
Get the mean longitude.
getLM() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldAuxiliaryElements
Get the mean longitude.
getLM() - Method in class org.orekit.propagation.SpacecraftState
Get the mean longitude argument (as per equinoctial parameters).
getLMa() - Method in class org.orekit.data.BodiesElements
Get the mean Mars longitude.
getLMa() - Method in class org.orekit.data.FieldBodiesElements
Get the mean Mars longitude.
getLMaDot() - Method in class org.orekit.data.BodiesElements
Get the mean Mars longitude time derivative.
getLMaDot() - Method in class org.orekit.data.FieldBodiesElements
Get the mean Mars longitude time derivative.
getLMDot() - Method in class org.orekit.orbits.CartesianOrbit
Get the mean longitude argument derivative.
getLMDot() - Method in class org.orekit.orbits.CircularOrbit
Get the mean longitude argument derivative.
getLMDot() - Method in class org.orekit.orbits.EquinoctialOrbit
Get the mean longitude argument derivative.
getLMDot() - Method in class org.orekit.orbits.FieldCartesianOrbit
Get the mean longitude argument derivative.
getLMDot() - Method in class org.orekit.orbits.FieldCircularOrbit
Get the mean longitude argument derivative.
getLMDot() - Method in class org.orekit.orbits.FieldEquinoctialOrbit
Get the mean longitude argument derivative.
getLMDot() - Method in class org.orekit.orbits.FieldKeplerianOrbit
Get the mean longitude argument derivative.
getLMDot() - Method in class org.orekit.orbits.FieldOrbit
Get the mean longitude argument derivative.
getLMDot() - Method in class org.orekit.orbits.KeplerianOrbit
Get the mean longitude argument derivative.
getLMDot() - Method in class org.orekit.orbits.Orbit
Get the mean longitude argument derivative.
getLMe() - Method in class org.orekit.data.BodiesElements
Get the mean Mercury longitude.
getLMe() - Method in class org.orekit.data.FieldBodiesElements
Get the mean Mercury longitude.
getLMeDot() - Method in class org.orekit.data.BodiesElements
Get the mean Mercury longitude time derivative.
getLMeDot() - Method in class org.orekit.data.FieldBodiesElements
Get the mean Mercury longitude time derivative.
getLNe() - Method in class org.orekit.data.BodiesElements
Get the mean Neptune longitude.
getLNe() - Method in class org.orekit.data.FieldBodiesElements
Get the mean Neptune longitude.
getLNeDot() - Method in class org.orekit.data.BodiesElements
Get the mean Neptune longitude time derivative.
getLNeDot() - Method in class org.orekit.data.FieldBodiesElements
Get the mean Neptune longitude time derivative.
getLns(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldLnsCoefficients
Get the value of Lns(γ).
getLns(int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.LnsCoefficients
Get the value of Lns(γ).
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.
getLowElevationThreshold() - Method in class org.orekit.models.earth.troposphere.SaastamoinenModel
Get the low elevation threshold value for path delay computation.
getLowerCaseAbbreviation() - Method in enum org.orekit.time.Month
Get the lower case three letters abbreviation.
getLowerCaseName() - Method in enum org.orekit.time.Month
Get the lower case full name.
getLowReference() - Method in class org.orekit.estimation.measurements.gnss.AbstractLambdaMethod
Get a reference to the lower triangular matrix of the decomposition.
getLPosition(LagrangianPoints) - Method in class org.orekit.bodies.CR3BPSystem
Get the position of the Lagrangian point in the CR3BP Rotating frame.
getLPrime() - Method in class org.orekit.data.DelaunayArguments
Get the mean anomaly of the Sun.
getLPrime() - Method in class org.orekit.data.FieldDelaunayArguments
Get the mean anomaly of the Sun.
getLPrimeDot() - Method in class org.orekit.data.DelaunayArguments
Get the mean anomaly of the Sun time derivative.
getLPrimeDot() - Method in class org.orekit.data.FieldDelaunayArguments
Get the mean anomaly of the Sun time derivative.
getLSa() - Method in class org.orekit.data.BodiesElements
Get the mean Saturn longitude.
getLSa() - Method in class org.orekit.data.FieldBodiesElements
Get the mean Saturn longitude.
getLSaDot() - Method in class org.orekit.data.BodiesElements
Get the mean Saturn longitude time derivative.
getLSaDot() - Method in class org.orekit.data.FieldBodiesElements
Get the mean Saturn longitude time derivative.
getLst81Adj() - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherDataLoader.LineParameters
Gets the last 81-day arithmetic average of F10.7 (adjusted).
getLst81Obs() - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherDataLoader.LineParameters
Gets the last 81-day arithmetic average of F10.7 (observed).
getLUr() - Method in class org.orekit.data.BodiesElements
Get the mean Uranus longitude.
getLUr() - Method in class org.orekit.data.FieldBodiesElements
Get the mean Uranus longitude.
getLUrDot() - Method in class org.orekit.data.BodiesElements
Get the mean Uranus longitude time derivative.
getLUrDot() - Method in class org.orekit.data.FieldBodiesElements
Get the mean Uranus longitude time derivative.
getLv() - Method in class org.orekit.orbits.CartesianOrbit
Get the true longitude argument.
getLv() - Method in class org.orekit.orbits.CircularOrbit
Get the true longitude argument.
getLv() - Method in class org.orekit.orbits.EquinoctialOrbit
Get the true longitude argument.
getLv() - Method in class org.orekit.orbits.FieldCartesianOrbit
Get the true longitude argument.
getLv() - Method in class org.orekit.orbits.FieldCircularOrbit
Get the true longitude argument.
getLv() - Method in class org.orekit.orbits.FieldEquinoctialOrbit
Get the true longitude argument.
getLv() - Method in class org.orekit.orbits.FieldKeplerianOrbit
Get the true longitude argument.
getLv() - Method in class org.orekit.orbits.FieldOrbit
Get the true longitude argument.
getLv() - Method in class org.orekit.orbits.KeplerianOrbit
Get the true longitude argument.
getLv() - Method in class org.orekit.orbits.Orbit
Get the true longitude argument.
getLv() - Method in class org.orekit.propagation.FieldSpacecraftState
Get the true latitude argument (as per equinoctial parameters).
getLv() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
Get the true longitude.
getLv() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldAuxiliaryElements
Get the true longitude.
getLv() - Method in class org.orekit.propagation.SpacecraftState
Get the true latitude argument (as per equinoctial parameters).
getLvDot() - Method in class org.orekit.orbits.CartesianOrbit
Get the true longitude argument derivative.
getLvDot() - Method in class org.orekit.orbits.CircularOrbit
Get the true longitude argument derivative.
getLvDot() - Method in class org.orekit.orbits.EquinoctialOrbit
Get the true longitude argument derivative.
getLvDot() - Method in class org.orekit.orbits.FieldCartesianOrbit
Get the true longitude argument derivative.
getLvDot() - Method in class org.orekit.orbits.FieldCircularOrbit
Get the true longitude argument derivative.
getLvDot() - Method in class org.orekit.orbits.FieldEquinoctialOrbit
Get the true longitude argument derivative.
getLvDot() - Method in class org.orekit.orbits.FieldKeplerianOrbit
Get the true longitude argument derivative.
getLvDot() - Method in class org.orekit.orbits.FieldOrbit
Get the true longitude argument derivative.
getLvDot() - Method in class org.orekit.orbits.KeplerianOrbit
Get the true longitude argument derivative.
getLvDot() - Method in class org.orekit.orbits.Orbit
Get the true longitude argument derivative.
getLVe() - Method in class org.orekit.data.BodiesElements
Get the mean Venus longitude.
getLVe() - Method in class org.orekit.data.FieldBodiesElements
Get the mean Venus longitude.
getLVeDot() - Method in class org.orekit.data.BodiesElements
Get the mean Venus longitude time derivative.
getLVeDot() - Method in class org.orekit.data.FieldBodiesElements
Get the mean Venus longitude time derivative.
getLyapunovOrbitalPeriod(double) - Method in class org.orekit.orbits.RichardsonExpansion
Return the orbital period of the Halo Orbit.
getM0() - Method in class org.orekit.gnss.BeidouAlmanac
 
getM0() - Method in class org.orekit.gnss.GalileoAlmanac
 
getM0() - Method in class org.orekit.gnss.GPSAlmanac
 
getM0() - Method in class org.orekit.gnss.IRNSSAlmanac
 
getM0() - Method in class org.orekit.gnss.QZSSAlmanac
 
getM0() - Method in interface org.orekit.propagation.analytical.gnss.GNSSOrbitalElements
Gets the Mean Anomaly at Reference Time.
getMainStateEquations(ODEIntegrator) - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
Get the differential equations to integrate (for main state only).
getMainStateEquations(FieldODEIntegrator<T>) - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator
Get the differential equations to integrate (for main state only).
getMainStateEquations(FieldODEIntegrator<T>) - Method in class org.orekit.propagation.numerical.FieldNumericalPropagator
Get the differential equations to integrate (for main state only).
getMainStateEquations(ODEIntegrator) - Method in class org.orekit.propagation.numerical.GLONASSNumericalPropagator
 
getMainStateEquations(ODEIntegrator) - Method in class org.orekit.propagation.numerical.NumericalPropagator
Get the differential equations to integrate (for main state only).
getMainStateEquations(ODEIntegrator) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator
Get the differential equations to integrate (for main state only).
getMainStateEquations(FieldODEIntegrator<T>) - Method in class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator
Get the differential equations to integrate (for main state only).
getManagedAdditionalStates() - Method in class org.orekit.propagation.AbstractPropagator
Get all the names of all managed states.
getManagedAdditionalStates() - Method in class org.orekit.propagation.analytical.Ephemeris
Get all the names of all managed states.
getManagedAdditionalStates() - Method in class org.orekit.propagation.FieldAbstractPropagator
Get all the names of all managed states.
getManagedAdditionalStates() - Method in interface org.orekit.propagation.FieldPropagator
Get all the names of all managed states.
getManagedAdditionalStates() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
Get all the names of all managed states.
getManagedAdditionalStates() - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator
Get all the names of all managed states.
getManagedAdditionalStates() - Method in interface org.orekit.propagation.Propagator
Get all the names of all managed states.
getManeuver(int) - Method in class org.orekit.files.ccsds.APMFile
Get a maneuver.
getManeuver(int) - Method in class org.orekit.files.ccsds.OPMFile
Get a maneuver.
getManeuverAttitudeProvider() - Method in class org.orekit.forces.maneuvers.propulsion.ThrustDirectionAndAttitudeProvider
Attitude provider to use.
getManeuvers() - Method in class org.orekit.files.ccsds.APMFile
Get a list of all maneuvers.
getManeuvers() - Method in class org.orekit.files.ccsds.OPMFile
Get a list of all maneuvers.
getManeuverTriggers() - Method in class org.orekit.forces.maneuvers.Maneuver
Get the maneuver triggers.
getManifolds(SpacecraftState, boolean) - Method in class org.orekit.orbits.LibrationOrbit
Return a manifold direction from one position on a libration Orbit.
getMapper() - Method in class org.orekit.propagation.numerical.AbsolutePartialDerivativesEquations
Get a mapper between two-dimensional Jacobians and one-dimensional additional state.
getMapper() - Method in class org.orekit.propagation.numerical.EpochDerivativesEquations
Get a mapper between two-dimensional Jacobians and one-dimensional additional state.
getMapper() - Method in class org.orekit.propagation.numerical.PartialDerivativesEquations
Get a mapper between two-dimensional Jacobians and one-dimensional additional state.
getMapper() - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPartialDerivativesEquations
Get a mapper between two-dimensional Jacobians and one-dimensional additional state.
getMargin() - Method in class org.orekit.geometry.fov.AbstractFieldOfView
Get the angular margin to apply (radians).
getMargin() - Method in interface org.orekit.geometry.fov.FieldOfView
Get the angular margin to apply (radians).
getMargin() - Method in class org.orekit.propagation.events.GeographicZoneDetector
Get the angular margin to apply (radians).
getMarkerName() - Method in class org.orekit.gnss.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() - Method in interface org.orekit.bodies.CelestialBodies
Get the Mars singleton body.
getMars() - Static method in class org.orekit.bodies.CelestialBodyFactory
Get the Mars singleton body.
getMars() - Method in class org.orekit.bodies.LazyLoadedCelestialBodies
 
getMass() - Method in class org.orekit.files.ccsds.OGMFile
Get the spacecraft mass.
getMass(AbsoluteDate) - Method in class org.orekit.propagation.analytical.AbstractAnalyticalPropagator
Get the mass.
getMass(AbsoluteDate) - Method in class org.orekit.propagation.analytical.AdapterPropagator
Get the mass.
getMass(AbsoluteDate) - Method in class org.orekit.propagation.analytical.AggregateBoundedPropagator
 
getMass(AbsoluteDate) - Method in class org.orekit.propagation.analytical.EcksteinHechlerPropagator
Get the mass.
getMass(AbsoluteDate) - Method in class org.orekit.propagation.analytical.Ephemeris
Get the mass.
getMass(FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.analytical.FieldAbstractAnalyticalPropagator
Get the mass.
getMass(FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.analytical.FieldEcksteinHechlerPropagator
Get the mass.
getMass(FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.analytical.FieldKeplerianPropagator
Get the mass.
getMass(AbsoluteDate) - Method in class org.orekit.propagation.analytical.gnss.AbstractGNSSPropagator
Get the mass.
getMass(AbsoluteDate) - Method in class org.orekit.propagation.analytical.gnss.GLONASSAnalyticalPropagator
Get the mass.
getMass(AbsoluteDate) - Method in class org.orekit.propagation.analytical.gnss.SBASPropagator
Get the mass.
getMass(AbsoluteDate) - Method in class org.orekit.propagation.analytical.KeplerianPropagator
Get the mass.
getMass(AbsoluteDate) - Method in class org.orekit.propagation.analytical.tle.TLEPropagator
Get the mass.
getMass() - Method in class org.orekit.propagation.conversion.DSSTPropagatorBuilder
Get the mass.
getMass() - Method in class org.orekit.propagation.conversion.NumericalPropagatorBuilder
Get the mass.
getMass() - Method in class org.orekit.propagation.FieldSpacecraftState
Gets the current mass.
getMass(FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.integration.FieldIntegratedEphemeris
Get the mass.
getMass(AbsoluteDate) - Method in class org.orekit.propagation.integration.IntegratedEphemeris
Get the mass.
getMass() - Method in class org.orekit.propagation.SpacecraftState
Gets the current mass.
getMassDerivatives(SpacecraftState, double[]) - Method in interface org.orekit.forces.maneuvers.propulsion.PropulsionModel
Get the mass derivative (i.e.
getMassDerivatives(FieldSpacecraftState<T>, T[]) - Method in interface org.orekit.forces.maneuvers.propulsion.PropulsionModel
Get the mass derivative (i.e.
getMassDerivatives(SpacecraftState, double[]) - Method in interface org.orekit.forces.maneuvers.propulsion.ThrustPropulsionModel
Get the mass derivative (i.e.
getMassDerivatives(FieldSpacecraftState<T>, T[]) - Method in interface org.orekit.forces.maneuvers.propulsion.ThrustPropulsionModel
Get the mass derivative (i.e.
getMassRatio() - Method in class org.orekit.bodies.CR3BPSystem
Get the CR3BP mass ratio of the system mu2/(mu1+mu2).
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.models.earth.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.models.earth.atmosphere.data.CssiSpaceWeatherData
Gets the available data range maximum date.
getMaxDate() - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherDataLoader
Gets the available data range maximum date.
getMaxDate() - Method in class org.orekit.models.earth.atmosphere.data.MarshallSolarActivityFutureEstimation
Gets the available data range maximum date.
getMaxDate() - Method in interface org.orekit.models.earth.atmosphere.DTM2000InputParameters
Gets the available data range maximum date.
getMaxDate() - Method in interface org.orekit.models.earth.atmosphere.JB2008InputParameters
Gets the available data range maximum date.
getMaxDate() - Method in interface org.orekit.models.earth.atmosphere.NRLMSISE00InputParameters
Gets the available data range maximum date.
getMaxDate() - Method in class org.orekit.propagation.analytical.AggregateBoundedPropagator
 
getMaxDate() - Method in class org.orekit.propagation.analytical.Ephemeris
Get the last date of the range.
getMaxDate() - Method in interface org.orekit.propagation.BoundedPropagator
Get the last date of the range.
getMaxDate() - Method in interface org.orekit.propagation.FieldBoundedPropagator
Get the last date of the range.
getMaxDate() - Method in class org.orekit.propagation.integration.FieldIntegratedEphemeris
Get the last date of the range.
getMaxDate() - Method in class org.orekit.propagation.integration.IntegratedEphemeris
Get the last date of the range.
getMaxDegree() - Method in class org.orekit.forces.gravity.potential.CachedNormalizedSphericalHarmonicsProvider
Get the maximal supported degree.
getMaxDegree() - Method in class org.orekit.forces.gravity.potential.OceanTidesWave
Get the maximum supported degree.
getMaxDegree() - Method in interface org.orekit.forces.gravity.potential.SphericalHarmonicsProvider
Get the maximal supported degree.
getMaxDistance() - Method in class org.orekit.estimation.measurements.gnss.AbstractLambdaMethod
Get the maximum of distance among the solutions found.
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.
getMaxSolution() - Method in class org.orekit.estimation.measurements.gnss.AbstractLambdaMethod
Get the maximum number of solutions seeked.
getMaxSpan() - Method in class org.orekit.utils.GenericTimeStampedCache
Get the maximum duration span in seconds of one slot.
getMaxTimeBeetween2Measurement() - Method in class org.orekit.estimation.measurements.gnss.AbstractCycleSlipDetector
Get the maximum time lapse between 2 measurements without considering a cycle-slip has occurring between both.
getMaxValue() - Method in class org.orekit.utils.ParameterDriver
Get maximum parameter value.
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, AuxiliaryElements, double[]) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution
Computes the mean equinoctial elements rates dai / dt.
getMeanElementRate(FieldSpacecraftState<T>, FieldAuxiliaryElements<T>, T[]) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution
Computes the mean equinoctial elements rates dai / dt.
getMeanElementRate(SpacecraftState, AuxiliaryElements, double[]) - Method in interface org.orekit.propagation.semianalytical.dsst.forces.DSSTForceModel
Computes the mean equinoctial elements rates dai / dt.
getMeanElementRate(FieldSpacecraftState<T>, FieldAuxiliaryElements<T>, T[]) - Method in interface org.orekit.propagation.semianalytical.dsst.forces.DSSTForceModel
Computes the mean equinoctial elements rates dai / dt.
getMeanElementRate(SpacecraftState, AuxiliaryElements, double[]) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTNewtonianAttraction
Computes the mean equinoctial elements rates dai / dt.
getMeanElementRate(FieldSpacecraftState<T>, FieldAuxiliaryElements<T>, T[]) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTNewtonianAttraction
Computes the mean equinoctial elements rates dai / dt.
getMeanElementRate(SpacecraftState, AuxiliaryElements, double[]) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseral
Computes the mean equinoctial elements rates dai / dt.
getMeanElementRate(FieldSpacecraftState<T>, FieldAuxiliaryElements<T>, T[]) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseral
Computes the mean equinoctial elements rates dai / dt.
getMeanElementRate(SpacecraftState, AuxiliaryElements, double[]) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBody
Computes the mean equinoctial elements rates dai / dt.
getMeanElementRate(FieldSpacecraftState<T>, FieldAuxiliaryElements<T>, T[]) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBody
Computes the mean equinoctial elements rates dai / dt.
getMeanElementRate(SpacecraftState, AuxiliaryElements, double[]) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonal
Computes the mean equinoctial elements rates dai / dt.
getMeanElementRate(FieldSpacecraftState<T>, FieldAuxiliaryElements<T>, T[]) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonal
Computes the mean equinoctial elements rates dai / dt.
getMeanElementTheory() - Method in class org.orekit.files.ccsds.OMMFile.OMMMetaData
Get the description of the Mean Element Theory.
getMeanFlux(AbsoluteDate) - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherData
Get the value of the mean solar flux.
getMeanFlux(AbsoluteDate) - Method in class org.orekit.models.earth.atmosphere.data.MarshallSolarActivityFutureEstimation
Get the value of the mean solar flux.
getMeanFlux(AbsoluteDate) - Method in interface org.orekit.models.earth.atmosphere.DTM2000InputParameters
Get the value of the mean solar flux.
getMeanMotion() - Method in class org.orekit.files.ccsds.OMMFile
Get the orbit mean motion.
getMeanMotion() - Method in class org.orekit.gnss.BeidouAlmanac
 
getMeanMotion() - Method in class org.orekit.gnss.GalileoAlmanac
 
getMeanMotion() - Method in class org.orekit.gnss.GPSAlmanac
 
getMeanMotion() - Method in class org.orekit.gnss.IRNSSAlmanac
 
getMeanMotion() - Method in class org.orekit.gnss.QZSSAlmanac
 
getMeanMotion() - Method in interface org.orekit.propagation.analytical.gnss.GNSSOrbitalElements
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.
getMeanMotion() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldAuxiliaryElements
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.
getMeanObliquityFunction(TimeScales) - Method in enum org.orekit.utils.IERSConventions
Get the function computing mean obliquity of the ecliptic.
getMeasurement() - Method in class org.orekit.files.ccsds.TDMFile.Observation
Getter for the measurement.
getMeasurements() - Method in class org.orekit.estimation.measurements.MultiplexedMeasurement
Get the underlying measurements.
getMeasurementsParametersDrivers(boolean) - Method in class org.orekit.estimation.leastsquares.BatchLSEstimator
Get the measurements parameters supported by this estimator (including measurements and modifiers).
getMeasurementType() - Method in class org.orekit.gnss.CombinedObservationData
Get the measurement type.
getMeasurementType() - Method in enum org.orekit.gnss.ObservationType
Get the measurement type.
getMelbourneWubbenaCombination(SatelliteSystem) - Static method in class org.orekit.estimation.measurements.gnss.MeasurementCombinationFactory
Get the Melbourne-Wübbena combination of measurements.
getMercury() - Method in interface org.orekit.bodies.CelestialBodies
Get the Mercury singleton body.
getMercury() - Static method in class org.orekit.bodies.CelestialBodyFactory
Get the Mercury singleton body.
getMercury() - Method in class org.orekit.bodies.LazyLoadedCelestialBodies
 
getMessage(Locale) - Method in interface org.orekit.errors.LocalizedException
Gets the message in a specified locale.
getMessage(Locale) - Method in exception org.orekit.errors.OrekitException
Gets the message in a specified locale.
getMessage() - Method in exception org.orekit.errors.OrekitException
getMessage(Locale) - Method in exception org.orekit.errors.OrekitIllegalArgumentException
Gets the message in a specified locale.
getMessage() - Method in exception org.orekit.errors.OrekitIllegalArgumentException
getMessage(Locale) - Method in exception org.orekit.errors.OrekitIllegalStateException
Gets the message in a specified locale.
getMessage() - Method in exception org.orekit.errors.OrekitIllegalStateException
getMessage(Locale) - Method in exception org.orekit.errors.OrekitInternalError
Gets the message in a specified locale.
getMessage() - Method in exception org.orekit.errors.OrekitInternalError
getMessage(Locale) - Method in exception org.orekit.errors.OrekitIOException
Gets the message in a specified locale.
getMessage() - Method in exception org.orekit.errors.OrekitIOException
getMessage(Locale) - Method in exception org.orekit.errors.OrekitParseException
Gets the message in a specified locale.
getMessage() - Method in exception org.orekit.errors.OrekitParseException
getMetaData() - Method in class org.orekit.files.ccsds.AEMFile.AttitudeEphemeridesBlock
Get the meta-data for the block.
getMetaData() - Method in class org.orekit.files.ccsds.APMFile
Get the meta data.
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.APMFile
Get the comment for meta-data.
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.GNSSDate
Get the number of milliseconds since week start.
getMinAlt() - Method in class org.orekit.models.earth.atmosphere.HarrisPriester
Get the minimal altitude for the model.
getMinDate() - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherData
Gets the available data range minimum date.
getMinDate() - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherDataLoader
Gets the available data range minimum date.
getMinDate() - Method in class org.orekit.models.earth.atmosphere.data.MarshallSolarActivityFutureEstimation
Gets the available data range minimum date.
getMinDate() - Method in interface org.orekit.models.earth.atmosphere.DTM2000InputParameters
Gets the available data range minimum date.
getMinDate() - Method in interface org.orekit.models.earth.atmosphere.JB2008InputParameters
Gets the available data range minimum date.
getMinDate() - Method in interface org.orekit.models.earth.atmosphere.NRLMSISE00InputParameters
Gets the available data range minimum date.
getMinDate() - Method in class org.orekit.propagation.analytical.AggregateBoundedPropagator
 
getMinDate() - Method in class org.orekit.propagation.analytical.Ephemeris
Get the first date of the range.
getMinDate() - Method in interface org.orekit.propagation.BoundedPropagator
Get the first date of the range.
getMinDate() - Method in interface org.orekit.propagation.FieldBoundedPropagator
Get the first date of the range.
getMinDate() - Method in class org.orekit.propagation.integration.FieldIntegratedEphemeris
Get the first date of the range.
getMinDate() - Method in class org.orekit.propagation.integration.IntegratedEphemeris
Get the first date of the range.
getMinElevation() - Method in class org.orekit.gnss.DOPComputer
Get the minimum elevation.
getMinElevation() - Method in class org.orekit.propagation.events.ElevationDetector
Returns the currently configured minimum valid elevation value.
getMinElevation() - Method in class org.orekit.propagation.events.FieldElevationDetector
Returns the currently configured minimum valid elevation value.
getMinMeasurementNumber() - Method in class org.orekit.estimation.measurements.gnss.AbstractCycleSlipDetector
Get the minimum number of measurement needed before being able to figure out cycle-slip occurrence.
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.ADMParser
Get initial date.
getMissionReferenceDate() - Method in class org.orekit.files.ccsds.NDMFile
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) - Method in class org.orekit.frames.AbstractFrames
 
getMOD(IERSConventions) - Method in class org.orekit.frames.AbstractFrames
 
getMOD(boolean) - Method in interface org.orekit.frames.Frames
Get the MOD reference frame.
getMOD(IERSConventions) - Method in interface org.orekit.frames.Frames
Get the MOD reference frame.
getMOD(boolean) - Static method in class org.orekit.frames.FramesFactory
Get the MOD reference frame.
getMOD(IERSConventions) - Static method in class org.orekit.frames.FramesFactory
Get the MOD reference frame.
getMode() - Method in class org.orekit.files.ccsds.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() - Method in class org.orekit.time.AbstractTimeScales
 
getModifiedJulianEpoch(Field<T>) - Static method in class org.orekit.time.FieldAbsoluteDate
Reference epoch for modified julian dates: 1858-11-17T00:00:00 Terrestrial Time.
getModifiedJulianEpoch() - Method in interface org.orekit.time.TimeScales
Reference epoch for modified julian dates: 1858-11-17T00:00:00 Terrestrial Time.
getModifiedRodrigues(double) - Method in class org.orekit.utils.AngularCoordinates
Convert rotation, rate and acceleration to modified Rodrigues vector and derivatives.
getModifiedRodrigues(double) - Method in class org.orekit.utils.FieldAngularCoordinates
Convert rotation, rate and acceleration to modified Rodrigues vector and derivatives.
getModifiers() - Method in class org.orekit.estimation.measurements.AbstractMeasurement
Get the modifiers that apply to a measurement.
getModifiers() - Method in class org.orekit.estimation.measurements.generation.AbstractMeasurementBuilder
Get the modifiers that apply to a measurement.
getModifiers() - Method in interface org.orekit.estimation.measurements.generation.MeasurementBuilder
Get the modifiers that apply to a measurement.
getModifiers() - Method in interface org.orekit.estimation.measurements.ObservedMeasurement
Get the modifiers that apply to a measurement.
getMomentum() - Method in class org.orekit.utils.FieldPVCoordinates
Gets the momentum.
getMomentum() - Method in class org.orekit.utils.PVCoordinates
Gets the momentum.
getMonth() - Method in class org.orekit.time.DateComponents
Get the month.
getMonth(int) - Static method in enum org.orekit.time.Month
Get the month corresponding to a number.
getMonthEnum() - Method in class org.orekit.time.DateComponents
Get the month as an enumerate.
getMoon() - Method in interface org.orekit.bodies.CelestialBodies
Get the Moon singleton body.
getMoon() - Static method in class org.orekit.bodies.CelestialBodyFactory
Get the Moon singleton body.
getMoon() - Method in class org.orekit.bodies.LazyLoadedCelestialBodies
 
getMu() - Method in class org.orekit.files.ccsds.ADMParser
Get gravitational coefficient.
getMu() - Method in class org.orekit.files.ccsds.NDMFile
Get the used gravitational coefficient.
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(Field<T>) - Method in class org.orekit.forces.gravity.NewtonianAttraction
Get the central attraction coefficient μ.
getMu() - Method in class org.orekit.forces.gravity.potential.CachedNormalizedSphericalHarmonicsProvider
Get the central body attraction coefficient.
getMu() - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
Get the central body attraction coefficient.
getMu() - Method in interface org.orekit.forces.gravity.potential.SphericalHarmonicsProvider
Get the central body attraction coefficient.
getMu() - Method in class org.orekit.orbits.FieldOrbit
Get the central attraction coefficient used for position and velocity conversions (m³/s²).
getMu() - Method in class org.orekit.orbits.Orbit
Get the central acceleration constant.
getMU() - Method in class org.orekit.propagation.analytical.gnss.AbstractGNSSPropagator
Get the Earth gravity coefficient used for GNSS propagation.
getMU() - Static method in class org.orekit.propagation.analytical.gnss.GLONASSAnalyticalPropagator
Get the Earth gravity coefficient used for GLONASS propagation.
getMU() - Method in class org.orekit.propagation.analytical.gnss.SBASPropagator
Get the Earth gravity coefficient used for SBAS propagation.
getMU() - Static method in class org.orekit.propagation.analytical.tle.TLEPropagator
Get the Earth gravity coefficient used for TLE propagation.
getMu() - Method in class org.orekit.propagation.conversion.AbstractPropagatorBuilder
Get the central attraction coefficient (µ - m³/s²) value.
getMu() - Method in class org.orekit.propagation.FieldSpacecraftState
Get the central attraction coefficient.
getMu() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
Get the central attraction coefficient μ.
getMu() - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator
Get the central attraction coefficient μ.
getMu() - Method in class org.orekit.propagation.integration.FieldStateMapper
Get the central attraction coefficient μ.
getMu() - Method in class org.orekit.propagation.integration.StateMapper
Get the central attraction coefficient μ.
getMu() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTNewtonianAttraction
Get the central attraction coefficient μ.
getMu() - Method in class org.orekit.propagation.SpacecraftState
Get the central attraction coefficient.
getMuCreated() - Method in class org.orekit.files.ccsds.ODMFile
Get the gravitational coefficient created from the knowledge of the central body.
getMuParsed() - Method in class org.orekit.files.ccsds.ODMFile
Get the gravitational coefficient parsed in the ODM File.
getMuSet() - Method in class org.orekit.files.ccsds.ODMFile
Get the gravitational coefficient set by the user.
getMuUsed() - Method in class org.orekit.files.ccsds.ODMFile
Get the used gravitational coefficient.
getN() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.CoefficientsFactory.NSKey
Get n.
getN4() - Method in class org.orekit.gnss.GLONASSAlmanac
 
getN4() - Method in class org.orekit.gnss.GLONASSEphemeris
 
getN4() - Method in interface org.orekit.propagation.analytical.gnss.GLONASSOrbitalElements
Get the number of the current four year interval.
getNa() - Method in class org.orekit.gnss.GLONASSAlmanac
 
getNa() - Method in class org.orekit.gnss.GLONASSEphemeris
 
getNa() - Method in interface org.orekit.propagation.analytical.gnss.GLONASSOrbitalElements
Get the number of the current day in a four year interval.
getNadir() - Method in class org.orekit.bodies.FieldGeodeticPoint
Get the direction below the point, expressed in parent shape frame.
getNadir() - Method in class org.orekit.bodies.GeodeticPoint
Get the direction below the point, expressed in parent shape frame.
getNadir() - Method in class org.orekit.frames.TopocentricFrame
Get the nadir direction of topocentric frame, expressed in parent shape frame.
getName() - Method in interface org.orekit.bodies.CelestialBody
Get the name of the body.
getName() - Method in class org.orekit.bodies.CR3BPSystem
Get the name of the CR3BP system.
getName() - Method in class org.orekit.compiler.plugin.DefaultDataContextPlugin
 
getName() - Method in class org.orekit.data.NamedData
Get the name of the data.
getName() - Method in class org.orekit.estimation.measurements.gnss.AbstractDualFrequencyCombination
Get the name of the combination of measurements.
getName() - Method in class org.orekit.estimation.measurements.gnss.AbstractSingleFrequencyCombination
Get the name of the combination of measurements.
getName() - Method in enum org.orekit.estimation.measurements.gnss.CombinationType
Get the name of the combination of measurements.
getName() - Method in interface org.orekit.estimation.measurements.gnss.MeasurementCombination
Get the name of the combination of measurements.
getName() - Method in class org.orekit.estimation.measurements.gnss.MelbourneWubbenaCombination
Get the name of the combination of measurements.
getName() - Method in enum org.orekit.files.ccsds.AEMAttitudeType
Get the name of the attitude type.
getName() - Method in class org.orekit.forces.maneuvers.Maneuver
Get the name of the maneuver.
getName() - Method in class org.orekit.forces.maneuvers.propulsion.AbstractConstantThrustPropulsionModel
Get the maneuver name.
getName() - Method in interface org.orekit.forces.maneuvers.propulsion.PropulsionModel
Get the maneuver name.
getName() - Method in interface org.orekit.forces.maneuvers.trigger.ManeuverTriggers
Get the maneuver name.
getName() - Method in class org.orekit.frames.Frame
Get the name.
getName() - Method in enum org.orekit.frames.ITRFVersion
Get the name the frame version.
getName() - Method in enum org.orekit.frames.Predefined
Get the name of the frame.
getName() - Method in enum org.orekit.gnss.antenna.SatelliteType
Get the IGS name for the antenna code.
getName() - Method in 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 class org.orekit.propagation.integration.AbstractJacobiansMapper
Get the name of the partial Jacobians.
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.cr3bp.STMEquations
Get the name of the additional state.
getName() - Method in class org.orekit.propagation.numerical.EpochDerivativesEquations
Get the name of the additional state.
getName() - Method in class org.orekit.propagation.numerical.PartialDerivativesEquations
Get the name of the additional state.
getName() - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPartialDerivativesEquations
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.
getNarrowLaneCombination(SatelliteSystem) - Static method in class org.orekit.estimation.measurements.gnss.MeasurementCombinationFactory
Get the Narrow-Lane combination of measurements.
getNbManeuvers() - Method in class org.orekit.files.ccsds.APMFile
Get the number of maneuvers present in the APM.
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
Get the fixed size of the lists returned by TimeStampedCache.getNeighbors(AbsoluteDate).
getNeighborsSize() - Method in interface org.orekit.utils.TimeStampedCache
Get the fixed size of the lists returned by TimeStampedCache.getNeighbors(AbsoluteDate).
getNeptune() - Method in interface org.orekit.bodies.CelestialBodies
Get the Neptune singleton body.
getNeptune() - Static method in class org.orekit.bodies.CelestialBodyFactory
Get the Neptune singleton body.
getNeptune() - Method in class org.orekit.bodies.LazyLoadedCelestialBodies
 
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.
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, 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.
getNormal(AbsoluteDate, Frame, FieldVector3D<DerivativeStructure>, FieldRotation<DerivativeStructure>) - Method in class org.orekit.forces.BoxAndSolarArraySpacecraft
Deprecated.
Method not used anymore, should have been deleted in 9.0 but was left over. To be deleted in the next major version.
getNormalGravity(double) - Method in class org.orekit.models.earth.ReferenceEllipsoid
Gets the normal gravity, that is gravity just due to the reference ellipsoid's potential.
getNormalizedCnm(int, int) - Method in interface org.orekit.forces.gravity.potential.NormalizedSphericalHarmonicsProvider.NormalizedSphericalHarmonics
Get a spherical harmonic cosine coefficient.
getNormalizedProvider(int, int) - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory
Get the gravity field coefficients provider from the first supported file.
getNormalizedProvider(double, double, TideSystem, double[][], double[][]) - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory
Create a time-independent NormalizedSphericalHarmonicsProvider from canonical coefficients.
getNormalizedProvider(UnnormalizedSphericalHarmonicsProvider) - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory
getNormalizedProvider(int, int) - Method in interface org.orekit.forces.gravity.potential.GravityFields
Get a gravity field normalized coefficients provider.
getNormalizedProvider(int, int) - Method in class org.orekit.forces.gravity.potential.LazyLoadedGravityFields
Get a gravity field normalized coefficients provider.
getNormalizedSnm(int, int) - Method in interface org.orekit.forces.gravity.potential.NormalizedSphericalHarmonicsProvider.NormalizedSphericalHarmonics
Get a spherical harmonic sine coefficient.
getNormalizedValue() - Method in class org.orekit.utils.ParameterDriver
Get normalized value.
getNorth() - Method in class org.orekit.bodies.FieldGeodeticPoint
Get the direction to the north of point, expressed in parent shape frame.
getNorth() - Method in class org.orekit.bodies.GeodeticPoint
Get the direction to the north of point, expressed in parent shape frame.
getNorth() - Method in class org.orekit.frames.TopocentricFrame
Get the north direction of topocentric frame, expressed in parent shape frame.
getNorthOffsetDriver() - Method in class org.orekit.estimation.measurements.GroundStation
Get a driver allowing to change station position along North axis.
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.
getNumberOfConstraints() - Method in class org.orekit.utils.AbstractMultipleShooting
Get the number of constraints.
getNumberOfEpochs() - Method in class org.orekit.files.sp3.SP3File
Returns the number of epochs contained in this orbit file.
getNumberOfFreeEpoch() - Method in class org.orekit.utils.AbstractMultipleShooting
Get the number of free epoch.
getNumberOfFreeVariables() - Method in class org.orekit.utils.AbstractMultipleShooting
Get the number of free variables.
getNutation() - Method in class org.orekit.files.ccsds.APMFile
Get the nutation angle of spin axis (rad).
getNutationArguments(TimeScales) - Method in enum org.orekit.utils.IERSConventions
Get the fundamental nutation arguments.
getNutationArguments(TimeScale) - Method in enum org.orekit.utils.IERSConventions
Get the fundamental nutation arguments.
getNutationArguments(TimeScale, TimeScales) - Method in enum org.orekit.utils.IERSConventions
Get the fundamental nutation arguments.
getNutationCorrectionConverter() - Method in enum org.orekit.utils.IERSConventions
Create a function converting nutation corrections between δX/δY and δΔψ/δΔε.
getNutationCorrectionConverter(TimeScales) - Method in enum org.orekit.utils.IERSConventions
Create a function converting nutation corrections between δX/δY and δΔψ/δΔε.
getNutationFunction() - Method in enum org.orekit.utils.IERSConventions
Get the function computing the nutation angles.
getNutationFunction(TimeScales) - Method in enum org.orekit.utils.IERSConventions
Get the function computing the nutation angles.
getNutationPeriod() - Method in class org.orekit.files.ccsds.APMFile
Get the body nutation period of the spin axis (s).
getNutationPhase() - Method in class org.orekit.files.ccsds.APMFile
Get the inertial nutation phase (rad).
getNutationReferenceEpoch() - Method in enum org.orekit.utils.IERSConventions
Get the reference epoch for fundamental nutation arguments.
getNutationReferenceEpoch(TimeScales) - Method in enum org.orekit.utils.IERSConventions
Get the reference epoch for fundamental nutation arguments.
getObjectID() - Method in class org.orekit.files.ccsds.ADMMetaData
Get the spacecraft ID for which the attitude data are provided.
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.ADMMetaData
Get the spacecraft name for which the attitude data are provided.
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.CombinedObservationDataSet
Get list of observation data.
getObservationData() - Method in class org.orekit.gnss.ObservationDataSet
Get list of observation data.
getObservationDataSets() - Method in class org.orekit.gnss.RinexLoader
Get parsed rinex observations data sets.
getObservations() - Method in class org.orekit.files.ccsds.TDMFile.ObservationsBlock
Get the list of Observations data lines.
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
Getter for the occulted body.
getOcculted() - Method in class org.orekit.propagation.events.FieldEclipseDetector
Get the occulted body.
getOccultedRadius() - Method in class org.orekit.propagation.events.EclipseDetector
Getter for the occultedRadius.
getOccultedRadius() - Method in class org.orekit.propagation.events.FieldEclipseDetector
Get the occulted body radius (m).
getOcculting() - Method in class org.orekit.propagation.events.EclipseDetector
Getter for the occulting body.
getOcculting() - Method in class org.orekit.propagation.events.FieldEclipseDetector
Get the occulting body.
getOccultingRadius() - Method in class org.orekit.propagation.events.FieldEclipseDetector
Get the occulting body radius (m).
getOceanLoadDeformationCoefficients() - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory
Get the configured ocean load deformation coefficients.
getOceanLoadDeformationCoefficients() - Method in class org.orekit.forces.gravity.potential.LazyLoadedGravityFields
Get the configured ocean load deformation coefficients.
getOceanPoleTide(EOPHistory) - Method in enum org.orekit.utils.IERSConventions
Get the function computing ocean pole tide (ΔC₂₁, ΔS₂₁).
getOceanTidesWaves(int, int) - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory
Get the ocean tides waves from the first supported file.
getOceanTidesWaves(int, int) - Method in interface org.orekit.forces.gravity.potential.GravityFields
Get the ocean tides waves.
getOceanTidesWaves(int, int) - Method in class org.orekit.forces.gravity.potential.LazyLoadedGravityFields
Get the ocean tides waves.
getODMFile() - Method in class org.orekit.files.ccsds.ODMMetaData
Get the ODM file to which these meta-data belong.
getOffset(AbsoluteDate) - Method in class org.orekit.forces.gravity.potential.CachedNormalizedSphericalHarmonicsProvider
Get the offset from reference date for the harmonics.
getOffset(AbsoluteDate) - Method in interface org.orekit.forces.gravity.potential.SphericalHarmonicsProvider
Get the offset from reference date for the harmonics.
getOffset() - Method in class org.orekit.time.OffsetModel
Offset at reference date in seconds (TAI minus UTC).
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
getOffsetToInertial(Frame, FieldAbsoluteDate<DerivativeStructure>, DSFactory, Map<String, Integer>) - Method in class org.orekit.estimation.measurements.GroundStation
getOffsetToInertial(Frame, AbsoluteDate, int, Map<String, Integer>) - Method in class org.orekit.estimation.measurements.GroundStation
Get the transform between offset frame and inertial frame with derivatives.
getOffsetToInertial(Frame, FieldAbsoluteDate<Gradient>, int, Map<String, Integer>) - Method in class org.orekit.estimation.measurements.GroundStation
Get the transform between offset frame and inertial frame with derivatives.
getOmega() - Method in class org.orekit.data.DelaunayArguments
Get the mean longitude of the ascending node of the Moon.
getOmega() - Method in class org.orekit.data.FieldDelaunayArguments
Get the mean longitude of the ascending node of the Moon.
getOmega0() - Method in class org.orekit.gnss.BeidouAlmanac
 
getOmega0() - Method in class org.orekit.gnss.GalileoAlmanac
 
getOmega0() - Method in class org.orekit.gnss.GPSAlmanac
 
getOmega0() - Method in class org.orekit.gnss.IRNSSAlmanac
 
getOmega0() - Method in class org.orekit.gnss.QZSSAlmanac
 
getOmega0() - Method in interface org.orekit.propagation.analytical.gnss.GNSSOrbitalElements
Gets the Longitude of Ascending Node of Orbit Plane at Weekly Epoch.
getOmegaDot() - Method in class org.orekit.data.DelaunayArguments
Get the mean longitude of the ascending node of the Moon time derivative.
getOmegaDot() - Method in class org.orekit.data.FieldDelaunayArguments
Get the mean longitude of the ascending node of the Moon time derivative.
getOmegaDot() - Method in class org.orekit.gnss.BeidouAlmanac
 
getOmegaDot() - Method in class org.orekit.gnss.GalileoAlmanac
 
getOmegaDot() - Method in class org.orekit.gnss.GPSAlmanac
 
getOmegaDot() - Method in class org.orekit.gnss.IRNSSAlmanac
 
getOmegaDot() - Method in class org.orekit.gnss.QZSSAlmanac
 
getOmegaDot() - Method in interface org.orekit.propagation.analytical.gnss.GNSSOrbitalElements
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
Get the current orbit.
getOrbit() - Method in class org.orekit.propagation.SpacecraftState
Get the current orbit.
getOrbitalParametersDrivers(boolean) - Method in class org.orekit.estimation.leastsquares.BatchLSEstimator
Get the orbital parameters supported by this estimator.
getOrbitalParametersDrivers(boolean) - Method in class org.orekit.estimation.sequential.KalmanEstimator
Get the orbital parameters supported by this estimator.
getOrbitalParametersDrivers() - Method in class org.orekit.propagation.conversion.AbstractPropagatorBuilder
Get the drivers for the configurable orbital parameters.
getOrbitalParametersDrivers() - Method in interface org.orekit.propagation.conversion.PropagatorBuilder
Get the drivers for the configurable orbital parameters.
getOrbitalPeriod() - Method in class org.orekit.orbits.CR3BPDifferentialCorrection
Get the orbital period of the required orbit.
getOrbitalPeriod() - Method in class org.orekit.orbits.LibrationOrbit
Return the orbital period of the libration orbit.
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.
getOrbitType() - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator
Get propagation parameter type.
getOrbitType() - Method in class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator
Get propagation parameter type.
getOrbitTypeKey() - Method in class org.orekit.files.sp3.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.
getOriginal() - Method in class org.orekit.propagation.events.NegateDetector
Get the delegate event detector.
getOriginator() - Method in class org.orekit.files.ccsds.NDMFile
Get the file originator.
getP() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
Get the y component of inclination vector.
getP() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldAuxiliaryElements
Get the y component of inclination vector.
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.BeidouAlmanac
 
getPa() - Method in class org.orekit.gnss.GalileoAlmanac
 
getPa() - Method in class org.orekit.gnss.GLONASSAlmanac
 
getPa() - Method in class org.orekit.gnss.GPSAlmanac
 
getPa() - Method in class org.orekit.gnss.IRNSSAlmanac
 
getPa() - Method in class org.orekit.gnss.QZSSAlmanac
 
getPa() - Method in interface org.orekit.propagation.analytical.gnss.GLONASSOrbitalElements
Get the Argument of Perigee.
getPa() - Method in interface org.orekit.propagation.analytical.gnss.GNSSOrbitalElements
Gets the Argument of Perigee.
getPaDot() - Method in class org.orekit.data.BodiesElements
Get the general accumulated precession in longitude time derivative.
getPaDot() - Method in class org.orekit.data.FieldBodiesElements
Get the general accumulated precession in longitude time derivative.
getParameterDerivatives(ParameterDriver) - Method in class org.orekit.estimation.measurements.EstimatedMeasurement
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.
getParameterDriver(String) - Method in class org.orekit.forces.inertia.InertialForces
Get parameter value from its name.
getParameters(FieldSpacecraftState<DerivativeStructure>, IonosphericModel) - Method in class org.orekit.estimation.measurements.modifiers.IonosphericDSConverter
Deprecated.
Get the ionospheric model parameters.
getParameters(FieldSpacecraftState<Gradient>, IonosphericModel) - Method in class org.orekit.estimation.measurements.modifiers.IonosphericGradientConverter
Get the ionospheric model parameters.
getParameters(FieldSpacecraftState<DerivativeStructure>, DiscreteTroposphericModel) - Method in class org.orekit.estimation.measurements.modifiers.TroposphericDSConverter
Deprecated.
Get the tropospheric model parameters.
getParameters(FieldSpacecraftState<Gradient>, DiscreteTroposphericModel) - Method in class org.orekit.estimation.measurements.modifiers.TroposphericGradientConverter
Get the tropospheric model parameters.
getParameters() - Method in interface org.orekit.forces.ForceModel
Get force model parameters.
getParameters(Field<T>) - Method in interface org.orekit.forces.ForceModel
Get force model parameters.
getParameters() - Method in interface org.orekit.models.earth.ionosphere.IonosphericModel
Get ionospheric model parameters.
getParameters(Field<T>) - Method in interface org.orekit.models.earth.ionosphere.IonosphericModel
Get ionospheric model parameters.
getParameters() - Method in interface org.orekit.models.earth.troposphere.MappingFunction
Get tropospheric model parameters.
getParameters(Field<T>) - Method in interface org.orekit.models.earth.troposphere.MappingFunction
Get tropospheric model parameters.
getParameters() - Method in class org.orekit.propagation.integration.AbstractJacobiansMapper
Get the number of parameters.
getParameters() - Method in interface org.orekit.propagation.semianalytical.dsst.forces.DSSTForceModel
Get force model parameters.
getParameters(Field<T>) - Method in interface org.orekit.propagation.semianalytical.dsst.forces.DSSTForceModel
Get force model parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.AbstractMeasurement
Get the drivers for this measurement parameters, including its modifiers parameters.
getParametersDrivers() - Method in interface org.orekit.estimation.measurements.EstimationModifier
Get the drivers for this modifier parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.gnss.WindUp
Get the drivers for this modifier parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.AngularIonosphericDelayModifier
Get the drivers for this modifier parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.AngularRadioRefractionModifier
Get the drivers for this modifier parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.AngularTroposphericDelayModifier
Get the drivers for this modifier parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.Bias
Get the drivers for this modifier parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.OnBoardAntennaInterSatellitesRangeModifier
Get the drivers for this modifier parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.OnBoardAntennaPhaseModifier
Get the drivers for this modifier parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.OnBoardAntennaRangeModifier
Get the drivers for this modifier parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.OnBoardAntennaTurnAroundRangeModifier
Get the drivers for this modifier parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.OutlierFilter
Get the drivers for this modifier parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.PhaseAmbiguityModifier
Get the drivers for this modifier parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.PhaseIonosphericDelayModifier
Get the drivers for this modifier parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.PhaseTroposphericDelayModifier
Get the drivers for this modifier parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.RangeIonosphericDelayModifier
Get the drivers for this modifier parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.RangeRateIonosphericDelayModifier
Get the drivers for this modifier parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.RangeRateTroposphericDelayModifier
Get the drivers for this modifier parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.RangeTroposphericDelayModifier
Get the drivers for this modifier parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.ShapiroInterSatelliteRangeModifier
Get the drivers for this modifier parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.ShapiroPhaseModifier
Get the drivers for this modifier parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.ShapiroRangeModifier
Get the drivers for this modifier parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.TurnAroundRangeIonosphericDelayModifier
Get the drivers for this modifier parameters.
getParametersDrivers() - Method in class org.orekit.estimation.measurements.modifiers.TurnAroundRangeTroposphericDelayModifier
Get the drivers for this modifier parameters.
getParametersDrivers() - Method in interface org.orekit.estimation.measurements.ObservedMeasurement
Get the drivers for this measurement parameters, including its modifiers parameters.
getParametersDrivers() - Method in class org.orekit.forces.drag.DragForce
Get the drivers for force model parameters.
getParametersDrivers() - Method in class org.orekit.forces.drag.TimeSpanDragForce
Get the drivers for force model parameters.
getParametersDrivers() - Method in interface org.orekit.forces.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.SingleBodyAbsoluteAttraction
Get the drivers for force model parameters.
getParametersDrivers() - Method in class org.orekit.forces.gravity.SingleBodyRelativeAttraction
Get the drivers for force model parameters.
getParametersDrivers() - Method in class org.orekit.forces.gravity.SolidTides
Get the drivers for force model parameters.
getParametersDrivers() - Method in class org.orekit.forces.gravity.ThirdBodyAttraction
Get the drivers for force model parameters.
getParametersDrivers() - Method in class org.orekit.forces.HarmonicParametricAcceleration
Get the drivers for force model parameters.
getParametersDrivers() - Method in class org.orekit.forces.inertia.InertialForces
Get the drivers for force model parameters.
getParametersDrivers() - Method in class org.orekit.forces.maneuvers.Maneuver
 
getParametersDrivers() - Method in class org.orekit.forces.maneuvers.propulsion.BasicConstantThrustPropulsionModel
Get the propulsion model parameter drivers.
getParametersDrivers() - Method in interface org.orekit.forces.maneuvers.propulsion.PropulsionModel
Get the propulsion model parameter drivers.
getParametersDrivers() - Method in class org.orekit.forces.maneuvers.propulsion.ScaledConstantThrustPropulsionModel
Get the propulsion model parameter drivers.
getParametersDrivers() - Method in interface org.orekit.forces.maneuvers.trigger.ManeuverTriggers
Get the maneuver triggers parameter drivers.
getParametersDrivers() - Method in class org.orekit.forces.PolynomialParametricAcceleration
Get the drivers for force model parameters.
getParametersDrivers() - Method in class org.orekit.forces.radiation.ECOM2
Get the drivers for force model parameters.
getParametersDrivers() - Method in class org.orekit.forces.radiation.SolarRadiationPressure
Get the drivers for force model parameters.
getParametersDrivers() - Method in class org.orekit.models.earth.ionosphere.EstimatedIonosphericModel
 
getParametersDrivers() - Method in class org.orekit.models.earth.ionosphere.GlobalIonosphereMapModel
 
getParametersDrivers() - Method in interface org.orekit.models.earth.ionosphere.IonosphericModel
Get the drivers for ionospheric model parameters.
getParametersDrivers() - Method in class org.orekit.models.earth.ionosphere.KlobucharIonoModel
 
getParametersDrivers() - Method in class org.orekit.models.earth.ionosphere.NeQuickModel
 
getParametersDrivers() - Method in class org.orekit.models.earth.troposphere.EstimatedTroposphericModel
 
getParametersDrivers() - Method in class org.orekit.models.earth.troposphere.FixedTroposphericDelay
 
getParametersDrivers() - Method in class org.orekit.models.earth.troposphere.GlobalMappingFunctionModel
Get the drivers for tropospheric model parameters.
getParametersDrivers() - Method in interface org.orekit.models.earth.troposphere.MappingFunction
Get the drivers for tropospheric model parameters.
getParametersDrivers() - Method in class org.orekit.models.earth.troposphere.MariniMurrayModel
 
getParametersDrivers() - Method in class org.orekit.models.earth.troposphere.MendesPavlisModel
Get the drivers for tropospheric model parameters.
getParametersDrivers() - Method in class org.orekit.models.earth.troposphere.NiellMappingFunctionModel
 
getParametersDrivers() - Method in class org.orekit.models.earth.troposphere.SaastamoinenModel
 
getParametersDrivers() - Method in class org.orekit.models.earth.troposphere.TimeSpanEstimatedTroposphericModel
Get the drivers for tropospheric model parameters.
getParametersDrivers() - Method in class org.orekit.models.earth.troposphere.ViennaOneModel
Get the drivers for tropospheric model parameters.
getParametersDrivers() - Method in class org.orekit.models.earth.troposphere.ViennaThreeModel
Get the drivers for tropospheric model parameters.
getParametersDrivers() - Method in class org.orekit.propagation.numerical.cr3bp.CR3BPForceModel
Get the drivers for force model parameters.
getParametersDrivers() - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution
Get the drivers for force model parameters.
getParametersDrivers() - Method in interface org.orekit.propagation.semianalytical.dsst.forces.DSSTForceModel
Get the drivers for force model parameters.
getParametersDrivers() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTNewtonianAttraction
Get the drivers for force model parameters.
getParametersDrivers() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseral
Get the drivers for force model parameters.
getParametersDrivers() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBody
Get the drivers for force model parameters.
getParametersDrivers() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonal
Get the drivers for force model parameters.
getParametersDriversWithoutMu() - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution
Get the drivers for force model parameters except the one for the central attraction coefficient.
getParametersDriversWithoutMu() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTAtmosphericDrag
Get the drivers for force model parameters except the one for the central attraction coefficient.
getParametersDriversWithoutMu() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTSolarRadiationPressure
Get the drivers for force model parameters except the one for the central attraction coefficient.
getParametersJacobian(SpacecraftState, double[][]) - Method in class org.orekit.propagation.integration.AbstractJacobiansMapper
Get the Jacobian with respect to parameters from a one-dimensional additional state array.
getParametersJacobian(SpacecraftState, double[][]) - Method in class org.orekit.propagation.numerical.JacobiansMapper
Get the Jacobian with respect to parameters from a one-dimensional additional state array.
getParametersJacobian(SpacecraftState, double[][]) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTJacobiansMapper
Get the Jacobian with respect to parameters from a one-dimensional additional state array.
getParent() - Method in class org.orekit.frames.Frame
Get the parent frame.
getParentShape() - Method in class org.orekit.frames.TopocentricFrame
Get the body shape on which the local point is defined.
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() - Method in class org.orekit.time.AbstractTimeScales
 
getPastInfinity(Field<T>) - Static method in class org.orekit.time.FieldAbsoluteDate
Dummy date at infinity in the past direction.
getPastInfinity() - Method in interface org.orekit.time.TimeScales
Dummy date at infinity in the past direction.
getPatchedSpacecraftState() - Method in class org.orekit.utils.AbstractMultipleShooting
Get the list of patched spacecraft states.
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(Frequency, Vector3D) - Method in class org.orekit.gnss.antenna.Antenna
Get the value of the phase center variation in a signal direction.
getPhaseCenterVariation(Vector3D) - Method in class org.orekit.gnss.antenna.FrequencyPattern
Get the value of the phase center variation in a signal direction.
getPhaseMinusCodeCombination(SatelliteSystem) - Static method in class org.orekit.estimation.measurements.gnss.MeasurementCombinationFactory
Get the phase minus code combination of measurements.
getPhaseShiftCorrections() - Method in class org.orekit.gnss.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 class org.orekit.estimation.sequential.DSSTKalmanModel
Get the "physical" estimated covariance matrix (i.e.
getPhysicalEstimatedCovarianceMatrix() - Method in interface org.orekit.estimation.sequential.KalmanEstimation
Get the "physical" estimated covariance matrix (i.e.
getPhysicalEstimatedCovarianceMatrix() - Method in class org.orekit.estimation.sequential.KalmanEstimator
Get the "physical" estimated covariance matrix (i.e.
getPhysicalEstimatedCovarianceMatrix() - Method in class org.orekit.estimation.sequential.KalmanModel
Get the "physical" estimated covariance matrix (i.e.
getPhysicalEstimatedState() - Method in class org.orekit.estimation.sequential.DSSTKalmanModel
Get the "physical" estimated state (i.e.
getPhysicalEstimatedState() - Method in interface org.orekit.estimation.sequential.KalmanEstimation
Get the "physical" estimated state (i.e.
getPhysicalEstimatedState() - Method in class org.orekit.estimation.sequential.KalmanEstimator
Get the "physical" estimated state (i.e.
getPhysicalEstimatedState() - Method in class org.orekit.estimation.sequential.KalmanModel
Get the "physical" estimated state (i.e.
getPhysicalInnovationCovarianceMatrix() - Method in class org.orekit.estimation.sequential.DSSTKalmanModel
Get the physical innovation covariance matrix.
getPhysicalInnovationCovarianceMatrix() - Method in interface org.orekit.estimation.sequential.KalmanEstimation
Get the physical innovation covariance matrix.
getPhysicalInnovationCovarianceMatrix() - Method in class org.orekit.estimation.sequential.KalmanModel
Get the physical innovation covariance matrix.
getPhysicalKalmanGain() - Method in class org.orekit.estimation.sequential.DSSTKalmanModel
Get the physical Kalman gain matrix.
getPhysicalKalmanGain() - Method in interface org.orekit.estimation.sequential.KalmanEstimation
Get the physical Kalman gain matrix.
getPhysicalKalmanGain() - Method in class org.orekit.estimation.sequential.KalmanModel
Get the physical Kalman gain matrix.
getPhysicalMeasurementJacobian() - Method in class org.orekit.estimation.sequential.DSSTKalmanModel
Get the physical Jacobian of the measurement with respect to the state (H matrix).
getPhysicalMeasurementJacobian() - Method in interface org.orekit.estimation.sequential.KalmanEstimation
Get the physical Jacobian of the measurement with respect to the state (H matrix).
getPhysicalMeasurementJacobian() - Method in class org.orekit.estimation.sequential.KalmanModel
Get the physical Jacobian of the measurement with respect to the state (H matrix).
getPhysicalStateTransitionMatrix() - Method in class org.orekit.estimation.sequential.DSSTKalmanModel
Get physical state transition matrix between previous state and estimated (but not yet corrected) state.
getPhysicalStateTransitionMatrix() - Method in interface org.orekit.estimation.sequential.KalmanEstimation
Get physical state transition matrix between previous state and estimated (but not yet corrected) state.
getPhysicalStateTransitionMatrix() - Method in class org.orekit.estimation.sequential.KalmanModel
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() - Method in interface org.orekit.bodies.CelestialBodies
Get the Pluto singleton body.
getPluto() - Static method in class org.orekit.bodies.CelestialBodyFactory
Get the Pluto singleton body.
getPluto() - Method in class org.orekit.bodies.LazyLoadedCelestialBodies
 
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.
getPositionAngleType() - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator
Get propagation parameter type.
getPositionAngleType() - Method in class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator
Get propagation parameter type.
getPositionScale() - Method in class org.orekit.propagation.conversion.AbstractPropagatorBuilder
Get the position scale.
getPotential(SpacecraftState) - Method in class org.orekit.propagation.numerical.cr3bp.CR3BPForceModel
Calculate spacecraft potential.
getPotential(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.numerical.cr3bp.CR3BPForceModel
Calculate spacecraft potential.
getPrecessionFunction() - Method in enum org.orekit.utils.IERSConventions
Get the function computing the precession angles.
getPrecessionFunction(TimeScales) - Method in enum org.orekit.utils.IERSConventions
Get the function computing the precession angles.
getPredictedMeasurement() - Method in class org.orekit.estimation.sequential.DSSTKalmanModel
Get the predicted measurement.
getPredictedMeasurement() - Method in interface org.orekit.estimation.sequential.KalmanEstimation
Get the predicted measurement.
getPredictedMeasurement() - Method in class org.orekit.estimation.sequential.KalmanModel
Get the predicted measurement.
getPredictedSpacecraftStates() - Method in class org.orekit.estimation.sequential.DSSTKalmanModel
Get the predicted spacecraft states.
getPredictedSpacecraftStates() - Method in interface org.orekit.estimation.sequential.KalmanEstimation
Get the predicted spacecraft states.
getPredictedSpacecraftStates() - Method in class org.orekit.estimation.sequential.KalmanModel
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.weather.GlobalPressureTemperature2Model
Returns the pressure at the station [hPa].
getPressure() - Method in class org.orekit.models.earth.weather.GlobalPressureTemperatureModel
Get the atmospheric pressure of the station depending its position.
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.
getPrimary() - Method in class org.orekit.bodies.CR3BPSystem
Get the primary CelestialBody.
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.BeidouAlmanac
 
getPRN() - Method in class org.orekit.gnss.GalileoAlmanac
 
getPRN() - Method in class org.orekit.gnss.GPSAlmanac
 
getPRN() - Method in class org.orekit.gnss.IRNSSAlmanac
 
getPRN() - Method in class org.orekit.gnss.QZSSAlmanac
 
getPRN() - Method in interface org.orekit.propagation.analytical.gnss.GNSSOrbitalElements
Gets the PRN number of the GNSS satellite.
getPRN() - Method in interface org.orekit.propagation.analytical.gnss.SBASOrbitalElements
Gets the PRN number of the SBAS satellite.
getPrnNumber() - Method in class org.orekit.gnss.antenna.SatelliteAntenna
Get PRN number.
getPrnNumber() - Method in class org.orekit.gnss.CombinedObservationDataSet
Get PRN number.
getPrnNumber() - Method in class org.orekit.gnss.ObservationDataSet
Get PRN number.
getPRNNumbers() - Method in class org.orekit.gnss.SEMParser
Gets the PRN numbers of all the GPS almanacs read from the file.
getPRNNumbers() - Method in class org.orekit.gnss.YUMAParser
Gets the PRN numbers of all the GPS almanacs read from the file.
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(boolean) - Method in class org.orekit.estimation.sequential.KalmanEstimator
Get the propagator parameters supported by this estimator.
getPropagationParametersDrivers() - Method in class org.orekit.propagation.conversion.AbstractPropagatorBuilder
Get the drivers for the configurable propagation parameters.
getPropagationParametersDrivers() - Method in interface org.orekit.propagation.conversion.PropagatorBuilder
Get the drivers for the configurable propagation parameters.
getPropagationParametersEvolution() - Method in class org.orekit.estimation.sequential.UnivariateProcessNoise
Getter for the propagationParametersEvolution.
getPropagator(ObservableSatellite) - Method in class org.orekit.estimation.measurements.generation.Generator
Get a registered propagator.
getPropagator() - Method in interface org.orekit.files.general.EphemerisFile.EphemerisSegment
View this ephemeris segment as a propagator.
getPropagator() - Method in interface org.orekit.files.general.EphemerisFile.SatelliteEphemeris
View this ephemeris as a propagator, combining data from all segments.
getPropagator() - Method in class org.orekit.files.sp3.SP3File.SP3Ephemeris
 
getPropagator() - Method in class org.orekit.propagation.analytical.AdapterPropagator
Get the reference propagator.
getPropagatorIndex() - Method in class org.orekit.estimation.measurements.ObservableSatellite
Get the index of the propagator related to this satellite.
getPropagatorList() - Method in class org.orekit.utils.AbstractMultipleShooting
Get the list of propagators.
getPropagatorParametersDrivers(boolean) - Method in class org.orekit.estimation.leastsquares.BatchLSEstimator
Get the propagator parameters supported by this estimator.
getPropagators() - Method in class org.orekit.propagation.PropagatorsParallelizer
Get an unmodifiable list of the underlying mono-satellite propagators.
getPropulsionModel() - Method in class org.orekit.forces.maneuvers.Maneuver
Get the propulsion model.
getProvider(boolean, int, int) - Method in class org.orekit.forces.gravity.potential.EGMFormatReader
Get a provider for read spherical harmonics coefficients.
getProvider(boolean, int, int) - Method in class org.orekit.forces.gravity.potential.GRGSFormatReader
Get a provider for read spherical harmonics coefficients.
getProvider(boolean, int, int) - Method in class org.orekit.forces.gravity.potential.ICGEMFormatReader
Get a provider for read spherical harmonics coefficients.
getProvider(boolean, int, int) - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
Get a provider for read spherical harmonics coefficients.
getProvider(boolean, int, int) - Method in class org.orekit.forces.gravity.potential.SHMFormatReader
Get a provider for read spherical harmonics coefficients.
getProvider() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonal
Get the spherical harmonics provider.
getProviders() - Method in class org.orekit.data.DataProvidersManager
Get an unmodifiable view of the list of supported providers.
getProximityAngle() - Method in class org.orekit.propagation.events.AngularSeparationDetector
Get the proximity angle (rad).
getPVCoordinates() - Method in class org.orekit.files.ccsds.OPMFile
Get the position/velocity coordinates contained in the OPM.
getPVCoordinates(AbsoluteDate, Frame) - Method in class org.orekit.frames.TopocentricFrame
Get the PVCoordinates of the topocentric frame origin in the selected frame.
getPVCoordinates(Frame) - Method in class org.orekit.orbits.FieldOrbit
Get the TimeStampedPVCoordinates in a specified frame.
getPVCoordinates(FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.orbits.FieldOrbit
Get the FieldPVCoordinates of the body in the selected frame.
getPVCoordinates() - Method in class org.orekit.orbits.FieldOrbit
Get the TimeStampedPVCoordinates in definition frame.
getPVCoordinates(Frame) - Method in class org.orekit.orbits.Orbit
Get the TimeStampedPVCoordinates in a specified frame.
getPVCoordinates(AbsoluteDate, Frame) - Method in class org.orekit.orbits.Orbit
Get the PVCoordinates of the body in the selected frame.
getPVCoordinates() - Method in class org.orekit.orbits.Orbit
Get the TimeStampedPVCoordinates in definition frame.
getPVCoordinates(AbsoluteDate, Frame) - Method in class org.orekit.propagation.AbstractPropagator
Get the PVCoordinates of the body in the selected frame.
getPVCoordinates(AbsoluteDate, Frame) - Method in class org.orekit.propagation.analytical.AggregateBoundedPropagator
 
getPVCoordinates(AbsoluteDate, Frame) - Method in class org.orekit.propagation.analytical.Ephemeris
Get the PVCoordinates of the body in the selected frame.
getPVCoordinates(AbsoluteDate) - Method in class org.orekit.propagation.analytical.tle.TLEPropagator
Get the extrapolated position and velocity from an initial TLE.
getPVCoordinates(FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.propagation.FieldAbstractPropagator
Get the FieldPVCoordinates of the body in the selected frame.
getPVCoordinates() - Method in class org.orekit.propagation.FieldSpacecraftState
Get the TimeStampedFieldPVCoordinates in orbit definition frame.
getPVCoordinates(Frame) - Method in class org.orekit.propagation.FieldSpacecraftState
Get the TimeStampedFieldPVCoordinates in given output frame.
getPVCoordinates(FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.propagation.integration.FieldIntegratedEphemeris
Get the FieldPVCoordinates 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(FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.propagation.numerical.FieldNumericalPropagator
Get the FieldPVCoordinates of the body in the selected frame.
getPVCoordinates(AbsoluteDate, Frame) - Method in class org.orekit.propagation.numerical.NumericalPropagator
Get the PVCoordinates of the body in the selected frame.
getPVCoordinates() - Method in class org.orekit.propagation.SpacecraftState
Get the TimeStampedPVCoordinates in orbit definition frame.
getPVCoordinates(Frame) - Method in class org.orekit.propagation.SpacecraftState
Get the TimeStampedPVCoordinates in given output frame.
getPVCoordinates() - Method in class org.orekit.utils.AbsolutePVCoordinates
Get the TimeStampedPVCoordinates.
getPVCoordinates(Frame) - Method in class org.orekit.utils.AbsolutePVCoordinates
Get the TimeStampedPVCoordinates in a specified frame.
getPVCoordinates(AbsoluteDate, Frame) - Method in class org.orekit.utils.AbsolutePVCoordinates
 
getPVCoordinates(FieldAbsoluteDate<T>, Frame) - Method in interface org.orekit.utils.ExtendedPVCoordinatesProvider
Get the FieldPVCoordinates of the body in the selected frame.
getPVCoordinates() - Method in class org.orekit.utils.FieldAbsolutePVCoordinates
Get the TimeStampedFieldPVCoordinates.
getPVCoordinates(Frame) - Method in class org.orekit.utils.FieldAbsolutePVCoordinates
Get the TimeStampedFieldPVCoordinates in a specified frame.
getPVCoordinates(FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.utils.FieldAbsolutePVCoordinates
 
getPVCoordinates(FieldAbsoluteDate<T>, Frame) - Method in interface org.orekit.utils.FieldPVCoordinatesProvider
Get the FieldPVCoordinates 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.
getPVCoordinatesProvider() - Method in class org.orekit.propagation.events.AlignmentDetector
Get the body to align.
getPVInPZ90(SpacecraftState) - Method in class org.orekit.propagation.numerical.GLONASSNumericalPropagator
This method transforms the PV coordinates obtained after the numerical integration in the ECEF PZ-90.
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
Deprecated.
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 .
getPZ9011(IERSConventions, boolean) - Method in class org.orekit.frames.AbstractFrames
 
getPZ9011(IERSConventions, boolean) - Method in interface org.orekit.frames.Frames
Get the PZ-90.11 (Parametry Zemly – 1990.11) reference frame.
getPZ9011(IERSConventions, boolean) - Static method in class org.orekit.frames.FramesFactory
Get the PZ-90.11 (Parametry Zemly – 1990.11) reference frame.
getQ() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
Get the x component of inclination vector.
getQ() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldAuxiliaryElements
Get the x component of inclination vector.
getQuaternion() - Method in class org.orekit.files.ccsds.APMFile
Get the quaternion.
getQuaternionDot() - Method in class org.orekit.files.ccsds.APMFile
Get the derivative of the quaternion.
getQuaternionFrameAString() - Method in class org.orekit.files.ccsds.APMFile
Get the reference frame specifying one frame of the transformation.
getQuaternionFrameBString() - Method in class org.orekit.files.ccsds.APMFile
Get the reference frame specifying the second portion of the transformation.
getQZSS() - Method in class org.orekit.time.LazyLoadedTimeScales
 
getQZSS() - Method in interface org.orekit.time.TimeScales
Get the Quasi-Zenith Satellite System time scale.
getQZSS() - Static method in class org.orekit.time.TimeScalesFactory
Get the Quasi-Zenith Satellite System time scale.
getQzssEpoch() - Method in class org.orekit.time.AbstractTimeScales
 
getQzssEpoch() - Method in interface org.orekit.time.TimeScales
Reference epoch for QZSS weeks: 1980-01-06T00:00:00 QZSS time.
getQZSSOrbitalElements() - Method in class org.orekit.propagation.analytical.gnss.QZSSPropagator
Gets the underlying QZSS orbital elements.
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(Vector3D, Frame, AbsoluteDate) - Method in class org.orekit.frames.TopocentricFrame
Get the range of a point with regards to the topocentric frame center point.
getRange(FieldVector3D<T>, Frame, FieldAbsoluteDate<T>) - Method in class org.orekit.frames.TopocentricFrame
Get the range of a point with regards to the topocentric frame center point.
getRange1() - Method in class org.orekit.estimation.iod.IodGooding
Get the range for observation (1).
getRange2() - Method in class org.orekit.estimation.iod.IodGooding
Get the range for observation (2).
getRange3() - Method in class org.orekit.estimation.iod.IodGooding
Get the range for observation (3).
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(PVCoordinates, Frame, AbsoluteDate) - Method in class org.orekit.frames.TopocentricFrame
Get the range rate of a point with regards to the topocentric frame center point.
getRangeRate(FieldPVCoordinates<T>, Frame, FieldAbsoluteDate<T>) - Method in class org.orekit.frames.TopocentricFrame
Get the range rate of a point with regards to the topocentric frame center point.
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.
getRateFrameString() - Method in class org.orekit.files.ccsds.AEMFile.AttitudeEphemeridesBlock
Get the rate frame specifier as it appeared in the file.
getRateFrameString() - Method in class org.orekit.files.ccsds.APMFile
Get the frame of reference in which the Euler angles are expressed.
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.CombinedObservationDataSet
Get receiver clock offset.
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.
getRealAPV(AbsolutePVCoordinates, AbsoluteDate, Frame) - Method in class org.orekit.bodies.CR3BPSystem
Get the AbsolutePVCoordinates from normalized units to standard units in an output frame.
getReceiveBand() - Method in class org.orekit.files.ccsds.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.
getRefFrameAString() - Method in class org.orekit.files.ccsds.AEMFile.AttitudeEphemeridesBlock
Get the reference frame A specifier as it appeared in the file.
getRefFrameBString() - Method in class org.orekit.files.ccsds.AEMFile.AttitudeEphemeridesBlock
Get the reference frame B specifier as it appeared in the file.
getRefFrameString() - Method in class org.orekit.files.ccsds.APMFile.APMManeuver
Get Coordinate system for the torque 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.
getResults() - Method in class org.orekit.estimation.measurements.gnss.AbstractCycleSlipDetector
Get on all the results computed by the detector (e.g.: dates of cycle-slip).
getRetrogradeFactor() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
Get the retrograde factor.
getRetrogradeFactor() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldAuxiliaryElements
Get the retrograde factor.
getRevAtEpoch() - Method in class org.orekit.files.ccsds.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).
getRnml(T, int, int, int, int, int) - Static method in class org.orekit.propagation.semianalytical.dsst.utilities.UpperBounds
Get the upper bound value Rεn,m,l(γ).
getRolloverReference() - Static method in class org.orekit.time.GNSSDate
Get the reference date ensuring continuity across GNSS week rollover.
getRoot() - Static method in class org.orekit.frames.Frame
Get the unique root frame.
getRotatingFrame() - Method in class org.orekit.bodies.CR3BPSystem
Get the CR3BP Rotating Frame.
getRotation() - Method in class org.orekit.attitudes.Attitude
Get the attitude rotation.
getRotation() - Method in class org.orekit.attitudes.FieldAttitude
Get the attitude rotation.
getRotation() - Method in class org.orekit.frames.FieldTransform
Get the underlying elementary rotation.
getRotation() - Method in class org.orekit.frames.Transform
Get the underlying elementary rotation.
getRotation() - Method in class org.orekit.utils.AngularCoordinates
Get the rotation.
getRotation() - Method in class org.orekit.utils.FieldAngularCoordinates
Get the rotation.
getRotationAcceleration() - Method in class org.orekit.attitudes.Attitude
Get the satellite rotation acceleration.
getRotationAcceleration() - Method in class org.orekit.attitudes.FieldAttitude
Get the satellite rotation acceleration.
getRotationAcceleration() - Method in class org.orekit.frames.FieldTransform
Get the second time derivative of the rotation.
getRotationAcceleration() - Method in class org.orekit.frames.Transform
Get the second time derivative of the rotation.
getRotationAcceleration() - Method in class org.orekit.utils.AngularCoordinates
Get the rotation acceleration.
getRotationAcceleration() - Method in class org.orekit.utils.FieldAngularCoordinates
Get the rotation acceleration.
getRotationAngles() - Method in class org.orekit.files.ccsds.APMFile
Get the coordinates of the Euler angles (rad).
getRotationOrder() - Method in class org.orekit.files.ccsds.AEMFile.AttitudeEphemeridesBlock
Get the rotation order for Euler angles.
getRotationOrder(String) - Static method in enum org.orekit.files.ccsds.AEMParser.AEMRotationOrder
Get the rotation order for the given name.
getRotationRate() - Method in class org.orekit.frames.FieldTransform
Get the first time derivative of the rotation.
getRotationRate() - Method in class org.orekit.frames.Transform
Get the first time derivative of the rotation.
getRotationRate() - Method in class org.orekit.utils.AngularCoordinates
Get the rotation rate.
getRotationRate() - Method in class org.orekit.utils.FieldAngularCoordinates
Get the rotation rate.
getRotationRates() - Method in class org.orekit.files.ccsds.APMFile
Get the rates of the Euler angles (rad/s).
getS() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.CoefficientsFactory.NSKey
Get s.
getS10(AbsoluteDate) - Method in interface org.orekit.models.earth.atmosphere.JB2008InputParameters
Get the EUV index (26-34 nm) scaled to F10.
getS10B(AbsoluteDate) - Method in interface org.orekit.models.earth.atmosphere.JB2008InputParameters
Get the EUV 81-day averaged centered index.
getSample() - Method in class org.orekit.propagation.conversion.AbstractPropagatorConverter
Get the states sample.
getSatConfiguration() - Method in class org.orekit.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.
getSatelliteName() - Method in class org.orekit.estimation.measurements.gnss.CycleSlipDetectorResults
Get the satellite name.
getSatelliteNumber() - Method in class org.orekit.propagation.analytical.tle.TLE
Get the satellite id.
getSatelliteRevolution() - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator
Get the number of satellite revolutions to use for converting osculating to mean elements.
getSatelliteRevolution() - Method in class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator
Get the number of satellite revolutions to use for converting osculating to mean elements.
getSatellites() - Method in class org.orekit.estimation.measurements.AbstractMeasurement
Get the satellites related to this measurement.
getSatellites() - Method in class org.orekit.estimation.measurements.generation.AbstractMeasurementBuilder
Get the satellites related to this measurement.
getSatellites() - Method in interface org.orekit.estimation.measurements.ObservedMeasurement
Get the satellites related to this measurement.
getSatellites() - Method in class org.orekit.files.ccsds.AEMFile
Get the attitude loaded ephemeris for each satellite in the file.
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 class org.orekit.gnss.CombinedObservationDataSet
Get Satellite System.
getSatelliteSystem() - Method in enum org.orekit.gnss.Frequency
Get the satellite system for which this frequency is defined.
getSatelliteSystem() - Method in class org.orekit.gnss.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() - Method in interface org.orekit.bodies.CelestialBodies
Get the Saturn singleton body.
getSaturn() - Static method in class org.orekit.bodies.CelestialBodyFactory
Get the Saturn singleton body.
getSaturn() - Method in class org.orekit.bodies.LazyLoadedCelestialBodies
 
getSBASOrbitalElements() - Method in class org.orekit.propagation.analytical.gnss.SBASPropagator
Get the underlying SBAS orbital elements.
getScale() - Method in class org.orekit.utils.ParameterDriver
Get scale.
getSecInDay() - Method in class org.orekit.time.GLONASSDate
Get the number of seconds since Na start.
getSecond() - Method in class org.orekit.time.TimeComponents
Get the seconds number.
getSecondary() - Method in class org.orekit.bodies.CR3BPSystem
Get the secondary CelestialBody.
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.AEMFile.AemSatelliteEphemeris
Get the segments of the attitude ephemeris.
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.
getSelectedCoefficients() - Method in class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator
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.EpochDerivativesEquations
Get the selected parameters, in Jacobian matrix column order.
getSelectedParameters() - Method in class org.orekit.propagation.numerical.PartialDerivativesEquations
Get the selected parameters, in Jacobian matrix column order.
getSelectedParameters() - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPartialDerivativesEquations
Get the selected parameters, in Jacobian matrix column order.
getSelectedPropagationDriversForBuilder(int) - Method in class org.orekit.estimation.leastsquares.BatchLSModel
Get the selected propagation drivers for a propagatorBuilder.
getSelectedPropagationDriversForBuilder(int) - Method in interface org.orekit.estimation.leastsquares.BatchLSODModel
Get the selected propagation drivers for a propagatorBuilder.
getSelectedPropagationDriversForBuilder(int) - Method in class org.orekit.estimation.leastsquares.DSSTBatchLSModel
Get the selected propagation drivers for a propagatorBuilder.
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.
getSignalCode() - Method in enum org.orekit.gnss.ObservationType
Get the signal code.
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.
getSingularPoints() - Method in class org.orekit.models.earth.tessellation.AlongTrackAiming
Get points at which aiming direction cannot be computed.
getSingularPoints() - Method in class org.orekit.models.earth.tessellation.ConstantAzimuthAiming
Get points at which aiming direction cannot be computed.
getSingularPoints() - Method in class org.orekit.models.earth.tessellation.DivertedSingularityAiming
Get points at which aiming direction cannot be computed.
getSingularPoints() - Method in interface org.orekit.models.earth.tessellation.TileAiming
Get points at which aiming direction cannot be computed.
getSiteLocation() - Method in class org.orekit.models.earth.displacement.OceanLoadingCoefficients
Get the site location.
getSiteName() - Method in class org.orekit.models.earth.displacement.OceanLoadingCoefficients
Get the site name.
getSites() - Method in class org.orekit.models.earth.displacement.OceanLoadingCoefficientsBLQFactory
Get the list of sites for which we have found coefficients, in lexicographic order ignoring case.
getSize() - Method in class org.orekit.estimation.measurements.gnss.AbstractLambdaMethod
Get the size of the problem.
getSize() - Method in class org.orekit.utils.LoveNumbers
Get the size of the arrays.
getSj(int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.CjSjCoefficient
Get the Sj coefficient.
getSj(int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldCjSjCoefficient
Get the Sj coefficient.
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.BeidouAlmanac
 
getSma() - Method in class org.orekit.gnss.GalileoAlmanac
 
getSma() - Method in class org.orekit.gnss.GPSAlmanac
 
getSma() - Method in class org.orekit.gnss.IRNSSAlmanac
 
getSma() - Method in class org.orekit.gnss.QZSSAlmanac
 
getSma() - Method in interface org.orekit.propagation.analytical.gnss.GNSSOrbitalElements
Gets the Semi-Major Axis.
getSma() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
Get the semi-major axis.
getSma() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldAuxiliaryElements
Get the semi-major axis.
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() - Method in interface org.orekit.bodies.CelestialBodies
Get the solar system barycenter aggregated body.
getSolarSystemBarycenter() - Static method in class org.orekit.bodies.CelestialBodyFactory
Get the solar system barycenter aggregated body.
getSolarSystemBarycenter() - Method in class org.orekit.bodies.LazyLoadedCelestialBodies
 
getSolidPoleTide(EOPHistory) - Method in enum org.orekit.utils.IERSConventions
Get the function computing solid pole tide (ΔC₂₁, ΔS₂₁).
getSolution() - Method in class org.orekit.estimation.measurements.gnss.IntegerLeastSquareSolution
Get the solution array.
getSolutionsSize() - Method in class org.orekit.estimation.measurements.gnss.AbstractLambdaMethod
Get the number of solutions found.
getSource() - Method in class org.orekit.gnss.GPSAlmanac
Gets the source of this GPS almanac.
getSource() - Method in class org.orekit.gnss.QZSSAlmanac
Gets the source of this QZSS 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.forces.drag.DragForce
Get spacecraft that are sensitive to atmospheric drag forces.
getSpacecraft() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTAtmosphericDrag
Get spacecraft shape.
getSpacecraft() - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTSolarRadiationPressure
Get spacecraft shape.
getSpacecraftComment() - Method in class org.orekit.files.ccsds.APMFile
Get the comment for spacecraft.
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.
getSpinAlpha() - Method in class org.orekit.files.ccsds.APMFile
Get the right ascension of spin axis vector (rad).
getSpinAngle() - Method in class org.orekit.files.ccsds.APMFile
Get the phase of the satellite about the spin axis (rad).
getSpinAngleVel() - Method in class org.orekit.files.ccsds.APMFile
Get the angular velocity of satellite around spin axis (rad/s).
getSpinComment() - Method in class org.orekit.files.ccsds.APMFile
Get the comment for spin data.
getSpinDelta() - Method in class org.orekit.files.ccsds.APMFile
Get the declination of the spin axis vector (rad).
getSpinDirection() - Method in class org.orekit.files.ccsds.APMFile
Get the rotation direction of the Spin angles.
getSpinFrameAString() - Method in class org.orekit.files.ccsds.APMFile
Get the reference frame specifying one frame of the transformation (spin).
getSpinFrameBString() - Method in class org.orekit.files.ccsds.APMFile
Get the reference frame specifying the second portion of the transformation (spin).
getSquaredDistance() - Method in class org.orekit.estimation.measurements.gnss.IntegerLeastSquareSolution
Get the squared distance to the corresponding float solution.
getStandardModel(double, double) - Static method in class org.orekit.models.earth.troposphere.MariniMurrayModel
Create a new Marini-Murray model using a standard atmosphere model.
getStandardModel(double, double) - Static method in class org.orekit.models.earth.troposphere.MendesPavlisModel
Create a new Mendes-Pavlis model using a standard atmosphere model.
getStandardModel() - Static method in class org.orekit.models.earth.troposphere.SaastamoinenModel
Create a new Saastamoinen model using a standard atmosphere model.
getStart() - Method in class org.orekit.estimation.measurements.generation.AbstractMeasurementBuilder
Get the start of the measurements time span.
getStart() - Method in class org.orekit.files.ccsds.AEMFile.AemSatelliteEphemeris
Get the start date of the attitude ephemeris.
getStart() - Method in class org.orekit.files.ccsds.AEMFile.AttitudeEphemeridesBlock
Get the start date of this attitude data segment.
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.forces.maneuvers.trigger.DateBasedManeuverTriggers
Get the start date.
getStartDate() - Method in class org.orekit.frames.EOPHistory
Get the date of the first available Earth Orientation Parameters.
getStartDate() - Method in class org.orekit.propagation.AbstractPropagator
Get the start date.
getStartDate() - Method in class org.orekit.propagation.FieldAbstractPropagator
Get the start date.
getStartFiringDetector() - Method in class org.orekit.forces.maneuvers.trigger.EventBasedManeuverTriggers
Getter for the start firing detector.
getStartTime() - Method in class org.orekit.files.ccsds.AEMFile.AttitudeEphemeridesBlock
Get start of total time span covered by attitude data.
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(IonosphericModel) - Method in class org.orekit.estimation.measurements.modifiers.IonosphericDSConverter
Deprecated.
Get the state with the number of parameters consistent with ionospheric model.
getState(IonosphericModel) - Method in class org.orekit.estimation.measurements.modifiers.IonosphericGradientConverter
Get the state with the number of parameters consistent with ionospheric model.
getState(DiscreteTroposphericModel) - Method in class org.orekit.estimation.measurements.modifiers.TroposphericDSConverter
Deprecated.
Get the state with the number of parameters consistent with tropospheric model.
getState(DiscreteTroposphericModel) - Method in class org.orekit.estimation.measurements.modifiers.TroposphericGradientConverter
Get the state with the number of parameters consistent with tropospheric model.
getState() - Method in class org.orekit.propagation.events.EventsLogger.LoggedEvent
Get the triggering state.
getState() - Method in class org.orekit.propagation.events.FieldEventsLogger.FieldLoggedEvent
Get the triggering state.
getState() - Method in class org.orekit.propagation.events.handlers.FieldRecordAndContinue.Event
Get the spacecraft's state at the event.
getState() - Method in class org.orekit.propagation.events.handlers.RecordAndContinue.Event
Get the spacecraft's state at the event.
getStateDerivatives(int) - Method in class org.orekit.estimation.measurements.EstimatedMeasurement
Get the partial derivatives of the simulated measurement with respect to state Cartesian coordinates.
getStateJacobian(SpacecraftState, double[][]) - Method in class org.orekit.propagation.integration.AbstractJacobiansMapper
Get the Jacobian with respect to state from a one-dimensional additional state array.
getStateJacobian(SpacecraftState, double[][]) - Method in class org.orekit.propagation.numerical.JacobiansMapper
Get the Jacobian with respect to state from a one-dimensional additional state array.
getStateJacobian(SpacecraftState, double[][]) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTJacobiansMapper
Get the Jacobian with respect to state from a one-dimensional additional state array.
getStates() - Method in class org.orekit.estimation.measurements.EstimatedMeasurement
Get the states of the spacecrafts.
getStateSize() - Method in class org.orekit.estimation.measurements.EstimatedMeasurement
Get state size.
getStateTransitionMatrix(SpacecraftState) - Method in class org.orekit.propagation.numerical.cr3bp.STMEquations
Method returning the State Transition Matrix.
getStation() - Method in class org.orekit.estimation.measurements.AngularAzEl
Get the ground station from which measurement is performed.
getStation() - Method in class org.orekit.estimation.measurements.AngularRaDec
Get the ground station from which measurement is performed.
getStation() - Method in class org.orekit.estimation.measurements.gnss.Phase
Get the ground station from which measurement is performed.
getStation() - Method in class org.orekit.estimation.measurements.Range
Get the ground station from which measurement is performed.
getStation() - Method in class org.orekit.estimation.measurements.RangeRate
Get the ground station from which measurement is performed.
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.AEMFile.AemSatelliteEphemeris
Get the end date of the attitude ephemeris.
getStop() - Method in class org.orekit.files.ccsds.AEMFile.AttitudeEphemeridesBlock
Get the end date of this attitude data segment.
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.
getStopFiringDetector() - Method in class org.orekit.forces.maneuvers.trigger.EventBasedManeuverTriggers
Getter for the stop firing detector.
getStopTime() - Method in class org.orekit.files.ccsds.AEMFile.AttitudeEphemeridesBlock
Get end of total time span covered by attitude data.
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.
getStream(T) - Method in class org.orekit.data.AbstractListCrawler
Get the stream to read from an input.
getStream(File) - Method in class org.orekit.data.FilesListCrawler
Get the stream to read from an input.
getStream(URL) - Method in class org.orekit.data.NetworkCrawler
Get the stream to read from an input.
getStreamOpener() - Method in class org.orekit.data.NamedData
Get the data stream opener.
getStrengthLevel() - Method in class org.orekit.models.earth.atmosphere.data.MarshallSolarActivityFutureEstimation
Get the strength level for activity.
getStuffReference() - Method in class org.orekit.estimation.measurements.gnss.AbstractCycleSlipDetector
Get the stuff (all the things needed for, the detector).
getSun() - Method in interface org.orekit.bodies.CelestialBodies
Get the Sun singleton body.
getSun() - Static method in class org.orekit.bodies.CelestialBodyFactory
Get the Sun singleton body.
getSun() - Method in class org.orekit.bodies.LazyLoadedCelestialBodies
 
getSunEarthCR3BP() - Static method in class org.orekit.bodies.CR3BPFactory
Get the Sun-Earth CR3BP singleton bodies pair.
getSunJupiterCR3BP() - Static method in class org.orekit.bodies.CR3BPFactory
Get the Sun-Jupiter CR3BP singleton bodies pair.
getSupportedNames() - Method in class org.orekit.data.AbstractSelfFeedingLoader
Get the supported names regular expression.
getSupportedNames() - Method in class org.orekit.forces.gravity.potential.AstronomicalAmplitudeReader
Get the regular expression for supported files names.
getSupportedNames() - Method in class org.orekit.forces.gravity.potential.OceanTidesReader
Get the regular expression for supported files names.
getSupportedNames() - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
Get the regular expression for supported files names.
getSupportedNames() - Method in class org.orekit.gnss.SEMParser
 
getSupportedNames() - Method in class org.orekit.gnss.YUMAParser
 
getSupportedNames() - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherData
 
getSupportedNames() - Method in class org.orekit.models.earth.atmosphere.data.MarshallSolarActivityFutureEstimation
 
getSupportedNames() - Method in class org.orekit.models.earth.ionosphere.KlobucharIonoCoefficientsLoader
 
getSupportedNames() - Method in class org.orekit.models.earth.troposphere.ViennaModelCoefficientsLoader
 
getSVN() - Method in class org.orekit.gnss.GPSAlmanac
Gets the satellite "SVN" reference number.
getSystem(CelestialBody, CelestialBody, double) - Static method in class org.orekit.bodies.CR3BPFactory
Get the corresponding CR3BP System.
getTabDensity() - Method in class org.orekit.models.earth.atmosphere.HarrisPriester
Get the current density table.
getTable() - Method in class org.orekit.attitudes.TabulatedLofOffset
Get an unmodifiable view of the tabulated attitudes.
getTAI() - Method in class org.orekit.time.LazyLoadedTimeScales
 
getTAI() - Method in interface org.orekit.time.TimeScales
Get the International Atomic Time scale.
getTAI() - Static method in class org.orekit.time.TimeScalesFactory
Get the International Atomic Time scale.
getTargetPV(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.BodyCenterPointing
Compute the target point position/velocity in specified frame.
getTargetPV(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.BodyCenterPointing
Compute the target point position/velocity in specified frame.
getTargetPV(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.GroundPointing
Compute the target point position/velocity in specified frame.
getTargetPV(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.GroundPointing
Compute the target point position/velocity in specified frame.
getTargetPV(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.LofOffsetPointing
Compute the target point position/velocity in specified frame.
getTargetPV(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.LofOffsetPointing
Compute the target point position/velocity in specified frame.
getTargetPV(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.NadirPointing
Compute the target point position/velocity in specified frame.
getTargetPV(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.NadirPointing
Compute the target point position/velocity in specified frame.
getTargetPV(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.TargetPointing
Compute the target point position/velocity in specified frame.
getTargetPV(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.TargetPointing
Compute the target point position/velocity in specified frame.
getTargetPV(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.YawCompensation
Compute the target point position/velocity in specified frame.
getTargetPV(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.YawCompensation
Compute the target point position/velocity in specified frame.
getTargetPV(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.YawSteering
Compute the target point position/velocity in specified frame.
getTargetPV(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.YawSteering
Compute the target point position/velocity in specified frame.
getTargetSize() - Method in class org.orekit.propagation.conversion.AbstractPropagatorConverter
Get the size of the target.
getTauMultiplier() - Method in class org.orekit.models.earth.displacement.Tide
Get the multiplier for the τ Doodson argument.
getTC() - Method in class org.orekit.data.DelaunayArguments
Get the offset in Julian centuries.
getTC() - Method in class org.orekit.data.FieldDelaunayArguments
Get the offset in Julian centuries.
getTCB() - Method in class org.orekit.time.LazyLoadedTimeScales
 
getTCB() - Method in interface org.orekit.time.TimeScales
Get the Barycentric Coordinate Time scale.
getTCB() - Static method in class org.orekit.time.TimeScalesFactory
Get the Barycentric Coordinate Time scale.
getTCG() - Method in class org.orekit.time.LazyLoadedTimeScales
 
getTCG() - Method in interface org.orekit.time.TimeScales
Get the Geocentric Coordinate Time scale.
getTCG() - Static method in class org.orekit.time.TimeScalesFactory
Get the Geocentric Coordinate Time scale.
getTDB() - Method in class org.orekit.time.LazyLoadedTimeScales
 
getTDB() - Method in interface org.orekit.time.TimeScales
Get the Barycentric Dynamic Time scale.
getTDB() - Static method in class org.orekit.time.TimeScalesFactory
Get the Barycentric Dynamic Time scale.
getTdim() - Method in class org.orekit.bodies.CR3BPSystem
Get the CR3BP orbital period of m2 around m1.
getTdop() - Method in class org.orekit.gnss.DOP
Gets the time dilution of precision.
getTEC(AbsoluteDate, GeodeticPoint) - Method in class org.orekit.models.earth.ionosphere.GlobalIonosphereMapModel
Computes the Total Electron Content (TEC) at a given date by performing a temporal interpolation with the two closest date in the IONEX file.
getTEC(FieldAbsoluteDate<T>, GeodeticPoint) - Method in class org.orekit.models.earth.ionosphere.GlobalIonosphereMapModel
Computes the Total Electron Content (TEC) at a given date by performing a temporal interpolation with the two closest date in the IONEX file.
getTEME() - Method in class org.orekit.frames.AbstractFrames
 
getTEME() - Method in interface org.orekit.frames.Frames
Get the TEME reference frame.
getTEME() - Static method in class org.orekit.frames.FramesFactory
Get the TEME reference frame.
getTemperature() - Method in class org.orekit.models.earth.EarthStandardAtmosphereRefraction
Get the local temperature at the evaluation location.
getTemperature() - Method in class org.orekit.models.earth.weather.GlobalPressureTemperature2Model
Returns the temperature at the station [K].
getTemperature() - Method in class org.orekit.models.earth.weather.GlobalPressureTemperatureModel
Get the atmospheric temperature of the station depending its position.
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.
getTGD() - Method in interface org.orekit.propagation.analytical.gnss.IRNSSOrbitalElements
Gets the estimated group delay differential TGD for L5-S correction.
getTGD() - Method in interface org.orekit.propagation.analytical.gnss.QZSSOrbitalElements
Gets the estimated group delay differential TGD between SV clock and L1C/A.
getTGD1() - Method in interface org.orekit.propagation.analytical.gnss.BeidouOrbitalElements
Gets the estimated group delay differential TGD1 for B1I signal.
getTGD2() - Method in interface org.orekit.propagation.analytical.gnss.BeidouOrbitalElements
Gets the estimated group delay differential TGD for B2I signal.
getTheoreticalStandardDeviation() - Method in class org.orekit.estimation.measurements.AbstractMeasurement
Get the theoretical standard deviation.
getTheoreticalStandardDeviation() - Method in class org.orekit.estimation.measurements.generation.AbstractMeasurementBuilder
Get the theoretical standard deviation.
getTheoreticalStandardDeviation() - Method in interface org.orekit.estimation.measurements.ObservedMeasurement
Get the theoretical standard deviation.
getTheta0() - Method in class org.orekit.models.earth.EarthITU453AtmosphereRefraction
Get the station elevation angle under free-space propagation .
getThetaMin() - Method in class org.orekit.models.earth.EarthITU453AtmosphereRefraction
Get the station minimal elevation angle.
getThreeHourlyAp() - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherDataLoader.LineParameters
Gets the array of the eight three-hourly Ap indices for the current entry.
getThreeHourlyAp(int) - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherDataLoader.LineParameters
Gets the three-hourly Ap index at index i from the threeHourlyAp array.
getThreeHourlyKP(AbsoluteDate) - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherData
Get the value of the 3 hours geomagnetic index.
getThreeHourlyKp() - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherDataLoader.LineParameters
Gets the array of the eight three-hourly Kp indices for the current entry.
getThreeHourlyKp(int) - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherDataLoader.LineParameters
Gets the three-hourly Kp index at index i from the threeHourlyKp array.
getThreeHourlyKP(AbsoluteDate) - Method in class org.orekit.models.earth.atmosphere.data.MarshallSolarActivityFutureEstimation
Get the value of the 3 hours geomagnetic index.
getThreeHourlyKP(AbsoluteDate) - Method in interface org.orekit.models.earth.atmosphere.DTM2000InputParameters
Get the value of the 3 hours geomagnetic index.
getThreshold() - Method in class org.orekit.propagation.events.AbstractDetector
Get the convergence threshold in the event time search.
getThreshold() - Method in class org.orekit.propagation.events.AdapterDetector
Get the convergence threshold in the event time search.
getThreshold() - Method in interface org.orekit.propagation.events.EventDetector
Get the convergence threshold in the event time search.
getThreshold() - Method in class org.orekit.propagation.events.FieldAbstractDetector
Get the convergence threshold in the event time search.
getThreshold() - Method in interface org.orekit.propagation.events.FieldEventDetector
Get the convergence threshold in the event time search.
getThrust() - Method in class org.orekit.forces.maneuvers.ConfigurableLowThrustManeuver
Get the thrust.
getThrust() - Method in class org.orekit.forces.maneuvers.ConstantThrustManeuver
Get the thrust.
getThrust() - Method in class org.orekit.forces.maneuvers.propulsion.AbstractConstantThrustPropulsionModel
Get the thrust value (N).
getThrust(SpacecraftState) - Method in interface org.orekit.forces.maneuvers.propulsion.ThrustPropulsionModel
Get the thrust norm (N).
getThrustDirectionProvider() - Method in class org.orekit.forces.maneuvers.ConfigurableLowThrustManeuver
Getter on Thrust direction and spaceraft attitude provided by an external object.
getThrusterAxisInSatelliteFrame() - Method in class org.orekit.forces.maneuvers.propulsion.ThrustDirectionAndAttitudeProvider
Thruster axis in satellite frame.
getThrustVector() - Method in class org.orekit.forces.maneuvers.ConstantThrustManeuver
Get the thrust vector (N) in S/C frame.
getThrustVector(SpacecraftState) - Method in class org.orekit.forces.maneuvers.propulsion.AbstractConstantThrustPropulsionModel
Get the thrust vector in spacecraft frame (N).
getThrustVector(SpacecraftState, double[]) - Method in class org.orekit.forces.maneuvers.propulsion.AbstractConstantThrustPropulsionModel
Get the thrust vector in spacecraft frame (N).
getThrustVector(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.maneuvers.propulsion.AbstractConstantThrustPropulsionModel
Get the thrust vector in spacecraft frame (N).
getThrustVector() - Method in class org.orekit.forces.maneuvers.propulsion.AbstractConstantThrustPropulsionModel
Get the thrust vector in spacecraft frame (N).
getThrustVector(double[]) - Method in class org.orekit.forces.maneuvers.propulsion.AbstractConstantThrustPropulsionModel
Get the thrust vector in spacecraft frame (N).
getThrustVector(T[]) - Method in class org.orekit.forces.maneuvers.propulsion.AbstractConstantThrustPropulsionModel
Get the thrust vector in spacecraft frame (N).
getThrustVector() - Method in class org.orekit.forces.maneuvers.propulsion.BasicConstantThrustPropulsionModel
Get the thrust vector in spacecraft frame (N).
getThrustVector(double[]) - Method in class org.orekit.forces.maneuvers.propulsion.BasicConstantThrustPropulsionModel
Get the thrust vector in spacecraft frame (N).
getThrustVector(T[]) - Method in class org.orekit.forces.maneuvers.propulsion.BasicConstantThrustPropulsionModel
Get the thrust vector in spacecraft frame (N).
getThrustVector() - Method in class org.orekit.forces.maneuvers.propulsion.ScaledConstantThrustPropulsionModel
Get the thrust vector in spacecraft frame (N).
getThrustVector(double[]) - Method in class org.orekit.forces.maneuvers.propulsion.ScaledConstantThrustPropulsionModel
Get the thrust vector in spacecraft frame (N).
getThrustVector(T[]) - Method in class org.orekit.forces.maneuvers.propulsion.ScaledConstantThrustPropulsionModel
Get the thrust vector in spacecraft frame (N).
getThrustVector(SpacecraftState) - Method in interface org.orekit.forces.maneuvers.propulsion.ThrustPropulsionModel
Get the thrust vector in spacecraft frame (N).
getThrustVector(SpacecraftState, double[]) - Method in interface org.orekit.forces.maneuvers.propulsion.ThrustPropulsionModel
Get the thrust vector in spacecraft frame (N).
getThrustVector(FieldSpacecraftState<T>, T[]) - Method in interface org.orekit.forces.maneuvers.propulsion.ThrustPropulsionModel
Get the thrust vector in spacecraft frame (N).
getTidalDisplacementFrequencyCorrectionDiurnal() - Method in enum org.orekit.utils.IERSConventions
Get the correction function for tidal displacement for diurnal tides.
getTidalDisplacementFrequencyCorrectionDiurnal(String, int, int, int, int, int) - Static method in enum org.orekit.utils.IERSConventions
Get the correction function for tidal displacement for diurnal tides.
getTidalDisplacementFrequencyCorrectionZonal() - Method in enum org.orekit.utils.IERSConventions
Get the correction function for tidal displacement for zonal tides.
getTidalDisplacementFrequencyCorrectionZonal(String, int, int, int, int, int) - Static method in enum org.orekit.utils.IERSConventions
Get the correction function for tidal displacement for zonal tides.
getTide(int, int) - Method in class org.orekit.models.earth.displacement.OceanLoadingCoefficients
Get the tide.
getTideFrequencyDependenceFunction(TimeScale) - Method in enum org.orekit.utils.IERSConventions
Get the function computing frequency dependent terms (ΔC₂₀, ΔC₂₁, ΔS₂₁, ΔC₂₂, ΔS₂₂).
getTideFrequencyDependenceFunction(TimeScale, TimeScales) - Method in enum org.orekit.utils.IERSConventions
Get the function computing frequency dependent terms (ΔC₂₀, ΔC₂₁, ΔS₂₁, ΔC₂₂, ΔS₂₂).
getTideSystem() - Method in class org.orekit.forces.gravity.HolmesFeatherstoneAttractionModel
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.BeidouAlmanac
 
getTime() - Method in class org.orekit.gnss.GalileoAlmanac
 
getTime() - Method in class org.orekit.gnss.GLONASSAlmanac
 
getTime() - Method in class org.orekit.gnss.GLONASSEphemeris
 
getTime() - Method in class org.orekit.gnss.GPSAlmanac
 
getTime() - Method in class org.orekit.gnss.IRNSSAlmanac
 
getTime() - Method in class org.orekit.gnss.QZSSAlmanac
 
getTime() - Method in interface org.orekit.propagation.analytical.gnss.GLONASSOrbitalElements
Get the Reference Time.
getTime() - Method in interface org.orekit.propagation.analytical.gnss.GNSSOrbitalElements
Gets the Reference Time of the GNSS orbit as a duration from week start.
getTime() - Method in interface org.orekit.propagation.analytical.gnss.SBASOrbitalElements
Gets the Reference Time of the SBAS orbit in GPS seconds of the week.
getTime() - Method in class org.orekit.time.DateTimeComponents
Get the time component.
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.ADMMetaData
Get the time scale.
getTimeScale() - Method in class org.orekit.files.ccsds.AEMFile.AttitudeEphemeridesBlock
Get the time scale for this data segment.
getTimeScale(IERSConventions) - Method in enum org.orekit.files.ccsds.CcsdsTimeScale
Get the corresponding TimeScale.
getTimeScale(IERSConventions, TimeScales) - Method in enum org.orekit.files.ccsds.CcsdsTimeScale
Get the corresponding TimeScale.
getTimeScale() - Method in class org.orekit.files.ccsds.ODMMetaData
Get the time scale.
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
 
getTimeScales() - Method in class org.orekit.data.CompositeDataContext
 
getTimeScales() - Method in interface org.orekit.data.DataContext
Get a factory for constructing TimeScales based on the auxiliary data in this context.
getTimeScales() - Method in class org.orekit.data.ExceptionalDataContext
 
getTimeScales() - Method in class org.orekit.data.LazyLoadedDataContext
 
getTimeScales() - Method in class org.orekit.frames.AbstractFrames
Get the time scales.
getTimeScales() - Method in class org.orekit.frames.EOPHistory
Get the time scales used in computing EOP corrections.
getTimeScales() - Static method in class org.orekit.time.TimeScalesFactory
Get the instance of TimeScales that is called by all of the static methods in this class.
getTimeScaleString() - Method in class org.orekit.files.ccsds.AEMFile.AttitudeEphemeridesBlock
Get the time scale for this data segment.
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.ADMMetaData
Get the Time System.
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) - Method in class org.orekit.frames.AbstractFrames
 
getTIRF(IERSConventions, boolean) - Method in class org.orekit.frames.AbstractFrames
 
getTIRF(IERSConventions) - Method in interface org.orekit.frames.Frames
Get the TIRF reference frame, ignoring tidal effects.
getTIRF(IERSConventions, boolean) - Method in interface org.orekit.frames.Frames
Get the TIRF reference frame.
getTIRF(IERSConventions) - Static method in class org.orekit.frames.FramesFactory
Get the TIRF reference frame, ignoring tidal effects.
getTIRF(IERSConventions, boolean) - Static method in class org.orekit.frames.FramesFactory
Get the TIRF reference frame.
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.
getTN() - Method in interface org.orekit.propagation.analytical.gnss.GLONASSOrbitalElements
Get the correction to the satellite time relative to GLONASS system time.
getToc() - Method in interface org.orekit.propagation.analytical.gnss.GNSSOrbitalElements
Gets the clock correction reference time toc.
getToc() - Method in interface org.orekit.propagation.analytical.gnss.SBASOrbitalElements
Gets the clock correction reference time toc.
getTOD(boolean) - Method in class org.orekit.frames.AbstractFrames
 
getTOD(IERSConventions, boolean) - Method in class org.orekit.frames.AbstractFrames
 
getTOD(boolean) - Method in interface org.orekit.frames.Frames
Get the TOD reference frame.
getTOD(IERSConventions, boolean) - Method in interface org.orekit.frames.Frames
Get the TOD reference frame.
getTOD(boolean) - Static method in class org.orekit.frames.FramesFactory
Get the TOD reference frame.
getTOD(IERSConventions, boolean) - Static method in class org.orekit.frames.FramesFactory
Get the TOD reference frame.
getTopocentricFrame() - Method in class org.orekit.propagation.events.ElevationDetector
Returns the currently configured topocentric frame definitions.
getTopocentricFrame() - Method in class org.orekit.propagation.events.ElevationExtremumDetector
Returns the topocentric frame centered on ground point.
getTopocentricFrame() - Method in class org.orekit.propagation.events.FieldElevationDetector
Returns the currently configured topocentric frame definitions.
getTorque() - Method in class org.orekit.files.ccsds.APMFile.APMManeuver
Get the torque vector (N.m).
getTotalEclipse() - Method in class org.orekit.propagation.events.EclipseDetector
Get the total eclipse detection flag.
getTotalEclipse() - Method in class org.orekit.propagation.events.FieldEclipseDetector
Get the total eclipse detection flag.
getTotalIntensity() - Method in class org.orekit.models.earth.GeoMagneticElements
Returns the total intensity of the magnetic field (= norm of the field vector).
getTransform(AbsoluteDate) - Method in class org.orekit.estimation.measurements.EstimatedEarthFrameProvider
Get the Transform corresponding to specified date.
getTransform(FieldAbsoluteDate<T>) - Method in class org.orekit.estimation.measurements.EstimatedEarthFrameProvider
Get the FieldTransform corresponding to specified date.
getTransform(FieldAbsoluteDate<DerivativeStructure>, DSFactory, Map<String, Integer>) - Method in class org.orekit.estimation.measurements.EstimatedEarthFrameProvider
getTransform(FieldAbsoluteDate<Gradient>, int, Map<String, Integer>) - Method in class org.orekit.estimation.measurements.EstimatedEarthFrameProvider
Get the transform with derivatives.
getTransform(AbsoluteDate) - Method in class org.orekit.frames.EclipticProvider
 
getTransform(FieldAbsoluteDate<T>) - Method in class org.orekit.frames.EclipticProvider
 
getTransform(AbsoluteDate) - Method in class org.orekit.frames.FixedTransformProvider
Get the Transform corresponding to specified date.
getTransform(FieldAbsoluteDate<T>) - Method in class org.orekit.frames.FixedTransformProvider
Get the FieldTransform corresponding to specified date.
getTransform(AbsoluteDate) - Method in class org.orekit.frames.GTODProvider
Get the Transform corresponding to specified date.
getTransform(FieldAbsoluteDate<T>) - Method in class org.orekit.frames.GTODProvider
Get the FieldTransform corresponding to specified date.
getTransform(AbsoluteDate) - Method in class org.orekit.frames.HelmertTransformation
Get the Transform corresponding to specified date.
getTransform(FieldAbsoluteDate<T>) - Method in class org.orekit.frames.HelmertTransformation
Get the FieldTransform corresponding to specified date.
getTransform(AbsoluteDate) - Method in class org.orekit.frames.InterpolatingTransformProvider
Get the Transform corresponding to specified date.
getTransform(FieldAbsoluteDate<T>) - Method in class org.orekit.frames.InterpolatingTransformProvider
Get the FieldTransform corresponding to specified date.
getTransform(AbsoluteDate) - Method in class org.orekit.frames.ITRFVersion.Converter
Get the Transform corresponding to specified date.
getTransform(FieldAbsoluteDate<T>) - Method in class org.orekit.frames.ITRFVersion.Converter
Get the FieldTransform corresponding to specified date.
getTransform(AbsoluteDate) - Method in class org.orekit.frames.L1TransformProvider
Get the Transform corresponding to specified date.
getTransform(FieldAbsoluteDate<T>) - Method in class org.orekit.frames.L1TransformProvider
Get the FieldTransform corresponding to specified date.
getTransform(AbsoluteDate) - Method in class org.orekit.frames.ShiftingTransformProvider
Get the Transform corresponding to specified date.
getTransform(FieldAbsoluteDate<T>) - Method in class org.orekit.frames.ShiftingTransformProvider
Get the FieldTransform corresponding to specified date.
getTransform(AbsoluteDate) - Method in interface org.orekit.frames.TransformProvider
Get the Transform corresponding to specified date.
getTransform(FieldAbsoluteDate<T>) - Method in interface org.orekit.frames.TransformProvider
Get the FieldTransform corresponding to specified date.
getTransformation() - Method in enum org.orekit.frames.HelmertTransformation.Predefined
Get the underlying HelmertTransformation.
getTransformation(TimeScale) - 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.forces.drag.TimeSpanDragForce
Get the TimeSpanMap.Transitions of the drag sensitive time span map.
getTransitions() - Method in class org.orekit.models.earth.troposphere.TimeSpanEstimatedTroposphericModel
Get the TimeSpanMap.Transitions of the tropospheric model time span map.
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.
getTriggeredEnd() - Method in class org.orekit.forces.maneuvers.trigger.EventBasedManeuverTriggers
Getter for the triggered date of engine stop.
getTriggeredIncreasing() - Method in enum org.orekit.propagation.events.FilterType
Get the increasing status of triggered events.
getTriggeredStart() - Method in class org.orekit.forces.maneuvers.trigger.EventBasedManeuverTriggers
Getter triggered date of engine start.
getTroposphericModel(AbsoluteDate) - Method in class org.orekit.models.earth.troposphere.TimeSpanEstimatedTroposphericModel
Get the EstimatedTroposphericModel model valid at a date.
getTrueAnomaly() - Method in class org.orekit.orbits.FieldKeplerianOrbit
Get the true anomaly.
getTrueAnomaly() - Method in class org.orekit.orbits.KeplerianOrbit
Get the true anomaly.
getTrueAnomalyDot() - Method in class org.orekit.orbits.FieldKeplerianOrbit
Get the true anomaly derivative.
getTrueAnomalyDot() - Method in class org.orekit.orbits.KeplerianOrbit
Get the true anomaly derivative.
getTT() - Method in class org.orekit.time.LazyLoadedTimeScales
 
getTT() - Method in interface org.orekit.time.TimeScales
Get the Terrestrial Time scale.
getTT() - Static method in class org.orekit.time.TimeScalesFactory
Get the Terrestrial Time scale.
getTurnaroundDenominator() - Method in class org.orekit.files.ccsds.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(int, int) - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory
Get the gravity field coefficients provider from the first supported file.
getUnnormalizedProvider(double, double, TideSystem, double[][], double[][]) - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory
Create a time-independent UnnormalizedSphericalHarmonicsProvider from canonical coefficients.
getUnnormalizedProvider(NormalizedSphericalHarmonicsProvider) - Static method in class org.orekit.forces.gravity.potential.GravityFieldFactory
getUnnormalizedProvider(int, int) - Method in interface org.orekit.forces.gravity.potential.GravityFields
Get a gravity field unnormalized coefficients provider.
getUnnormalizedProvider(int, int) - Method in class org.orekit.forces.gravity.potential.LazyLoadedGravityFields
Get a gravity field unnormalized coefficients provider.
getUnnormalizedSnm(int, int) - Method in interface org.orekit.forces.gravity.potential.UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics
Get a spherical harmonic sine coefficient.
getUpperCaseAbbreviation() - Method in enum org.orekit.time.Month
Get the upper case three letters abbreviation.
getUpperCaseName() - Method in enum org.orekit.time.Month
Get the upper case full name.
getURA() - Method in class org.orekit.gnss.GPSAlmanac
Gets the average URA number.
getUranus() - Method in interface org.orekit.bodies.CelestialBodies
Get the Uranus singleton body.
getUranus() - Static method in class org.orekit.bodies.CelestialBodyFactory
Get the Uranus singleton body.
getUranus() - Method in class org.orekit.bodies.LazyLoadedCelestialBodies
 
getUseableStartTime() - Method in class org.orekit.files.ccsds.AEMFile.AttitudeEphemeridesBlock
Get start of useable time span covered by attitude data.
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.AEMFile.AttitudeEphemeridesBlock
Get end of useable time span covered by ephemerides data.
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.
getUsedObservationData() - Method in class org.orekit.gnss.CombinedObservationData
Get the list of observation data used to perform the combination of measurements.
getUserDefinedParameters() - Method in class org.orekit.files.ccsds.OGMFile
Get the map of user defined parameter keywords and their corresponding values.
getUT1(EOPHistory) - Method in class org.orekit.time.AbstractTimeScales
Get the Universal Time 1 scale.
getUT1(IERSConventions, boolean) - Method in class org.orekit.time.AbstractTimeScales
 
getUT1(IERSConventions, boolean) - Method in class org.orekit.time.LazyLoadedTimeScales
 
getUT1(EOPHistory) - Method in class org.orekit.time.LazyLoadedTimeScales
Get the Universal Time 1 scale.
getUT1(IERSConventions, boolean) - Method in interface org.orekit.time.TimeScales
Get the Universal Time 1 scale.
getUT1(IERSConventions, boolean) - Static method in class org.orekit.time.TimeScalesFactory
Get the Universal Time 1 scale.
getUT1(EOPHistory) - Static method in class org.orekit.time.TimeScalesFactory
Get the Universal Time 1 scale.
getUT1MinusUTC() - Method in class org.orekit.frames.EOPEntry
Get the UT1-UTC value.
getUT1MinusUTC(AbsoluteDate) - Method in class org.orekit.frames.EOPHistory
Get the UT1-UTC value.
getUT1MinusUTC(FieldAbsoluteDate<T>) - Method in class org.orekit.frames.EOPHistory
Get the UT1-UTC value.
getUtc() - Method in class org.orekit.frames.AbstractEopLoader
Get the UTC time scale.
getUTC() - Method in class org.orekit.time.LazyLoadedTimeScales
 
getUTC() - Method in interface org.orekit.time.TimeScales
Get the Universal Time Coordinate scale.
getUTC() - Static method in class org.orekit.time.TimeScalesFactory
Get the Universal Time Coordinate scale.
getUTCScale() - Method in class org.orekit.time.UT1Scale
Get the associated UTC scale.
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.
getValidUntil() - Method in class org.orekit.gnss.antenna.SatelliteAntenna
Get end of validity.
getValue() - Method in class org.orekit.estimation.sequential.MeasurementDecorator
getValue() - Method in class org.orekit.gnss.CombinedObservationData
Get the combined observed value.
getValue() - Method in class org.orekit.gnss.ObservationData
Get the observed value.
getValue(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldGammaMnsFunction
Get Γ function value.
getValue(int, int, int) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.GammaMnsFunction
Get Γ function value.
getValue(int, T) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.FieldHansenTesseralLinear
Compute the value of the Hansen coefficient Kj-n-1, s.
getValue(int, T) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.FieldHansenThirdBodyLinear
Compute the value of the Hansen coefficient K₀n, s.
getValue(int, T) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.FieldHansenZonalLinear
Get the K₀-n-1,s coefficient value.
getValue(int, double) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenTesseralLinear
Compute the value of the Hansen coefficient Kj-n-1, s.
getValue(int, double) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenThirdBodyLinear
Compute the value of the Hansen coefficient K₀n, s.
getValue(int, double) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenZonalLinear
Get the K₀-n-1,s coefficient value.
getValue(int, int, int, DerivativeStructure) - Static method in class org.orekit.propagation.semianalytical.dsst.utilities.JacobiPolynomials
Deprecated.
getValue(int, int, int, Gradient) - Static method in class org.orekit.propagation.semianalytical.dsst.utilities.JacobiPolynomials
Returns the value and derivatives of the Jacobi polynomial Plv,w evaluated at γ.
getValue(int, int, int, FieldDerivativeStructure<T>) - Static method in class org.orekit.propagation.semianalytical.dsst.utilities.JacobiPolynomials
getValue(int, int, int, FieldGradient<T>) - Static method in class org.orekit.propagation.semianalytical.dsst.utilities.JacobiPolynomials
Returns the value and derivatives of the Jacobi polynomial Plv,w evaluated at γ.
getValue(int, int, int, int) - Static method in class org.orekit.propagation.semianalytical.dsst.utilities.NewcombOperators
Get the Newcomb operator evaluated at n, s, ρ, σ.
getValue() - Method in class org.orekit.utils.ParameterDriver
Get current parameter value.
getValue(DSFactory, Map<String, Integer>) - Method in class org.orekit.utils.ParameterDriver
Deprecated.
as of 10.2, replaced by ParameterDriver.getValue(int, Map)
getValue(int, Map<String, Integer>) - Method in class org.orekit.utils.ParameterDriver
Get the value as a gradient.
getValuesSamples() - Method in class org.orekit.utils.InterpolationTableLoader
Returns a copy of the values samples for the interpolation function.
getVdim() - Method in class org.orekit.bodies.CR3BPSystem
Get the CR3BP orbital velocity of m2.
getVdop() - Method in class org.orekit.gnss.DOP
Gets the vertical dilution of precision.
getVectorF() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
Get equinoctial frame vector f.
getVectorF() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldAuxiliaryElements
Get equinoctial frame vector f.
getVectorG() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
Get equinoctial frame vector g.
getVectorG() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldAuxiliaryElements
Get equinoctial frame vector g.
getVectorW() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
Get equinoctial frame vector w.
getVectorW() - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldAuxiliaryElements
Get equinoctial frame vector w.
getVeis1950() - Method in class org.orekit.frames.AbstractFrames
 
getVeis1950() - Method in interface org.orekit.frames.Frames
Get the VEIS 1950 reference frame.
getVeis1950() - Static method in class org.orekit.frames.FramesFactory
Get the VEIS 1950 reference frame.
getVelocity() - Method in class org.orekit.estimation.measurements.PV
Get the velocity.
getVelocity() - Method in class org.orekit.files.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(AbsoluteDate, Vector3D, Frame) - Method in interface org.orekit.models.earth.atmosphere.Atmosphere
Get the inertial velocity of atmosphere molecules.
getVelocity(FieldAbsoluteDate<T>, FieldVector3D<T>, Frame) - Method in interface org.orekit.models.earth.atmosphere.Atmosphere
Get the inertial velocity of atmosphere molecules.
getVelocity() - Method in class org.orekit.utils.FieldPVCoordinates
Gets the velocity.
getVelocity() - Method in class org.orekit.utils.PVCoordinates
Gets the velocity.
getVenus() - Method in interface org.orekit.bodies.CelestialBodies
Get the Venus singleton body.
getVenus() - Static method in class org.orekit.bodies.CelestialBodyFactory
Get the Venus singleton body.
getVenus() - Method in class org.orekit.bodies.LazyLoadedCelestialBodies
 
getVersion() - Method in class org.orekit.frames.ITRFVersionLoader.ITRFVersionConfiguration
Get ITRF version.
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.weather.GlobalPressureTemperature2Model
Returns the water vapor pressure at the station [hPa].
getWavelength() - Method in class org.orekit.estimation.measurements.gnss.Phase
Get the wavelength.
getWavelength() - Method in enum org.orekit.gnss.Frequency
Get the wavelength in meters.
getWaves() - Method in class org.orekit.forces.gravity.potential.OceanTidesReader
Get the loaded waves.
getWeek() - Method in class org.orekit.gnss.BeidouAlmanac
 
getWeek() - Method in class org.orekit.gnss.GalileoAlmanac
 
getWeek() - Method in class org.orekit.gnss.GPSAlmanac
 
getWeek() - Method in class org.orekit.gnss.IRNSSAlmanac
 
getWeek() - Method in class org.orekit.gnss.QZSSAlmanac
 
getWeek() - Method in interface org.orekit.propagation.analytical.gnss.GNSSOrbitalElements
Gets the Reference Week of the GNSS orbit.
getWeek() - Method in interface org.orekit.propagation.analytical.gnss.SBASOrbitalElements
Gets the Reference Week of the SBAS orbit.
getWeekNumber() - Method in class org.orekit.time.GNSSDate
Get the week number since the GNSS reference epoch.
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.
getWideLaneCombination(SatelliteSystem) - Static method in class org.orekit.estimation.measurements.gnss.MeasurementCombinationFactory
Get the Wide-Lane combination of measurements.
getWindUp(SatelliteSystem, int, String) - Method in class org.orekit.estimation.measurements.gnss.WindUpFactory
Get a modifier for a satellite/receiver pair.
getWMM(double) - Static method in class org.orekit.models.earth.GeoMagneticFieldFactory
Get the WMM model for the given year.
getWMM(double) - Method in interface org.orekit.models.earth.GeoMagneticFields
Get the WMM model for the given year.
getWMM(double) - Method in class org.orekit.models.earth.LazyLoadedGeoMagneticFields
 
getX() - Method in class org.orekit.frames.EOPEntry
Get the X component of the pole motion.
getX() - Method in class org.orekit.geometry.fov.SmoothFieldOfView
Get the X axis defining FoV boundary.
getX() - Method in class org.orekit.gnss.GLONASSEphemeris
 
getX() - Method in interface org.orekit.propagation.analytical.gnss.GLONASSOrbitalElements
Get the ECEF-X component of satellite coordinates in PZ-90 datum.
getX() - Method in interface org.orekit.propagation.analytical.gnss.SBASOrbitalElements
Get the ECEF-X component of satellite coordinates.
getXDot() - Method in class org.orekit.gnss.GLONASSEphemeris
 
getXDot() - Method in interface org.orekit.propagation.analytical.gnss.GLONASSOrbitalElements
Get the ECEF-X component of satellite velocity vector in PZ-90 datum.
getXDot() - Method in interface org.orekit.propagation.analytical.gnss.SBASOrbitalElements
Get the ECEF-X component of satellite velocity vector.
getXDotDot() - Method in class org.orekit.gnss.GLONASSEphemeris
 
getXDotDot() - Method in interface org.orekit.propagation.analytical.gnss.GLONASSOrbitalElements
Get the GLONASS ECEF-X component of satellite acceleration vector in PZ-90 datum.
getXDotDot() - Method in interface org.orekit.propagation.analytical.gnss.SBASOrbitalElements
Get the ECEF-X component of satellite acceleration vector.
getXM10(AbsoluteDate) - Method in interface org.orekit.models.earth.atmosphere.JB2008InputParameters
Get the MG2 index scaled to F10.
getXM10B(AbsoluteDate) - Method in interface org.orekit.models.earth.atmosphere.JB2008InputParameters
Get the MG2 81-day average centered index.
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.
getXYSpXY2Function(TimeScales) - Method in enum org.orekit.utils.IERSConventions
Get the function computing the Celestial Intermediate Pole and Celestial Intermediate Origin components.
getY() - Method in class org.orekit.frames.EOPEntry
Get the Y component of the pole motion.
getY() - Method in class org.orekit.geometry.fov.SmoothFieldOfView
Get the Y axis defining FoV boundary.
getY() - Method in class org.orekit.gnss.GLONASSEphemeris
 
getY() - Method in interface org.orekit.propagation.analytical.gnss.GLONASSOrbitalElements
Get the ECEF-Y component of satellite coordinates in PZ-90 datum.
getY() - Method in interface org.orekit.propagation.analytical.gnss.SBASOrbitalElements
Get the ECEF-Y component of satellite coordinates.
getY10(AbsoluteDate) - Method in interface org.orekit.models.earth.atmosphere.JB2008InputParameters
Get the Solar X-Ray & Lya index scaled to F10.
getY10B(AbsoluteDate) - Method in interface org.orekit.models.earth.atmosphere.JB2008InputParameters
Get the Solar X-Ray & Lya 81-day ave.
getYawAngle(PVCoordinatesProvider, AbsoluteDate, Frame) - Method in class org.orekit.attitudes.YawCompensation
Compute the yaw compensation angle at date.
getYawAngle(FieldPVCoordinatesProvider<T>, FieldAbsoluteDate<T>, Frame) - Method in class org.orekit.attitudes.YawCompensation
Compute the yaw compensation angle at date.
getYDot() - Method in class org.orekit.gnss.GLONASSEphemeris
 
getYDot() - Method in interface org.orekit.propagation.analytical.gnss.GLONASSOrbitalElements
Get the ECEF-Y component of satellite velocity vector in PZ-90 datum.
getYDot() - Method in interface org.orekit.propagation.analytical.gnss.SBASOrbitalElements
Get the ECEF-Y component of satellite velocity vector.
getYDotDot() - Method in class org.orekit.gnss.GLONASSEphemeris
 
getYDotDot() - Method in interface org.orekit.propagation.analytical.gnss.GLONASSOrbitalElements
Get the GLONASS ECEF-Y component of satellite acceleration vector in PZ-90 datum.
getYDotDot() - Method in interface org.orekit.propagation.analytical.gnss.SBASOrbitalElements
Get the ECEF-Y component of satellite acceleration vector.
getYear() - Method in enum org.orekit.frames.ITRFVersion
Get the reference year of the frame version.
getYear() - Method in class org.orekit.time.DateComponents
Get the year number.
getYp() - Method in class org.orekit.frames.FieldPoleCorrection
Get the yp parameter.
getYp() - Method in class org.orekit.frames.PoleCorrection
Get the yp parameter.
getZ() - Method in class org.orekit.geometry.fov.SmoothFieldOfView
Get the Z axis defining FoV boundary.
getZ() - Method in class org.orekit.gnss.GLONASSEphemeris
 
getZ() - Method in interface org.orekit.propagation.analytical.gnss.GLONASSOrbitalElements
Get the ECEF-Z component of satellite coordinates in PZ-90 datum.
getZ() - Method in interface org.orekit.propagation.analytical.gnss.SBASOrbitalElements
Get the ECEF-Z component of satellite coordinates.
getZDot() - Method in class org.orekit.gnss.GLONASSEphemeris
 
getZDot() - Method in interface org.orekit.propagation.analytical.gnss.GLONASSOrbitalElements
Get the ECEF-Z component of satellite velocity vector in PZ-90 datum.
getZDot() - Method in interface org.orekit.propagation.analytical.gnss.SBASOrbitalElements
Get the ECEF-Z component of satellite velocity vector.
getZDotDot() - Method in class org.orekit.gnss.GLONASSEphemeris
 
getZDotDot() - Method in interface org.orekit.propagation.analytical.gnss.GLONASSOrbitalElements
Get the GLONASS ECEF-Z component of satellite acceleration vector in PZ-90 datum.
getZDotDot() - Method in interface org.orekit.propagation.analytical.gnss.SBASOrbitalElements
Get the ECEF-Z component of satellite acceleration vector.
getZenith() - Method in class org.orekit.bodies.FieldGeodeticPoint
Get the direction above the point, expressed in parent shape frame.
getZenith() - Method in class org.orekit.bodies.GeodeticPoint
Get the direction above the point, expressed in parent shape frame.
getZenith() - Method in class org.orekit.frames.TopocentricFrame
Get the zenith direction of topocentric frame, expressed in parent shape frame.
getZenithAmplitude(int, int) - Method in class org.orekit.models.earth.displacement.OceanLoadingCoefficients
Get the amplitude along zenith axis.
getZenithDelay() - Method in class org.orekit.models.earth.troposphere.ViennaModelCoefficientsLoader
Returns the zenith delay array.
getZenithOffsetDriver() - Method in class org.orekit.estimation.measurements.GroundStation
Get a driver allowing to change station position along Zenith axis.
getZenithPhase(int, int) - Method in class org.orekit.models.earth.displacement.OceanLoadingCoefficients
Get the phase along zenith axis.
getZero(Field<T>) - Static method in class org.orekit.utils.FieldPVCoordinates
Get fixed position/velocity at origin (both p, v and a are zero vectors).
getZInverseTransformationReference() - Method in class org.orekit.estimation.measurements.gnss.AbstractLambdaMethod
Get a reference to the Z inverse transformation matrix.
getZipJarCrawler(T) - Method in class org.orekit.data.AbstractListCrawler
Get a zip/jar crawler for an input.
getZipJarCrawler(File) - Method in class org.orekit.data.FilesListCrawler
Get a zip/jar crawler for an input.
getZipJarCrawler(URL) - Method in class org.orekit.data.NetworkCrawler
Get a zip/jar crawler for an input.
getZone() - Method in class org.orekit.geometry.fov.PolygonalFieldOfView
Get the interior zone.
getZone() - Method in class org.orekit.propagation.events.FootprintOverlapDetector
Get the geographic zone triggering the events.
getZone() - Method in class org.orekit.propagation.events.GeographicZoneDetector
Get the geographic zone.
GHIJjsPolynomials - Class in org.orekit.propagation.semianalytical.dsst.utilities
Compute the Gjs, Hjs, Ijs and Jjs polynomials in the equinoctial elements h, k and the direction cosines α and β and their partial derivatives with respect to k, h, α and β.
GHIJjsPolynomials(double, double, double, double) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.GHIJjsPolynomials
Create a set of Gjs, Hjs, Ijs and Jjs polynomials.
GHmsjPolynomials - Class in org.orekit.propagation.semianalytical.dsst.utilities
Compute the Gmsj and the Hmsj polynomials in the equinoctial elements h, k and the direction cosines α and β and their partial derivatives with respect to k, h, α and β.
GHmsjPolynomials(double, double, double, double, int) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.GHmsjPolynomials
Create a set of Gmsj and Hmsj polynomials.
GillIntegratorBuilder - Class in org.orekit.propagation.conversion
Builder for GillIntegrator.
GillIntegratorBuilder(double) - Constructor for class org.orekit.propagation.conversion.GillIntegratorBuilder
Build a new instance.
GlobalIonosphereMapModel - Class in org.orekit.models.earth.ionosphere
Global Ionosphere Map (GIM) model.
GlobalIonosphereMapModel(String) - Constructor for class org.orekit.models.earth.ionosphere.GlobalIonosphereMapModel
Constructor with supported names given by user.
GlobalIonosphereMapModel(String, DataProvidersManager, TimeScale) - Constructor for class org.orekit.models.earth.ionosphere.GlobalIonosphereMapModel
Constructor that uses user defined supported names and data context.
GlobalMappingFunctionModel - Class in org.orekit.models.earth.troposphere
The Global Mapping Function model for radio techniques.
GlobalMappingFunctionModel(double, double) - Constructor for class org.orekit.models.earth.troposphere.GlobalMappingFunctionModel
Build a new instance.
GlobalMappingFunctionModel(double, double, TimeScale) - Constructor for class org.orekit.models.earth.troposphere.GlobalMappingFunctionModel
Build a new instance.
GlobalPressureTemperature2Model - Class in org.orekit.models.earth.weather
The Global Pressure and Temperature 2 (GPT2) model.
GlobalPressureTemperature2Model(String, double, double, Geoid) - Constructor for class org.orekit.models.earth.weather.GlobalPressureTemperature2Model
Constructor with supported names given by user.
GlobalPressureTemperature2Model(String, double, double, Geoid, DataProvidersManager, TimeScale) - Constructor for class org.orekit.models.earth.weather.GlobalPressureTemperature2Model
Constructor with supported names and source of GPT2 auxiliary data given by user.
GlobalPressureTemperature2Model(double, double, Geoid) - Constructor for class org.orekit.models.earth.weather.GlobalPressureTemperature2Model
Constructor with default supported names.
GlobalPressureTemperatureModel - Class in org.orekit.models.earth.weather
The Global Pressure and Temperature model.
GlobalPressureTemperatureModel(double, double, Frame) - Constructor for class org.orekit.models.earth.weather.GlobalPressureTemperatureModel
Build a new instance.
GlobalPressureTemperatureModel(double, double, Frame, DataContext) - Constructor for class org.orekit.models.earth.weather.GlobalPressureTemperatureModel
Build a new instance.
Glonass - Class in org.orekit.gnss.attitude
Attitude providers for Glonass navigation satellites.
Glonass(double, AbsoluteDate, AbsoluteDate, ExtendedPVCoordinatesProvider, Frame) - Constructor for class org.orekit.gnss.attitude.Glonass
Simple constructor.
GLONASS_EPOCH - Static variable in class org.orekit.time.AbsoluteDate
Reference epoch for GLONASS four-year interval number: 1996-01-01T00:00:00 GLONASS time.
GLONASS_EPOCH - Static variable in class org.orekit.time.DateComponents
Reference epoch for GLONASS four-year interval number: 1996-01-01.
GLONASS_MU - Static variable in interface org.orekit.propagation.analytical.gnss.GLONASSOrbitalElements
Value of the Earth's universal gravitational parameter for GLONASS user in m³/s².
GLONASS_PI - Static variable in interface org.orekit.propagation.analytical.gnss.GLONASSOrbitalElements
Value of Pi for conversion from semicircles to radian.
GLONASSAlmanac - Class in org.orekit.gnss
This class holds a GLONASS almanac as read from .agl files.
GLONASSAlmanac(int, int, int, int, int, double, double, double, double, double, double, double, double, double, double) - Constructor for class org.orekit.gnss.GLONASSAlmanac
Constructor.
GLONASSAlmanac(int, int, int, int, int, double, double, double, double, double, double, double, double, double, double, TimeScale) - Constructor for class org.orekit.gnss.GLONASSAlmanac
Constructor.
GLONASSAnalyticalPropagator - Class in org.orekit.propagation.analytical.gnss
This class aims at propagating a GLONASS orbit from GLONASSOrbitalElements.
GLONASSAnalyticalPropagator.Builder - Class in org.orekit.propagation.analytical.gnss
This nested class aims at building a GLONASSPropagator.
GLONASSDate - Class in org.orekit.time
Container for date in GLONASS form.
GLONASSDate(int, int, double) - Constructor for class org.orekit.time.GLONASSDate
Build an instance corresponding to a GLONASS date.
GLONASSDate(int, int, double, TimeScale) - Constructor for class org.orekit.time.GLONASSDate
Build an instance corresponding to a GLONASS date.
GLONASSDate(AbsoluteDate) - Constructor for class org.orekit.time.GLONASSDate
Build an instance from an absolute date.
GLONASSDate(AbsoluteDate, TimeScale) - Constructor for class org.orekit.time.GLONASSDate
Build an instance from an absolute date.
GLONASSEphemeris - Class in org.orekit.gnss
Class for GLONASS ephemeris used by the GLONASSNumericalPropagator.
GLONASSEphemeris(int, int, double, double, double, double, double, double, double, double, double, double) - Constructor for class org.orekit.gnss.GLONASSEphemeris
Build a new instance.
GLONASSEphemeris(int, int, double, double, double, double, double, double, double, double, double, double, AbsoluteDate) - Constructor for class org.orekit.gnss.GLONASSEphemeris
Build a new instance.
GLONASSNumericalPropagator - Class in org.orekit.propagation.numerical
This class propagates GLONASS orbits using numerical integration.
GLONASSNumericalPropagator(GLONASSNumericalPropagator.Builder) - Constructor for class org.orekit.propagation.numerical.GLONASSNumericalPropagator
Private constructor.
GLONASSNumericalPropagator.Builder - Class in org.orekit.propagation.numerical
This nested class aims at building a GLONASSNumericalPropagator.
GLONASSOrbitalElements - Interface in org.orekit.propagation.analytical.gnss
This interface provides the minimal set of orbital elements needed by the GLONASSAnalyticalPropagator and the GLONASSNumericalPropagator.
GLONASSScale - Class in org.orekit.time
GLONASS time scale.
GMSTScale - Class in org.orekit.time
Greenwich Mean Sidereal Time.
GNSSAttitudeProvider - Interface in org.orekit.gnss.attitude
Attitude providers for navigation satellites.
GNSSDate - Class in org.orekit.time
Container for date in GNSS form.
GNSSDate(int, double, SatelliteSystem) - Constructor for class org.orekit.time.GNSSDate
Build an instance corresponding to a GNSS date.
GNSSDate(int, double, SatelliteSystem, TimeScales) - Constructor for class org.orekit.time.GNSSDate
Build an instance corresponding to a GNSS date.
GNSSDate(AbsoluteDate, SatelliteSystem) - Constructor for class org.orekit.time.GNSSDate
Build an instance from an absolute date.
GNSSDate(AbsoluteDate, SatelliteSystem, TimeScales) - Constructor for class org.orekit.time.GNSSDate
Build an instance from an absolute date.
GNSSOrbitalElements - Interface in org.orekit.propagation.analytical.gnss
This interface provides the minimal set of orbital elements needed by the AbstractGNSSPropagator.
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.
GPSAlmanac(String, int, int, int, double, double, double, double, double, double, double, double, double, double, int, int, int, AbsoluteDate) - Constructor for class org.orekit.gnss.GPSAlmanac
Constructor.
GPSBlockIIA - Class in org.orekit.gnss.attitude
Attitude providers for GPS block IIA navigation satellites.
GPSBlockIIA(double, double, AbsoluteDate, AbsoluteDate, ExtendedPVCoordinatesProvider, Frame) - Constructor for class org.orekit.gnss.attitude.GPSBlockIIA
Simple constructor.
GPSBlockIIF - Class in org.orekit.gnss.attitude
Attitude providers for GPS block IIF navigation satellites.
GPSBlockIIF(double, double, AbsoluteDate, AbsoluteDate, ExtendedPVCoordinatesProvider, Frame) - Constructor for class org.orekit.gnss.attitude.GPSBlockIIF
Simple constructor.
GPSBlockIIR - Class in org.orekit.gnss.attitude
Attitude providers for GPS block IIR navigation satellites.
GPSBlockIIR(double, AbsoluteDate, AbsoluteDate, ExtendedPVCoordinatesProvider, Frame) - Constructor for class org.orekit.gnss.attitude.GPSBlockIIR
Simple constructor.
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.
GRAPHICCombination - Class in org.orekit.estimation.measurements.gnss
GRoup And Phase Ionospheric Calibration (GRAPHIC) combination.
GravityFieldFactory - Class in org.orekit.forces.gravity.potential
Factory used to read gravity field files in several supported formats.
GravityFields - Interface in org.orekit.forces.gravity.potential
Defines methods for obtaining gravity fields.
GRGS_FILENAME - Static variable in class org.orekit.forces.gravity.potential.GravityFieldFactory
Default regular expression for GRGS files.
GRGSFormatReader - Class in org.orekit.forces.gravity.potential
Reader for the GRGS gravity field format.
GRGSFormatReader(String, boolean) - Constructor for class org.orekit.forces.gravity.potential.GRGSFormatReader
Simple constructor.
GRGSFormatReader(String, boolean, TimeScale) - Constructor for class org.orekit.forces.gravity.potential.GRGSFormatReader
Simple constructor.
GRIM5C1_EARTH_ANGULAR_VELOCITY - Static variable in interface org.orekit.utils.Constants
Earth angular velocity from GRIM5C1 model: 7.292115e-5 rad/s.
GRIM5C1_EARTH_C20 - Static variable in interface org.orekit.utils.Constants
Earth un-normalized second zonal coefficient from GRIM5C1 model: -1.082626110612609e-3.
GRIM5C1_EARTH_C30 - Static variable in interface org.orekit.utils.Constants
Earth un-normalized third zonal coefficient from GRIM5C1 model: 2.536150841690056e-6.
GRIM5C1_EARTH_C40 - Static variable in interface org.orekit.utils.Constants
Earth un-normalized fourth zonal coefficient from GRIM5C1 model: 1.61936352497151e-6.
GRIM5C1_EARTH_C50 - Static variable in interface org.orekit.utils.Constants
Earth un-normalized fifth zonal coefficient from GRIM5C1 model: 2.231013736607540e-7.
GRIM5C1_EARTH_C60 - Static variable in interface org.orekit.utils.Constants
Earth un-normalized sixth zonal coefficient from GRIM5C1 model: -5.402895357302363e-7.
GRIM5C1_EARTH_EQUATORIAL_RADIUS - Static variable in interface org.orekit.utils.Constants
Earth equatorial radius from GRIM5C1 model: 6378136.46 m.
GRIM5C1_EARTH_FLATTENING - Static variable in interface org.orekit.utils.Constants
Earth flattening from GRIM5C1 model: 1.0 / 298.25765.
GRIM5C1_EARTH_MU - Static variable in interface org.orekit.utils.Constants
Earth gravitational constant from GRIM5C1 model: 3.986004415e14 m³/s².
GroundAtNightDetector - Class in org.orekit.propagation.events
Detector for ground location being at night.
GroundAtNightDetector(TopocentricFrame, PVCoordinatesProvider, double, AtmosphericRefractionModel) - Constructor for class org.orekit.propagation.events.GroundAtNightDetector
Simple constructor.
GroundFieldOfViewDetector - Class in org.orekit.propagation.events
Finder for satellite entry/exit events with respect to a sensor Field Of View attached to an arbitrary frame.
GroundFieldOfViewDetector(Frame, FieldOfView) - Constructor for class org.orekit.propagation.events.GroundFieldOfViewDetector
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.
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
GTODProvider(IERSConventions, EOPHistory, TimeScales) - Constructor for class org.orekit.frames.GTODProvider
Simple constructor.
GzipFilter - Class in org.orekit.data
Filter for gzip compressed data.
GzipFilter() - Constructor for class org.orekit.data.GzipFilter
 

H

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.
H_X - Static variable in enum org.orekit.orbits.OrbitType
Name for inclination vector first component.
H_Y - Static variable in enum org.orekit.orbits.OrbitType
Name for inclination vector second component .
HaloOrbit - Class in org.orekit.orbits
Class calculating different parameters of a Halo Orbit.
HaloOrbit(CR3BPSystem, PVCoordinates, double) - Constructor for class org.orekit.orbits.HaloOrbit
Simple Constructor.
HaloOrbit(RichardsonExpansion, double, LibrationOrbitFamily) - Constructor for class org.orekit.orbits.HaloOrbit
Simple Constructor.
HaloXZPlaneCrossingDetector - Class in org.orekit.propagation.events
Detector for XZ Plane crossing.
HaloXZPlaneCrossingDetector(double, double) - Constructor for class org.orekit.propagation.events.HaloXZPlaneCrossingDetector
Simple Constructor.
handleStep(SpacecraftState, boolean) - Method in class org.orekit.files.ccsds.StreamingAemWriter.AEMSegment
Handle the current step.
handleStep(SpacecraftState, boolean) - Method in class org.orekit.files.ccsds.StreamingOemWriter.Segment
 
handleStep(FieldSpacecraftState<T>, boolean) - Method in interface org.orekit.propagation.sampling.FieldOrekitFixedStepHandler
Handle the current step.
handleStep(FieldSpacecraftState<T>, boolean) - Method in class org.orekit.propagation.sampling.FieldOrekitFixedStepHandlerMultiplexer
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(List<OrekitStepInterpolator>, boolean) - Method in interface org.orekit.propagation.sampling.MultiSatStepHandler
Handle the current step.
handleStep(SpacecraftState, boolean) - Method in interface org.orekit.propagation.sampling.OrekitFixedStepHandler
Handle the current step.
handleStep(SpacecraftState, boolean) - Method in class org.orekit.propagation.sampling.OrekitFixedStepHandlerMultiplexer
Handle the current step.
handleStep(OrekitStepInterpolator, boolean) - Method in interface org.orekit.propagation.sampling.OrekitStepHandler
Handle the current step.
handleStep(OrekitStepInterpolator, boolean) - Method in class org.orekit.propagation.sampling.OrekitStepHandlerMultiplexer
Handle the current step.
handleStep(OrekitStepInterpolator, boolean) - Method in class org.orekit.propagation.sampling.OrekitStepNormalizer
Handle the last accepted step.
HansenTesseralLinear - Class in org.orekit.propagation.semianalytical.dsst.utilities.hansen
Hansen coefficients K(t,n,s) for t!=0 and n < 0.
HansenTesseralLinear(int, int, int, int, int) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenTesseralLinear
Constructor.
HansenThirdBodyLinear - Class in org.orekit.propagation.semianalytical.dsst.utilities.hansen
Hansen coefficients K(t,n,s) for t=0 and n > 0.
HansenThirdBodyLinear(int, int) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenThirdBodyLinear
Constructor.
HansenUtilities - Class in org.orekit.propagation.semianalytical.dsst.utilities.hansen
Utilities class.
HansenZonalLinear - Class in org.orekit.propagation.semianalytical.dsst.utilities.hansen
Hansen coefficients K(t,n,s) for t=0 and n < 0.
HansenZonalLinear(int, int) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenZonalLinear
Constructor.
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.models.earth.atmosphere
This atmosphere model is the realization of the Modified Harris-Priester model.
HarrisPriester(PVCoordinatesProvider, OneAxisEllipsoid) - Constructor for class org.orekit.models.earth.atmosphere.HarrisPriester
Simple constructor for Modified Harris-Priester atmosphere model.
HarrisPriester(PVCoordinatesProvider, OneAxisEllipsoid, double) - Constructor for class org.orekit.models.earth.atmosphere.HarrisPriester
Constructor for Modified Harris-Priester atmosphere model.
HarrisPriester(PVCoordinatesProvider, OneAxisEllipsoid, double[][]) - Constructor for class org.orekit.models.earth.atmosphere.HarrisPriester
Constructor for Modified Harris-Priester atmosphere model.
HarrisPriester(PVCoordinatesProvider, OneAxisEllipsoid, double[][], double) - Constructor for class org.orekit.models.earth.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.estimation.measurements.gnss.IntegerLeastSquareSolution
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>, T) - 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.
HatanakaCompressFilter - Class in org.orekit.gnss
Decompression filter for Hatanaka compressed RINEX files.
HatanakaCompressFilter() - Constructor for class org.orekit.gnss.HatanakaCompressFilter
 
HELIUM - Static variable in class org.orekit.models.earth.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.
HighamHall54IntegratorBuilder - Class in org.orekit.propagation.conversion
Builder for HighamHall54Integrator.
HighamHall54IntegratorBuilder(double, double, double) - Constructor for class org.orekit.propagation.conversion.HighamHall54IntegratorBuilder
Build a new instance.
HolmesFeatherstoneAttractionModel - Class in org.orekit.forces.gravity
This class represents the gravitational field of a celestial body.
HolmesFeatherstoneAttractionModel(Frame, NormalizedSphericalHarmonicsProvider) - Constructor for class org.orekit.forces.gravity.HolmesFeatherstoneAttractionModel
Creates a new instance.
HYDROGEN - Static variable in class org.orekit.models.earth.atmosphere.DTM2000
Identifier for hydrogen.
hyperbolicEccentricToMean(T, T) - Static method in class org.orekit.orbits.FieldKeplerianOrbit
Computes the mean anomaly from the hyperbolic eccentric anomaly.
hyperbolicEccentricToMean(double, double) - Static method in class org.orekit.orbits.KeplerianOrbit
Computes the mean 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.
hyperbolicEccentricToTrue(double, double) - Static method in class org.orekit.orbits.KeplerianOrbit
Computes the true anomaly from the hyperbolic eccentric anomaly.

I

i - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator
final inclination.
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.
ICGEMFormatReader(String, boolean, TimeScale) - Constructor for class org.orekit.forces.gravity.potential.ICGEMFormatReader
Simple constructor.
IDENTITY - Static variable in class org.orekit.frames.Transform
Identity transform.
IDENTITY - Static variable in class org.orekit.utils.AngularCoordinates
Fixed orientation parallel with reference frame (identity rotation, zero rotation rate and acceleration).
IDENTITY_PROVIDER - Static variable in class org.orekit.frames.TransformProviderUtils
Identity provider.
IERS2003_EARTH_ANGULAR_VELOCITY - Static variable in interface org.orekit.utils.Constants
Earth angular velocity from IERS2003 model: 7.292115e-5 rad/s.
IERS2003_EARTH_C20 - Static variable in interface org.orekit.utils.Constants
Earth un-normalized second zonal coefficient from IERS2003 model: -1.0826359e-3.
IERS2003_EARTH_EQUATORIAL_RADIUS - Static variable in interface org.orekit.utils.Constants
Earth equatorial radius from IERS2003 model: 6378136.6 m.
IERS2003_EARTH_FLATTENING - Static variable in interface org.orekit.utils.Constants
Earth flattening from IERS2003 model: 1.0 / 298.25642.
IERS2003_EARTH_MU - Static variable in interface org.orekit.utils.Constants
Earth gravitational constant from IERS2003 model: 3.986004418e14 m³/s².
IERS2010_EARTH_ANGULAR_VELOCITY - Static variable in interface org.orekit.utils.Constants
Earth angular velocity from IERS2010 model: 7.292115e-5 rad/s.
IERS2010_EARTH_C20 - Static variable in interface org.orekit.utils.Constants
Earth un-normalized second zonal coefficient from IERS2010 model: -1.0826359e-3.
IERS2010_EARTH_EQUATORIAL_RADIUS - Static variable in interface org.orekit.utils.Constants
Earth equatorial radius from IERS2010 model: 6378136.6 m.
IERS2010_EARTH_FLATTENING - Static variable in interface org.orekit.utils.Constants
Earth flattening from IERS2010 model: 1.0 / 298.25642.
IERS2010_EARTH_MU - Static variable in interface org.orekit.utils.Constants
Earth gravitational constant from IERS2010 model: 3.986004418e14 m³/s².
IERS96_EARTH_ANGULAR_VELOCITY - Static variable in interface org.orekit.utils.Constants
Earth angular velocity from IERS96 model: 7.292115e-5 rad/s.
IERS96_EARTH_C20 - Static variable in interface org.orekit.utils.Constants
Earth un-normalized second zonal coefficient from IERS96 model: -1.0826359e-3.
IERS96_EARTH_EQUATORIAL_RADIUS - Static variable in interface org.orekit.utils.Constants
Earth equatorial radius from IERS96 model: 6378136.49 m.
IERS96_EARTH_FLATTENING - Static variable in interface org.orekit.utils.Constants
Earth flattening from IERS96 model: 1.0 / 298.25642.
IERS96_EARTH_MU - Static variable in interface org.orekit.utils.Constants
Earth gravitational constant from IERS96 model: 3.986004418e14 m³/s².
IERSConventions - Enum in org.orekit.utils
Supported IERS conventions.
IERSConventions.NutationCorrectionConverter - Interface in org.orekit.utils
Interface for functions converting nutation corrections between δΔψ/δΔε to δX/δY.
ImmutableTimeStampedCache<T extends TimeStamped> - Class in org.orekit.utils
A cache of TimeStamped data that provides concurrency through immutability.
ImmutableTimeStampedCache(int, Collection<? extends T>) - Constructor for class org.orekit.utils.ImmutableTimeStampedCache
Create a new cache with the given neighbors size and data.
ImpulseManeuver<T extends EventDetector> - Class in org.orekit.forces.maneuvers
Impulse maneuver model.
ImpulseManeuver(T, Vector3D, double) - Constructor for class org.orekit.forces.maneuvers.ImpulseManeuver
Build a new instance.
ImpulseManeuver(T, AttitudeProvider, Vector3D, double) - Constructor for class org.orekit.forces.maneuvers.ImpulseManeuver
Build a new instance.
INC - Static variable in enum org.orekit.orbits.OrbitType
Name for inclination.
InertialForces - Class in org.orekit.forces.inertia
Inertial force model.
InertialForces(Frame) - Constructor for class org.orekit.forces.inertia.InertialForces
Simple constructor.
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.
InertialProvider(Frame) - Constructor for class org.orekit.attitudes.InertialProvider
Creates new instance aligned with the given frame.
InertialProvider(Rotation, Frame) - Constructor for class org.orekit.attitudes.InertialProvider
Creates new instance with a fixed attitude in the given frame.
init(JavacTask, String...) - Method in class org.orekit.compiler.plugin.DefaultDataContextPlugin
 
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.
init(SpacecraftState, AbsoluteDate, double) - Method in class org.orekit.files.ccsds.StreamingAemWriter.AEMSegment
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) - 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.ImpulseManeuver
Initialize event handler at the start of a propagation.
init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.forces.maneuvers.Maneuver
Initialize the force model at the start of propagation.
init(SpacecraftState, AbsoluteDate) - Method in interface org.orekit.forces.maneuvers.propulsion.PropulsionModel
Initialization method.
init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.forces.maneuvers.trigger.DateBasedManeuverTriggers
Initialization method.
init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.forces.maneuvers.trigger.EventBasedManeuverTriggers
Initialization method.
init(SpacecraftState, AbsoluteDate) - Method in interface org.orekit.forces.maneuvers.trigger.ManeuverTriggers
Initialization method.
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(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(SpacecraftState, AbsoluteDate) - Method in interface org.orekit.propagation.events.handlers.EventHandler
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(SpacecraftState, AbsoluteDate) - Method in class org.orekit.propagation.events.MagneticFieldDetector
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(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>, T) - Method in interface org.orekit.propagation.sampling.FieldOrekitFixedStepHandler
Initialize step handler at the start of a propagation.
init(FieldSpacecraftState<T>, FieldAbsoluteDate<T>, T) - Method in class org.orekit.propagation.sampling.FieldOrekitFixedStepHandlerMultiplexer
Initialize step handler at the start of a 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(List<SpacecraftState>, AbsoluteDate) - Method in interface org.orekit.propagation.sampling.MultiSatStepHandler
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(SpacecraftState, AbsoluteDate, double) - Method in class org.orekit.propagation.sampling.OrekitFixedStepHandlerMultiplexer
Initialize step handler at the start of a propagation.
init(SpacecraftState, AbsoluteDate) - Method in interface org.orekit.propagation.sampling.OrekitStepHandler
Initialize step handler at the start of a propagation.
init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.propagation.sampling.OrekitStepHandlerMultiplexer
Initialize step handler at the start of a propagation.
init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.propagation.sampling.OrekitStepNormalizer
Initialize step handler at the start of a propagation.
initialIsOsculating() - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator
Check if the initial state is provided in osculating elements.
initialIsOsculating() - Method in class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator
Check if the initial state is provided in osculating elements.
initialize(boolean, FieldAbsoluteDate<T>) - Method in interface org.orekit.propagation.integration.FieldModeHandler
Initialize the mode handler.
initialize(boolean, AbsoluteDate) - Method in interface org.orekit.propagation.integration.ModeHandler
Initialize the mode handler.
initialize(AuxiliaryElements, PropagationType, double[]) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution
Performs initialization prior to propagation for the current force model.
initialize(FieldAuxiliaryElements<T>, PropagationType, T[]) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution
Performs initialization prior to propagation for the current force model.
initialize(AuxiliaryElements, PropagationType, double[]) - Method in interface org.orekit.propagation.semianalytical.dsst.forces.DSSTForceModel
Performs initialization prior to propagation for the current force model.
initialize(FieldAuxiliaryElements<T>, PropagationType, T[]) - Method in interface org.orekit.propagation.semianalytical.dsst.forces.DSSTForceModel
Performs initialization prior to propagation for the current force model.
initialize(AuxiliaryElements, PropagationType, double[]) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTNewtonianAttraction
Performs initialization prior to propagation for the current force model.
initialize(FieldAuxiliaryElements<T>, PropagationType, T[]) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTNewtonianAttraction
Performs initialization prior to propagation for the current force model.
initialize(AuxiliaryElements, PropagationType, double[]) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseral
Performs initialization prior to propagation for the current force model.
initialize(FieldAuxiliaryElements<T>, PropagationType, T[]) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseral
Performs initialization prior to propagation for the current force model.
initialize(AuxiliaryElements, PropagationType, double[]) - 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(FieldAuxiliaryElements<T>, PropagationType, T[]) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBody
Performs initialization prior to propagation for the current force model.
initialize(AuxiliaryElements, PropagationType, double[]) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonal
Performs initialization prior to propagation for the current force model.
initialize(FieldAuxiliaryElements<T>, PropagationType, T[]) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonal
Performs initialization prior to propagation for the current force model.
initializePropagation() - Method in class org.orekit.propagation.AbstractPropagator
Initialize propagation.
initializePropagation() - Method in class org.orekit.propagation.FieldAbstractPropagator
Initialize propagation.
initMapper() - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
Initialize the mapper.
initMapper(Field<T>) - 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(FieldAbsoluteDate<T>) - 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(FieldAbsoluteDate<T>) - 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.UTCScale
Check if date is within a leap second introduction in this time scale.
IntegerBootstrapping - Class in org.orekit.estimation.measurements.gnss
Bootstrapping engine for ILS problem solving.
IntegerBootstrapping(double) - Constructor for class org.orekit.estimation.measurements.gnss.IntegerBootstrapping
Constructor for the bootstrapping ambiguity estimator.
integerGaussTransformation(int, int) - Method in class org.orekit.estimation.measurements.gnss.AbstractLambdaMethod
Perform one integer Gauss transformation.
IntegerLeastSquareSolution - Class in org.orekit.estimation.measurements.gnss
Class holding a solution to an Integer Least Square problem.
IntegerLeastSquareSolution(long[], double) - Constructor for class org.orekit.estimation.measurements.gnss.IntegerLeastSquareSolution
Simple constructor.
IntegerLeastSquareSolver - Interface in org.orekit.estimation.measurements.gnss
Interface for algorithms solving integer least square problems.
IntegratedEphemeris - Class in org.orekit.propagation.integration
This class stores sequentially generated orbital parameters for later retrieval.
IntegratedEphemeris(AbsoluteDate, AbsoluteDate, AbsoluteDate, StateMapper, PropagationType, DenseOutputModel, Map<String, double[]>, List<AdditionalStateProvider>, String[]) - Constructor for class org.orekit.propagation.integration.IntegratedEphemeris
Creates a new instance of IntegratedEphemeris.
IntegratedPropagatorBuilder - Interface in org.orekit.propagation.conversion
Base class for orbit determination model builders.
INTERMEDIATE_SUFFIX - Static variable in class org.orekit.estimation.measurements.GroundStation
Suffix for ground station intermediate frame name.
interpolate(AbsoluteDate, Stream<Attitude>) - Method in class org.orekit.attitudes.Attitude
Get an interpolated instance.
interpolate(FieldAbsoluteDate<T>, Stream<FieldAttitude<T>>) - Method in class org.orekit.attitudes.FieldAttitude
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>, 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.
interpolate(AbsoluteDate, Stream<Transform>) - Method in class org.orekit.frames.Transform
Get an interpolated instance.
interpolate(AbsoluteDate, CartesianDerivativesFilter, AngularDerivativesFilter, Collection<Transform>) - Static method in class org.orekit.frames.Transform
Interpolate a transform from a sample set of existing transforms.
interpolate(AbsoluteDate, 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(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(AbsoluteDate, Stream<Orbit>) - Method in class org.orekit.orbits.KeplerianOrbit
Get an interpolated instance.
interpolate(FieldAbsoluteDate<T>, Stream<FieldSpacecraftState<T>>) - Method in class org.orekit.propagation.FieldSpacecraftState
Get an interpolated instance.
interpolate(AbsoluteDate, Stream<SpacecraftState>) - Method in class org.orekit.propagation.SpacecraftState
Get an interpolated instance.
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(AbsoluteDate, Collection<T>) - Method in interface org.orekit.time.TimeInterpolable
Get an interpolated instance.
interpolate(AbsoluteDate, Stream<T>) - Method in interface org.orekit.time.TimeInterpolable
Get an interpolated instance.
interpolate(AbsoluteDate, Stream<AbsolutePVCoordinates>) - Method in class org.orekit.utils.AbsolutePVCoordinates
 
interpolate(Frame, AbsoluteDate, CartesianDerivativesFilter, Stream<AbsolutePVCoordinates>) - Static method in class org.orekit.utils.AbsolutePVCoordinates
Interpolate position-velocity.
interpolate(FieldAbsoluteDate<T>, Stream<FieldAbsolutePVCoordinates<T>>) - Method in class org.orekit.utils.FieldAbsolutePVCoordinates
 
interpolate(Frame, FieldAbsoluteDate<T>, CartesianDerivativesFilter, Stream<FieldAbsolutePVCoordinates<T>>) - Static method in class org.orekit.utils.FieldAbsolutePVCoordinates
Interpolate position-velocity.
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(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(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.
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.
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(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.
inverseDecomposition() - Method in class org.orekit.estimation.measurements.gnss.AbstractLambdaMethod
Inverse the decomposition.
inverseDecomposition() - Method in class org.orekit.estimation.measurements.gnss.LambdaMethod
Inverse the decomposition.
inverseDecomposition() - Method in class org.orekit.estimation.measurements.gnss.ModifiedLambdaMethod
Inverse the decomposition.
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.
IodLaplace - Class in org.orekit.estimation.iod
Laplace angles-only initial orbit determination, assuming Keplerian motion.
IodLaplace(double) - Constructor for class org.orekit.estimation.iod.IodLaplace
Constructor.
IonosphereFreeCombination - Class in org.orekit.estimation.measurements.gnss
Ionosphere-free combination.
IonosphericDSConverter - Class in org.orekit.estimation.measurements.modifiers
Deprecated.
as of 10.2, replaced by IonosphericGradientConverter
IonosphericDSConverter(SpacecraftState, int, AttitudeProvider) - Constructor for class org.orekit.estimation.measurements.modifiers.IonosphericDSConverter
Deprecated.
Simple constructor.
IonosphericGradientConverter - Class in org.orekit.estimation.measurements.modifiers
Converter for states and parameters arrays.
IonosphericGradientConverter(SpacecraftState, int, AttitudeProvider) - Constructor for class org.orekit.estimation.measurements.modifiers.IonosphericGradientConverter
Simple constructor.
IonosphericMappingFunction - Interface in org.orekit.models.earth.ionosphere
Interface for mapping functions used in the ionospheric delay computation.
IonosphericModel - Interface in org.orekit.models.earth.ionosphere
Defines a ionospheric model, used to calculate the path delay imposed to electro-magnetic signals between an orbital satellite and a ground station.
IRNSS_EPOCH - Static variable in class org.orekit.time.AbsoluteDate
Reference epoch for IRNSS weeks: 1999-08-22T00:00:00 IRNSS time.
IRNSS_EPOCH - Static variable in class org.orekit.time.DateComponents
Reference epoch for IRNSS weeks: 1999-08-22.
IRNSS_MU - Static variable in interface org.orekit.propagation.analytical.gnss.IRNSSOrbitalElements
WGS 84 value of the Earth's universal gravitational parameter for IRNSS user in m³/s².
IRNSS_PI - Static variable in interface org.orekit.propagation.analytical.gnss.IRNSSOrbitalElements
Value of Pi for conversion from semicircles to radian.
IRNSS_WEEK_IN_SECONDS - Static variable in interface org.orekit.propagation.analytical.gnss.IRNSSOrbitalElements
Duration of the IRNSS week in seconds.
IRNSS_WEEK_NB - Static variable in interface org.orekit.propagation.analytical.gnss.IRNSSOrbitalElements
Number of weeks in the IRNSS cycle.
IRNSSAlmanac - Class in org.orekit.gnss
Class for IRNSS almanac.
IRNSSAlmanac(int, int, double, double, double, double, double, double, double, double, double, double, AbsoluteDate) - Constructor for class org.orekit.gnss.IRNSSAlmanac
Constructor.
IRNSSOrbitalElements - Interface in org.orekit.propagation.analytical.gnss
This interface provides the minimal set of orbital elements needed by the IRNSSPropagator.
IRNSSPropagator - Class in org.orekit.propagation.analytical.gnss
This class aims at propagating a IRNSS orbit from IRNSSOrbitalElements.
IRNSSPropagator.Builder - Class in org.orekit.propagation.analytical.gnss
This nested class aims at building a IRNSSPropagator.
IRNSSScale - Class in org.orekit.time
IRNSS time scale (also called IRNWT for IRNSS NetWork Time).
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.
isAfter(TimeStamped) - Method in class org.orekit.time.AbsoluteDate
Check if the instance represents a time that is strictly after another.
isAfter(FieldTimeStamped<T>) - Method in class org.orekit.time.FieldAbsoluteDate
Check if the instance represents a time that is strictly after another.
isAfterOrEqualTo(TimeStamped) - Method in class org.orekit.time.AbsoluteDate
Check if the instance represents a time that is after or equal to another.
isAfterOrEqualTo(FieldTimeStamped<T>) - Method in class org.orekit.time.FieldAbsoluteDate
Check if the instance represents a time that is after or equal to another.
isBefore(TimeStamped) - Method in class org.orekit.time.AbsoluteDate
Check if the instance represents a time that is strictly before another.
isBefore(FieldTimeStamped<T>) - Method in class org.orekit.time.FieldAbsoluteDate
Check if the instance represents a time that is strictly before another.
isBeforeOrEqualTo(TimeStamped) - Method in class org.orekit.time.AbsoluteDate
Check if the instance represents a time that is before or equal to another.
isBeforeOrEqualTo(FieldTimeStamped<T>) - Method in class org.orekit.time.FieldAbsoluteDate
Check if the instance represents a time that is before or equal to another.
isBetween(TimeStamped, TimeStamped) - Method in class org.orekit.time.AbsoluteDate
Check if the instance represents a time that is strictly between two others representing the boundaries of a time span.
isBetween(FieldTimeStamped<T>, FieldTimeStamped<T>) - Method in class org.orekit.time.FieldAbsoluteDate
Check if the instance represents a time that is strictly between two others representing the boundaries of a time span.
isBetweenOrEqualTo(TimeStamped, TimeStamped) - Method in class org.orekit.time.AbsoluteDate
Check if the instance represents a time that is between two others representing the boundaries of a time span, or equal to one of them.
isBetweenOrEqualTo(FieldTimeStamped<T>, FieldTimeStamped<T>) - Method in class org.orekit.time.FieldAbsoluteDate
Check if the instance represents a time that is between two others representing the boundaries of a time span, or equal to one of them.
isChildOf(Frame) - Method in class org.orekit.frames.Frame
Determine if a Frame is a child of another one.
isClosedOrbit() - Method in class org.orekit.utils.AbstractMultipleShooting
Get he flag representing if the orbit is closed.
isCloseTo(TimeStamped, double) - Method in class org.orekit.time.AbsoluteDate
Check if the instance time is close to another.
isCloseTo(FieldTimeStamped<T>, double) - Method in class org.orekit.time.FieldAbsoluteDate
Check if the instance time is close to another.
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.
isDSStateDerivative(FieldSpacecraftState<T>) - Method in class org.orekit.forces.drag.AbstractDragForceModel
Check if a field state corresponds to derivatives with respect to state.
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.
isEqualTo(TimeStamped) - Method in class org.orekit.time.AbsoluteDate
Check if the instance represents the same time as another.
isEqualTo(FieldTimeStamped<T>) - Method in class org.orekit.time.FieldAbsoluteDate
Check if the instance represents the same time as another.
isFiring(SpacecraftState) - Method in class org.orekit.forces.maneuvers.ConstantThrustManeuver
Check if maneuvering is on.
isFiring(FieldSpacecraftState<T>) - Method in class org.orekit.forces.maneuvers.ConstantThrustManeuver
Check if maneuvering is on.
isFiring(AbsoluteDate) - Method in class org.orekit.forces.maneuvers.ConstantThrustManeuver
Check if maneuvering is on.
isFiring(AbsoluteDate, double[]) - Method in class org.orekit.forces.maneuvers.trigger.DateBasedManeuverTriggers
Find out if the maneuver is firing or not.
isFiring(FieldAbsoluteDate<T>, T[]) - Method in class org.orekit.forces.maneuvers.trigger.DateBasedManeuverTriggers
 
isFiring(AbsoluteDate) - Method in class org.orekit.forces.maneuvers.trigger.DateBasedManeuverTriggers
Check if maneuvering is on.
isFiring(AbsoluteDate, double[]) - Method in class org.orekit.forces.maneuvers.trigger.EventBasedManeuverTriggers
Find out if the maneuver is firing or not.
isFiring(FieldAbsoluteDate<T>, T[]) - Method in class org.orekit.forces.maneuvers.trigger.EventBasedManeuverTriggers
Find out if the maneuver is firing or not.
isFiring(AbsoluteDate) - Method in class org.orekit.forces.maneuvers.trigger.EventBasedManeuverTriggers
Check if maneuvering is on.
isFiring(AbsoluteDate, double[]) - Method in interface org.orekit.forces.maneuvers.trigger.ManeuverTriggers
Find out if the maneuver is firing or not.
isFiring(FieldAbsoluteDate<T>, T[]) - Method in interface org.orekit.forces.maneuvers.trigger.ManeuverTriggers
Find out if the maneuver is firing or not.
isFiringOnInitialState(SpacecraftState) - Method in class org.orekit.forces.maneuvers.trigger.EventBasedManeuverTriggers
Method to check if the thruster is firing on initialization.
isFirst() - Method in class org.orekit.files.ccsds.AEMFile.AttitudeEphemeridesBlock
Get the flag for the placement of the quaternion QC in the attitude data.
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.
isForwardPropagation() - Method in class org.orekit.estimation.leastsquares.BatchLSModel
Return the forward propagation flag.
isForwardPropagation() - Method in interface org.orekit.estimation.leastsquares.BatchLSODModel
Return the forward propagation flag.
isForwardPropagation() - Method in class org.orekit.estimation.leastsquares.DSSTBatchLSModel
Return the forward propagation flag.
isGradientStateDerivative(FieldSpacecraftState<T>) - Method in class org.orekit.forces.drag.AbstractDragForceModel
Check if a field state corresponds to derivatives with respect to state.
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.FieldRecordAndContinue.Event
Is the g() function increasing?
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.
isInitialize() - Method in class org.orekit.propagation.numerical.PartialDerivativesEquations
Get the flag for the initialization of the state jacobian.
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.
isOrbitDefined() - Method in class org.orekit.propagation.FieldSpacecraftState
Check if the state contains an orbit part.
isOrbitDefined() - Method in class org.orekit.propagation.SpacecraftState
Check if the state contains an orbit part.
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.ADMParser
Get EOP interpolation method.
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.
isSimpleEop() - Method in class org.orekit.frames.EOPHistory
Determine if this history uses simplified EOP corrections.
isSupported(DataProvider) - Method in class org.orekit.data.DataProvidersManager
Check if some provider is supported.
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.
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.
isValid(int) - Method in class org.orekit.frames.ITRFVersionLoader.ITRFVersionConfiguration
Check if configuration entry is valid for a date.
isVariable(DerivativeStructure, int) - Method in class org.orekit.forces.drag.AbstractDragForceModel
Check if a derivative represents a specified variable.
isVariable(Gradient, int) - Method in class org.orekit.forces.drag.AbstractDragForceModel
Check if a derivative represents a specified variable.
ITRFVersion - Enum in org.orekit.frames
Enumerate for ITRF versions.
ITRFVersion.Converter - Class in org.orekit.frames
Specialized transform provider between ITRF frames.
ITRFVersionConfiguration(String, ITRFVersion, int, int) - Constructor for class org.orekit.frames.ITRFVersionLoader.ITRFVersionConfiguration
Simple constructor.
ITRFVersionLoader - Class in org.orekit.frames
Loader for ITRF version configuration file.
ITRFVersionLoader(String) - Constructor for class org.orekit.frames.ITRFVersionLoader
Build a loader for ITRF version configuration file.
ITRFVersionLoader(String, DataProvidersManager) - Constructor for class org.orekit.frames.ITRFVersionLoader
Build a loader for ITRF version configuration file.
ITRFVersionLoader() - Constructor for class org.orekit.frames.ITRFVersionLoader
Build a loader for ITRF version configuration file using the default name.
ITRFVersionLoader.ITRFVersionConfiguration - Class in org.orekit.frames
ITRF version configuration entry.
ItrfVersionProvider - Interface in org.orekit.frames
Interface for retrieving the ITRF version for a given set of EOP data.

J

J2000_EPOCH - Static variable in class org.orekit.time.AbsoluteDate
J2000.0 Reference epoch: 2000-01-01T12:00:00 Terrestrial Time (not UTC).
J2000_EPOCH - Static variable in class org.orekit.time.DateComponents
J2000.0 Reference epoch: 2000-01-01.
J2DifferentialEffect - Class in org.orekit.propagation.analytical
Analytical model for J2 effect.
J2DifferentialEffect(SpacecraftState, AdapterPropagator.DifferentialEffect, boolean, UnnormalizedSphericalHarmonicsProvider) - Constructor for class org.orekit.propagation.analytical.J2DifferentialEffect
Simple constructor.
J2DifferentialEffect(Orbit, Orbit, boolean, UnnormalizedSphericalHarmonicsProvider) - Constructor for class org.orekit.propagation.analytical.J2DifferentialEffect
Simple constructor.
J2DifferentialEffect(SpacecraftState, AdapterPropagator.DifferentialEffect, boolean, double, double, double) - Constructor for class org.orekit.propagation.analytical.J2DifferentialEffect
Simple constructor.
J2DifferentialEffect(Orbit, Orbit, boolean, double, double, double) - Constructor for class org.orekit.propagation.analytical.J2DifferentialEffect
Simple constructor.
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.
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.models.earth.atmosphere
This is the realization of the Jacchia-Bowman 2008 atmospheric model.
JB2008(JB2008InputParameters, PVCoordinatesProvider, BodyShape) - Constructor for class org.orekit.models.earth.atmosphere.JB2008
Constructor with space environment information for internal computation.
JB2008(JB2008InputParameters, PVCoordinatesProvider, BodyShape, TimeScale) - Constructor for class org.orekit.models.earth.atmosphere.JB2008
Constructor with space environment information for internal computation.
JB2008InputParameters - Interface in org.orekit.models.earth.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(String, JPLEphemeridesLoader.EphemerisType, DataProvidersManager, TimeScales, Frame) - 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_EPOCH - Static variable in class org.orekit.time.DateTimeComponents
The Julian Epoch.
JULIAN_YEAR - Static variable in interface org.orekit.utils.Constants
Duration of a Julian year: 365.25 Constants.JULIAN_DAY.
JUPITER - Static variable in class org.orekit.bodies.CelestialBodyFactory
Predefined name for Jupiter.
JUPITER_SEMI_MAJOR_AXIS - Static variable in interface org.orekit.propagation.numerical.cr3bp.CR3BPConstants
Jupiter semi-major axis in meters.

K

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.
KalmanModel - Class in org.orekit.estimation.sequential
Class defining the process model dynamics to use with a KalmanEstimator.
KalmanModel(List<IntegratedPropagatorBuilder>, List<CovarianceMatrixProvider>, ParameterDriversList) - Constructor for class org.orekit.estimation.sequential.KalmanModel
Kalman process model constructor (package private).
KalmanObserver - Interface in org.orekit.estimation.sequential
Observer for Kalman filter estimations.
KalmanODModel - Interface in org.orekit.estimation.sequential
Interface for models used in the Kalman orbit determination process.
KeplerianOrbit - Class in org.orekit.orbits
This class handles traditional Keplerian orbital parameters.
KeplerianOrbit(double, double, double, double, double, double, PositionAngle, Frame, AbsoluteDate, double) - Constructor for class org.orekit.orbits.KeplerianOrbit
Creates a new instance.
KeplerianOrbit(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(TimeStampedPVCoordinates, Frame, double) - Constructor for class org.orekit.orbits.KeplerianOrbit
Constructor from Cartesian parameters.
KeplerianOrbit(PVCoordinates, Frame, AbsoluteDate, double) - Constructor for class org.orekit.orbits.KeplerianOrbit
Constructor from Cartesian parameters.
KeplerianOrbit(Orbit) - Constructor for class org.orekit.orbits.KeplerianOrbit
Constructor from any kind of orbital parameters.
KeplerianPropagator - Class in org.orekit.propagation.analytical
Simple Keplerian orbit propagator.
KeplerianPropagator(Orbit) - Constructor for class org.orekit.propagation.analytical.KeplerianPropagator
Build a propagator from orbit only.
KeplerianPropagator(Orbit, double) - Constructor for class org.orekit.propagation.analytical.KeplerianPropagator
Build a propagator from orbit and central attraction coefficient μ.
KeplerianPropagator(Orbit, AttitudeProvider) - Constructor for class org.orekit.propagation.analytical.KeplerianPropagator
Build a propagator from orbit and attitude provider.
KeplerianPropagator(Orbit, AttitudeProvider, double) - Constructor for class org.orekit.propagation.analytical.KeplerianPropagator
Build a propagator from orbit, attitude provider and central attraction coefficient μ.
KeplerianPropagator(Orbit, AttitudeProvider, double, double) - Constructor for class org.orekit.propagation.analytical.KeplerianPropagator
Build propagator from orbit, attitude provider, central attraction coefficient μ and mass.
KeplerianPropagatorBuilder - Class in org.orekit.propagation.conversion
Builder for Keplerian propagator.
KeplerianPropagatorBuilder(Orbit, PositionAngle, double) - Constructor for class org.orekit.propagation.conversion.KeplerianPropagatorBuilder
Build a new instance.
KeplerianPropagatorBuilder(Orbit, PositionAngle, double, AttitudeProvider) - Constructor for class org.orekit.propagation.conversion.KeplerianPropagatorBuilder
Build a new instance.
Keyword - Enum in org.orekit.files.ccsds
Keywords for CCSDS Navigation Data Messages.
KlobucharIonoCoefficientsLoader - Class in org.orekit.models.earth.ionosphere
Loads Klobuchar-Style ionospheric coefficients a given input stream.
KlobucharIonoCoefficientsLoader(String) - Constructor for class org.orekit.models.earth.ionosphere.KlobucharIonoCoefficientsLoader
Constructor with supported names given by user.
KlobucharIonoCoefficientsLoader(String, DataProvidersManager) - Constructor for class org.orekit.models.earth.ionosphere.KlobucharIonoCoefficientsLoader
Constructor that uses user defined supported names and data context.
KlobucharIonoCoefficientsLoader() - Constructor for class org.orekit.models.earth.ionosphere.KlobucharIonoCoefficientsLoader
Constructor with default supported names.
KlobucharIonoModel - Class in org.orekit.models.earth.ionosphere
Klobuchar ionospheric delay model.
KlobucharIonoModel(double[], double[]) - Constructor for class org.orekit.models.earth.ionosphere.KlobucharIonoModel
Create a new Klobuchar ionospheric delay model, when a single frequency system is used.
KlobucharIonoModel(double[], double[], TimeScale) - Constructor for class org.orekit.models.earth.ionosphere.KlobucharIonoModel
Create a new Klobuchar ionospheric delay model, when a single frequency system is used.

L

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.
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.
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.
LagrangianPoints - Enum in org.orekit.utils
Enumerate for selecting which Lagrangian Point to consider in different classes.
LambdaMethod - Class in org.orekit.estimation.measurements.gnss
Decorrelation/reduction engine for LAMBDA method.
LambdaMethod() - Constructor for class org.orekit.estimation.measurements.gnss.LambdaMethod
 
LatitudeCrossingDetector - Class in org.orekit.propagation.events
Detector for geographic latitude crossing.
LatitudeCrossingDetector(OneAxisEllipsoid, double) - Constructor for class org.orekit.propagation.events.LatitudeCrossingDetector
Build a new detector.
LatitudeCrossingDetector(double, double, OneAxisEllipsoid, double) - Constructor for class org.orekit.propagation.events.LatitudeCrossingDetector
Build a detector.
LatitudeExtremumDetector - Class in org.orekit.propagation.events
Detector for geographic latitude extremum.
LatitudeExtremumDetector(OneAxisEllipsoid) - Constructor for class org.orekit.propagation.events.LatitudeExtremumDetector
Build a new detector.
LatitudeExtremumDetector(double, double, OneAxisEllipsoid) - Constructor for class org.orekit.propagation.events.LatitudeExtremumDetector
Build a detector.
LazyLoadedCelestialBodies - Class in org.orekit.bodies
This class lazily loads auxiliary data when it is needed by a requested body.
LazyLoadedCelestialBodies(DataProvidersManager, TimeScales, Frame) - Constructor for class org.orekit.bodies.LazyLoadedCelestialBodies
Create a celestial body factory with the given auxiliary data sources.
LazyLoadedDataContext - Class in org.orekit.data
A data context that aims to match the behavior of Orekit 10.0 regarding auxiliary data.
LazyLoadedDataContext() - Constructor for class org.orekit.data.LazyLoadedDataContext
Create a new data context that only loads auxiliary data when it is first accessed and allows configuration of the auxiliary data sources until then.
LazyLoadedEop - Class in org.orekit.frames
Loads Earth Orientation Parameters (EOP) from a configured set of EOPHistoryLoaders on demand.
LazyLoadedEop(DataProvidersManager) - Constructor for class org.orekit.frames.LazyLoadedEop
Create a new instance for loading EOP data from multiple EOPHistoryLoaders.
LazyLoadedFrames - Class in org.orekit.frames
This class lazily loads auxiliary data when it is needed by a requested frame.
LazyLoadedFrames(LazyLoadedEop, TimeScales, CelestialBodies) - Constructor for class org.orekit.frames.LazyLoadedFrames
Create a collection of frames from the given auxiliary data.
LazyLoadedGeoMagneticFields - Class in org.orekit.models.earth
Loads magnetic fields on request and can be configured after creation.
LazyLoadedGeoMagneticFields(DataProvidersManager) - Constructor for class org.orekit.models.earth.LazyLoadedGeoMagneticFields
Create a factory for magnetic fields that uses the given data manager to load magnetic field files.
LazyLoadedGravityFields - Class in org.orekit.forces.gravity.potential
Loads gravity fields when first requested and can be configured until then.
LazyLoadedGravityFields(DataProvidersManager, TimeScale) - Constructor for class org.orekit.forces.gravity.potential.LazyLoadedGravityFields
Create a factory for gravity fields that uses the given data manager to load the gravity field files.
LazyLoadedTimeScales - Class in org.orekit.time
An implementation of TimeScales that loads auxiliary data, leap seconds and UT1-UTC, when it is first accessed.
LazyLoadedTimeScales(LazyLoadedEop) - Constructor for class org.orekit.time.LazyLoadedTimeScales
Create a new set of time scales with the given sources of auxiliary data.
LibrationOrbit - Class in org.orekit.orbits
Base class for libration orbits.
LibrationOrbit(CR3BPSystem, PVCoordinates, double) - Constructor for class org.orekit.orbits.LibrationOrbit
Constructor.
LibrationOrbitFamily - Enum in org.orekit.orbits
Enumerate for Libration Orbit family.
LibrationOrbitType - Enum in org.orekit.orbits
Enumerate for Libration Orbit type.
LIFT_RATIO - Static variable in interface org.orekit.forces.drag.DragSensitive
Parameter name for lift ration enabling Jacobian processing.
lIndex(int, int) - Method in class org.orekit.estimation.measurements.gnss.AbstractLambdaMethod
Get the index of an entry in the lower triangular matrix.
LineParameters(AbsoluteDate, double[], double, double[], double, double, int, double, double, double, double, double) - Constructor for class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherDataLoader.LineParameters
Constructor.
LineReader(String, BufferedReader) - Constructor for class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherDataLoader.LineReader
Create a line reader.
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(InputStream, String) - Method in interface org.orekit.data.DataLoader
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() - Method in class org.orekit.gnss.SEMParser
Loads almanacs.
loadData(InputStream, String) - Method in class org.orekit.gnss.SEMParser
 
loadData() - Method in class org.orekit.gnss.YUMAParser
Loads almanacs.
loadData(InputStream, String) - Method in class org.orekit.gnss.YUMAParser
 
loadData(InputStream, String) - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherDataLoader
Load data from a stream.
loadData(InputStream, String) - Method in class org.orekit.models.earth.atmosphere.data.MarshallSolarActivityFutureEstimation
Load data from a stream.
loadData(InputStream, String) - Method in class org.orekit.models.earth.GeoMagneticModelLoader
Load data from a stream.
loadData(InputStream, String) - Method in class org.orekit.models.earth.ionosphere.KlobucharIonoCoefficientsLoader
Load Klobuchar-Style ionospheric coefficients read from some file.
loadData(InputStream, String) - Method in class org.orekit.models.earth.troposphere.ViennaModelCoefficientsLoader
 
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.ionosphere.KlobucharIonoCoefficientsLoader
Load the data using supported names .
loadKlobucharIonosphericCoefficients(DateComponents) - Method in class org.orekit.models.earth.ionosphere.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.
loadViennaCoefficients() - Method in class org.orekit.models.earth.troposphere.ViennaModelCoefficientsLoader
Load the data using supported names .
loadViennaCoefficients(DateTimeComponents) - Method in class org.orekit.models.earth.troposphere.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(OneAxisEllipsoid, double) - Constructor for class org.orekit.propagation.events.LongitudeCrossingDetector
Build a new detector.
LongitudeCrossingDetector(double, double, OneAxisEllipsoid, double) - Constructor for class org.orekit.propagation.events.LongitudeCrossingDetector
Build a detector.
LongitudeExtremumDetector - Class in org.orekit.propagation.events
Detector for geographic longitude extremum.
LongitudeExtremumDetector(OneAxisEllipsoid) - Constructor for class org.orekit.propagation.events.LongitudeExtremumDetector
Build a new detector.
LongitudeExtremumDetector(double, double, OneAxisEllipsoid) - Constructor for class org.orekit.propagation.events.LongitudeExtremumDetector
Build a detector.
LoveNumbers - Class in org.orekit.utils
Container for Love numbers.
LoveNumbers(double[][], double[][], double[][]) - Constructor for class org.orekit.utils.LoveNumbers
Simple constructor.
ltdlDecomposition() - Method in class org.orekit.estimation.measurements.gnss.AbstractLambdaMethod
Perform Lᵀ.D.L = Q decomposition of the covariance matrix.
ltdlDecomposition() - Method in class org.orekit.estimation.measurements.gnss.LambdaMethod
Perform Lᵀ.D.L = Q decomposition of the covariance matrix.
ltdlDecomposition() - Method in class org.orekit.estimation.measurements.gnss.ModifiedLambdaMethod
Compute the LᵀDL factorization with symmetric pivoting decomposition of Q (symmetric definite positive matrix) with a minimum symmetric pivoting: Q = ZᵀLᵀDLZ.
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.
LyapunovOrbit - Class in org.orekit.orbits
Class calculating different parameters of a Lyapunov Orbit.
LyapunovOrbit(CR3BPSystem, PVCoordinates, double) - Constructor for class org.orekit.orbits.LyapunovOrbit
Simple Constructor.
LyapunovOrbit(RichardsonExpansion, double) - Constructor for class org.orekit.orbits.LyapunovOrbit
Simple Constructor.

M

M2 - Static variable in class org.orekit.models.earth.displacement.Tide
M₂ tide.
MagneticFieldDetector - Class in org.orekit.propagation.events
Detector for South-Atlantic anomaly frontier crossing.
MagneticFieldDetector(double, GeoMagneticFieldFactory.FieldModel, OneAxisEllipsoid) - Constructor for class org.orekit.propagation.events.MagneticFieldDetector
Build a new detector.
MagneticFieldDetector(double, GeoMagneticFieldFactory.FieldModel, OneAxisEllipsoid, boolean) - Constructor for class org.orekit.propagation.events.MagneticFieldDetector
Build a new detector.
MagneticFieldDetector(double, double, double, GeoMagneticFieldFactory.FieldModel, OneAxisEllipsoid, boolean) - Constructor for class org.orekit.propagation.events.MagneticFieldDetector
Build a detector.
MagneticFieldDetector(double, double, double, GeoMagneticFieldFactory.FieldModel, OneAxisEllipsoid, boolean, DataContext) - Constructor for class org.orekit.propagation.events.MagneticFieldDetector
Build a detector.
manageData(ObservationDataSet) - Method in class org.orekit.estimation.measurements.gnss.AbstractCycleSlipDetector
The method is in charge of collecting the measurements, manage them, and call the detection method.
manageData(ObservationDataSet) - Method in class org.orekit.estimation.measurements.gnss.GeometryFreeCycleSlipDetector
The method is in charge of collecting the measurements, manage them, and call the detection method.
manageData(ObservationDataSet) - Method in class org.orekit.estimation.measurements.gnss.PhaseMinusCodeCycleSlipDetector
The method is in charge of collecting the measurements, manage them, and call the detection method.
Maneuver() - Constructor for class org.orekit.files.ccsds.OPMFile.Maneuver
Simple constructor.
Maneuver - Class in org.orekit.forces.maneuvers
A generic model for maneuvers.
Maneuver(AttitudeProvider, ManeuverTriggers, PropulsionModel) - Constructor for class org.orekit.forces.maneuvers.Maneuver
Generic maneuver constructor.
ManeuverTriggers - Interface in org.orekit.forces.maneuvers.trigger
Generic interface for the maneuver triggers used in a Maneuver.
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>, T, Frame) - Method in enum org.orekit.orbits.OrbitType
Convert state array to orbital parameters.
mapArrayToState(T, T[], T[], PropagationType) - Method in class org.orekit.propagation.integration.FieldStateMapper
Map the raw double components to a spacecraft state.
mapArrayToState(FieldAbsoluteDate<T>, T[], T[], PropagationType) - Method in class org.orekit.propagation.integration.FieldStateMapper
Map the raw double components to a spacecraft state.
mapArrayToState(double, double[], double[], PropagationType) - Method in class org.orekit.propagation.integration.StateMapper
Map the raw double components to a spacecraft state.
mapArrayToState(AbsoluteDate, double[], double[], PropagationType) - Method in class org.orekit.propagation.integration.StateMapper
Map the raw double components to a spacecraft state.
mapDateToDouble(FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.integration.FieldStateMapper
Map a date to a raw double time offset.
mapDateToDouble(AbsoluteDate) - Method in class org.orekit.propagation.integration.StateMapper
Map a date to a raw double time offset.
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.
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.
mapOrbitToArray(Orbit, PositionAngle, double[], double[]) - Method in enum org.orekit.orbits.OrbitType
Convert orbit to state array.
mapOrbitToArray(FieldOrbit<T>, PositionAngle, T[], T[]) - Method in enum org.orekit.orbits.OrbitType
Convert orbit to state array.
mappingFactor(double) - Method in interface org.orekit.models.earth.ionosphere.IonosphericMappingFunction
This method allows the computation of the ionospheric mapping factor.
mappingFactor(T) - Method in interface org.orekit.models.earth.ionosphere.IonosphericMappingFunction
This method allows the computation of the ionospheric mapping factor.
mappingFactor(double) - Method in class org.orekit.models.earth.ionosphere.SingleLayerModelMappingFunction
This method allows the computation of the ionospheric mapping factor.
mappingFactor(T) - Method in class org.orekit.models.earth.ionosphere.SingleLayerModelMappingFunction
This method allows the computation of the ionospheric mapping factor.
mappingFactors(double, double, double[], AbsoluteDate) - Method in class org.orekit.models.earth.troposphere.EstimatedTroposphericModel
 
mappingFactors(T, T, T[], FieldAbsoluteDate<T>) - Method in class org.orekit.models.earth.troposphere.EstimatedTroposphericModel
 
mappingFactors(double, double, double[], AbsoluteDate) - Method in class org.orekit.models.earth.troposphere.FixedTroposphericDelay
 
mappingFactors(T, T, T[], FieldAbsoluteDate<T>) - Method in class org.orekit.models.earth.troposphere.FixedTroposphericDelay
 
mappingFactors(double, double, double[], AbsoluteDate) - Method in class org.orekit.models.earth.troposphere.GlobalMappingFunctionModel
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.troposphere.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.troposphere.MappingFunction
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.troposphere.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.troposphere.MariniMurrayModel
 
mappingFactors(T, T, T[], FieldAbsoluteDate<T>) - Method in class org.orekit.models.earth.troposphere.MariniMurrayModel
 
mappingFactors(double, double, double[], AbsoluteDate) - Method in class org.orekit.models.earth.troposphere.MendesPavlisModel
With the Mendes Pavlis tropospheric model, the mapping function is not split into hydrostatic and wet component.
mappingFactors(T, T, T[], FieldAbsoluteDate<T>) - Method in class org.orekit.models.earth.troposphere.MendesPavlisModel
This method allows the computation of the hydrostatic and wet mapping functions.
mappingFactors(double, double, double[], AbsoluteDate) - Method in class org.orekit.models.earth.troposphere.NiellMappingFunctionModel
 
mappingFactors(T, T, T[], FieldAbsoluteDate<T>) - Method in class org.orekit.models.earth.troposphere.NiellMappingFunctionModel
 
mappingFactors(double, double, double[], AbsoluteDate) - Method in class org.orekit.models.earth.troposphere.SaastamoinenModel
 
mappingFactors(T, T, T[], FieldAbsoluteDate<T>) - Method in class org.orekit.models.earth.troposphere.SaastamoinenModel
 
mappingFactors(double, double, double[], AbsoluteDate) - Method in class org.orekit.models.earth.troposphere.TimeSpanEstimatedTroposphericModel
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.troposphere.TimeSpanEstimatedTroposphericModel
This method allows the computation of the hydrostatic and wet mapping functions.
mappingFactors(double, double, double[], AbsoluteDate) - Method in class org.orekit.models.earth.troposphere.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.troposphere.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.troposphere.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.troposphere.ViennaThreeModel
This method allows the computation of the hydrostatic and wet mapping functions.
MappingFunction - Interface in org.orekit.models.earth.troposphere
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.
MariniMurrayModel - Class in org.orekit.models.earth.troposphere
The Marini-Murray tropospheric delay model for laser ranging.
MariniMurrayModel(double, double, double, double, double) - Constructor for class org.orekit.models.earth.troposphere.MariniMurrayModel
Create a new Marini-Murray model for the troposphere using the given environmental conditions.
MARS - Static variable in class org.orekit.bodies.CelestialBodyFactory
Predefined name for Mars.
MarshallSolarActivityFutureEstimation - Class in org.orekit.models.earth.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.models.earth.atmosphere.data.MarshallSolarActivityFutureEstimation
Simple constructor.
MarshallSolarActivityFutureEstimation(String, MarshallSolarActivityFutureEstimation.StrengthLevel, DataProvidersManager, TimeScale) - Constructor for class org.orekit.models.earth.atmosphere.data.MarshallSolarActivityFutureEstimation
Constructor that allows specifying the source of the MSAFE auxiliary data files.
MarshallSolarActivityFutureEstimation.StrengthLevel - Enum in org.orekit.models.earth.atmosphere.data
Strength level of activity.
mass(double) - Method in class org.orekit.propagation.analytical.gnss.BeidouPropagator.Builder
Sets the mass.
mass(double) - Method in class org.orekit.propagation.analytical.gnss.GalileoPropagator.Builder
Sets the mass.
mass(double) - Method in class org.orekit.propagation.analytical.gnss.GLONASSAnalyticalPropagator.Builder
Sets the mass.
mass(double) - Method in class org.orekit.propagation.analytical.gnss.GPSPropagator.Builder
Sets the mass.
mass(double) - Method in class org.orekit.propagation.analytical.gnss.IRNSSPropagator.Builder
Sets the mass.
mass(double) - Method in class org.orekit.propagation.analytical.gnss.QZSSPropagator.Builder
Sets the mass.
mass(double) - Method in class org.orekit.propagation.analytical.gnss.SBASPropagator.Builder
Sets the mass.
mass(double) - Method in class org.orekit.propagation.numerical.GLONASSNumericalPropagator.Builder
Sets the mass.
MASS_RATIO_SUFFIX - Static variable in class org.orekit.propagation.numerical.cr3bp.CR3BPForceModel
Suffix for parameter name for Mass Ratio enabling Jacobian processing.
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.
MEAN_ANOM - Static variable in enum org.orekit.orbits.OrbitType
Name for mean anomaly.
MEAN_LAT_ARG - Static variable in enum org.orekit.orbits.OrbitType
Name for mean argument of latitude.
MEAN_LON_ARG - Static variable in enum org.orekit.orbits.OrbitType
Name for mean argument of longitude.
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(T, T) - Static method in class org.orekit.orbits.FieldKeplerianOrbit
Computes the elliptic eccentric anomaly from the mean anomaly.
meanToEllipticEccentric(double, double) - Static method in class org.orekit.orbits.KeplerianOrbit
Computes the elliptic 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.
meanToHyperbolicEccentric(double, double) - Static method in class org.orekit.orbits.KeplerianOrbit
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.
MeasurementCombination - Interface in org.orekit.estimation.measurements.gnss
Interface for combination of measurements.
MeasurementCombinationFactory - Class in org.orekit.estimation.measurements.gnss
Factory for predefined combination of 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.
MeasurementFilter<T extends ObservedMeasurement<T>> - Interface in org.orekit.estimation.measurements.filtering
Interface for measurement pre-processing filter.
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.
MelbourneWubbenaCombination - Class in org.orekit.estimation.measurements.gnss
Melbourne-Wübbena combination.
MendesPavlisModel - Class in org.orekit.models.earth.troposphere
The Mendes - Pavlis tropospheric delay model for optical techniques.
MendesPavlisModel(double, double, double, double, double) - Constructor for class org.orekit.models.earth.troposphere.MendesPavlisModel
Create a new Mendes-Pavlis model for the troposphere.
MERCURY - Static variable in class org.orekit.bodies.CelestialBodyFactory
Predefined name for Mercury.
MF - Static variable in class org.orekit.models.earth.displacement.Tide
Mf tide.
MidpointIntegratorBuilder - Class in org.orekit.propagation.conversion
Builder for MidpointIntegrator.
MidpointIntegratorBuilder(double) - Constructor for class org.orekit.propagation.conversion.MidpointIntegratorBuilder
Build a new instance.
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(FieldAbsoluteDate<T>) - 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(FieldAbsoluteDate<T>) - 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.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.
missingCoefficientsAllowed() - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
Check if missing coefficients are allowed in the input data.
MM - Static variable in class org.orekit.models.earth.displacement.Tide
Mm tide.
ModeHandler - Interface in org.orekit.propagation.integration
Common interface for all propagator mode handlers initialization.
modelCalled(Orbit[], Map<ObservedMeasurement<?>, EstimatedMeasurement<?>>) - Method in interface org.orekit.estimation.leastsquares.ModelObserver
Notification callback for orbit changes.
ModelObserver - Interface in org.orekit.estimation.leastsquares
Observer for model calls.
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.
ModifiedLambdaMethod - Class in org.orekit.estimation.measurements.gnss
Decorrelation/reduction engine for Modified LAMBDA method.
ModifiedLambdaMethod() - Constructor for class org.orekit.estimation.measurements.gnss.ModifiedLambdaMethod
 
modify(EstimatedMeasurement<T>) - Method in interface org.orekit.estimation.measurements.EstimationModifier
Apply a modifier to an estimated measurement.
modify(EstimatedMeasurement<Phase>) - Method in class org.orekit.estimation.measurements.gnss.WindUp
Apply a modifier to an estimated measurement.
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<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<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.OnBoardAntennaPhaseModifier
Apply a modifier to an estimated measurement.
modify(EstimatedMeasurement<Range>) - Method in class org.orekit.estimation.measurements.modifiers.OnBoardAntennaRangeModifier
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<T>) - Method in class org.orekit.estimation.measurements.modifiers.OutlierFilter
Apply a modifier to an estimated measurement.
modify(EstimatedMeasurement<Phase>) - Method in class org.orekit.estimation.measurements.modifiers.PhaseAmbiguityModifier
 
modify(EstimatedMeasurement<Phase>) - Method in class org.orekit.estimation.measurements.modifiers.PhaseIonosphericDelayModifier
 
modify(EstimatedMeasurement<Phase>) - Method in class org.orekit.estimation.measurements.modifiers.PhaseTroposphericDelayModifier
Apply a modifier to an estimated measurement.
modify(EstimatedMeasurement<Range>) - Method in class org.orekit.estimation.measurements.modifiers.RangeIonosphericDelayModifier
 
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<Range>) - Method in class org.orekit.estimation.measurements.modifiers.RangeTroposphericDelayModifier
Apply a modifier to an estimated measurement.
modify(EstimatedMeasurement<InterSatellitesRange>) - Method in class org.orekit.estimation.measurements.modifiers.ShapiroInterSatelliteRangeModifier
Apply a modifier to an estimated measurement.
modify(EstimatedMeasurement<Phase>) - Method in class org.orekit.estimation.measurements.modifiers.ShapiroPhaseModifier
Apply a modifier to an estimated measurement.
modify(EstimatedMeasurement<Range>) - Method in class org.orekit.estimation.measurements.modifiers.ShapiroRangeModifier
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.
MOLECULAR_NITROGEN - Static variable in class org.orekit.models.earth.atmosphere.DTM2000
Identifier for molecular nitrogen.
MOLECULAR_OXYGEN - Static variable in class org.orekit.models.earth.atmosphere.DTM2000
Identifier for molecular oxygen.
monitorDetector(T) - Method in class org.orekit.propagation.events.EventsLogger
Monitor an event detector.
monitorDetector(D) - Method in class org.orekit.propagation.events.FieldEventsLogger
Monitor an event detector.
Month - Enum in org.orekit.time
Enumerate representing a calendar month.
MOON - Static variable in class org.orekit.bodies.CelestialBodyFactory
Predefined name for Moon.
MOON_EQUATORIAL_RADIUS - Static variable in interface org.orekit.utils.Constants
Moon equatorial radius: 1737400 m.
MOON_SEMI_MAJOR_AXIS - Static variable in interface org.orekit.propagation.numerical.cr3bp.CR3BPConstants
Moon semi-major axis in meters.
mu(double) - Method in class org.orekit.propagation.analytical.gnss.SBASPropagator.Builder
Sets the Earth gravity coefficient.
MultipleShooter - Class in org.orekit.utils
Multiple shooting method applicable for trajectories, in an ephemeris model.
MultipleShooter(List<SpacecraftState>, List<NumericalPropagator>, List<AdditionalEquations>, double, double) - Constructor for class org.orekit.utils.MultipleShooter
Simple Constructor.
MultipleShooting - Interface in org.orekit.utils
Interface for Multiple shooting methods.
MultiplexedMeasurement - Class in org.orekit.estimation.measurements
Class multiplexing several measurements as one.
MultiplexedMeasurement(List<ObservedMeasurement<?>>) - Constructor for class org.orekit.estimation.measurements.MultiplexedMeasurement
Simple constructor.
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

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.
NarrowLaneCombination - Class in org.orekit.estimation.measurements.gnss
Narrow-Lane combination.
NAUTICAL_DAWN_DUSK_ELEVATION - Static variable in class org.orekit.propagation.events.GroundAtNightDetector
Sun elevation at nautical dawn/dusk (12° below horizon).
NDMFile - Class in org.orekit.files.ccsds
The NDMFile (Navigation Data Message) class represents the navigation messages used by the CCSDS format, (i.e.
NDMFile() - Constructor for class org.orekit.files.ccsds.NDMFile
Constructor.
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.
NEPTUNE - Static variable in class org.orekit.bodies.CelestialBodyFactory
Predefined name for Neptune.
NeQuickModel - Class in org.orekit.models.earth.ionosphere
NeQuick ionospheric delay model.
NeQuickModel(double[]) - Constructor for class org.orekit.models.earth.ionosphere.NeQuickModel
Build a new instance.
NeQuickModel(double[], TimeScale) - Constructor for class org.orekit.models.earth.ionosphere.NeQuickModel
Build a new instance.
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.
newBulletinBParser(IERSConventions, ItrfVersionProvider, TimeScales) - Static method in interface org.orekit.frames.EOPHistoryLoader.Parser
Create a new parser for EOP data in the Bulletin B format.
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.
newEopC04Parser(IERSConventions, ItrfVersionProvider, TimeScales) - Static method in interface org.orekit.frames.EOPHistoryLoader.Parser
Create a new parser for EOP data in the EOP C04 format.
newFinalsColumnsParser(IERSConventions, ItrfVersionProvider, TimeScales, boolean) - Static method in interface org.orekit.frames.EOPHistoryLoader.Parser
Create a new parser for EOP data in the rapid and predicted columnar format.
newFinalsXmlParser(IERSConventions, ItrfVersionProvider, TimeScales) - Static method in interface org.orekit.frames.EOPHistoryLoader.Parser
Create a new parser for EOP data in the rapid and predicted XML format.
newSegment(Map<Keyword, String>) - Method in class org.orekit.files.ccsds.StreamingAemWriter
Create a writer for a new AEM attitude ephemeris segment.
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.troposphere
The Niell Mapping Function model for radio wavelengths.
NiellMappingFunctionModel(double) - Constructor for class org.orekit.models.earth.troposphere.NiellMappingFunctionModel
Builds a new instance.
NiellMappingFunctionModel(double, TimeScale) - Constructor for class org.orekit.models.earth.troposphere.NiellMappingFunctionModel
Builds a new instance.
NodeDetector - Class in org.orekit.propagation.events
Finder for node crossing events.
NodeDetector(Orbit, Frame) - Constructor for class org.orekit.propagation.events.NodeDetector
Build a new instance.
NodeDetector(double, Orbit, Frame) - Constructor for class org.orekit.propagation.events.NodeDetector
Build a new instance.
nonCentralPart(AbsoluteDate, Vector3D, double) - Method in class org.orekit.forces.gravity.HolmesFeatherstoneAttractionModel
Compute the non-central part of the gravity field.
normalize() - Method in class org.orekit.utils.FieldPVCoordinates
Normalize the position part of the instance.
normalize() - Method in class org.orekit.utils.PVCoordinates
Normalize the position part of the instance.
normalizeAngle(T, T) - Static method in class org.orekit.orbits.FieldCircularOrbit
normalizeAngle(T, T) - Static method in class org.orekit.orbits.FieldEquinoctialOrbit
normalizeAngle(T, T) - Static method in class org.orekit.orbits.FieldKeplerianOrbit
normalizeAngle(T, T) - Static method in class org.orekit.propagation.analytical.FieldEcksteinHechlerPropagator
normalizeAngle(T, T) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldAuxiliaryElements
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.
NORTH_POLE - Static variable in class org.orekit.bodies.GeodeticPoint
North pole.
notCombine(EventDetector) - Static method in class org.orekit.propagation.events.BooleanDetector
Create a new event detector that negates the g function of another detector.
NRLMSISE00 - Class in org.orekit.models.earth.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.models.earth.atmosphere.NRLMSISE00
Constructor.
NRLMSISE00(NRLMSISE00InputParameters, PVCoordinatesProvider, BodyShape, TimeScale) - Constructor for class org.orekit.models.earth.atmosphere.NRLMSISE00
Constructor.
NRLMSISE00.FieldOutput<T extends RealFieldElement<T>> - Class in org.orekit.models.earth.atmosphere
This class is a placeholder for the computed densities and temperatures.
NRLMSISE00InputParameters - Interface in org.orekit.models.earth.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_CORRECTION - Static variable in class org.orekit.frames.PoleCorrection
Null correction (xp = 0, yp = 0).
numberOfCandidates() - Method in interface org.orekit.estimation.measurements.gnss.AmbiguityAcceptance
Get the number of candidate solutions to search for.
numberOfCandidates() - Method in class org.orekit.estimation.measurements.gnss.SimpleRatioAmbiguityAcceptance
Get the number of candidate solutions to search for.
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.
NumericalPropagator(ODEIntegrator, AttitudeProvider) - 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.
NumericalPropagatorBuilder(Orbit, ODEIntegratorBuilder, PositionAngle, double, AttitudeProvider) - 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.
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.
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.
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.
OceanLoadingCoefficientsBLQFactory(String, DataProvidersManager) - Constructor for class org.orekit.models.earth.displacement.OceanLoadingCoefficientsBLQFactory
This constructor allows specification of the source of the BLQ auxiliary data files.
OceanTides - Class in org.orekit.forces.gravity
Ocean tides force model.
OceanTides(Frame, double, double, int, int, IERSConventions, UT1Scale) - Constructor for class org.orekit.forces.gravity.OceanTides
Simple constructor.
OceanTides(Frame, double, double, boolean, double, int, int, int, IERSConventions, UT1Scale) - Constructor for class org.orekit.forces.gravity.OceanTides
Simple constructor.
OceanTides(Frame, double, double, boolean, double, int, int, int, IERSConventions, UT1Scale, GravityFields) - 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.
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).
ODMMetaData(ODMFile) - Constructor for class org.orekit.files.ccsds.ODMMetaData
Create a new meta-data.
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
ODMParser(AbsoluteDate, double, IERSConventions, boolean, int, int, String, DataContext) - 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.
OEMParser(DataContext) - Constructor for class org.orekit.files.ccsds.OEMParser
Constructor with data context.
OemSatelliteEphemeris(String, double, List<OEMFile.EphemeridesBlock>) - Constructor for class org.orekit.files.ccsds.OEMFile.OemSatelliteEphemeris
Create a container for the set of ephemeris blocks in the file that pertain to a single satellite.
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.
of(TimeScales, CelestialBodies) - Static method in interface org.orekit.frames.Frames
Create a set of frames from the given data.
of(TimeScales, Supplier<Frame>) - Static method in interface org.orekit.frames.Frames
Create a set of frames from the given data.
of(Collection<? extends OffsetModel>, BiFunction<? super IERSConventions, ? super TimeScales, ? extends Collection<? extends EOPEntry>>) - Static method in interface org.orekit.time.TimeScales
Create a set of time scales where all the data is loaded from the given functions.
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, double, VisibilityTrigger) - Method in class org.orekit.geometry.fov.CircularFieldOfView
Get the offset of target body with respect to the Field Of View Boundary.
offsetFromBoundary(Vector3D, double, VisibilityTrigger) - Method in class org.orekit.geometry.fov.EllipticalFieldOfView
Get the offset of target body with respect to the Field Of View Boundary.
offsetFromBoundary(Vector3D, double, VisibilityTrigger) - Method in interface org.orekit.geometry.fov.FieldOfView
Get the offset of target body with respect to the Field Of View Boundary.
offsetFromBoundary(Vector3D, double, VisibilityTrigger) - Method in class org.orekit.geometry.fov.PolygonalFieldOfView
Get the offset of target body with respect to the Field Of View Boundary.
offsetFromBoundary(Vector3D) - Method in class org.orekit.propagation.events.FieldOfView
offsetFromTAI(AbsoluteDate) - 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.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(FieldAbsoluteDate<T>) - 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(FieldAbsoluteDate<T>) - 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(FieldAbsoluteDate<T>) - 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(FieldAbsoluteDate<T>) - 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(FieldAbsoluteDate<T>) - 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(FieldAbsoluteDate<T>) - 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(FieldAbsoluteDate<T>) - 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(FieldAbsoluteDate<T>) - 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(FieldAbsoluteDate<T>) - 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(FieldAbsoluteDate<T>) - 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(FieldAbsoluteDate<T>) - 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(FieldAbsoluteDate<T>) - 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(FieldAbsoluteDate<T>) - 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.UTCScale
Get the offset to convert locations from TAIScale to instance.
OffsetModel - Class in org.orekit.time
TAI UTC offset model.
OffsetModel(DateComponents, int, double, double) - Constructor for class org.orekit.time.OffsetModel
Constructor for a linear offset model.
OffsetModel(DateComponents, int) - Constructor for class org.orekit.time.OffsetModel
Constructor for a constant 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.
OMMParser(DataContext) - Constructor for class org.orekit.files.ccsds.OMMParser
Constructor with data context.
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.
OnBoardAntennaPhaseModifier - Class in org.orekit.estimation.measurements.modifiers
On-board antenna offset effect on phase measurements.
OnBoardAntennaPhaseModifier(Vector3D) - Constructor for class org.orekit.estimation.measurements.modifiers.OnBoardAntennaPhaseModifier
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.
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.
OPMParser(DataContext) - Constructor for class org.orekit.files.ccsds.OPMParser
Constructor with data context.
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.
OrbitType - Enum in org.orekit.orbits
Enumerate for orbital parameters types.
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.
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.
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(Localizable, Object...) - Constructor for exception org.orekit.errors.OrekitException
Simple constructor.
OrekitException(OrekitException) - Constructor for exception org.orekit.errors.OrekitException
Copy constructor.
OrekitException(Localizable, Throwable) - Constructor for exception org.orekit.errors.OrekitException
Simple constructor.
OrekitException(Throwable, Localizable, Object...) - Constructor for exception org.orekit.errors.OrekitException
Simple constructor.
OrekitException(MathRuntimeException) - Constructor for exception org.orekit.errors.OrekitException
Simple constructor.
OrekitFixedStepHandler - Interface in org.orekit.propagation.sampling
This interface is a space-dynamics aware fixed size step handler.
OrekitFixedStepHandlerMultiplexer - Class in org.orekit.propagation.sampling
This class gathers several OrekitFixedStepHandler instances into one.
OrekitFixedStepHandlerMultiplexer() - Constructor for class org.orekit.propagation.sampling.OrekitFixedStepHandlerMultiplexer
Simple constructor.
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.annotation - package org.orekit.annotation
This package is the top level package for Orekit's specific annotations.
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.compiler.plugin - package org.orekit.compiler.plugin
This package provides elements to handle data context plugin.
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
This package provides initial orbit determination methods.
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.filtering - package org.orekit.estimation.measurements.filtering
This package provides measurement pre-processing filters.
org.orekit.estimation.measurements.generation - package org.orekit.estimation.measurements.generation
This package provides Orbit Determination measurements generation.
org.orekit.estimation.measurements.gnss - package org.orekit.estimation.measurements.gnss
This package provides methods to handle GNSS measurements.
org.orekit.estimation.measurements.modifiers - package org.orekit.estimation.measurements.modifiers
This package provides measurement modifier.
org.orekit.estimation.sequential - package org.orekit.estimation.sequential
The sequential package provides an implementation of a Kalman Filter engine to perform an orbit determination.
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 elements data stored in CCSDS Navigation 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.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.inertia - package org.orekit.forces.inertia
This package provides inertial force model.
org.orekit.forces.maneuvers - package org.orekit.forces.maneuvers
This package provides models of simple maneuvers.
org.orekit.forces.maneuvers.propulsion - package org.orekit.forces.maneuvers.propulsion
This package provides propulsion models intended to be used with class Maneuver.
org.orekit.forces.maneuvers.trigger - package org.orekit.forces.maneuvers.trigger
This package provides maneuver triggers' models intended to be used with class Maneuver.
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.geometry.fov - package org.orekit.geometry.fov
This package provides classes for representing a spacecraft sensor Field Of View.
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.atmosphere - package org.orekit.models.earth.atmosphere
This package provides the atmosphere model interface and several implementations.
org.orekit.models.earth.atmosphere.data - package org.orekit.models.earth.atmosphere.data
This package provides classes to get atmospheric data, including solar flux and planetary geomagnetic indices.
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.ionosphere - package org.orekit.models.earth.ionosphere
This package provides models that simulate the impact of the ionosphere.
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.models.earth.troposphere - package org.orekit.models.earth.troposphere
This package provides models that simulate the impact of the troposphere.
org.orekit.models.earth.weather - package org.orekit.models.earth.weather
This package provides models that simulate global weather conditions on Earth.
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.numerical.cr3bp - package org.orekit.propagation.numerical.cr3bp
Top level package for CR3BP Models used with a numerical propagator.
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.
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.
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

P1 - Static variable in class org.orekit.models.earth.displacement.Tide
P₁ tide.
PA - Static variable in enum org.orekit.orbits.OrbitType
Name for perigee argument.
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(InputStream, String) - Method in class org.orekit.data.PoissonSeriesParser
Parse a stream.
parse(String) - Method in class org.orekit.data.PolynomialParser
Parse a polynomial expression.
parse(InputStream, String) - Method in class org.orekit.data.SimpleTimeStampedTableParser
Parse a stream.
parse(String) - Method in class org.orekit.files.ccsds.ADMParser
Parse a CCSDS Attitude Data Message.
parse(InputStream) - Method in class org.orekit.files.ccsds.ADMParser
Parse a CCSDS Attitude Data Message.
parse(InputStream, String) - Method in class org.orekit.files.ccsds.ADMParser
Parse a CCSDS Attitude Data Message.
parse(String) - Method in class org.orekit.files.ccsds.AEMParser
Parse a CCSDS Attitude Data Message.
parse(InputStream) - Method in class org.orekit.files.ccsds.AEMParser
Parse a CCSDS Attitude Data Message.
parse(InputStream, String) - Method in class org.orekit.files.ccsds.AEMParser
Parse a CCSDS Attitude Data Message.
parse(BufferedReader, String) - Method in class org.orekit.files.ccsds.AEMParser
Parse an attitude ephemeris file from a stream.
parse(String) - Method in class org.orekit.files.ccsds.APMParser
Parse a CCSDS Attitude Data Message.
parse(InputStream) - Method in class org.orekit.files.ccsds.APMParser
Parse a CCSDS Attitude Data Message.
parse(InputStream, String) - Method in class org.orekit.files.ccsds.APMParser
Parse a CCSDS Attitude Data Message.
parse(String) - Method in class org.orekit.files.ccsds.ODMParser
Parse a CCSDS Orbit Data Message.
parse(InputStream) - Method in class org.orekit.files.ccsds.ODMParser
Parse a CCSDS Orbit Data Message.
parse(InputStream, String) - Method in class org.orekit.files.ccsds.ODMParser
Parse a CCSDS Orbit Data Message.
parse(String) - Method in class org.orekit.files.ccsds.OEMParser
Parse a CCSDS Orbit Data Message.
parse(InputStream) - Method in class org.orekit.files.ccsds.OEMParser
Parse a CCSDS Orbit Data Message.
parse(InputStream, String) - Method in class org.orekit.files.ccsds.OEMParser
Parse a CCSDS Orbit Data Message.
parse(BufferedReader, String) - Method in class org.orekit.files.ccsds.OEMParser
 
parse(String) - Method in class org.orekit.files.ccsds.OMMParser
Parse a CCSDS Orbit Data Message.
parse(InputStream) - Method in class org.orekit.files.ccsds.OMMParser
Parse a CCSDS Orbit Data Message.
parse(InputStream, String) - Method in class org.orekit.files.ccsds.OMMParser
Parse a CCSDS Orbit Data Message.
parse(String) - Method in class org.orekit.files.ccsds.OPMParser
Parse a CCSDS Orbit Data Message.
parse(InputStream) - Method in class org.orekit.files.ccsds.OPMParser
Parse a CCSDS Orbit Data Message.
parse(InputStream, String) - Method in class org.orekit.files.ccsds.OPMParser
Parse a CCSDS Orbit Data Message.
parse(String) - Method in class org.orekit.files.ccsds.TDMParser
Parse a CCSDS Tracking Data Message.
parse(InputStream) - Method in class org.orekit.files.ccsds.TDMParser
Parse a CCSDS Tracking Data Message.
parse(InputStream, String) - Method in class org.orekit.files.ccsds.TDMParser
Parse a CCSDS Tracking Data Message.
parse(BufferedReader, String) - Method in interface org.orekit.files.general.EphemerisFileParser
Parse an ephemeris file from a stream.
parse(String) - Method in interface org.orekit.files.general.EphemerisFileParser
Parse an ephemeris file from a file on the local file system.
parse(InputStream) - Method in class org.orekit.files.sp3.SP3Parser
Parse a SP3 file from an input stream using the UTF-8 charset.
parse(String) - Method in class org.orekit.files.sp3.SP3Parser
 
parse(BufferedReader, String) - Method in class org.orekit.files.sp3.SP3Parser
 
parse(InputStream, String) - Method in interface org.orekit.frames.EOPHistoryLoader.Parser
Parse EOP from the given input stream.
parse(InputStream, String) - Method in class org.orekit.time.TAIUTCDatFilesLoader.Parser
Load UTC-TAI offsets entries read from some file.
parse(InputStream, String) - Method in class org.orekit.time.UTCTAIHistoryFilesLoader.Parser
Load UTC-TAI offsets entries read from some file.
parse(InputStream, String) - Method in interface org.orekit.time.UTCTAIOffsetsLoader.Parser
Parse leap seconds from the input stream.
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[], TimeScale) - 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).
parseCCSDSCalendarSegmentedTimeCode(byte, byte[], TimeScale) - 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(byte, byte[], DateComponents, TimeScale) - 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).
parseCCSDSDaySegmentedTimeCode(Field<T>, byte, byte[], DateComponents, TimeScale) - 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(byte, byte, byte[], AbsoluteDate, 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).
parseCCSDSUnsegmentedTimeCode(Field<T>, byte, byte, byte[], FieldAbsoluteDate<T>, FieldAbsoluteDate<T>) - Static method in class org.orekit.time.FieldAbsoluteDate
Build an instance from a CCSDS Unsegmented Time Code (CUC).
parseCoefficient(String, List<List<Double>>, int, int, String, String) - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
Parse a coefficient.
parseCoefficient(String, double[][], int, int, String, String) - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
Parse a coefficient.
parseComment(KeyValue, List<String>) - Method in class org.orekit.files.ccsds.ADMParser
Parse a comment line.
parseComment(KeyValue, List<String>) - Method in class org.orekit.files.ccsds.ODMParser
Parse a comment line.
parseDate(String, CcsdsTimeScale) - Method in class org.orekit.files.ccsds.ADMParser
Parse a date.
parseDate(String, IERSConventions, AbsoluteDate) - Method in enum org.orekit.files.ccsds.CcsdsTimeScale
Parse a date in this time scale.
parseDate(String, IERSConventions, AbsoluteDate, TimeScales) - Method in enum org.orekit.files.ccsds.CcsdsTimeScale
Parse a date in this time scale.
parseDate(String, CcsdsTimeScale) - Method in class org.orekit.files.ccsds.ODMParser
Parse a date.
parseDate(String) - Static method in class org.orekit.time.DateComponents
Parse a string in ISO-8601 format to build a date.
parseDateTime(String) - Static method in class org.orekit.time.DateTimeComponents
Parse a string in ISO-8601 format to build a date/time.
parseDouble(String) - Static method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
Parse a double from a string.
parseGeneralStateDataEntry(KeyValue, APMFile, List<String>) - Method in class org.orekit.files.ccsds.ADMParser
Parse a general state data key = value entry.
parseGeneralStateDataEntry(KeyValue, OGMFile, List<String>) - Method in class org.orekit.files.ccsds.ODMParser
Parse a general state data key = value entry.
parseHeaderEntry(KeyValue, ADMFile, List<String>) - Method in class org.orekit.files.ccsds.ADMParser
Parse an entry from the header.
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, ADMMetaData, List<String>) - Method in class org.orekit.files.ccsds.ADMParser
Parse a meta-data key = value entry.
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
 
Parser() - Constructor for class org.orekit.time.TAIUTCDatFilesLoader.Parser
Simple constructor.
Parser() - Constructor for class org.orekit.time.UTCTAIHistoryFilesLoader.Parser
Simple constructor.
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.
PAST_INFINITY - Static variable in class org.orekit.time.AbsoluteDate
Dummy date at infinity in the past direction.
pathDelay(SpacecraftState, TopocentricFrame, double, double[]) - Method in class org.orekit.models.earth.ionosphere.EstimatedIonosphericModel
Calculates the ionospheric path delay for the signal path from a ground station to a satellite.
pathDelay(double, double, double[]) - Method in class org.orekit.models.earth.ionosphere.EstimatedIonosphericModel
Calculates the ionospheric path delay for the signal path from a ground station to a satellite.
pathDelay(FieldSpacecraftState<T>, TopocentricFrame, double, T[]) - Method in class org.orekit.models.earth.ionosphere.EstimatedIonosphericModel
Calculates the ionospheric path delay for the signal path from a ground station to a satellite.
pathDelay(T, double, T[]) - Method in class org.orekit.models.earth.ionosphere.EstimatedIonosphericModel
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.ionosphere.GlobalIonosphereMapModel
Calculates the ionospheric path delay for the signal path from a ground station to a satellite.
pathDelay(SpacecraftState, TopocentricFrame, double, double[]) - Method in class org.orekit.models.earth.ionosphere.GlobalIonosphereMapModel
 
pathDelay(FieldAbsoluteDate<T>, GeodeticPoint, T, double) - Method in class org.orekit.models.earth.ionosphere.GlobalIonosphereMapModel
Calculates the ionospheric path delay for the signal path from a ground station to a satellite.
pathDelay(FieldSpacecraftState<T>, TopocentricFrame, double, T[]) - Method in class org.orekit.models.earth.ionosphere.GlobalIonosphereMapModel
 
pathDelay(SpacecraftState, TopocentricFrame, double, double[]) - Method in interface org.orekit.models.earth.ionosphere.IonosphericModel
Calculates the ionospheric path delay for the signal path from a ground station to a satellite.
pathDelay(FieldSpacecraftState<T>, TopocentricFrame, double, T[]) - Method in interface org.orekit.models.earth.ionosphere.IonosphericModel
Calculates the ionospheric path delay for the signal path from a ground station to a satellite.
pathDelay(AbsoluteDate, GeodeticPoint, double, double, double, double[]) - Method in class org.orekit.models.earth.ionosphere.KlobucharIonoModel
Calculates the ionospheric path delay for the signal path from a ground station to a satellite.
pathDelay(SpacecraftState, TopocentricFrame, double, double[]) - Method in class org.orekit.models.earth.ionosphere.KlobucharIonoModel
Calculates the ionospheric path delay for the signal path from a ground station to a satellite.
pathDelay(FieldAbsoluteDate<T>, FieldGeodeticPoint<T>, T, T, double, T[]) - Method in class org.orekit.models.earth.ionosphere.KlobucharIonoModel
Calculates the ionospheric path delay for the signal path from a ground station to a satellite.
pathDelay(FieldSpacecraftState<T>, TopocentricFrame, double, T[]) - Method in class org.orekit.models.earth.ionosphere.KlobucharIonoModel
Calculates the ionospheric path delay for the signal path from a ground station to a satellite.
pathDelay(SpacecraftState, TopocentricFrame, double, double[]) - Method in class org.orekit.models.earth.ionosphere.NeQuickModel
 
pathDelay(FieldSpacecraftState<T>, TopocentricFrame, double, T[]) - Method in class org.orekit.models.earth.ionosphere.NeQuickModel
 
pathDelay(double, double, double[], AbsoluteDate) - Method in interface org.orekit.models.earth.troposphere.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 interface org.orekit.models.earth.troposphere.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.troposphere.EstimatedTroposphericModel
 
pathDelay(T, T, T[], FieldAbsoluteDate<T>) - Method in class org.orekit.models.earth.troposphere.EstimatedTroposphericModel
 
pathDelay(double, double, double[], AbsoluteDate) - Method in class org.orekit.models.earth.troposphere.FixedTroposphericDelay
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.troposphere.FixedTroposphericDelay
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.troposphere.MariniMurrayModel
 
pathDelay(T, T, T[], FieldAbsoluteDate<T>) - Method in class org.orekit.models.earth.troposphere.MariniMurrayModel
 
pathDelay(double, double, double[], AbsoluteDate) - Method in class org.orekit.models.earth.troposphere.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 class org.orekit.models.earth.troposphere.MendesPavlisModel
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.troposphere.SaastamoinenModel
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.troposphere.SaastamoinenModel
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.troposphere.TimeSpanEstimatedTroposphericModel
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.troposphere.TimeSpanEstimatedTroposphericModel
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.troposphere.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.troposphere.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.troposphere.ViennaThreeModel
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.troposphere.ViennaThreeModel
Calculates the tropospheric path delay for the signal path from a ground station to a satellite.
perige - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator
perigee, expressed in KM and ALTITUDE.
permutation(int, double) - Method in class org.orekit.estimation.measurements.gnss.AbstractLambdaMethod
Perform one symmetric permutation involving rows/columns k0 and k0+1.
Phase - Class in org.orekit.estimation.measurements.gnss
Class modeling a phase measurement from a ground station.
Phase(GroundStation, AbsoluteDate, double, double, double, double, ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.gnss.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.
PhaseBuilder - Class in org.orekit.estimation.measurements.gnss
Builder for Phase measurements.
PhaseBuilder(CorrelatedRandomVectorGenerator, GroundStation, double, double, double, ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.gnss.PhaseBuilder
Simple constructor.
PhaseCenterVariationFunction - Interface in org.orekit.gnss.antenna
Model for antennas phase center variations.
PhaseIonosphericDelayModifier - Class in org.orekit.estimation.measurements.modifiers
Class modifying theoretical phase measurement with ionospheric delay.
PhaseIonosphericDelayModifier(IonosphericModel, double) - Constructor for class org.orekit.estimation.measurements.modifiers.PhaseIonosphericDelayModifier
Constructor.
PhaseMinusCodeCombination - Class in org.orekit.estimation.measurements.gnss
Phase minus Code combination.
PhaseMinusCodeCycleSlipDetector - Class in org.orekit.estimation.measurements.gnss
Phase minus code cycle slip detectors.
PhaseMinusCodeCycleSlipDetector(double, double, int, int) - Constructor for class org.orekit.estimation.measurements.gnss.PhaseMinusCodeCycleSlipDetector
Polynomial single frequency cycle-slip detector Constructor.
PhaseTroposphericDelayModifier - Class in org.orekit.estimation.measurements.modifiers
Class modifying theoretical phase measurement with tropospheric delay.
PhaseTroposphericDelayModifier(DiscreteTroposphericModel) - Constructor for class org.orekit.estimation.measurements.modifiers.PhaseTroposphericDelayModifier
Constructor.
PLUTO - Static variable in class org.orekit.bodies.CelestialBodyFactory
Predefined name for Pluto.
pointAt(double) - Method in class org.orekit.bodies.Ellipse
Get a point of the 2D ellipse.
pointAtDistance(double, double, double) - Method in class org.orekit.frames.TopocentricFrame
Compute the point observed from the station at some specified distance.
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.
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.
PolygonalFieldOfView - Class in org.orekit.geometry.fov
Class representing a spacecraft sensor Field Of View with polygonal shape.
PolygonalFieldOfView(SphericalPolygonsSet, double) - Constructor for class org.orekit.geometry.fov.PolygonalFieldOfView
Build a new instance.
PolygonalFieldOfView(Vector3D, Vector3D, double, int, double) - Constructor for class org.orekit.geometry.fov.PolygonalFieldOfView
PolygonalFieldOfView(Vector3D, PolygonalFieldOfView.DefiningConeType, Vector3D, double, int, double) - Constructor for class org.orekit.geometry.fov.PolygonalFieldOfView
Build Field Of View with a regular polygon shape.
PolygonalFieldOfView.DefiningConeType - Enum in org.orekit.geometry.fov
Enumerate for cone/polygon relative position.
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.
POS_X - Static variable in enum org.orekit.orbits.OrbitType
Name for position along X.
POS_Y - Static variable in enum org.orekit.orbits.OrbitType
Name for position along Y.
POS_Z - Static variable in enum org.orekit.orbits.OrbitType
Name for position along Z.
Position - Class in org.orekit.estimation.measurements
Class modeling a position only measurement.
Position(AbsoluteDate, Vector3D, double, double, ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.Position
Constructor with one double for the standard deviation.
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, ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.Position
Constructor with full covariance matrix and all inputs.
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(OrbitType, PositionAngle, double) - Constructor for class org.orekit.propagation.events.PositionAngleDetector
Build a new detector.
PositionAngleDetector(double, double, OrbitType, PositionAngle, double) - Constructor for class org.orekit.propagation.events.PositionAngleDetector
Build a 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.
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.
PotentialCoefficientsReader(String, boolean, TimeScale) - Constructor for class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
Simple constructor.
Predefined - Enum in org.orekit.frames
Predefined frames provided by Frames.
processMeasurements(Iterable<ObservedMeasurement<?>>) - Method in class org.orekit.estimation.sequential.KalmanEstimator
Process several measurements.
projectToBoundary(Vector3D) - Method in class org.orekit.geometry.fov.CircularFieldOfView
Find the direction on Field Of View Boundary closest to a line of sight.
projectToBoundary(Vector3D) - Method in class org.orekit.geometry.fov.EllipticalFieldOfView
Find the direction on Field Of View Boundary closest to a line of sight.
projectToBoundary(Vector3D) - Method in interface org.orekit.geometry.fov.FieldOfView
Find the direction on Field Of View Boundary closest to a line of sight.
projectToBoundary(Vector3D) - Method in class org.orekit.geometry.fov.PolygonalFieldOfView
Find the direction on Field Of View Boundary closest to a line of sight.
projectToEllipse(Vector2D) - Method in class org.orekit.bodies.Ellipse
Find the closest ellipse point.
projectToEllipse(TimeStampedPVCoordinates) - Method in class org.orekit.bodies.Ellipse
Project position-velocity-acceleration on an ellipse.
projectToGround(Vector3D, AbsoluteDate, Frame) - Method in interface org.orekit.bodies.BodyShape
Project a point to the ground.
projectToGround(TimeStampedPVCoordinates, Frame) - Method in interface org.orekit.bodies.BodyShape
Project a moving point to the ground.
projectToGround(Vector3D, AbsoluteDate, Frame) - Method in class org.orekit.bodies.OneAxisEllipsoid
Project a point to the ground.
projectToGround(TimeStampedPVCoordinates, Frame) - Method in class org.orekit.bodies.OneAxisEllipsoid
Project a moving point to the ground.
projectToGround(Vector3D, AbsoluteDate, Frame) - Method in class org.orekit.models.earth.Geoid
 
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, AbsoluteDate) - Method in class org.orekit.propagation.analytical.AbstractAnalyticalPropagator
Propagate from a start date towards a target date.
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>) - 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>, FieldAbsoluteDate<T>) - Method in interface org.orekit.propagation.FieldPropagator
Propagate from a start date towards a target date.
propagate(AbsoluteDate) - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
Propagate towards a target date.
propagate(AbsoluteDate, AbsoluteDate) - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
Propagate from a start date towards a target date.
propagate(AbsoluteDate, boolean) - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
Propagation with or without event detection.
propagate(FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator
Propagate 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.
propagate(FieldAbsoluteDate<T>, boolean) - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator
Propagation with or without event detection.
propagate(AbsoluteDate) - Method in class org.orekit.propagation.numerical.GLONASSNumericalPropagator
Propagate towards a target date.
propagate(AbsoluteDate) - Method in interface org.orekit.propagation.Propagator
Propagate towards a target date.
propagate(AbsoluteDate, AbsoluteDate) - Method in interface org.orekit.propagation.Propagator
Propagate from a start date towards a target date.
propagate(AbsoluteDate, AbsoluteDate) - Method in class org.orekit.propagation.PropagatorsParallelizer
Propagate from a start date towards a target date.
propagateInEcef(AbsoluteDate) - Method in class org.orekit.propagation.analytical.gnss.AbstractGNSSPropagator
Gets the PVCoordinates of the GNSS SV in ECEF frame.
propagateInEcef(AbsoluteDate) - Method in class org.orekit.propagation.analytical.gnss.GLONASSAnalyticalPropagator
Gets the PVCoordinates of the GLONASS SV in ECEF frame.
propagateInEcef(AbsoluteDate) - Method in class org.orekit.propagation.analytical.gnss.SBASPropagator
Gets the PVCoordinates of the GNSS 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(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(AbsoluteDate) - Method in class org.orekit.propagation.analytical.gnss.AbstractGNSSPropagator
Extrapolate an orbit up to a specific target date.
propagateOrbit(AbsoluteDate) - Method in class org.orekit.propagation.analytical.gnss.GLONASSAnalyticalPropagator
Extrapolate an orbit up to a specific target date.
propagateOrbit(AbsoluteDate) - Method in class org.orekit.propagation.analytical.gnss.SBASPropagator
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(FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.integration.FieldIntegratedEphemeris
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.
PropagationType - Enum in org.orekit.propagation
Enumerate to define the propagation type used by the propagator.
Propagator - Interface in org.orekit.propagation
This interface provides a way to propagate an orbit at any time.
PropagatorBuilder - Interface in org.orekit.propagation.conversion
This interface is the top-level abstraction to build propagators for conversion.
PropagatorConverter - Interface in org.orekit.propagation.conversion
This interface is the top-level abstraction for propagators conversions.
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.
PropulsionModel - Interface in org.orekit.forces.maneuvers.propulsion
Generic interface for a propulsion model used in a Maneuver.
PV - Class in org.orekit.estimation.measurements
Class modeling a position-velocity measurement.
PV(AbsoluteDate, Vector3D, Vector3D, double, double, double, ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.PV
Constructor with two double for the standard deviations.
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, ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.PV
Constructor with one vector for the standard deviations.
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, ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.PV
Constructor with full covariance matrix and all inputs.
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(Vector3D, Vector3D) - Constructor for class org.orekit.utils.PVCoordinates
Builds a PVCoordinates triplet with zero acceleration.
PVCoordinates(Vector3D, Vector3D, Vector3D) - Constructor for class org.orekit.utils.PVCoordinates
Builds a PVCoordinates triplet.
PVCoordinates(double, PVCoordinates) - Constructor for class org.orekit.utils.PVCoordinates
Multiplicative constructor.
PVCoordinates(PVCoordinates, PVCoordinates) - Constructor for class org.orekit.utils.PVCoordinates
Subtractive constructor.
PVCoordinates(double, PVCoordinates, double, PVCoordinates) - Constructor for class org.orekit.utils.PVCoordinates
Linear constructor.
PVCoordinates(double, PVCoordinates, double, PVCoordinates, double, PVCoordinates) - Constructor for class org.orekit.utils.PVCoordinates
Linear constructor.
PVCoordinates(double, PVCoordinates, double, PVCoordinates, double, PVCoordinates, double, PVCoordinates) - Constructor for class org.orekit.utils.PVCoordinates
Linear constructor.
PVCoordinates(FieldVector3D<DerivativeStructure>) - Constructor for class org.orekit.utils.PVCoordinates
Builds a PVCoordinates triplet from a FieldVector3D<DerivativeStructure>.
PVCoordinatesProvider - Interface in org.orekit.utils
Interface for PV coordinates providers.

Q

Q1 - Static variable in class org.orekit.models.earth.displacement.Tide
Q₁ tide.
QZSS_EPOCH - Static variable in class org.orekit.time.AbsoluteDate
Reference epoch for QZSS weeks: 1980-01-06T00:00:00 QZSS time.
QZSS_EPOCH - Static variable in class org.orekit.time.DateComponents
Reference epoch for QZSS weeks: 1980-01-06.
QZSS_MU - Static variable in interface org.orekit.propagation.analytical.gnss.QZSSOrbitalElements
WGS 84 value of the Earth's universal gravitational parameter for QZSS user in m³/s².
QZSS_PI - Static variable in interface org.orekit.propagation.analytical.gnss.QZSSOrbitalElements
Value of Pi for conversion from semicircles to radian.
QZSS_WEEK_IN_SECONDS - Static variable in interface org.orekit.propagation.analytical.gnss.QZSSOrbitalElements
Duration of the QZSS week in seconds.
QZSS_WEEK_NB - Static variable in interface org.orekit.propagation.analytical.gnss.QZSSOrbitalElements
Number of weeks in the QZSS cycle.
QZSSAlmanac - Class in org.orekit.gnss
This class holds a QZSS almanac as read from YUMA files.
QZSSAlmanac(String, int, int, double, double, double, double, double, double, double, double, double, double, int) - Constructor for class org.orekit.gnss.QZSSAlmanac
Constructor.
QZSSAlmanac(String, int, int, double, double, double, double, double, double, double, double, double, double, int, AbsoluteDate) - Constructor for class org.orekit.gnss.QZSSAlmanac
Constructor.
QZSSOrbitalElements - Interface in org.orekit.propagation.analytical.gnss
This interface provides the minimal set of orbital elements needed by the QZSSPropagator.
QZSSPropagator - Class in org.orekit.propagation.analytical.gnss
This class aims at propagating a QZSS orbit from QZSSOrbitalElements.
QZSSPropagator.Builder - Class in org.orekit.propagation.analytical.gnss
This nested class aims at building a QZSSPropagator.
QZSSScale - Class in org.orekit.time
QZSS time scale.

R

RAAN - Static variable in enum org.orekit.orbits.OrbitType
Name for right ascension of ascending node.
radiationPressureAcceleration(AbsoluteDate, Frame, Vector3D, Rotation, double, Vector3D, double[]) - 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.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(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(AbsoluteDate, Frame, Vector3D, Rotation, double, Vector3D, double[]) - 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.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(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(AbsoluteDate, Frame, Vector3D, Rotation, double, Vector3D, double[]) - Method in interface org.orekit.forces.radiation.RadiationSensitive
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.
radiusCorrection(double) - Method in enum org.orekit.propagation.events.VisibilityTrigger
Apply radius correction.
Range - Class in org.orekit.estimation.measurements
Class modeling a range measurement from a ground station.
Range(GroundStation, boolean, AbsoluteDate, double, double, double, ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.Range
Simple constructor.
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, double) - 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, 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, SpacecraftState) - Method in class org.orekit.estimation.measurements.modifiers.RangeRateTroposphericDelayModifier
Compute the measurement error due to Troposphere.
rangeRateErrorTroposphericModel(GroundStation, FieldSpacecraftState<T>, T[]) - 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, double, 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.
readGravityField(int, int) - Method in class org.orekit.forces.gravity.potential.LazyLoadedGravityFields
Read a gravity field coefficients provider from the first supported file.
readLine() - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherDataLoader.LineReader
Read a line from the input data stream.
readLineOrThrow(Localizable, Object...) - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherDataLoader.LineReader
Read a line from the input data stream, or if the end of the stream has been reached throw an exception.
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 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.
recoverAmbiguities() - Method in class org.orekit.estimation.measurements.gnss.AbstractLambdaMethod
Recover ambiguities prior to the Z-transformation.
recoverAmbiguities() - Method in class org.orekit.estimation.measurements.gnss.IntegerBootstrapping
Recover ambiguities prior to the Z-transformation.
reduction() - Method in class org.orekit.estimation.measurements.gnss.AbstractLambdaMethod
Perform LAMBDA reduction.
reduction() - Method in class org.orekit.estimation.measurements.gnss.LambdaMethod
Perform LAMBDA reduction.
reduction() - Method in class org.orekit.estimation.measurements.gnss.ModifiedLambdaMethod
Perform MLAMBDA reduction.
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.DSSTNewtonianAttraction
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(Propagator) - Method in class org.orekit.attitudes.AttitudesSequence
Register all wrapped switch events to the propagator.
registerSwitchEvents(Field<T>, FieldPropagator<T>) - Method in class org.orekit.attitudes.AttitudesSequence
Register all wrapped switch events to the propagator.
reinitializeBegin(OrekitStepInterpolator) - Method in class org.orekit.propagation.events.EventState
Reinitialize the beginning of the step.
reinitializeBegin(FieldOrekitStepInterpolator<T>) - Method in class org.orekit.propagation.events.FieldEventState
Reinitialize the beginning of the step.
Relativity - Class in org.orekit.forces.gravity
Post-Newtonian correction force due to general relativity.
Relativity(double) - Constructor for class org.orekit.forces.gravity.Relativity
Create a force model to add post-Newtonian acceleration corrections to an Earth orbit.
removeForceModels() - Method in class org.orekit.propagation.numerical.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 (except central attraction).
removeForceModels() - Method in class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator
Remove all perturbing force models from the global perturbation model (except central attraction).
removeObserver(ParameterObserver) - Method in class org.orekit.utils.ParameterDriver
Remove an observer.
removeProvider(DataProvider) - Method in class org.orekit.data.DataProvidersManager
Remove one provider.
removeSolution() - Method in class org.orekit.estimation.measurements.gnss.AbstractLambdaMethod
Remove spurious solution.
replaceObserver(ParameterObserver, ParameterObserver) - Method in class org.orekit.utils.ParameterDriver
Replace an observer.
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.
resetActiveProvider(AttitudeProvider) - Method in class org.orekit.attitudes.AttitudesSequence
Reset the active provider.
resetFitting(AbsoluteDate, double...) - Method in class org.orekit.utils.SecularAndHarmonic
Reset fitting.
resetInitialState(SpacecraftState) - Method in class org.orekit.propagation.AbstractPropagator
Reset the propagator initial state.
resetInitialState(SpacecraftState) - Method in class org.orekit.propagation.analytical.AdapterPropagator
Reset the propagator initial state.
resetInitialState(SpacecraftState) - Method in class org.orekit.propagation.analytical.AggregateBoundedPropagator
 
resetInitialState(SpacecraftState) - Method in class org.orekit.propagation.analytical.EcksteinHechlerPropagator
Reset the propagator initial state.
resetInitialState(SpacecraftState, PropagationType) - 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(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.analytical.FieldEcksteinHechlerPropagator
Reset the propagator initial state.
resetInitialState(FieldSpacecraftState<T>, PropagationType) - 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(SpacecraftState) - Method in class org.orekit.propagation.analytical.gnss.AbstractGNSSPropagator
Reset the propagator initial state.
resetInitialState(SpacecraftState) - Method in class org.orekit.propagation.analytical.gnss.GLONASSAnalyticalPropagator
Reset the propagator initial state.
resetInitialState(SpacecraftState) - Method in class org.orekit.propagation.analytical.gnss.SBASPropagator
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(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(SpacecraftState) - Method in class org.orekit.propagation.integration.IntegratedEphemeris
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.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.
resetInitialState(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator
Reset the initial 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(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(SpacecraftState, boolean) - Method in class org.orekit.propagation.analytical.gnss.AbstractGNSSPropagator
Reset an intermediate state.
resetIntermediateState(SpacecraftState, boolean) - Method in class org.orekit.propagation.analytical.gnss.GLONASSAnalyticalPropagator
Reset an intermediate state.
resetIntermediateState(SpacecraftState, boolean) - Method in class org.orekit.propagation.analytical.gnss.SBASPropagator
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(FieldSpacecraftState<T>, boolean) - Method in class org.orekit.propagation.integration.FieldIntegratedEphemeris
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.
resetOrbit(Orbit) - Method in interface org.orekit.propagation.conversion.IntegratedPropagatorBuilder
Reset the orbit in the propagator builder.
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(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(T, SpacecraftState) - Method in interface org.orekit.propagation.events.handlers.EventHandler
Reset the state prior to continue propagation.
resetState(KK, FieldSpacecraftState<T>) - Method in interface org.orekit.propagation.events.handlers.FieldEventHandler
Reset the state prior to continue propagation.
resetState(T, FieldSpacecraftState<E>) - Method in class org.orekit.propagation.events.handlers.FieldRecordAndContinue
 
resetState(T, SpacecraftState) - Method in class org.orekit.propagation.events.handlers.RecordAndContinue
 
ResidualFilter<T extends ObservedMeasurement<T>> - Class in org.orekit.estimation.measurements.filtering
Residual pre-processing filter.
ResidualFilter(double) - Constructor for class org.orekit.estimation.measurements.filtering.ResidualFilter
Constructor.
restrictStep(SpacecraftState, SpacecraftState) - Method in interface org.orekit.propagation.sampling.OrekitStepInterpolator
Create a new restricted version of the instance.
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.
RichardsonExpansion - Class in org.orekit.orbits
Class implementing the Third-Order Richardson Expansion.
RichardsonExpansion(CR3BPSystem, LagrangianPoints) - Constructor for class org.orekit.orbits.RichardsonExpansion
Simple Constructor.
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, Vector3D, Vector3D, double, AbsoluteDate, AbsoluteDate, int, int) - Constructor for class org.orekit.gnss.RinexHeader
Simple constructor, for Rinex 2 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.
RinexLoader - Class in org.orekit.gnss
Loader for Rinex measurements files.
RinexLoader(String) - Constructor for class org.orekit.gnss.RinexLoader
Simple constructor.
RinexLoader(String, DataProvidersManager, TimeScales) - Constructor for class org.orekit.gnss.RinexLoader
Create a RINEX loader/parser with the given source of RINEX auxiliary data files.
RinexLoader(InputStream, String) - Constructor for class org.orekit.gnss.RinexLoader
Simple constructor.
RinexLoader(InputStream, String, TimeScales) - Constructor for class org.orekit.gnss.RinexLoader
Loads RINEX from the given input stream using the specified auxiliary data.
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(PVCoordinates) - Method in enum org.orekit.frames.LOFType
Get the rotation from inertial frame to local orbital frame.
rotationFromInertial(Field<T>, FieldPVCoordinates<T>) - Method in enum org.orekit.frames.LOFType
Get the rotation from inertial frame to local orbital frame.

S

S2 - Static variable in class org.orekit.models.earth.displacement.Tide
S₂ tide.
s4 - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator
s* new value for the contant s.
SaastamoinenModel - Class in org.orekit.models.earth.troposphere
The modified Saastamoinen model.
SaastamoinenModel(double, double, double) - Constructor for class org.orekit.models.earth.troposphere.SaastamoinenModel
Create a new Saastamoinen model for the troposphere using the given environmental conditions and table from the reference book.
SaastamoinenModel(double, double, double, String) - Constructor for class org.orekit.models.earth.troposphere.SaastamoinenModel
Create a new Saastamoinen model for the troposphere using the given environmental conditions.
SaastamoinenModel(double, double, double, String, DataProvidersManager) - Constructor for class org.orekit.models.earth.troposphere.SaastamoinenModel
Create a new Saastamoinen model for the troposphere using the given environmental conditions.
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.
SatelliteAntenna - Class in org.orekit.gnss.antenna
GNSS satellite antenna model.
SatelliteAntenna(String, String, Map<Frequency, FrequencyPattern>, SatelliteSystem, int, SatelliteType, int, String, AbsoluteDate, AbsoluteDate) - Constructor for class org.orekit.gnss.antenna.SatelliteAntenna
Simple constructor.
SatelliteSystem - Enum in org.orekit.gnss
Enumerate for satellite system.
SatelliteType - Enum in org.orekit.gnss.antenna
Enumerate for satellite types.
SATURN - Static variable in class org.orekit.bodies.CelestialBodyFactory
Predefined name for Saturn.
SBAS_MU - Static variable in interface org.orekit.propagation.analytical.gnss.SBASOrbitalElements
WGS 84 value of the Earth's universal gravitational parameter for SBAS user in m³/s².
SBASOrbitalElements - Interface in org.orekit.propagation.analytical.gnss
This interface provides the minimal set of orbital elements needed by the SBASPropagator.
SBASPropagator - Class in org.orekit.propagation.analytical.gnss
This class aims at propagating a SBAS orbit from SBASOrbitalElements.
SBASPropagator.Builder - Class in org.orekit.propagation.analytical.gnss
This nested class aims at building a SBASPropagator.
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.
ScaledConstantThrustPropulsionModel - Class in org.orekit.forces.maneuvers.propulsion
Thrust propulsion model with parameters (for estimation) represented by scale factors on the X, Y and Z axis of the spacecraft frame.
ScaledConstantThrustPropulsionModel(double, double, Vector3D, String) - Constructor for class org.orekit.forces.maneuvers.propulsion.ScaledConstantThrustPropulsionModel
Constructor with min/max deviation for the scale factors.
Scheduler<T extends ObservedMeasurement<T>> - Interface in org.orekit.estimation.measurements.generation
Interface for generating measurements sequences.
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.
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, Frames) - Static method in class org.orekit.propagation.analytical.tle.TLEPropagator
Selects the extrapolator to use with the selected TLE.
selectExtrapolator(TLE, AttitudeProvider, double) - Static method in class org.orekit.propagation.analytical.tle.TLEPropagator
Selects the extrapolator to use with the selected TLE.
selectExtrapolator(TLE, AttitudeProvider, double, Frame) - Static method in class org.orekit.propagation.analytical.tle.TLEPropagator
Selects the extrapolator to use with the selected TLE.
selectionChanged(boolean, ParameterDriver) - Method in interface org.orekit.utils.ParameterObserver
Notify that a parameter selection status has been changed.
selectTransformer(Transformer, double, boolean) - Method in enum org.orekit.propagation.events.FilterType
Get next function transformer in the specified direction.
SEMParser - Class in org.orekit.gnss
This class reads SEM almanac files and provides GPS almanacs.
SEMParser(String) - Constructor for class org.orekit.gnss.SEMParser
Simple constructor.
SEMParser(String, DataProvidersManager, TimeScales) - Constructor for class org.orekit.gnss.SEMParser
Create a SEM loader/parser with the given source of SEM auxiliary data files.
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.
setAttitudeDataLinesComment(List<String>) - Method in class org.orekit.files.ccsds.AEMFile.AttitudeEphemeridesBlock
Set the attitude data lines comment.
setAttitudeDirection(String) - Method in class org.orekit.files.ccsds.AEMFile.AttitudeEphemeridesBlock
Set the rotation direction of the attitude.
setAttitudeProvider(AttitudeProvider) - Method in class org.orekit.propagation.AbstractPropagator
Set attitude provider.
setAttitudeProvider(AttitudeProvider) - Method in class org.orekit.propagation.conversion.AbstractPropagatorBuilder
Set the attitude provider.
setAttitudeProvider(AttitudeProvider) - Method in class org.orekit.propagation.FieldAbstractPropagator
Set attitude provider.
setAttitudeProvider(AttitudeProvider) - Method in interface org.orekit.propagation.FieldPropagator
Set attitude provider.
setAttitudeProvider(AttitudeProvider) - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
Set attitude provider.
setAttitudeProvider(AttitudeProvider) - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator
Set attitude provider.
setAttitudeProvider(AttitudeProvider) - Method in interface org.orekit.propagation.Propagator
Set attitude provider.
setAttitudeProvider(AttitudeProvider) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator
Set attitude provider.
setAttitudeProvider(AttitudeProvider) - Method in class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator
Set attitude provider.
setAttitudeQuaternionDirection(String) - Method in class org.orekit.files.ccsds.APMFile
Set the rotation direction of the attitude quaternion.
setAttitudeType(String) - Method in class org.orekit.files.ccsds.AEMFile.AttitudeEphemeridesBlock
Set the format of the data lines in the message.
setCacheSlotsNumber(int) - Static method in class org.orekit.utils.OrekitConfiguration
Set the number of slots to use in caches.
setCenterBody(CelestialBody) - Method in class org.orekit.files.ccsds.ADMMetaData
Set the CelestialBody corresponding to the center name.
setCenterBody(CelestialBody) - Method in class org.orekit.files.ccsds.ODMMetaData
Set the CelestialBody corresponding to the center name.
setCenterName(String) - Method in class org.orekit.files.ccsds.ADMMetaData
Set the origin of reference frame.
setCenterName(String) - Method in class org.orekit.files.ccsds.ODMMetaData
Set the origin of reference frame.
setClosedOrbitConstraint(boolean) - Method in class org.orekit.utils.AbstractMultipleShooting
Set the constraint of a closed orbit or not.
setComment(List<String>) - Method in class org.orekit.files.ccsds.ADMMetaData
Set the meta-data comment.
setComment(List<String>) - Method in class org.orekit.files.ccsds.APMFile.APMManeuver
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.ODMMetaData
Set the meta-data comment.
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.
setConventions(IERSConventions) - Method in class org.orekit.files.ccsds.NDMFile
Set IERS conventions.
setConvergenceChecker(ConvergenceChecker<LeastSquaresProblem.Evaluation>) - Method in class org.orekit.estimation.leastsquares.BatchLSEstimator
Set a custom convergence checker.
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.NDMFile
Set the file creation date and time in UTC.
setDataContext(DataContext) - Method in class org.orekit.files.ccsds.NDMFile
Set the data context.
setDataQuality(String) - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData
Setter for the dataQuality.
setDefault(LazyLoadedDataContext) - Static method in interface org.orekit.data.DataContext
Set the default data context that is used to implement Orekit's static factories.
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.APMFile.APMManeuver
Set duration (value is 0 for impulsive maneuver).
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.
setEOPContinuityThreshold(double) - Method in class org.orekit.frames.LazyLoadedEop
Set the threshold to check EOP continuity.
setEOPContinuityThreshold(double) - Method in class org.orekit.frames.LazyLoadedFrames
Set the threshold to check EOP continuity.
setEphemeridesDataLinesComment(List<String>) - Method in class org.orekit.files.ccsds.OEMFile.EphemeridesBlock
Set the ephemerides data lines comment.
setEphemerisMode() - Method in class org.orekit.propagation.AbstractPropagator
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() - 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(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() - 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 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.APMFile
Set the epoch of the data.
setEpoch(AbsoluteDate) - Method in class org.orekit.files.ccsds.TDMFile.Observation
Setter for the epoch.
setEpochComment(List<String>) - Method in class org.orekit.files.ccsds.APMFile
Set the comment for epoch.
setEpochFreedom(int, boolean) - Method in class org.orekit.utils.AbstractMultipleShooting
Set the epoch a patch point to free or not.
setEpochStart(AbsoluteDate) - Method in class org.orekit.files.ccsds.APMFile.APMManeuver
Set epoch start.
setEstimatedValue(double...) - Method in class org.orekit.estimation.measurements.EstimatedMeasurement
Set the estimated value.
setEulerComment(List<String>) - Method in class org.orekit.files.ccsds.APMFile
Set the comment for Euler angles.
setEulerDirection(String) - Method in class org.orekit.files.ccsds.APMFile
Set the rotation direction of the attitude Euler angles (A2B or B2A).
setEulerFrameAString(String) - Method in class org.orekit.files.ccsds.APMFile
Set the reference frame specifying one frame of the transformation.
setEulerFrameBString(String) - Method in class org.orekit.files.ccsds.APMFile
Set the reference frame specifying the second portion of the transformation.
setEulerRotSeq(String) - Method in class org.orekit.files.ccsds.AEMFile.AttitudeEphemeridesBlock
Set the rotation sequence of the Euler angles (e.g., 312, where X=1, Y=2, Z=3).
setEulerRotSeq(String) - Method in class org.orekit.files.ccsds.APMFile
Set the rotation order for Euler angles (X=1, Y=2, Z=3).
setEvaluationsCounter(Incrementor) - Method in class org.orekit.estimation.leastsquares.BatchLSModel
Set the counter for evaluations.
setEvaluationsCounter(Incrementor) - Method in interface org.orekit.estimation.leastsquares.BatchLSODModel
Set the counter for evaluations.
setEvaluationsCounter(Incrementor) - Method in class org.orekit.estimation.leastsquares.DSSTBatchLSModel
Set the counter for evaluations.
setFiring(boolean, AbsoluteDate) - Method in class org.orekit.forces.maneuvers.trigger.EventBasedManeuverTriggers
Set the firing start or end date depending on the firing flag.
setFormatVersion(double) - Method in class org.orekit.files.ccsds.NDMFile
Set the CCSDS NDM (ADM or ODM) format version.
setFrameEpoch(AbsoluteDate) - Method in class org.orekit.files.ccsds.ODMMetaData
Set epoch of reference frame, if not intrinsic to the definition of the reference frame.
setFrameEpochString(String) - Method in class org.orekit.files.ccsds.ODMMetaData
Set epoch of reference frame, if not intrinsic to the definition of the reference frame.
setFrameString(String) - Method in class org.orekit.files.ccsds.ODMMetaData
Set the reference frame name.
setFreqOffset(double) - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData
Setter for the freqOffset.
setHasCreatableBody(boolean) - Method in class org.orekit.files.ccsds.ADMMetaData
Set boolean testing whether the body corresponding to the centerName attribute can be created through the CelestialBodies.
setHasCreatableBody(boolean) - Method in class org.orekit.files.ccsds.ODMMetaData
Set boolean testing whether the body corresponding to the centerName attribute can be created through the CelestialBodies.
setHasRefFrameEpoch(boolean) - Method in class org.orekit.files.ccsds.OEMFile.EphemeridesBlock
Set boolean testing whether the reference frame has an epoch associated to it.
setHeaderComment(List<String>) - Method in class org.orekit.files.ccsds.NDMFile
Set the header comment.
setI11(double) - Method in class org.orekit.files.ccsds.APMFile
Set the moment of Inertia about the 1-axis (N.m²).
setI12(double) - Method in class org.orekit.files.ccsds.APMFile
Set the moment of Inertia about the 1 and 2 axes (N.m²).
setI13(double) - Method in class org.orekit.files.ccsds.APMFile
Set the moment of Inertia about the 1 and 3 axes (N.m²).
setI22(double) - Method in class org.orekit.files.ccsds.APMFile
Set the moment of Inertia about the 2-axis (N.m²).
setI23(double) - Method in class org.orekit.files.ccsds.APMFile
Set the moment of Inertia about the 2 and 3 axes (N.m²).
setI33(double) - Method in class org.orekit.files.ccsds.APMFile
Set the moment of Inertia about the 3-axis (N.m²).
setIgnoreCentralAttraction(boolean) - Method in class org.orekit.propagation.numerical.FieldNumericalPropagator
Set the flag to ignore or not the creation of a NewtonianAttraction.
setIgnoreCentralAttraction(boolean) - Method in class org.orekit.propagation.numerical.NumericalPropagator
Set the flag to ignore or not the creation of a NewtonianAttraction.
setInertiaRefFrameString(String) - Method in class org.orekit.files.ccsds.APMFile
Set the coordinate system for the inertia tensor.
setInitialJacobians(SpacecraftState, double[][], double[][], double[]) - Method in class org.orekit.propagation.integration.AbstractJacobiansMapper
Set the Jacobian with respect to state into a one-dimensional additional state array.
setInitialJacobians(SpacecraftState) - Method in class org.orekit.propagation.numerical.EpochDerivativesEquations
Set the initial value of the Jacobian with respect to state and parameter.
setInitialJacobians(SpacecraftState, double[][], double[][]) - Method in class org.orekit.propagation.numerical.EpochDerivativesEquations
Set the initial value of the Jacobian with respect to state and parameter.
setInitialJacobians(SpacecraftState, double[][], double[][], double[]) - Method in class org.orekit.propagation.numerical.JacobiansMapper
Set the Jacobian with respect to state into a one-dimensional additional state array.
setInitialJacobians(SpacecraftState) - Method in class org.orekit.propagation.numerical.PartialDerivativesEquations
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, double[][], double[][], double[]) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTJacobiansMapper
Set the Jacobian with respect to state into a one-dimensional additional state array.
setInitialJacobians(SpacecraftState) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPartialDerivativesEquations
Set the initial value of the Jacobian with respect to state and parameter.
setInitialJacobians(SpacecraftState, double[][], double[][]) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPartialDerivativesEquations
Set the initial value of the Jacobian with respect to state and parameter.
setInitialPhi(SpacecraftState) - Method in class org.orekit.propagation.numerical.cr3bp.STMEquations
Method adding the standard initial values of the additional state to the initial spacecraft state.
setInitialState(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.numerical.FieldNumericalPropagator
Set the initial state.
setInitialState(SpacecraftState) - Method in class org.orekit.propagation.numerical.NumericalPropagator
Set the initial state.
setInitialState(SpacecraftState) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator
Set the initial state with osculating orbital elements.
setInitialState(SpacecraftState, PropagationType) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator
Set the initial state.
setInitialState(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator
Set the initial state with osculating orbital elements.
setInitialState(FieldSpacecraftState<T>, PropagationType) - Method in class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator
Set the initial state.
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.
setInterpolationDegree(int) - Method in class org.orekit.files.ccsds.AEMFile.AttitudeEphemeridesBlock
Set the interpolation degree.
setInterpolationDegree(int) - Method in class org.orekit.files.ccsds.OEMFile.EphemeridesBlock
Set the interpolation degree.
setInterpolationGridToFixedNumberOfPoints(int) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator
Set the interpolation grid generator.
setInterpolationGridToFixedNumberOfPoints(int) - Method in class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator
Set the interpolation grid generator.
setInterpolationGridToMaxTimeGap(double) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator
Set the interpolation grid generator.
setInterpolationGridToMaxTimeGap(T) - Method in class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator
Set the interpolation grid generator.
setInterpolationMethod(String) - Method in class org.orekit.files.ccsds.AEMFile.AttitudeEphemeridesBlock
Set the interpolation method to be used.
setInterpolationMethod(String) - Method in class org.orekit.files.ccsds.OEMFile.EphemeridesBlock
Set the interpolation method to be used.
setIsFirst(boolean) - Method in class org.orekit.files.ccsds.AEMFile.AttitudeEphemeridesBlock
Set the flag for the placement of the quaternion QC in the attitude data.
setIterationsCounter(Incrementor) - Method in class org.orekit.estimation.leastsquares.BatchLSModel
Set the counter for iterations.
setIterationsCounter(Incrementor) - Method in interface org.orekit.estimation.leastsquares.BatchLSODModel
Set the counter for iterations.
setIterationsCounter(Incrementor) - Method in class org.orekit.estimation.leastsquares.DSSTBatchLSModel
Set the counter for iterations.
setKeyword(String) - Method in class org.orekit.files.ccsds.TDMFile.Observation
Setter for the keyword.
setLaunchNumber(int) - Method in class org.orekit.files.ccsds.ADMMetaData
Set the launch number.
setLaunchNumber(int) - Method in class org.orekit.files.ccsds.ODMMetaData
Set the launch number.
setLaunchPiece(String) - Method in class org.orekit.files.ccsds.ADMMetaData
Set the piece of launch.
setLaunchPiece(String) - Method in class org.orekit.files.ccsds.ODMMetaData
Set the piece of launch.
setLaunchYear(int) - Method in class org.orekit.files.ccsds.ADMMetaData
Set the launch year.
setLaunchYear(int) - Method in class org.orekit.files.ccsds.ODMMetaData
Set the launch year.
setLowElevationThreshold(double) - Method in class org.orekit.models.earth.troposphere.SaastamoinenModel
Set the low elevation threshold value for path delay computation.
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.DSSTPropagatorBuilder
Set the initial mass.
setMass(double) - Method in class org.orekit.propagation.conversion.NumericalPropagatorBuilder
Set the initial mass.
setMasterMode(double, OrekitFixedStepHandler) - Method in class org.orekit.propagation.AbstractPropagator
Set the propagator to master mode with fixed steps.
setMasterMode(OrekitStepHandler) - Method in class org.orekit.propagation.AbstractPropagator
Set the propagator to master mode with variable steps.
setMasterMode(T, FieldOrekitFixedStepHandler<T>) - Method in class org.orekit.propagation.FieldAbstractPropagator
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(T, FieldOrekitFixedStepHandler<T>) - Method in interface org.orekit.propagation.FieldPropagator
Set the propagator to master mode with fixed steps.
setMasterMode(FieldOrekitStepHandler<T>) - Method in interface org.orekit.propagation.FieldPropagator
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(FieldOrekitStepHandler<T>) - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator
Set the propagator to master mode with variable steps.
setMasterMode(double, OrekitFixedStepHandler) - Method in interface org.orekit.propagation.Propagator
Set the propagator to master mode with fixed steps.
setMasterMode(OrekitStepHandler) - Method in interface org.orekit.propagation.Propagator
Set the propagator to master mode with variable steps.
setMatrix(PolynomialFunction[][]) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.PolynomialFunctionMatrix
Set values for all elements.
setMatrixLine(int, PolynomialFunction[]) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.PolynomialFunctionMatrix
Set the value of a line of the matrix.
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.
setMissionReferenceDate(AbsoluteDate) - Method in class org.orekit.files.ccsds.NDMFile
Set reference date for Mission Elapsed Time and Mission Relative Time time systems.
setMode(String) - Method in class org.orekit.files.ccsds.TDMFile.TDMMetaData
Setter for the mode.
setMu(double) - Method in class org.orekit.files.ccsds.NDMFile
Set the used gravitational coefficient.
setMu(double) - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
Set the central body attraction coefficient.
setMu(double) - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
Set the central attraction coefficient μ.
setMu(T) - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator
Set the central attraction coefficient μ.
setMu(T) - Method in class org.orekit.propagation.numerical.FieldNumericalPropagator
Set the central attraction coefficient μ.
setMu(double) - Method in class org.orekit.propagation.numerical.NumericalPropagator
Set the central attraction coefficient μ.
setMu(double) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator
Set the central attraction coefficient μ.
setMu(T) - Method in class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator
Set the central attraction coefficient μ.
setMuSet(double) - Method in class org.orekit.files.ccsds.ODMFile
Set the gravitational coefficient set by the user.
setMuUsed() - Method in class org.orekit.files.ccsds.ODMFile
Set the gravitational coefficient created from the knowledge of the central body.
setName(int, SatelliteSystem) - Method in class org.orekit.estimation.measurements.gnss.AbstractCycleSlipDetector
Create the name of a satellite from its PRN number and satellite System it belongs to.
setName(String) - Method in class org.orekit.utils.ParameterDriver
Change the name of this parameter driver.
setNormalizedValue(double) - Method in class org.orekit.utils.ParameterDriver
Set normalized value.
setNutation(double) - Method in class org.orekit.files.ccsds.APMFile
Set the nutation angle of spin axis (rad).
setNutationPeriod(double) - Method in class org.orekit.files.ccsds.APMFile
Set the body nutation period of the spin axis (s).
setNutationPhase(double) - Method in class org.orekit.files.ccsds.APMFile
Set the inertial nutation phase (rad).
setObjectID(String) - Method in class org.orekit.files.ccsds.ADMMetaData
Set the spacecraft ID for which the attitude data are provided.
setObjectID(String) - Method in class org.orekit.files.ccsds.ODMMetaData
Set the spacecraft ID for which the orbit state is provided.
setObjectName(String) - Method in class org.orekit.files.ccsds.ADMMetaData
Set the spacecraft name for which the attitude data are provided.
setObjectName(String) - Method in class org.orekit.files.ccsds.ODMMetaData
Set the spacecraft name for which the orbit state is provided.
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.NDMFile
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.
setPatchPointComponentFreedom(int, int, boolean) - Method in class org.orekit.utils.AbstractMultipleShooting
Set a component of a patch point to free or not.
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(PositionAngle) - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
Set position angle type.
setPositionAngleType(PositionAngle) - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator
Set position angle type.
setPositionAngleType() - Method in class org.orekit.propagation.integration.FieldStateMapper
Set position angle type.
setPositionAngleType() - Method in class org.orekit.propagation.integration.StateMapper
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
setQuaternion(Quaternion) - Method in class org.orekit.files.ccsds.APMFile
Set the quaternion.
setQuaternionDot(Quaternion) - Method in class org.orekit.files.ccsds.APMFile
Set the derivative of the quaternion.
setQuaternionFrameAString(String) - Method in class org.orekit.files.ccsds.APMFile
Set the reference frame specifying one frame of the transformation.
setQuaternionFrameBString(String) - Method in class org.orekit.files.ccsds.APMFile
Set the reference frame specifying the second portion of the transformation.
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.
setRateFrameString(String) - Method in class org.orekit.files.ccsds.AEMFile.AttitudeEphemeridesBlock
Set the rate frame name.
setRateFrameString(String) - Method in class org.orekit.files.ccsds.APMFile
Set the frame of reference in which the Euler angles are expressed.
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.ODMMetaData
Set the reference frame in which data are given: used for state vector and Keplerian elements data (and for the covariance reference frame if none is given).
setRefFrame(Frame) - Method in class org.orekit.files.ccsds.OPMFile.Maneuver
Set Coordinate system for velocity increment vector, for absolute frames.
setRefFrameAString(String) - Method in class org.orekit.files.ccsds.AEMFile.AttitudeEphemeridesBlock
Set the reference frame A name.
setRefFrameBString(String) - Method in class org.orekit.files.ccsds.AEMFile.AttitudeEphemeridesBlock
Set the reference frame B name.
setRefFrameString(String) - Method in class org.orekit.files.ccsds.APMFile.APMManeuver
Set Coordinate system for the torque 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.GNSSDate
Set a reference date for ensuring continuity across GNSS week rollover.
setRotationAngles(Vector3D) - Method in class org.orekit.files.ccsds.APMFile
Set the coordinates of the Euler angles (rad).
setRotationOrder(RotationOrder) - Method in class org.orekit.files.ccsds.AEMFile.AttitudeEphemeridesBlock
Set the rotation order for Euler angles.
setRotationRates(Vector3D) - Method in class org.orekit.files.ccsds.APMFile
Set the rates of the Euler angles (rad/s).
setSatelliteRevolution(int) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator
Override the default value of the parameter.
setSatelliteRevolution(int) - Method in class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator
Override the default value of the parameter.
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.
setSelectedCoefficients(Set<String>) - Method in class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator
Set the selected short periodic coefficients that must be stored as additional states.
setShortPeriodJacobians(SpacecraftState) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTJacobiansMapper
Compute the derivatives of the short period terms related to the additional state parameters.
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.
setSpacecraftComment(List<String>) - Method in class org.orekit.files.ccsds.APMFile
Set the comment for spacecraft.
setSpinAlpha(double) - Method in class org.orekit.files.ccsds.APMFile
Set the right ascension of spin axis vector (rad).
setSpinAngle(double) - Method in class org.orekit.files.ccsds.APMFile
Set the phase of the satellite about the spin axis (rad).
setSpinAngleVel(double) - Method in class org.orekit.files.ccsds.APMFile
Set the angular velocity of satellite around spin axis (rad/s).
setSpinComment(List<String>) - Method in class org.orekit.files.ccsds.APMFile
Set the comment for spin data.
setSpinDelta(double) - Method in class org.orekit.files.ccsds.APMFile
Set the declination of the spin axis vector (rad).
setSpinDirection(String) - Method in class org.orekit.files.ccsds.APMFile
Set the rotation direction of the Spin angles.
setSpinFrameAString(String) - Method in class org.orekit.files.ccsds.APMFile
Set the reference frame specifying one frame of the transformation (spin).
setSpinFrameBString(String) - Method in class org.orekit.files.ccsds.APMFile
Set the reference frame specifying the second portion of the transformation (spin).
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.AEMFile.AttitudeEphemeridesBlock
Set start of total time span covered by attitude data.
setStartTime(AbsoluteDate) - Method in class org.orekit.files.ccsds.OEMFile.EphemeridesBlock
Set start of total time span covered by ephemerides data and covariance data.
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.AEMFile.AttitudeEphemeridesBlock
Set end of total time span covered by attitude data.
setStopTime(AbsoluteDate) - Method in class org.orekit.files.ccsds.OEMFile.EphemeridesBlock
Set end of total time span covered by ephemerides data and covariance data.
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.
setSupportedNames(String) - Method in class org.orekit.data.AbstractSelfFeedingLoader
Set the supported names regular expression.
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.ADMMetaData
Set the Time System.
setTimeSystem(CcsdsTimeScale) - Method in class org.orekit.files.ccsds.ODMMetaData
Set the Time System that: for OPM, is used for metadata, state vector, maneuver and covariance data, for OMM, is used for metadata, orbit state and covariance data, for OEM, is used for metadata, ephemeris and covariance data.
setTimeSystem(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.
setTorque(Vector3D) - Method in class org.orekit.files.ccsds.APMFile.APMManeuver
Set the torque vector (N.m).
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(ODEIntegrator, EventDetector) - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
Wrap an Orekit event detector and register it to the integrator.
setUpEventDetector(FieldODEIntegrator<T>, FieldEventDetector<T>) - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator
Wrap an Orekit event detector and register it to the integrator.
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.
setUseableStartTime(AbsoluteDate) - Method in class org.orekit.files.ccsds.AEMFile.AttitudeEphemeridesBlock
Set start of useable time span covered by attitude data.
setUseableStartTime(AbsoluteDate) - Method in class org.orekit.files.ccsds.OEMFile.EphemeridesBlock
Set start of useable time span covered by ephemerides data, it may be necessary to allow for proper interpolation.
setUseableStopTime(AbsoluteDate) - Method in class org.orekit.files.ccsds.AEMFile.AttitudeEphemeridesBlock
Set end of useable time span covered by ephemerides data.
setUseableStopTime(AbsoluteDate) - Method in class org.orekit.files.ccsds.OEMFile.EphemeridesBlock
Set end of useable time span covered by ephemerides data, it may be necessary to allow for proper interpolation.
setValue(double) - Method in class org.orekit.utils.ParameterDriver
Set parameter value.
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(TLE, AttitudeProvider, double) - Constructor for class org.orekit.propagation.analytical.tle.SGP4
Constructor for a unique initial TLE.
SGP4(TLE, AttitudeProvider, double, Frame) - Constructor for class org.orekit.propagation.analytical.tle.SGP4
Constructor for a unique initial TLE.
SGP4 - Static variable in class org.orekit.propagation.analytical.tle.TLE
Identifier for SGP4 type of ephemeris.
SGP8 - Static variable in class org.orekit.propagation.analytical.tle.TLE
Identifier for SGP8 type of ephemeris.
shapiroCorrection(TimeStampedPVCoordinates, TimeStampedPVCoordinates) - Method in class org.orekit.estimation.measurements.modifiers.AbstractShapiroBaseModifier
Compute Shapiro path dilation between two points in a gravity field.
ShapiroInterSatelliteRangeModifier - Class in org.orekit.estimation.measurements.modifiers
Class modifying theoretical range measurement with Shapiro time delay.
ShapiroInterSatelliteRangeModifier(double) - Constructor for class org.orekit.estimation.measurements.modifiers.ShapiroInterSatelliteRangeModifier
Simple constructor.
ShapiroPhaseModifier - Class in org.orekit.estimation.measurements.modifiers
Class modifying theoretical phase measurement with Shapiro time delay.
ShapiroPhaseModifier(double) - Constructor for class org.orekit.estimation.measurements.modifiers.ShapiroPhaseModifier
Simple constructor.
ShapiroRangeModifier - Class in org.orekit.estimation.measurements.modifiers
Class modifying theoretical range measurement with Shapiro time delay.
ShapiroRangeModifier(double) - Constructor for class org.orekit.estimation.measurements.modifiers.ShapiroRangeModifier
Simple constructor.
shiftedBy(double) - Method in class org.orekit.attitudes.Attitude
Get a time-shifted attitude.
shiftedBy(double) - Method in class org.orekit.attitudes.FieldAttitude
Get a time-shifted attitude.
shiftedBy(T) - Method in class org.orekit.attitudes.FieldAttitude
Get a time-shifted attitude.
shiftedBy(double) - Method in class org.orekit.frames.FieldTransform
Get a time-shifted instance.
shiftedBy(T) - Method in class org.orekit.frames.FieldTransform
Get a time-shifted instance.
shiftedBy(double) - Method in class org.orekit.frames.Transform
Get a time-shifted instance.
shiftedBy(double) - Method in class org.orekit.orbits.CartesianOrbit
Get a time-shifted orbit.
shiftedBy(double) - Method in class org.orekit.orbits.CircularOrbit
Get a time-shifted orbit.
shiftedBy(double) - Method in class org.orekit.orbits.EquinoctialOrbit
Get a time-shifted orbit.
shiftedBy(double) - Method in class org.orekit.orbits.FieldCartesianOrbit
Get a time-shifted instance.
shiftedBy(T) - Method in class org.orekit.orbits.FieldCartesianOrbit
Get a time-shifted orbit.
shiftedBy(double) - Method in class org.orekit.orbits.FieldCircularOrbit
Get a time-shifted instance.
shiftedBy(T) - Method in class org.orekit.orbits.FieldCircularOrbit
Get a time-shifted orbit.
shiftedBy(double) - Method in class org.orekit.orbits.FieldEquinoctialOrbit
Get a time-shifted instance.
shiftedBy(T) - Method in class org.orekit.orbits.FieldEquinoctialOrbit
Get a time-shifted orbit.
shiftedBy(double) - Method in class org.orekit.orbits.FieldKeplerianOrbit
Get a time-shifted instance.
shiftedBy(T) - Method in class org.orekit.orbits.FieldKeplerianOrbit
Get a time-shifted orbit.
shiftedBy(T) - Method in class org.orekit.orbits.FieldOrbit
Get a time-shifted orbit.
shiftedBy(double) - Method in class org.orekit.orbits.KeplerianOrbit
Get a time-shifted orbit.
shiftedBy(double) - Method in class org.orekit.orbits.Orbit
Get a time-shifted orbit.
shiftedBy(double) - Method in class org.orekit.propagation.FieldSpacecraftState
Get a time-shifted state.
shiftedBy(T) - Method in class org.orekit.propagation.FieldSpacecraftState
Get a time-shifted state.
shiftedBy(double) - Method in class org.orekit.propagation.SpacecraftState
Get a time-shifted state.
shiftedBy(double) - Method in class org.orekit.time.AbsoluteDate
Get a time-shifted date.
shiftedBy(T) - Method in class org.orekit.time.FieldAbsoluteDate
Get a time-shifted date.
shiftedBy(double) - Method in class org.orekit.time.FieldAbsoluteDate
Get a time-shifted date.
shiftedBy(double) - Method in interface org.orekit.time.FieldTimeShiftable
Get a time-shifted instance.
shiftedBy(KK) - Method in interface org.orekit.time.FieldTimeShiftable
Get a time-shifted instance.
shiftedBy(double) - Method in interface org.orekit.time.TimeShiftable
Get a time-shifted instance.
shiftedBy(double) - Method in class org.orekit.utils.AbsolutePVCoordinates
Get a time-shifted state.
shiftedBy(double) - Method in class org.orekit.utils.AngularCoordinates
Get a time-shifted state.
shiftedBy(T) - Method in class org.orekit.utils.FieldAbsolutePVCoordinates
Get a time-shifted state.
shiftedBy(double) - Method in class org.orekit.utils.FieldAbsolutePVCoordinates
Get a time-shifted state.
shiftedBy(double) - Method in class org.orekit.utils.FieldAngularCoordinates
Get a time-shifted state.
shiftedBy(T) - Method in class org.orekit.utils.FieldAngularCoordinates
Get a time-shifted state.
shiftedBy(double) - Method in class org.orekit.utils.FieldPVCoordinates
Get a time-shifted state.
shiftedBy(T) - Method in class org.orekit.utils.FieldPVCoordinates
Get a time-shifted state.
shiftedBy(double) - Method in class org.orekit.utils.PVCoordinates
Get a time-shifted state.
shiftedBy(double) - Method in class org.orekit.utils.TimeStampedAngularCoordinates
Get a time-shifted state.
shiftedBy(double) - Method in class org.orekit.utils.TimeStampedFieldAngularCoordinates
Get a time-shifted state.
shiftedBy(T) - Method in class org.orekit.utils.TimeStampedFieldAngularCoordinates
Get a time-shifted state.
shiftedBy(double) - Method in class org.orekit.utils.TimeStampedFieldPVCoordinates
Get a time-shifted state.
shiftedBy(T) - Method in class org.orekit.utils.TimeStampedFieldPVCoordinates
Get a time-shifted state.
shiftedBy(double) - Method in class org.orekit.utils.TimeStampedPVCoordinates
Get a time-shifted state.
ShiftingTransformProvider - Class in org.orekit.frames
Transform provider using thread-safe shifts on transforms sample.
ShiftingTransformProvider(TransformProvider, CartesianDerivativesFilter, AngularDerivativesFilter, int, double, int, double, double) - Constructor for class org.orekit.frames.ShiftingTransformProvider
Simple constructor.
SHM_FILENAME - Static variable in class org.orekit.forces.gravity.potential.GravityFieldFactory
Default regular expression for SHM files.
SHMFormatReader - Class in org.orekit.forces.gravity.potential
Reader for the SHM gravity field format.
SHMFormatReader(String, boolean) - Constructor for class org.orekit.forces.gravity.potential.SHMFormatReader
Simple constructor.
SHMFormatReader(String, boolean, TimeScale) - Constructor for class org.orekit.forces.gravity.potential.SHMFormatReader
Simple constructor.
SHORT_PERIOD_PREFIX - Static variable in class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseral
Name of the prefix for short period coefficients keys.
SHORT_PERIOD_PREFIX - Static variable in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBody
Name of the prefix for short period coefficients keys.
SHORT_PERIOD_PREFIX - Static variable in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonal
Name of the prefix for short period coefficients keys.
ShortPeriodicsInterpolatedCoefficient - Class in org.orekit.propagation.semianalytical.dsst.utilities
Interpolated short periodics coefficients.
ShortPeriodicsInterpolatedCoefficient(int) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.ShortPeriodicsInterpolatedCoefficient
Simple constructor.
ShortPeriodTerms - Interface in org.orekit.propagation.semianalytical.dsst.forces
Additive short period terms contributing to the mean to osculating orbit mapping.
sign(double) - Method in class org.orekit.estimation.measurements.gnss.ModifiedLambdaMethod
Return the symbol of parameter a.
SignalCode - Enum in org.orekit.gnss
Enumerate for satellite signal code.
signalTimeOfFlight(TimeStampedPVCoordinates, Vector3D, AbsoluteDate) - Static method in class org.orekit.estimation.measurements.AbstractMeasurement
Compute propagation delay on a link leg (typically downlink or uplink).
signalTimeOfFlight(TimeStampedFieldPVCoordinates<T>, FieldVector3D<T>, FieldAbsoluteDate<T>) - Static method in class org.orekit.estimation.measurements.AbstractMeasurement
Compute propagation delay on a link leg (typically downlink or uplink).
signedAmplitude(SpacecraftState, double[]) - Method in class org.orekit.forces.AbstractParametricAcceleration
Compute the signed amplitude of the acceleration.
signedAmplitude(FieldSpacecraftState<T>, T[]) - 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(FieldSpacecraftState<T>, T[]) - 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.
signedAmplitude(FieldSpacecraftState<T>, T[]) - 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.models.earth.atmosphere
Simple exponential atmospheric model.
SimpleExponentialAtmosphere(BodyShape, double, double, double) - Constructor for class org.orekit.models.earth.atmosphere.SimpleExponentialAtmosphere
Create an exponential atmosphere.
SimpleRatioAmbiguityAcceptance - Class in org.orekit.estimation.measurements.gnss
Ambiguity acceptance test based on a ratio of the two best candidates.
SimpleRatioAmbiguityAcceptance(double) - Constructor for class org.orekit.estimation.measurements.gnss.SimpleRatioAmbiguityAcceptance
Simple constructor.
SimpleTimeStampedTableParser<T extends TimeStamped> - Class in org.orekit.data
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.
SingleBodyAbsoluteAttraction - Class in org.orekit.forces.gravity
Body attraction force model computed as absolute acceleration towards a body.
SingleBodyAbsoluteAttraction(CelestialBody) - Constructor for class org.orekit.forces.gravity.SingleBodyAbsoluteAttraction
Simple constructor.
SingleBodyRelativeAttraction - Class in org.orekit.forces.gravity
Body attraction force model computed as relative acceleration towards frame center.
SingleBodyRelativeAttraction(CelestialBody) - Constructor for class org.orekit.forces.gravity.SingleBodyRelativeAttraction
Simple constructor.
SingleLayerModelMappingFunction - Class in org.orekit.models.earth.ionosphere
Single Layer Model (SLM) ionospheric mapping function.
SingleLayerModelMappingFunction() - Constructor for class org.orekit.models.earth.ionosphere.SingleLayerModelMappingFunction
Constructor with default value.
SingleLayerModelMappingFunction(double) - Constructor for class org.orekit.models.earth.ionosphere.SingleLayerModelMappingFunction
Constructor.
sini0 - Variable in class org.orekit.propagation.analytical.tle.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.
SM_COEFFICIENTS - Static variable in class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseral
Identifier for sMm coefficients.
SmallManeuverAnalyticalModel - Class in org.orekit.forces.maneuvers
Analytical model for small maneuvers.
SmallManeuverAnalyticalModel(SpacecraftState, Vector3D, double) - Constructor for class org.orekit.forces.maneuvers.SmallManeuverAnalyticalModel
Build a maneuver defined in spacecraft frame.
SmallManeuverAnalyticalModel(SpacecraftState, Frame, Vector3D, double) - Constructor for class org.orekit.forces.maneuvers.SmallManeuverAnalyticalModel
Build a maneuver defined in user-specified frame.
SmoothFieldOfView - Class in org.orekit.geometry.fov
Class representing a spacecraft sensor Field Of View with shape defined by a smooth single loop.
SmoothFieldOfView(Vector3D, Vector3D, double) - Constructor for class org.orekit.geometry.fov.SmoothFieldOfView
Build a new instance.
SOLAR_SYSTEM_BARYCENTER - Static variable in class org.orekit.bodies.CelestialBodyFactory
Predefined name for solar system barycenter.
SolarRadiationPressure - Class in org.orekit.forces.radiation
Solar radiation pressure force model.
SolarRadiationPressure(ExtendedPVCoordinatesProvider, double, RadiationSensitive) - Constructor for class org.orekit.forces.radiation.SolarRadiationPressure
Simple constructor with default reference values.
SolarRadiationPressure(double, double, ExtendedPVCoordinatesProvider, double, RadiationSensitive) - Constructor for class org.orekit.forces.radiation.SolarRadiationPressure
Complete constructor.
SolidTides - Class in org.orekit.forces.gravity
Solid tides force model.
SolidTides(Frame, double, double, TideSystem, IERSConventions, UT1Scale, CelestialBody...) - Constructor for class org.orekit.forces.gravity.SolidTides
Simple constructor.
SolidTides(Frame, double, double, TideSystem, boolean, double, int, IERSConventions, UT1Scale, CelestialBody...) - Constructor for class org.orekit.forces.gravity.SolidTides
Simple constructor.
solveILS(int, double[], int[], RealMatrix) - Method in class org.orekit.estimation.measurements.gnss.AbstractLambdaMethod
Find the best solutions to an Integer Least Square problem.
solveILS(int, double[], int[], RealMatrix) - Method in interface org.orekit.estimation.measurements.gnss.IntegerLeastSquareSolver
Find the best solutions to an Integer Least Square problem.
sort() - Method in class org.orekit.utils.ParameterDriversList
Sort the parameters lexicographically.
SOUTH_POLE - Static variable in class org.orekit.bodies.GeodeticPoint
South pole.
SP3_FRAME_CENTER_STRING - Static variable in class org.orekit.files.sp3.SP3File
String representation of the center of ephemeris coordinate system.
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.
SP3Parser(double, int, Function<? super String, ? extends Frame>, TimeScales) - Constructor for class org.orekit.files.sp3.SP3Parser
Create an SP3 parser and specify the extra information needed to create a Propagator from the ephemeris data.
SpacecraftState - Class in org.orekit.propagation
This class is the representation of a complete state holding orbit, attitude and mass information at a given date.
SpacecraftState(Orbit) - Constructor for class org.orekit.propagation.SpacecraftState
Build a spacecraft state from orbit only.
SpacecraftState(Orbit, Attitude) - Constructor for class org.orekit.propagation.SpacecraftState
Build a spacecraft state from orbit and attitude provider.
SpacecraftState(Orbit, double) - Constructor for class org.orekit.propagation.SpacecraftState
Create a new instance from orbit and mass.
SpacecraftState(Orbit, Attitude, double) - Constructor for class org.orekit.propagation.SpacecraftState
Build a spacecraft state from orbit, attitude provider and mass.
SpacecraftState(Orbit, Map<String, double[]>) - Constructor for class org.orekit.propagation.SpacecraftState
Build a spacecraft state from orbit only.
SpacecraftState(Orbit, Attitude, Map<String, double[]>) - Constructor for class org.orekit.propagation.SpacecraftState
Build a spacecraft state from orbit and attitude provider.
SpacecraftState(Orbit, double, Map<String, double[]>) - Constructor for class org.orekit.propagation.SpacecraftState
Create a new instance from orbit and mass.
SpacecraftState(Orbit, Attitude, double, Map<String, double[]>) - Constructor for class org.orekit.propagation.SpacecraftState
Build a spacecraft state from orbit, attitude provider and mass.
SpacecraftState(AbsolutePVCoordinates) - Constructor for class org.orekit.propagation.SpacecraftState
Build a spacecraft state from orbit only.
SpacecraftState(AbsolutePVCoordinates, Attitude) - Constructor for class org.orekit.propagation.SpacecraftState
Build a spacecraft state from orbit and attitude provider.
SpacecraftState(AbsolutePVCoordinates, double) - Constructor for class org.orekit.propagation.SpacecraftState
Create a new instance from orbit and mass.
SpacecraftState(AbsolutePVCoordinates, Attitude, double) - Constructor for class org.orekit.propagation.SpacecraftState
Build a spacecraft state from orbit, attitude provider and mass.
SpacecraftState(AbsolutePVCoordinates, Map<String, double[]>) - Constructor for class org.orekit.propagation.SpacecraftState
Build a spacecraft state from orbit only.
SpacecraftState(AbsolutePVCoordinates, Attitude, Map<String, double[]>) - Constructor for class org.orekit.propagation.SpacecraftState
Build a spacecraft state from orbit and attitude provider.
SpacecraftState(AbsolutePVCoordinates, double, Map<String, double[]>) - Constructor for class org.orekit.propagation.SpacecraftState
Create a new instance from orbit and mass.
SpacecraftState(AbsolutePVCoordinates, Attitude, double, Map<String, double[]>) - Constructor for class org.orekit.propagation.SpacecraftState
Build a spacecraft state from orbit, attitude provider and mass.
SPEED_OF_LIGHT - Static variable in interface org.orekit.utils.Constants
Speed of light: 299792458.0 m/s.
SphericalHarmonicsProvider - Interface in org.orekit.forces.gravity.potential
Interface used to provide spherical harmonics coefficients.
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).
started(TaskEvent) - Method in class org.orekit.compiler.plugin.DefaultDataContextPlugin
 
startParse(String) - Method in class org.orekit.forces.gravity.potential.OceanTidesReader
Start parsing.
STATE_DIMENSION - Static variable in class org.orekit.propagation.integration.AbstractJacobiansMapper
State dimension, fixed to 6.
STATE_DIMENSION - Static variable in class org.orekit.propagation.numerical.AbsoluteJacobiansMapper
State dimension, fixed to 6.
STATE_DIMENSION - Static variable in class org.orekit.propagation.numerical.JacobiansMapper
State dimension, fixed to 6.
STATE_DIMENSION - Static variable in class org.orekit.propagation.semianalytical.dsst.DSSTJacobiansMapper
State dimension, fixed to 6.
stateChanged(SpacecraftState) - Method in class org.orekit.propagation.AbstractPropagator
Notify about a state change.
stateChanged(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.FieldAbstractPropagator
Notify about a state change.
StateFunction - Interface in org.orekit.utils
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.
StationDisplacement - Interface in org.orekit.models.earth.displacement
Interface for computing reference points displacement.
stec(AbsoluteDate, GeodeticPoint, GeodeticPoint) - Method in class org.orekit.models.earth.ionosphere.NeQuickModel
This method allows the computation of the Stant Total Electron Content (STEC).
stec(FieldAbsoluteDate<T>, FieldGeodeticPoint<T>, FieldGeodeticPoint<T>) - Method in class org.orekit.models.earth.ionosphere.NeQuickModel
This method allows the computation of the Stant Total Electron Content (STEC).
stillAcceptsData() - Method in interface org.orekit.data.DataLoader
Check if the loader still accepts new data.
stillAcceptsData() - Method in class org.orekit.forces.gravity.potential.AstronomicalAmplitudeReader
Check if the loader still accepts new data.
stillAcceptsData() - Method in class org.orekit.forces.gravity.potential.OceanTidesReader
Check if the loader still accepts new data.
stillAcceptsData() - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
Check if the loader still accepts new data.
stillAcceptsData() - Method in class org.orekit.gnss.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.atmosphere.data.CssiSpaceWeatherDataLoader
Check if the loader still accepts new data.
stillAcceptsData() - Method in class org.orekit.models.earth.atmosphere.data.MarshallSolarActivityFutureEstimation
Check if the loader still accepts new data.
stillAcceptsData() - Method in class org.orekit.models.earth.GeoMagneticModelLoader
Check if the loader still accepts new data.
stillAcceptsData() - Method in class org.orekit.models.earth.ionosphere.KlobucharIonoCoefficientsLoader
Check if the loader still accepts new data.
stillAcceptsData() - Method in class org.orekit.models.earth.troposphere.ViennaModelCoefficientsLoader
 
stillAcceptsData() - Method in class org.orekit.utils.InterpolationTableLoader
Check if the loader still accepts new data.
STMEquations - Class in org.orekit.propagation.numerical.cr3bp
Class calculating the state transition matrix coefficient for CR3BP Computation.
STMEquations(CR3BPSystem) - Constructor for class org.orekit.propagation.numerical.cr3bp.STMEquations
Simple constructor.
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
 
StreamingAemWriter - Class in org.orekit.files.ccsds
A writer for AEM files.
StreamingAemWriter(Appendable, TimeScale, Map<Keyword, String>) - Constructor for class org.orekit.files.ccsds.StreamingAemWriter
Create an AEM writer that streams data to the given output stream.
StreamingAemWriter.AEMSegment - Class in org.orekit.files.ccsds
A writer for a segment of an AEM.
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.
subtractOffset(AngularCoordinates) - Method in class org.orekit.utils.AngularCoordinates
Subtract an offset from the instance.
subtractOffset(FieldAngularCoordinates<T>) - Method in class org.orekit.utils.FieldAngularCoordinates
Subtract an offset from the instance.
subtractOffset(AngularCoordinates) - Method in class org.orekit.utils.TimeStampedAngularCoordinates
Subtract an offset from the instance.
subtractOffset(FieldAngularCoordinates<T>) - Method in class org.orekit.utils.TimeStampedFieldAngularCoordinates
Subtract an offset from the instance.
SUN - Static variable in class org.orekit.bodies.CelestialBodyFactory
Predefined name for Sun.
SUN_RADIUS - Static variable in interface org.orekit.utils.Constants
Sun radius: 695500000 m.
SUPPORTED_NAMES - Static variable in class org.orekit.frames.ITRFVersionLoader
Regular expression for supported files names.
supportsTimeTransform() - Method in class org.orekit.models.earth.GeoMagneticField
Indicates whether this model supports time transformation or not.
switchOccurred(AttitudeProvider, AttitudeProvider, SpacecraftState) - Method in interface org.orekit.attitudes.AttitudesSequence.SwitchHandler
Method called when attitude is switched from one law to another law.
sxpInitialize() - 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.
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.
TAIUTCDatFilesLoader(String, DataProvidersManager) - Constructor for class org.orekit.time.TAIUTCDatFilesLoader
Build a loader for tai-utc.dat file from USNO.
TAIUTCDatFilesLoader.Parser - Class in org.orekit.time
Internal class performing the parsing.
TargetPointing - Class in org.orekit.attitudes
This class handles target pointing attitude provider.
TargetPointing(Frame, Frame, Vector3D) - Constructor for class org.orekit.attitudes.TargetPointing
Creates a new instance from body frame and target expressed in Cartesian coordinates.
TargetPointing(Frame, GeodeticPoint, BodyShape) - Constructor for class org.orekit.attitudes.TargetPointing
Creates a new instance from body shape and target expressed in geodetic coordinates.
TCBScale - Class in org.orekit.time
Barycentric Coordinate Time.
TCGScale - Class in org.orekit.time
Geocentric Coordinate Time.
TDBScale - Class in org.orekit.time
Barycentric Dynamic Time.
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.
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.gnss.Phase
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.MultiplexedMeasurement
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.
ThirdBodyAttractionEpoch - Class in org.orekit.forces.gravity
Third body attraction force model.
ThirdBodyAttractionEpoch(CelestialBody) - Constructor for class org.orekit.forces.gravity.ThirdBodyAttractionEpoch
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
Deprecated.
THRUST - Static variable in class org.orekit.forces.maneuvers.propulsion.BasicConstantThrustPropulsionModel
Parameter name for thrust.
THRUST_SCALE - Static variable in class org.orekit.forces.maneuvers.propulsion.BasicConstantThrustPropulsionModel
Thrust scaling factor.
ThrustDirectionAndAttitudeProvider - Class in org.orekit.forces.maneuvers.propulsion
This class is used in to both manage the attitude of the satellite and the direction of thrust.
ThrustDirectionProvider - Interface in org.orekit.forces.maneuvers.propulsion
Interface to compute the thrust direction of a maneuver.
ThrustPropulsionModel - Interface in org.orekit.forces.maneuvers.propulsion
Interface for a thrust-based propulsion model.
THRUSTX_SCALE_FACTOR - Static variable in class org.orekit.forces.maneuvers.propulsion.ScaledConstantThrustPropulsionModel
Parameter name for the scale factor on the X component of the thrust in S/C frame.
THRUSTY_SCALE_FACTOR - Static variable in class org.orekit.forces.maneuvers.propulsion.ScaledConstantThrustPropulsionModel
Parameter name for the scale factor on the Y component of the thrust in S/C frame.
THRUSTZ_SCALE_FACTOR - Static variable in class org.orekit.forces.maneuvers.propulsion.ScaledConstantThrustPropulsionModel
Parameter name for the scale factor on the Z component of the thrust in S/C frame.
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, int, int, int, int, int) - Constructor for class org.orekit.models.earth.displacement.Tide
Simple constructor.
Tide(int) - Constructor for class org.orekit.models.earth.displacement.Tide
Simple constructor.
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.
TimeComponents - Class in org.orekit.time
Class representing a time within the day broken up as hour, minute and second components.
TimeComponents(int, int, double) - Constructor for class org.orekit.time.TimeComponents
Build a time from its clock elements.
TimeComponents(int, int, double, int) - Constructor for class org.orekit.time.TimeComponents
Build a time from its clock elements.
TimeComponents(double) - Constructor for class org.orekit.time.TimeComponents
Build a time from the second number within the day.
TimeComponents(int, double) - Constructor for class org.orekit.time.TimeComponents
Build a time from the second number within the day.
TimeDerivativesEquations - Interface in org.orekit.propagation.numerical
Interface summing up the contribution of several forces into orbit and mass derivatives.
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.
TimeScales - Interface in org.orekit.time
A collection of TimeScales.
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.
TimeSpanDragForce - Class in org.orekit.forces.drag
Time span atmospheric drag force model.
TimeSpanDragForce(Atmosphere, DragSensitive) - Constructor for class org.orekit.forces.drag.TimeSpanDragForce
Constructor with default UTC time scale for the default names of the drag parameter drivers.
TimeSpanDragForce(Atmosphere, DragSensitive, TimeScale) - Constructor for class org.orekit.forces.drag.TimeSpanDragForce
Constructor.
TimeSpanEstimatedTroposphericModel - Class in org.orekit.models.earth.troposphere
Time span estimated tropospheric model.
TimeSpanEstimatedTroposphericModel(EstimatedTroposphericModel) - Constructor for class org.orekit.models.earth.troposphere.TimeSpanEstimatedTroposphericModel
Constructor with default UTC time scale.
TimeSpanEstimatedTroposphericModel(EstimatedTroposphericModel, TimeScale) - Constructor for class org.orekit.models.earth.troposphere.TimeSpanEstimatedTroposphericModel
Constructor with default UTC time scale.
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, Rotation, Vector3D, Vector3D) - Constructor for class org.orekit.utils.TimeStampedAngularCoordinates
Builds a rotation/rotation rate pair.
TimeStampedAngularCoordinates(AbsoluteDate, PVCoordinates, PVCoordinates, PVCoordinates, PVCoordinates, double) - Constructor for class org.orekit.utils.TimeStampedAngularCoordinates
Build the rotation that transforms a pair of pv coordinates into another pair.
TimeStampedAngularCoordinates(AbsoluteDate, PVCoordinates, PVCoordinates) - Constructor for class org.orekit.utils.TimeStampedAngularCoordinates
Build one of the rotations that transform one pv coordinates into another one.
TimeStampedAngularCoordinates(AbsoluteDate, FieldRotation<DerivativeStructure>) - Constructor for class org.orekit.utils.TimeStampedAngularCoordinates
Builds a TimeStampedAngularCoordinates from a FieldRotation<DerivativeStructure>.
TimeStampedCache<T extends TimeStamped> - Interface in org.orekit.utils
Interface for a data structure that can provide concurrent access to TimeStamped data surrounding a given date.
TimeStampedCacheException - Exception in org.orekit.errors
This class is the base class for all specific exceptions thrown by during the GenericTimeStampedCache.
TimeStampedCacheException(Localizable, Object...) - Constructor for exception org.orekit.errors.TimeStampedCacheException
Simple constructor.
TimeStampedCacheException(Throwable, Localizable, Object...) - Constructor for exception org.orekit.errors.TimeStampedCacheException
Simple constructor.
TimeStampedCacheException(OrekitException) - Constructor for exception org.orekit.errors.TimeStampedCacheException
Simple constructor.
TimeStampedCacheException(MathRuntimeException) - Constructor for exception org.orekit.errors.TimeStampedCacheException
Simple constructor.
TimeStampedFieldAngularCoordinates<T extends RealFieldElement<T>> - Class in org.orekit.utils
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>, 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(AbsoluteDate, FieldRotation<T>, FieldVector3D<T>, FieldVector3D<T>) - Constructor for class org.orekit.utils.TimeStampedFieldAngularCoordinates
Builds a rotation/rotation rate pair.
TimeStampedFieldAngularCoordinates(FieldAbsoluteDate<T>, FieldRotation<T>, FieldVector3D<T>, FieldVector3D<T>) - Constructor for class org.orekit.utils.TimeStampedFieldAngularCoordinates
Builds a rotation/rotation rate pair.
TimeStampedFieldAngularCoordinates(Field<T>, TimeStampedAngularCoordinates) - Constructor for class org.orekit.utils.TimeStampedFieldAngularCoordinates
Builds an instance for a regular TimeStampedAngularCoordinates.
TimeStampedFieldAngularCoordinates(FieldAbsoluteDate<T>, FieldRotation<FieldDerivativeStructure<T>>) - Constructor for class org.orekit.utils.TimeStampedFieldAngularCoordinates
Builds a TimeStampedFieldAngularCoordinates from a FieldRotation<FieldDerivativeStructure>.
TimeStampedFieldPVCoordinates<T extends RealFieldElement<T>> - Class in org.orekit.utils
TimeStampedFieldPVCoordinates(AbsoluteDate, FieldVector3D<T>, FieldVector3D<T>, FieldVector3D<T>) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates
Builds a PVCoordinates pair.
TimeStampedFieldPVCoordinates(FieldAbsoluteDate<T>, 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(FieldAbsoluteDate<T>, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates
Basic constructor.
TimeStampedFieldPVCoordinates(AbsoluteDate, double, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates
Multiplicative constructor
TimeStampedFieldPVCoordinates(FieldAbsoluteDate<T>, double, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates
Multiplicative constructor
TimeStampedFieldPVCoordinates(AbsoluteDate, T, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates
Multiplicative constructor
TimeStampedFieldPVCoordinates(FieldAbsoluteDate<T>, T, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates
Multiplicative constructor
TimeStampedFieldPVCoordinates(AbsoluteDate, T, PVCoordinates) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates
Multiplicative constructor
TimeStampedFieldPVCoordinates(FieldAbsoluteDate<T>, T, PVCoordinates) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates
Multiplicative constructor
TimeStampedFieldPVCoordinates(AbsoluteDate, FieldPVCoordinates<T>, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates
Subtractive constructor
TimeStampedFieldPVCoordinates(FieldAbsoluteDate<T>, FieldPVCoordinates<T>, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates
Subtractive constructor
TimeStampedFieldPVCoordinates(AbsoluteDate, double, FieldPVCoordinates<T>, double, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates
Linear constructor
TimeStampedFieldPVCoordinates(FieldAbsoluteDate<T>, double, FieldPVCoordinates<T>, double, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates
Linear constructor
TimeStampedFieldPVCoordinates(AbsoluteDate, T, FieldPVCoordinates<T>, T, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates
Linear constructor
TimeStampedFieldPVCoordinates(FieldAbsoluteDate<T>, T, FieldPVCoordinates<T>, T, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates
Linear constructor
TimeStampedFieldPVCoordinates(AbsoluteDate, T, PVCoordinates, T, PVCoordinates) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates
Linear constructor
TimeStampedFieldPVCoordinates(FieldAbsoluteDate<T>, T, PVCoordinates, T, PVCoordinates) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates
Linear constructor
TimeStampedFieldPVCoordinates(AbsoluteDate, double, FieldPVCoordinates<T>, double, FieldPVCoordinates<T>, double, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates
Linear constructor
TimeStampedFieldPVCoordinates(FieldAbsoluteDate<T>, double, FieldPVCoordinates<T>, double, FieldPVCoordinates<T>, double, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates
Linear constructor
TimeStampedFieldPVCoordinates(AbsoluteDate, T, FieldPVCoordinates<T>, T, FieldPVCoordinates<T>, T, FieldPVCoordinates<T>) - 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(AbsoluteDate, T, PVCoordinates, 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(AbsoluteDate, double, FieldPVCoordinates<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(AbsoluteDate, 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, FieldPVCoordinates<T>, T, FieldPVCoordinates<T>, T, FieldPVCoordinates<T>, T, FieldPVCoordinates<T>) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates
Linear constructor
TimeStampedFieldPVCoordinates(AbsoluteDate, T, PVCoordinates, T, PVCoordinates, T, PVCoordinates, T, PVCoordinates) - Constructor for class org.orekit.utils.TimeStampedFieldPVCoordinates
Linear constructor
TimeStampedFieldPVCoordinates(FieldAbsoluteDate<T>, T, PVCoordinates, T, PVCoordinates, T, PVCoordinates, T, PVCoordinates) - 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>.
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, Vector3D, Vector3D, Vector3D) - Constructor for class org.orekit.utils.TimeStampedPVCoordinates
Builds a TimeStampedPVCoordinates pair.
TimeStampedPVCoordinates(AbsoluteDate, Vector3D, Vector3D) - Constructor for class org.orekit.utils.TimeStampedPVCoordinates
Build from position and velocity.
TimeStampedPVCoordinates(AbsoluteDate, PVCoordinates) - Constructor for class org.orekit.utils.TimeStampedPVCoordinates
Build from position velocity acceleration coordinates.
TimeStampedPVCoordinates(AbsoluteDate, double, PVCoordinates) - Constructor for class org.orekit.utils.TimeStampedPVCoordinates
Multiplicative constructor
TimeStampedPVCoordinates(AbsoluteDate, PVCoordinates, PVCoordinates) - Constructor for class org.orekit.utils.TimeStampedPVCoordinates
Subtractive constructor
TimeStampedPVCoordinates(AbsoluteDate, double, PVCoordinates, double, PVCoordinates) - Constructor for class org.orekit.utils.TimeStampedPVCoordinates
Linear constructor
TimeStampedPVCoordinates(AbsoluteDate, double, PVCoordinates, double, PVCoordinates, double, PVCoordinates) - Constructor for class org.orekit.utils.TimeStampedPVCoordinates
Linear constructor
TimeStampedPVCoordinates(AbsoluteDate, double, PVCoordinates, double, PVCoordinates, double, PVCoordinates, double, PVCoordinates) - Constructor for class org.orekit.utils.TimeStampedPVCoordinates
Linear constructor
TimeStampedPVCoordinates(AbsoluteDate, FieldVector3D<DerivativeStructure>) - Constructor for class org.orekit.utils.TimeStampedPVCoordinates
Builds a TimeStampedPVCoordinates triplet from a FieldVector3D<DerivativeStructure>.
TimeVectorFunction - Interface in org.orekit.time
This interface represents a multi-valued function of time.
TLE - Class in org.orekit.propagation.analytical.tle
This class is a container for a single set of TLE data.
TLE(String, String) - Constructor for class org.orekit.propagation.analytical.tle.TLE
Simple constructor from unparsed two lines.
TLE(String, String, TimeScale) - Constructor for class org.orekit.propagation.analytical.tle.TLE
Simple constructor from unparsed two lines using the given time scale as UTC.
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(int, char, int, int, String, int, int, AbsoluteDate, double, double, double, double, double, double, double, double, int, double, TimeScale) - Constructor for class org.orekit.propagation.analytical.tle.TLE
Simple constructor from already parsed elements using the given time scale as UTC.
tle - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator
Initial state.
TLEPropagator - Class in org.orekit.propagation.analytical.tle
This class provides elements to propagate TLE's.
TLEPropagator(TLE, AttitudeProvider, double) - Constructor for class org.orekit.propagation.analytical.tle.TLEPropagator
Protected constructor for derived classes.
TLEPropagator(TLE, AttitudeProvider, double, Frame) - 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.
TLEPropagatorBuilder(TLE, PositionAngle, double, DataContext) - Constructor for class org.orekit.propagation.conversion.TLEPropagatorBuilder
Build a new instance.
toAbsoluteDate() - Method in class org.orekit.time.FieldAbsoluteDate
Transform the FieldAbsoluteDate in an AbsoluteDate.
toAbsolutePVCoordinates() - Method in class org.orekit.utils.FieldAbsolutePVCoordinates
Converts to an AbsolutePVCoordinates instance.
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.
toDate(DateComponents) - Method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
Create a date from components.
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(T, FieldOrbit<T>, OrbitType) - Static method in class org.orekit.propagation.numerical.FieldNumericalPropagator
Estimate tolerance vectors for integrators.
tolerances(double, AbsolutePVCoordinates) - Static method in class org.orekit.propagation.numerical.NumericalPropagator
Estimate tolerance vectors for integrators when propagating in absolute position-velocity-acceleration.
tolerances(double, Orbit, OrbitType) - Static method in class org.orekit.propagation.numerical.NumericalPropagator
Estimate tolerance vectors for integrators when propagating in orbits.
tolerances(double, Orbit) - Static method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator
Estimate tolerance vectors for an AdaptativeStepsizeIntegrator.
tolerances(T, FieldOrbit<T>) - Static method in class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator
Estimate tolerance vectors for an AdaptativeStepsizeIntegrator.
toNonRotating(AbsoluteDate, double, double) - Method in interface org.orekit.utils.IERSConventions.NutationCorrectionConverter
Convert nutation corrections.
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.
toRadians(KeyValue) - Method in class org.orekit.files.ccsds.ADMParser
Convert a KeyValue in degrees to a real value in randians.
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.propagation.events.handlers.FieldRecordAndContinue.Event
 
toString() - Method in class org.orekit.propagation.events.handlers.RecordAndContinue.Event
 
toString() - Method in class org.orekit.propagation.FieldSpacecraftState
 
toString() - Method in class org.orekit.propagation.SpacecraftState
 
toString() - Method in class org.orekit.time.AbsoluteDate
Get a String representation of the instant location in UTC time scale.
toString(TimeScale) - Method in class org.orekit.time.AbsoluteDate
Get a String representation of the instant location.
toString(int) - Method in class org.orekit.time.AbsoluteDate
Get a String representation of the instant location for a local time.
toString(int, TimeScale) - Method in class org.orekit.time.AbsoluteDate
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, TimeScale) - Method in class org.orekit.time.AbsoluteDate
Get a String representation of the instant location for a time zone.
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(int) - 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(TimeScale) - Method in class org.orekit.time.FieldAbsoluteDate
Get a String representation of the instant location.
toString(int) - Method in class org.orekit.time.FieldAbsoluteDate
Get a String representation of the instant location for a local time.
toString(int, TimeScale) - 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.FieldAbsoluteDate
Get a String representation of the instant location for a time zone.
toString(TimeZone, TimeScale) - Method in class org.orekit.time.FieldAbsoluteDate
Get a String representation of the instant location for a time zone.
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 date, position, velocity, and acceleration.
toString(TimeScale) - Method in class org.orekit.utils.TimeStampedFieldPVCoordinates
Return a string representation of this date, position, velocity, and acceleration.
toString() - Method in class org.orekit.utils.TimeStampedPVCoordinates
Return a string representation of this date, position, velocity, and acceleration.
toString(TimeScale) - Method in class org.orekit.utils.TimeStampedPVCoordinates
Return a string representation of this date, position, velocity, and acceleration.
toStringRfc3339(TimeScale) - Method in class org.orekit.time.AbsoluteDate
Represent the given date as a string according to the format in RFC 3339.
toStringRfc3339() - Method in class org.orekit.time.DateTimeComponents
Represent the given date and time as a string according to the format in RFC 3339.
TOTAL_ZENITH_DELAY - Static variable in class org.orekit.models.earth.troposphere.EstimatedTroposphericModel
Name of the parameter of this model: the total zenith delay.
toTaylorProvider() - Method in class org.orekit.utils.AbsolutePVCoordinates
Create a local provider using simply Taylor expansion through AbsolutePVCoordinates.shiftedBy(double).
toTaylorProvider() - Method in class org.orekit.utils.FieldAbsolutePVCoordinates
Create a local provider using simply Taylor expansion through FieldAbsolutePVCoordinates.shiftedBy(double).
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 state defining frame to spacecraft frame.
toTransform() - Method in class org.orekit.propagation.SpacecraftState
Compute the transform from state defining frame to spacecraft frame.
toUnivariateDerivative1PV() - Method in class org.orekit.utils.FieldPVCoordinates
Transform the instance to a FieldPVCoordinates<FieldUnivariateDerivative1>.
toUnivariateDerivative1PV() - Method in class org.orekit.utils.PVCoordinates
Transform the instance to a FieldPVCoordinates<UnivariateDerivative1>.
toUnivariateDerivative1Rotation() - Method in class org.orekit.utils.AngularCoordinates
Transform the instance to a FieldRotation<UnivariateDerivative1>.
toUnivariateDerivative1Rotation() - Method in class org.orekit.utils.FieldAngularCoordinates
Transform the instance to a FieldRotation<UnivariateDerivative1>.
toUnivariateDerivative1Vector() - Method in class org.orekit.utils.FieldPVCoordinates
Transform the instance to a FieldVector3D<FieldUnivariateDerivative1>.
toUnivariateDerivative1Vector() - Method in class org.orekit.utils.PVCoordinates
Transform the instance to a FieldVector3D<UnivariateDerivative1>.
toUnivariateDerivative2PV() - Method in class org.orekit.utils.FieldPVCoordinates
Transform the instance to a FieldPVCoordinates<FieldUnivariateDerivative2>.
toUnivariateDerivative2PV() - Method in class org.orekit.utils.PVCoordinates
Transform the instance to a FieldPVCoordinates<UnivariateDerivative2>.
toUnivariateDerivative2Vector() - Method in class org.orekit.utils.FieldPVCoordinates
Transform the instance to a FieldVector3D<FieldUnivariateDerivative2>.
toUnivariateDerivative2Vector() - Method in class org.orekit.utils.PVCoordinates
Transform the instance to a FieldVector3D<UnivariateDerivative2>.
transform(Vector3D, Frame, AbsoluteDate) - Method in interface org.orekit.bodies.BodyShape
Transform a Cartesian point to a surface-relative point.
transform(FieldVector3D<T>, Frame, FieldAbsoluteDate<T>) - Method in interface org.orekit.bodies.BodyShape
Transform a Cartesian point to a surface-relative point.
transform(GeodeticPoint) - Method in interface org.orekit.bodies.BodyShape
Transform a surface-relative point to a Cartesian point.
transform(FieldGeodeticPoint<T>) - 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(FieldGeodeticPoint<T>) - Method in class org.orekit.bodies.OneAxisEllipsoid
Transform a surface-relative point to a Cartesian point.
transform(Vector3D, Frame, AbsoluteDate) - Method in class org.orekit.bodies.OneAxisEllipsoid
Transform a Cartesian point to a surface-relative point.
transform(FieldVector3D<T>, Frame, FieldAbsoluteDate<T>) - Method in class org.orekit.bodies.OneAxisEllipsoid
Transform a Cartesian point to a surface-relative 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, Vector3D) - Constructor for class org.orekit.frames.Transform
Build a translation transform.
Transform(AbsoluteDate, Rotation) - Constructor for class org.orekit.frames.Transform
Build a rotation transform.
Transform(AbsoluteDate, Vector3D, Vector3D) - Constructor for class org.orekit.frames.Transform
Build a translation transform, with its first time derivative.
Transform(AbsoluteDate, Vector3D, Vector3D, Vector3D) - Constructor for class org.orekit.frames.Transform
Build a translation transform, with its first and second time derivatives.
Transform(AbsoluteDate, PVCoordinates) - Constructor for class org.orekit.frames.Transform
Build a translation transform, with its first time derivative.
Transform(AbsoluteDate, Rotation, Vector3D) - Constructor for class org.orekit.frames.Transform
Build a rotation transform.
Transform(AbsoluteDate, Rotation, Vector3D, Vector3D) - Constructor for class org.orekit.frames.Transform
Build a rotation transform.
Transform(AbsoluteDate, AngularCoordinates) - Constructor for class org.orekit.frames.Transform
Build a rotation transform.
Transform(AbsoluteDate, Transform, Transform) - Constructor for class org.orekit.frames.Transform
Build a transform by combining two existing ones.
transform(Vector3D, Frame, AbsoluteDate) - Method in class org.orekit.models.earth.Geoid
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(GeodeticPoint) - Method in class org.orekit.models.earth.Geoid
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.
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(Line) - Method in class org.orekit.frames.FieldTransform
Transform a line.
transformLine(FieldLine<T>) - 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(Vector3D) - Method in class org.orekit.frames.FieldTransform
Transform a position vector (including translation effects).
transformPosition(FieldVector3D<T>) - 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).
transformPosition(FieldVector3D<T>) - Method in class org.orekit.frames.Transform
Transform a position vector (including translation effects).
TransformProvider - Interface in org.orekit.frames
Interface for Transform providers.
TransformProviderUtils - Class in org.orekit.frames
Utility for Transform providers.
transformPVCoordinates(PVCoordinates) - Method in class org.orekit.frames.FieldTransform
Transform TimeStampedPVCoordinates including kinematic effects.
transformPVCoordinates(TimeStampedPVCoordinates) - Method in class org.orekit.frames.FieldTransform
Transform TimeStampedPVCoordinates including kinematic effects.
transformPVCoordinates(FieldPVCoordinates<T>) - Method in class org.orekit.frames.FieldTransform
Transform TimeStampedFieldPVCoordinates including kinematic effects.
transformPVCoordinates(TimeStampedFieldPVCoordinates<T>) - Method in class org.orekit.frames.FieldTransform
Transform TimeStampedFieldPVCoordinates including kinematic effects.
transformPVCoordinates(PVCoordinates) - Method in class org.orekit.frames.Transform
Transform PVCoordinates including kinematic effects.
transformPVCoordinates(TimeStampedPVCoordinates) - Method in class org.orekit.frames.Transform
Transform TimeStampedPVCoordinates including kinematic effects.
transformPVCoordinates(FieldPVCoordinates<T>) - Method in class org.orekit.frames.Transform
Transform FieldPVCoordinates including kinematic effects.
transformPVCoordinates(TimeStampedFieldPVCoordinates<T>) - Method in class org.orekit.frames.Transform
Transform TimeStampedFieldPVCoordinates including kinematic effects.
transformVector(Vector3D) - Method in class org.orekit.frames.FieldTransform
Transform a vector (ignoring translation effects).
transformVector(FieldVector3D<T>) - 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).
transformVector(FieldVector3D<T>) - Method in class org.orekit.frames.Transform
Transform a vector (ignoring translation effects).
TroposphericDSConverter - Class in org.orekit.estimation.measurements.modifiers
Deprecated.
as of 10.2, replaced by TroposphericGradientConverter
TroposphericDSConverter(SpacecraftState, int, AttitudeProvider) - Constructor for class org.orekit.estimation.measurements.modifiers.TroposphericDSConverter
Deprecated.
Simple constructor.
TroposphericGradientConverter - Class in org.orekit.estimation.measurements.modifiers
Converter for states and parameters arrays.
TroposphericGradientConverter(SpacecraftState, int, AttitudeProvider) - Constructor for class org.orekit.estimation.measurements.modifiers.TroposphericGradientConverter
Simple constructor.
TRUE_ANOM - Static variable in enum org.orekit.orbits.OrbitType
Name for mean anomaly.
TRUE_LAT_ARG - Static variable in enum org.orekit.orbits.OrbitType
Name for mean argument of latitude.
TRUE_LON_ARG - Static variable in enum org.orekit.orbits.OrbitType
Name for mean argument of longitude.
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(T, T) - Static method in class org.orekit.orbits.FieldKeplerianOrbit
Computes the elliptic eccentric anomaly from the true anomaly.
trueToEllipticEccentric(double, double) - Static method in class org.orekit.orbits.KeplerianOrbit
Computes the elliptic 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.
trueToHyperbolicEccentric(double, double) - Static method in class org.orekit.orbits.KeplerianOrbit
Computes the hyperbolic eccentric anomaly from the true anomaly.
tryAdvance(SpacecraftState, OrekitStepInterpolator) - Method in class org.orekit.propagation.events.EventState
Try to accept the current history up to the given time.
tryAdvance(FieldSpacecraftState<T>, FieldOrekitStepInterpolator<T>) - Method in class org.orekit.propagation.events.FieldEventState
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.
TTScale - Class in org.orekit.time
Terrestrial Time as defined by IAU(1991) recommendation IV.
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, 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, double) - 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.
TWO_PI - Static variable in class org.orekit.propagation.semianalytical.dsst.utilities.FieldAuxiliaryElements
\(2\pi\) .
TwoBodiesBaryFrame - Class in org.orekit.frames
Class creating the inertial barycenter frame from two bodies.
TwoBodiesBaryFrame(CelestialBody, CelestialBody) - Constructor for class org.orekit.frames.TwoBodiesBaryFrame
Simple constructor.

U

unableToParseLine(Throwable) - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherDataLoader.LineReader
Annotate an exception with the file context.
unFixAmbiguity(ParameterDriver) - Method in class org.orekit.estimation.measurements.gnss.AmbiguitySolver
Un-fix an integer ambiguity (typically after a phase cycle slip).
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
 
UnnormalizedSphericalHarmonicsProvider - Interface in org.orekit.forces.gravity.potential
Interface used to provide un-normalized spherical harmonics coefficients.
UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics - Interface in org.orekit.forces.gravity.potential
Un-normalized spherical harmonics coefficients evaluated at a specific instant.
unwrap(MathRuntimeException) - Static method in exception org.orekit.errors.OrekitException
Recover a OrekitException, possibly embedded in a MathRuntimeException.
unwrap(OrekitException) - Static method in exception org.orekit.errors.TimeStampedCacheException
Recover a TimeStampedCacheException, possibly embedded in a OrekitException.
unwrap(MathRuntimeException) - Static method in exception org.orekit.errors.TimeStampedCacheException
Recover a TimeStampedCacheException, possibly embedded in a MathRuntimeException.
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.
updateAdditionalConstraints(int, double[]) - Method in class org.orekit.utils.AbstractMultipleShooting
Update the array of additional constraints.
updateAdditionalStates(SpacecraftState) - Method in class org.orekit.propagation.AbstractPropagator
Update state by adding all additional states.
updateAdditionalStates(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.FieldAbstractPropagator
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(double[], SpacecraftState...) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution
Update the short period terms.
updateShortPeriodTerms(T[], FieldSpacecraftState<T>...) - Method in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContribution
Update the short period terms.
updateShortPeriodTerms(double[], SpacecraftState...) - Method in interface org.orekit.propagation.semianalytical.dsst.forces.DSSTForceModel
Update the short period terms.
updateShortPeriodTerms(T[], FieldSpacecraftState<T>...) - Method in interface org.orekit.propagation.semianalytical.dsst.forces.DSSTForceModel
Update the short period terms.
updateShortPeriodTerms(double[], SpacecraftState...) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTNewtonianAttraction
Update the short period terms.
updateShortPeriodTerms(T[], FieldSpacecraftState<T>...) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTNewtonianAttraction
Update the short period terms.
updateShortPeriodTerms(double[], SpacecraftState...) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseral
Update the short period terms.
updateShortPeriodTerms(T[], FieldSpacecraftState<T>...) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseral
Update the short period terms.
updateShortPeriodTerms(double[], SpacecraftState...) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBody
Update the short period terms.
updateShortPeriodTerms(T[], FieldSpacecraftState<T>...) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBody
Update the short period terms.
updateShortPeriodTerms(double[], SpacecraftState...) - Method in class org.orekit.propagation.semianalytical.dsst.forces.DSSTZonal
Update the short period terms.
updateShortPeriodTerms(T[], FieldSpacecraftState<T>...) - 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 - Static variable in class org.orekit.bodies.CelestialBodyFactory
Predefined name for Uranus.
usesInterpolation() - Method in class org.orekit.frames.EOPHistory
Check if the instance uses interpolation on tidal corrections.
UT1Scale - Class in org.orekit.time
Universal Time 1.
UT1Scale(EOPHistory, UTCScale) - Constructor for class org.orekit.time.UT1Scale
Simple constructor.
utc - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator
UTC time scale.
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.
UTCTAIBulletinAFilesLoader(String, DataProvidersManager) - 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.
UTCTAIHistoryFilesLoader(DataProvidersManager) - Constructor for class org.orekit.time.UTCTAIHistoryFilesLoader
Build a loader for UTC-TAI history file.
UTCTAIHistoryFilesLoader.Parser - Class in org.orekit.time
Internal class performing the parsing.
UTCTAIOffsetsLoader - Interface in org.orekit.time
Interface for loading UTC-TAI offsets data files.
UTCTAIOffsetsLoader.Parser - Interface in org.orekit.time
Interface for parsing UTC-TAI offsets from a stream.
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 interface org.orekit.gnss.attitude.GNSSAttitudeProvider
Get end 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(BodiesElements) - Method in interface org.orekit.data.PoissonSeries.CompiledSeries
Evaluate a set of Poisson series.
value(FieldBodiesElements<S>) - Method in interface org.orekit.data.PoissonSeries.CompiledSeries
Evaluate a set of Poisson series.
value(BodiesElements) - Method in class org.orekit.data.PoissonSeries
Evaluate the value of the series.
value(FieldBodiesElements<T>) - Method in class org.orekit.data.PoissonSeries
Evaluate the value of the series.
value(double) - Method in class org.orekit.data.PolynomialNutation
Evaluate the value of the polynomial.
value(T) - Method in class org.orekit.data.PolynomialNutation
Evaluate the value of the polynomial.
value(RealVector) - Method in class org.orekit.estimation.leastsquares.BatchLSModel
value(RealVector) - Method in class org.orekit.estimation.leastsquares.DSSTBatchLSModel
value(AbsoluteDate, Vector3D, double) - Method in class org.orekit.forces.gravity.HolmesFeatherstoneAttractionModel
Compute the value of the gravity field.
value(double, double) - Method in interface org.orekit.gnss.antenna.PhaseCenterVariationFunction
Evaluate phase center variation in one signal direction.
value(FieldOrbit<T>) - Method in interface org.orekit.propagation.semianalytical.dsst.forces.FieldShortPeriodTerms
Evaluate the contributions of the short period terms.
value(Orbit) - Method in interface org.orekit.propagation.semianalytical.dsst.forces.ShortPeriodTerms
Evaluate the contributions of the short period terms.
value(FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldShortPeriodicsInterpolatedCoefficient
Compute the value of the coefficient.
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(FieldAbsoluteDate<T>) - 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(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(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.
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.estimation.measurements.gnss.CombinationType
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.AEMAttitudeType
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.files.ccsds.AEMParser.AEMRotationOrder
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.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.geometry.fov.PolygonalFieldOfView.DefiningConeType
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.gnss.SignalCode
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.models.earth.atmosphere.data.MarshallSolarActivityFutureEstimation.StrengthLevel
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.troposphere.ViennaModelType
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.orbits.LibrationOrbitFamily
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.orbits.LibrationOrbitType
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.VisibilityTrigger
Returns the enum constant of this type with the specified name.
valueOf(String) - Static method in enum org.orekit.propagation.PropagationType
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.
valueOf(String) - Static method in enum org.orekit.utils.LagrangianPoints
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.estimation.measurements.gnss.CombinationType
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.AEMAttitudeType
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.AEMParser.AEMRotationOrder
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.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.geometry.fov.PolygonalFieldOfView.DefiningConeType
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.gnss.SignalCode
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.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.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.troposphere.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.LibrationOrbitFamily
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.orbits.LibrationOrbitType
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.VisibilityTrigger
Returns an array containing the constants of this enum type, in the order they are declared.
values() - Static method in enum org.orekit.propagation.PropagationType
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.
values() - Static method in enum org.orekit.utils.LagrangianPoints
Returns an array containing the constants of this enum type, in the order they are declared.
VEL_X - Static variable in enum org.orekit.orbits.OrbitType
Name for velocity along X.
VEL_Y - Static variable in enum org.orekit.orbits.OrbitType
Name for velocity along Y.
VEL_Z - Static variable in enum org.orekit.orbits.OrbitType
Name for velocity along Z.
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.
VERTICAL_TOTAL_ELECTRON_CONTENT - Static variable in class org.orekit.models.earth.ionosphere.EstimatedIonosphericModel
Name of the parameter of this model: the Vertical Total Electron Content.
verticesRadius(double, int) - Method in enum org.orekit.geometry.fov.PolygonalFieldOfView.DefiningConeType
Compute radius of cone going through vertices.
ViennaModelCoefficientsLoader - Class in org.orekit.models.earth.troposphere
Loads Vienna tropospheric coefficients a given input stream.
ViennaModelCoefficientsLoader(String, double, double, ViennaModelType) - Constructor for class org.orekit.models.earth.troposphere.ViennaModelCoefficientsLoader
Constructor with supported names given by user.
ViennaModelCoefficientsLoader(String, double, double, ViennaModelType, DataProvidersManager) - Constructor for class org.orekit.models.earth.troposphere.ViennaModelCoefficientsLoader
Constructor with supported names and source of mapping function files given by the user.
ViennaModelCoefficientsLoader(double, double, ViennaModelType) - Constructor for class org.orekit.models.earth.troposphere.ViennaModelCoefficientsLoader
Constructor with default supported names.
ViennaModelType - Enum in org.orekit.models.earth.troposphere
Enumerate for Vienna tropospheric model 1 and 3.
ViennaOneModel - Class in org.orekit.models.earth.troposphere
The Vienna1 tropospheric delay model for radio techniques.
ViennaOneModel(double[], double[], double) - Constructor for class org.orekit.models.earth.troposphere.ViennaOneModel
Build a new instance.
ViennaOneModel(double[], double[], double, TimeScale) - Constructor for class org.orekit.models.earth.troposphere.ViennaOneModel
Build a new instance.
ViennaThreeModel - Class in org.orekit.models.earth.troposphere
The Vienna3 tropospheric delay model for radio techniques.
ViennaThreeModel(double[], double[], double, double) - Constructor for class org.orekit.models.earth.troposphere.ViennaThreeModel
Build a new instance.
ViennaThreeModel(double[], double[], double, double, TimeScale) - Constructor for class org.orekit.models.earth.troposphere.ViennaThreeModel
Build a new instance.
VisibilityTrigger - Enum in org.orekit.propagation.events
Enumerate for triggering visibility of spherical bodies.

W

WeatherModel - Interface in org.orekit.models.earth.weather
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.weather.GlobalPressureTemperature2Model
 
weatherParameters(double, AbsoluteDate) - Method in class org.orekit.models.earth.weather.GlobalPressureTemperatureModel
 
weatherParameters(double, AbsoluteDate) - Method in interface org.orekit.models.earth.weather.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.
WideLaneCombination - Class in org.orekit.estimation.measurements.gnss
Wide-Lane combination.
WindUp - Class in org.orekit.estimation.measurements.gnss
Modifier for wind-up effect in GNSS phase measurements.
WindUpFactory - Class in org.orekit.estimation.measurements.gnss
Factory for wind-up modifiers.
WindUpFactory() - Constructor for class org.orekit.estimation.measurements.gnss.WindUpFactory
Simple constructor.
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.ADMParser
Set IERS conventions.
withConventions(IERSConventions) - Method in class org.orekit.files.ccsds.AEMParser
Set IERS conventions.
withConventions(IERSConventions) - Method in class org.orekit.files.ccsds.APMParser
Set IERS conventions.
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.
withDataContext(DataContext) - Method in class org.orekit.files.ccsds.ADMParser
Set the data context.
withDataContext(DataContext) - Method in class org.orekit.files.ccsds.AEMParser
Set the data context.
withDataContext(DataContext) - Method in class org.orekit.files.ccsds.APMParser
Set the data context.
withDataContext(DataContext) - Method in class org.orekit.files.ccsds.ODMParser
Set the data context.
withDataContext(DataContext) - Method in class org.orekit.files.ccsds.OEMParser
 
withDataContext(DataContext) - Method in class org.orekit.files.ccsds.OMMParser
 
withDataContext(DataContext) - Method in class org.orekit.files.ccsds.OPMParser
 
withDataContext(DataContext) - Method in class org.orekit.files.ccsds.TDMParser
Set the data context.
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(Function<FieldSpacecraftState<T>, T>) - Method in class org.orekit.propagation.events.FieldFunctionalDetector
Create a new event detector with a new g function, keeping all other attributes the same.
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.
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.ADMParser
Set international designator.
withInternationalDesignator(int, int, String) - Method in class org.orekit.files.ccsds.AEMParser
Set international designator.
withInternationalDesignator(int, int, String) - Method in class org.orekit.files.ccsds.APMParser
Set international designator.
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.ADMParser
Set initial date.
withMissionReferenceDate(AbsoluteDate) - Method in class org.orekit.files.ccsds.AEMParser
Set initial date.
withMissionReferenceDate(AbsoluteDate) - Method in class org.orekit.files.ccsds.APMParser
Set initial date.
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.ADMParser
Set gravitational coefficient.
withMu(double) - Method in class org.orekit.files.ccsds.AEMParser
Set gravitational coefficient.
withMu(double) - Method in class org.orekit.files.ccsds.APMParser
Set gravitational coefficient.
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.ADMParser
Set EOP interpolation method.
withSimpleEOP(boolean) - Method in class org.orekit.files.ccsds.AEMParser
Set EOP interpolation method.
withSimpleEOP(boolean) - Method in class org.orekit.files.ccsds.APMParser
Set EOP interpolation method.
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.models.earth.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.
write(Appendable, AEMFile) - Method in class org.orekit.files.ccsds.AEMWriter
Write the passed in AEMFile using the passed in Appendable.
write(String, AEMFile) - Method in class org.orekit.files.ccsds.AEMWriter
Write the passed in AEMFile to a file at the output path specified.
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.
writeAttitudeEphemerisLine(TimeStampedAngularCoordinates, boolean, String, RotationOrder) - Method in class org.orekit.files.ccsds.StreamingAemWriter.AEMSegment
Write a single attitude ephemeris line according to section 4.2.4 and Table 4-4.
writeCovarianceMatrices(List<OEMFile.CovarianceMatrix>) - Method in class org.orekit.files.ccsds.StreamingOemWriter.Segment
Write covariance matrices of the segment according to section 5.2.5.
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.StreamingAemWriter
Writes the standard AEM header for the file.
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.StreamingAemWriter.AEMSegment
Write the ephemeris segment metadata.
writeMetadata() - Method in class org.orekit.files.ccsds.StreamingOemWriter.Segment
Write the ephemeris segment metadata.

X

xl - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator
L from SPTRCK #3.
xmdot - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator
common parameter for mean anomaly (M) computation.
xn0dp - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator
original recovered mean motion.
xnodcf - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator
common parameter for raan (OMEGA) computation.
xnode - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator
final RAAN.
xnodot - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator
common parameter for raan (OMEGA) computation.

Y

YawCompensation - Class in org.orekit.attitudes
This class handles yaw compensation attitude provider.
YawCompensation(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.
YUMAParser(String, DataProvidersManager, TimeScales) - Constructor for class org.orekit.gnss.YUMAParser
Create a YUMA loader/parser with the given source for YUMA auxiliary data files.

Z

ZERO - Static variable in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenUtilities
0 represented as a polynomial.
ZERO - Static variable in class org.orekit.utils.PVCoordinates
Fixed position/velocity at origin (both p, v and a are zero vectors).
zIndex(int, int) - Method in class org.orekit.estimation.measurements.gnss.AbstractLambdaMethod
Get the index of an entry in the Z transformation matrix.
ZIP_ARCHIVE_PATTERN - Static variable in interface org.orekit.data.DataProvider
Pattern for name of zip/jar archives.
ZipJarCrawler - Class in org.orekit.data
Helper class for loading data files from a zip/jar archive.
ZipJarCrawler(File) - Constructor for class org.orekit.data.ZipJarCrawler
Build a zip crawler for an archive file on filesystem.
ZipJarCrawler(String) - Constructor for class org.orekit.data.ZipJarCrawler
Build a zip crawler for an archive file in classpath.
ZipJarCrawler(ClassLoader, String) - Constructor for class org.orekit.data.ZipJarCrawler
Build a zip crawler for an archive file in classpath.
ZipJarCrawler(URL) - Constructor for class org.orekit.data.ZipJarCrawler
Build a zip crawler for an archive file on network.
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