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A

a - Variable in class org.orekit.propagation.analytical.tle.FieldTLEPropagator
final semi major axis.
a - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator
final semi major axis.
A - org.orekit.gnss.SignalCode
Galileo A PRS / IRNSS A SPS / GLONASS L1OCd and L2CSI / Beidou B1A and B3A codes.
A - Static variable in enum org.orekit.orbits.OrbitType
Name for semi major axis.
A_SBAS - org.orekit.files.rinex.navigation.SbasId
African Satellite-Based Augmentation System (ASECNA).
a0dp - Variable in class org.orekit.propagation.analytical.tle.FieldTLEPropagator
original recovered semi major axis.
a0dp - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator
original recovered semi major axis.
A2B - Static variable in class org.orekit.files.ccsds.ndm.adm.AttitudeEndpoints
Constant for A → B diraction.
A3OVK2 - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants
A3OVK2.
AberrationModifier - Class in org.orekit.estimation.measurements.modifiers
Class modifying theoretical angular measurement with (the inverse of) stellar aberration.
AberrationModifier() - Constructor for class org.orekit.estimation.measurements.modifiers.AberrationModifier
Empty constructor.
AberrationModifier(DataContext) - Constructor for class org.orekit.estimation.measurements.modifiers.AberrationModifier
Constructor.
AbsoluteDate - Class in org.orekit.time
This class represents a specific instant in time.
AbsoluteDate() - Constructor for class org.orekit.time.AbsoluteDate
Create an instance with a default value (AbsoluteDate.J2000_EPOCH).
AbsoluteDate(int, int, int, int, int, double, TimeScale) - Constructor for class org.orekit.time.AbsoluteDate
Build an instance from a location in a time scale.
AbsoluteDate(int, int, int, TimeScale) - Constructor for class org.orekit.time.AbsoluteDate
Build an instance from a location in a time scale.
AbsoluteDate(int, Month, int, int, int, double, TimeScale) - Constructor for class org.orekit.time.AbsoluteDate
Build an instance from a location in a time scale.
AbsoluteDate(int, Month, int, TimeScale) - Constructor for class org.orekit.time.AbsoluteDate
Build an instance from a location in a time scale.
AbsoluteDate(String, TimeScale) - Constructor for class org.orekit.time.AbsoluteDate
Build an instance from a location (parsed from a string) in a time scale.
AbsoluteDate(Instant) - Constructor for class org.orekit.time.AbsoluteDate
Build an instance from an instant in utc time scale.
AbsoluteDate(Instant, TimeScale) - Constructor for class org.orekit.time.AbsoluteDate
AbsoluteDate(Instant, UTCScale) - Constructor for class org.orekit.time.AbsoluteDate
Build an instance from an instant in the time scale.
AbsoluteDate(Date, TimeScale) - Constructor for class org.orekit.time.AbsoluteDate
Build an instance from a location in a time scale.
AbsoluteDate(AbsoluteDate, double) - Constructor for class org.orekit.time.AbsoluteDate
Build an instance from an elapsed duration since to another instant.
AbsoluteDate(AbsoluteDate, double, TimeScale) - Constructor for class org.orekit.time.AbsoluteDate
Build an instance from an apparent clock offset with respect to another instant in the perspective of a specific time scale.
AbsoluteDate(AbsoluteDate, long, TimeUnit) - Constructor for class org.orekit.time.AbsoluteDate
Build an instance from an elapsed duration since to another instant.
AbsoluteDate(DateComponents, TimeComponents, TimeScale) - Constructor for class org.orekit.time.AbsoluteDate
Build an instance from a location in a time scale.
AbsoluteDate(DateComponents, TimeScale) - Constructor for class org.orekit.time.AbsoluteDate
Build an instance from a location in a time scale.
AbsoluteDate(DateTimeComponents, TimeScale) - Constructor for class org.orekit.time.AbsoluteDate
Build an instance from a location in a time scale.
AbsolutePVCoordinates - Class in org.orekit.utils
Position - Velocity - Acceleration linked to a date and a frame.
AbsolutePVCoordinates(Frame, AbsoluteDate, FieldVector3D<U>) - Constructor for class org.orekit.utils.AbsolutePVCoordinates
Builds a AbsolutePVCoordinates triplet from a FieldVector3D<Derivative>.
AbsolutePVCoordinates(Frame, AbsoluteDate, Vector3D, Vector3D) - Constructor for class org.orekit.utils.AbsolutePVCoordinates
Build from position and velocity.
AbsolutePVCoordinates(Frame, AbsoluteDate, Vector3D, Vector3D, Vector3D) - Constructor for class org.orekit.utils.AbsolutePVCoordinates
Build from position, velocity, acceleration.
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, 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(AbsoluteDate, AbsolutePVCoordinates, AbsolutePVCoordinates) - Constructor for class org.orekit.utils.AbsolutePVCoordinates
Subtractive constructor
AbsolutePVCoordinatesHermiteInterpolator - Class in org.orekit.utils
Class using a Hermite interpolator to interpolate absolute position-velocity-acceleration coordinates.
AbsolutePVCoordinatesHermiteInterpolator(int, double, Frame, CartesianDerivativesFilter) - Constructor for class org.orekit.utils.AbsolutePVCoordinatesHermiteInterpolator
Constructor.
AbsolutePVCoordinatesHermiteInterpolator(int, Frame) - Constructor for class org.orekit.utils.AbsolutePVCoordinatesHermiteInterpolator
Constructor with : Default extrapolation threshold value (DEFAULT_EXTRAPOLATION_THRESHOLD_SEC s) Use of position and two time derivatives during interpolation As this implementation of interpolation is polynomial, it should be used only with small number of interpolation points (about 10-20 points) in order to avoid Runge's phenomenon and numerical problems (including NaN appearing).
AbsolutePVCoordinatesHermiteInterpolator(int, Frame, CartesianDerivativesFilter) - Constructor for class org.orekit.utils.AbsolutePVCoordinatesHermiteInterpolator
Constructor with default extrapolation threshold value (DEFAULT_EXTRAPOLATION_THRESHOLD_SEC s).
AbsolutePVCoordinatesHermiteInterpolator(Frame) - Constructor for class org.orekit.utils.AbsolutePVCoordinatesHermiteInterpolator
Constructor with : Default number of interpolation points of DEFAULT_INTERPOLATION_POINTS Default extrapolation threshold value (DEFAULT_EXTRAPOLATION_THRESHOLD_SEC s) Use of position and two time derivatives during interpolation As this implementation of interpolation is polynomial, it should be used only with small number of interpolation points (about 10-20 points) in order to avoid Runge's phenomenon and numerical problems (including NaN appearing).
ABSORPTION_COEFFICIENT - Static variable in interface org.orekit.forces.radiation.RadiationSensitive
Parameter name for absorption coefficient.
AbstractAlfriend1999 - Class in org.orekit.ssa.collision.shorttermencounter.probability.twod
Abstract class for Alfriend1999 normal and maximised methods as they share lots of similarities.
AbstractAlfriend1999(String) - Constructor for class org.orekit.ssa.collision.shorttermencounter.probability.twod.AbstractAlfriend1999
Default constructor.
AbstractAlmanac - Class in org.orekit.propagation.analytical.gnss.data
Base class for GNSS almanacs.
AbstractAlmanac(double, double, int) - Constructor for class org.orekit.propagation.analytical.gnss.data.AbstractAlmanac
Constructor.
AbstractAmbiguityModifier - Class in org.orekit.estimation.measurements.modifiers
Deprecated.
as of 12.1 ambiguity is managed directly by raw measurements Phase, OneWayGNSSPhase and InterSatellitesPhase
AbstractAmbiguityModifier(int, double) - Constructor for class org.orekit.estimation.measurements.modifiers.AbstractAmbiguityModifier
Deprecated.
Constructor.
AbstractAnalyticalGradientConverter - Class in org.orekit.propagation.analytical
Converter for analytical orbit propagator.
AbstractAnalyticalGradientConverter(AbstractAnalyticalPropagator, double, int) - Constructor for class org.orekit.propagation.analytical.AbstractAnalyticalGradientConverter
Constructor.
AbstractAnalyticalMatricesHarvester - Class in org.orekit.propagation.analytical
Base class harvester between two-dimensional Jacobian matrices and analytical orbit propagator.
AbstractAnalyticalMatricesHarvester(AbstractAnalyticalPropagator, String, RealMatrix, DoubleArrayDictionary) - Constructor for class org.orekit.propagation.analytical.AbstractAnalyticalMatricesHarvester
Simple constructor.
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.
AbstractAveragedOrbitalState - Class in org.orekit.propagation.conversion.averaging
Abstract class representing averaged orbital state.
AbstractAveragedOrbitalState(AbsoluteDate, Frame) - Constructor for class org.orekit.propagation.conversion.averaging.AbstractAveragedOrbitalState
Protected constructor.
AbstractBatchLSModel - Class in org.orekit.estimation.leastsquares
AbstractBatchLSModel(PropagatorBuilder[], List<ObservedMeasurement<?>>, ParameterDriversList, ModelObserver) - Constructor for class org.orekit.estimation.leastsquares.AbstractBatchLSModel
Constructor.
AbstractBodyAttraction - Class in org.orekit.forces.gravity
Abstract class for body attraction force model.
AbstractBodyAttraction(CelestialBody) - Constructor for class org.orekit.forces.gravity.AbstractBodyAttraction
Simple constructor.
AbstractBuilder<T extends AbstractBuilder<T>> - Class in org.orekit.files.ccsds.ndm
Abstract builder for all CCSDS Message files parsers/writers.
AbstractBuilder(IERSConventions, double, double, DataContext, AbsoluteDate, RangeUnitsConverter) - Constructor for class org.orekit.files.ccsds.ndm.AbstractBuilder
Complete constructor.
AbstractChaoMappingFunction - Class in org.orekit.models.earth.troposphere
Chao mapping function for radio wavelengths.
AbstractChaoMappingFunction(double, double, double, double) - Constructor for class org.orekit.models.earth.troposphere.AbstractChaoMappingFunction
Builds 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
Constructor with default control cost type.
AbstractConstantThrustPropulsionModel(double, double, Vector3D, Control3DVectorCostType, String) - Constructor for class org.orekit.forces.maneuvers.propulsion.AbstractConstantThrustPropulsionModel
Generic constructor.
AbstractConstituentParser<H extends Header,​T extends NdmConstituent<H,​?>,​P extends AbstractConstituentParser<H,​T,​?>> - Class in org.orekit.files.ccsds.utils.parsing
Parser for CCSDS messages.
AbstractConstituentParser(String, String, IERSConventions, boolean, DataContext, ParsedUnitsBehavior, Function<ParseToken, List<ParseToken>>[]) - Constructor for class org.orekit.files.ccsds.utils.parsing.AbstractConstituentParser
Complete 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) - Constructor for class org.orekit.propagation.events.AbstractDetector
Build a new instance.
AbstractDetector(AdaptableInterval, double, int, EventHandler) - 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 with default value for finite differences flag.
AbstractDragForceModel(Atmosphere, boolean) - Constructor for class org.orekit.forces.drag.AbstractDragForceModel
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.
AbstractEncodedMessage - Class in org.orekit.gnss.metric.parser
Encoded messages as a sequence of bytes.
AbstractEncodedMessage() - Constructor for class org.orekit.gnss.metric.parser.AbstractEncodedMessage
Empty constructor.
AbstractEncounterLOF - Class in org.orekit.frames.encounter
Abstract class for encounter frame between two objects.
AbstractEncounterLOF(FieldPVCoordinates<T>) - Constructor for class org.orekit.frames.encounter.AbstractEncounterLOF
Constructor with FieldPVCoordinates.
AbstractEncounterLOF(PVCoordinates) - Constructor for class org.orekit.frames.encounter.AbstractEncounterLOF
Constructor with PVCoordinates.
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.
AbstractEphemerisMessage - Class in org.orekit.propagation.analytical.gnss.data
Base class for ephemeris-based navigation messages.
AbstractEphemerisMessage() - Constructor for class org.orekit.propagation.analytical.gnss.data.AbstractEphemerisMessage
Constructor.
AbstractFieldIntegratorBuilder<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.conversion
Abstract class for FieldODEIntegratorBuilder.
AbstractFieldIntegratorBuilder() - Constructor for class org.orekit.propagation.conversion.AbstractFieldIntegratorBuilder
Empty 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.
AbstractFieldOrbitInterpolator<KK extends CalculusFieldElement<KK>> - Class in org.orekit.orbits
Abstract class for orbit interpolator.
AbstractFieldOrbitInterpolator(int, double, Frame) - Constructor for class org.orekit.orbits.AbstractFieldOrbitInterpolator
Constructor.
AbstractFieldTimeInterpolator<T extends FieldTimeStamped<KK>,​KK extends CalculusFieldElement<KK>> - Class in org.orekit.time
Abstract class for time interpolator.
AbstractFieldTimeInterpolator(int, double) - Constructor for class org.orekit.time.AbstractFieldTimeInterpolator
Constructor.
AbstractFieldTimeInterpolator.InterpolationData - Class in org.orekit.time
Nested class used to store interpolation data.
AbstractFixedStepFieldIntegratorBuilder<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.conversion
Abstract class for integrator builder using fixed step size.
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.
AbstractGaussianContribution.FieldFourierCjSjCoefficients<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.semianalytical.dsst.forces
Compute the Cij and the Sij coefficients with field elements.
AbstractGaussianContribution.FieldGaussianShortPeriodicCoefficients<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.semianalytical.dsst.forces
This class handles the short periodic coefficients described in Danielson 2.5.3-26.
AbstractGaussianContribution.FieldIntegrableFunction<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.semianalytical.dsst.forces
Internal class for numerical quadrature.
AbstractGaussianContribution.FieldSlot<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.semianalytical.dsst.forces
Coefficients valid for one time slot.
AbstractGaussianContribution.FieldUijVijCoefficients<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.semianalytical.dsst.forces
The Uij and Vij coefficients described by equations 2.5.3-(21) and 2.5.3-(22) from Danielson.
AbstractGaussianContribution.FourierCjSjCoefficients - Class in org.orekit.propagation.semianalytical.dsst.forces
Compute the Cij and the Sij coefficients.
AbstractGaussianContribution.GaussianShortPeriodicCoefficients - Class in org.orekit.propagation.semianalytical.dsst.forces
This class handles the short periodic coefficients described in Danielson 2.5.3-26.
AbstractGaussianContribution.GaussQuadrature - Class in org.orekit.propagation.semianalytical.dsst.forces
Class used to integrate a function of the orbital elements using the Gaussian quadrature rule to get the acceleration.
AbstractGaussianContribution.IntegrableFunction - Class in org.orekit.propagation.semianalytical.dsst.forces
Internal class for numerical quadrature.
AbstractGaussianContribution.Slot - Class in org.orekit.propagation.semianalytical.dsst.forces
Coefficients valid for one time slot.
AbstractGaussianContribution.UijVijCoefficients - Class in org.orekit.propagation.semianalytical.dsst.forces
The Uij and Vij coefficients described by equations 2.5.3-(21) and 2.5.3-(22) from Danielson.
AbstractGaussianContributionContext - Class in org.orekit.propagation.semianalytical.dsst.forces
This class is a container for the common parameters used in AbstractGaussianContribution.
AbstractGenerator - Class in org.orekit.files.ccsds.utils.generation
Base class for both Key-Value Notation and eXtended Markup Language generators for CCSDS messages.
AbstractGenerator(Appendable, String, double, boolean) - Constructor for class org.orekit.files.ccsds.utils.generation.AbstractGenerator
Simple constructor.
AbstractGlobalPressureTemperature - Class in org.orekit.models.earth.weather
Base class for Global Pressure and Temperature 2, 2w and 3 models.
AbstractGlobalPressureTemperature(DataSource, TimeScale, SeasonalModelType...) - Constructor for class org.orekit.models.earth.weather.AbstractGlobalPressureTemperature
Constructor with source of GPTn auxiliary data given by user.
AbstractGlobalPressureTemperature(Grid, TimeScale) - Constructor for class org.orekit.models.earth.weather.AbstractGlobalPressureTemperature
Deprecated.
as of 12.1 used only by GlobalPressureTemperature2Model
AbstractGradientConverter - Class in org.orekit.propagation.integration
Converter for states and parameters arrays.
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).
AbstractInterSatellitesMeasurement<T extends ObservedMeasurement<T>> - Class in org.orekit.estimation.measurements.gnss
Base class for measurement between two satellites that are both estimated.
AbstractInterSatellitesMeasurement(AbsoluteDate, double, double, double, ObservableSatellite, ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.gnss.AbstractInterSatellitesMeasurement
Constructor.
AbstractKalmanEstimator - Class in org.orekit.estimation.sequential
Base class for Kalman estimators.
AbstractKalmanEstimator(List<? extends PropagatorBuilder>) - Constructor for class org.orekit.estimation.sequential.AbstractKalmanEstimator
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
Constructor.
AbstractLightFluxModel - Class in org.orekit.forces.radiation
Abstract class for light flux models.
AbstractLightFluxModel(ExtendedPositionProvider) - Constructor for class org.orekit.forces.radiation.AbstractLightFluxModel
Constructor.
AbstractLimitedVariableStepFieldIntegratorBuilder<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.conversion
Abstract class for integrator using a limited number of variable steps.
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.
AbstractManeuverTriggers - Class in org.orekit.forces.maneuvers.trigger
Base class for triggers.
AbstractManeuverTriggers() - Constructor for class org.orekit.forces.maneuvers.trigger.AbstractManeuverTriggers
Simple constructor.
AbstractMatricesHarvester - Class in org.orekit.propagation
Base harvester between two-dimensional Jacobian matrices and one-dimensional additional state arrays.
AbstractMatricesHarvester(String, RealMatrix, DoubleArrayDictionary) - Constructor for class org.orekit.propagation.AbstractMatricesHarvester
Simple constructor.
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 multi-dimensional measurements.
AbstractMeasurement(AbsoluteDate, double, double, double, List<ObservableSatellite>) - Constructor for class org.orekit.estimation.measurements.AbstractMeasurement
Simple constructor for mono-dimensional measurements.
AbstractMeasurementBuilder<T extends ObservedMeasurement<T>> - Class in org.orekit.estimation.measurements.generation
Base class for measurements builders.
AbstractMeasurementBuilder(CorrelatedRandomVectorGenerator, double[], double[], ObservableSatellite...) - Constructor for class org.orekit.estimation.measurements.generation.AbstractMeasurementBuilder
Simple constructor.
AbstractMeasurementBuilder(CorrelatedRandomVectorGenerator, double, double, ObservableSatellite...) - Constructor for class org.orekit.estimation.measurements.generation.AbstractMeasurementBuilder
Simple constructor.
AbstractMessageParser<T> - Class in org.orekit.files.ccsds.utils.parsing
Parser for CCSDS messages.
AbstractMessageParser(String, String, Function<ParseToken, List<ParseToken>>[]) - Constructor for class org.orekit.files.ccsds.utils.parsing.AbstractMessageParser
Simple constructor.
AbstractMessageWriter<H extends Header,​S extends Segment<?,​?>,​F extends NdmConstituent<H,​S>> - Class in org.orekit.files.ccsds.utils.generation
Base class for Navigation Data Message (NDM) files.
AbstractMessageWriter(String, String, double, ContextBinding) - Constructor for class org.orekit.files.ccsds.utils.generation.AbstractMessageWriter
Constructor used to create a new NDM writer configured with the necessary parameters to successfully fill in all required fields that aren't part of a standard object.
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>, double, int, boolean, String) - Constructor for class org.orekit.utils.AbstractMultipleShooting
Simple Constructor.
AbstractNavigationMessage - Class in org.orekit.propagation.analytical.gnss.data
Base class for GNSS navigation messages.
AbstractNavigationMessage(double, double, int) - Constructor for class org.orekit.propagation.analytical.gnss.data.AbstractNavigationMessage
Constructor.
AbstractOnBoardMeasurement<T extends ObservedMeasurement<T>> - Class in org.orekit.estimation.measurements.gnss
Base class modeling a measurement where receiver is a satellite.
AbstractOnBoardMeasurement(AbsoluteDate, double, double, double, List<ObservableSatellite>) - Constructor for class org.orekit.estimation.measurements.gnss.AbstractOnBoardMeasurement
Constructor.
AbstractOneWayGNSSMeasurement<T extends ObservedMeasurement<T>> - Class in org.orekit.estimation.measurements.gnss
Base class for one-way GNSS measurement.
AbstractOneWayGNSSMeasurement(PVCoordinatesProvider, QuadraticClockModel, AbsoluteDate, double, double, double, ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.gnss.AbstractOneWayGNSSMeasurement
Simple constructor.
AbstractOrbitInterpolator - Class in org.orekit.orbits
Abstract class for orbit interpolator.
AbstractOrbitInterpolator(int, double, Frame) - Constructor for class org.orekit.orbits.AbstractOrbitInterpolator
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, PositionAngleType, double, boolean) - Constructor for class org.orekit.propagation.conversion.AbstractPropagatorBuilder
Build a new instance.
AbstractPropagatorBuilder(Orbit, PositionAngleType, 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, OneAxisEllipsoid) - Constructor for class org.orekit.forces.radiation.AbstractRadiationForceModel
Default constructor.
AbstractRelativisticClockModifier - Class in org.orekit.estimation.measurements.modifiers
Class modifying theoretical measurements with relativistic clock correction.
AbstractRelativisticClockModifier() - Constructor for class org.orekit.estimation.measurements.modifiers.AbstractRelativisticClockModifier
Simple constructor.
AbstractRelativisticClockOnBoardRangeRateModifier<T extends ObservedMeasurement<T>> - Class in org.orekit.estimation.measurements.modifiers
Class modifying theoretical range-rate measurement with relativistic frequency deviation.
AbstractRelativisticClockOnBoardRangeRateModifier(double) - Constructor for class org.orekit.estimation.measurements.modifiers.AbstractRelativisticClockOnBoardRangeRateModifier
Simple constructor.
AbstractRelativisticJ2ClockModifier - Class in org.orekit.estimation.measurements.modifiers
Class modifying theoretical measurements with relativistic J2 clock correction.
AbstractRelativisticJ2ClockModifier(double, double, double) - Constructor for class org.orekit.estimation.measurements.modifiers.AbstractRelativisticJ2ClockModifier
Constructor for the Relativistic J2 Clock modifier.
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.
AbstractShortTermEncounter1DNumerical2DPOCMethod - Class in org.orekit.ssa.collision.shorttermencounter.probability.twod
This abstract class serves as a foundation to create 1D numerical 2D probability of collision computing method.
AbstractShortTermEncounter1DNumerical2DPOCMethod(String, UnivariateIntegrator, int) - Constructor for class org.orekit.ssa.collision.shorttermencounter.probability.twod.AbstractShortTermEncounter1DNumerical2DPOCMethod
Customizable constructor.
AbstractShortTermEncounter2DPOCMethod - Class in org.orekit.ssa.collision.shorttermencounter.probability.twod
This abstract class serves as a foundation to create 2D probability of collision computing method assuming a short term encounter model.
AbstractShortTermEncounter2DPOCMethod(String) - Constructor for class org.orekit.ssa.collision.shorttermencounter.probability.twod.AbstractShortTermEncounter2DPOCMethod
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.
AbstractSolarActivityData<L extends AbstractSolarActivityDataLoader.LineParameters,​D extends AbstractSolarActivityDataLoader<L>> - Class in org.orekit.models.earth.atmosphere.data
Abstract class for solar activity data.
AbstractSolarActivityData(String, D, DataProvidersManager, TimeScale, int, double, double, double) - Constructor for class org.orekit.models.earth.atmosphere.data.AbstractSolarActivityData
 
AbstractSolarActivityData(DataSource, D, TimeScale, int, double, double, double) - Constructor for class org.orekit.models.earth.atmosphere.data.AbstractSolarActivityData
Simple constructor.
AbstractSolarActivityData.LocalSolarActivity - Class in org.orekit.models.earth.atmosphere.data
Container for weather parameters around current date.
AbstractSolarActivityData.SolarActivityGenerator - Class in org.orekit.models.earth.atmosphere.data
Generator used in the weather data cache.
AbstractSolarActivityDataLoader<L extends AbstractSolarActivityDataLoader.LineParameters> - Class in org.orekit.models.earth.atmosphere.data
Abstract class for solar activity data loader.
AbstractSolarActivityDataLoader(TimeScale) - Constructor for class org.orekit.models.earth.atmosphere.data.AbstractSolarActivityDataLoader
Constructor.
AbstractSolarActivityDataLoader.LineParameters - Class in org.orekit.models.earth.atmosphere.data
Container class for Solar activity indexes.
AbstractStateCovarianceInterpolator - Class in org.orekit.propagation
Abstract class for orbit and state covariance interpolator.
AbstractStateCovarianceInterpolator(int, double, TimeInterpolator<Orbit>, Frame, OrbitType, PositionAngleType) - Constructor for class org.orekit.propagation.AbstractStateCovarianceInterpolator
Constructor.
AbstractStateCovarianceInterpolator(int, double, TimeInterpolator<Orbit>, LOFType) - Constructor for class org.orekit.propagation.AbstractStateCovarianceInterpolator
Constructor.
AbstractStateModifier - Class in org.orekit.propagation
Abstract base class for modifying state during propagation.
AbstractStateModifier() - Constructor for class org.orekit.propagation.AbstractStateModifier
 
AbstractTimeInterpolator<T extends TimeStamped> - Class in org.orekit.time
Abstract class for time interpolator.
AbstractTimeInterpolator(int, double) - Constructor for class org.orekit.time.AbstractTimeInterpolator
Constructor.
AbstractTimeInterpolator.InterpolationData - Class in org.orekit.time
Nested class used to store interpolation data.
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.
AbstractVariableStepFieldIntegratorBuilder<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.conversion
Abstract class for integrator builder using variable step size.
AbstractVienna - Class in org.orekit.models.earth.troposphere
The Vienna tropospheric delay model for radio techniques.
AbstractVienna(ViennaAProvider, AzimuthalGradientProvider, TroposphericModel, TimeScale) - Constructor for class org.orekit.models.earth.troposphere.AbstractVienna
Build a new instance.
AbstractWindUp<T extends ObservedMeasurement<T>> - Class in org.orekit.estimation.measurements.gnss
Base class for wind-up effect computation.
AbstractWindUp(Dipole, Dipole) - Constructor for class org.orekit.estimation.measurements.gnss.AbstractWindUp
Simple constructor.
AbstractWriter - Class in org.orekit.files.ccsds.section
Top level class for writing CCSDS message sections.
AbstractWriter(String, String) - Constructor for class org.orekit.files.ccsds.section.AbstractWriter
Simple constructor.
ACC - org.orekit.files.ccsds.definitions.SpacecraftBodyFrame.BaseEquipment
Accelerometer.
ACC_DIR_SIGMA - org.orekit.files.ccsds.ndm.odm.ocm.ManeuverFieldType
One σ off-nominal acceleration direction.
ACC_INTERP - org.orekit.files.ccsds.ndm.odm.ocm.ManeuverFieldType
Interpolation mode between current and next acceleration line.
ACC_MAG_SIGMA - org.orekit.files.ccsds.ndm.odm.ocm.ManeuverFieldType
One σ percent error on acceleration magnitude.
ACC_X - org.orekit.files.ccsds.ndm.odm.ocm.ManeuverFieldType
Acceleration along X axis.
ACC_Y - org.orekit.files.ccsds.ndm.odm.ocm.ManeuverFieldType
Acceleration along Y axis.
ACC_Z - org.orekit.files.ccsds.ndm.odm.ocm.ManeuverFieldType
Acceleration along Z axis.
acceleration(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.drag.DragForce
Compute acceleration.
acceleration(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.drag.TimeSpanDragForce
Deprecated.
Compute acceleration.
acceleration(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.empirical.ParametricAcceleration
Compute acceleration.
acceleration(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.empirical.TimeSpanParametricAcceleration
Compute acceleration.
acceleration(FieldSpacecraftState<T>, T[]) - Method in interface org.orekit.forces.ForceModel
Compute acceleration.
acceleration(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.gravity.DeSitterRelativity
Compute acceleration.
acceleration(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.gravity.HolmesFeatherstoneAttractionModel
Compute acceleration.
acceleration(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.gravity.J2OnlyPerturbation
Compute acceleration.
acceleration(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.gravity.LenseThirringRelativity
Compute acceleration.
acceleration(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.gravity.NewtonianAttraction
Compute acceleration.
acceleration(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.gravity.OceanTides
Compute acceleration.
acceleration(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.gravity.Relativity
Compute acceleration.
acceleration(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.gravity.SingleBodyAbsoluteAttraction
Compute acceleration.
acceleration(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.gravity.SingleBodyRelativeAttraction
Compute acceleration.
acceleration(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.gravity.SolidTides
Compute acceleration.
acceleration(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.gravity.ThirdBodyAttraction
Compute acceleration.
acceleration(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.inertia.InertialForces
Compute acceleration.
acceleration(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.maneuvers.Maneuver
 
acceleration(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.radiation.ECOM2
Compute acceleration.
acceleration(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.radiation.KnockeRediffusedForceModel
Compute acceleration.
acceleration(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.radiation.RadiationPressureModel
Compute acceleration.
acceleration(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.forces.radiation.SolarRadiationPressure
Compute acceleration.
acceleration(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.propagation.numerical.cr3bp.CR3BPForceModel
Compute acceleration.
acceleration(SpacecraftState, double[]) - Method in class org.orekit.forces.drag.DragForce
Compute acceleration.
acceleration(SpacecraftState, double[]) - Method in class org.orekit.forces.drag.TimeSpanDragForce
Deprecated.
Compute acceleration.
acceleration(SpacecraftState, double[]) - Method in class org.orekit.forces.empirical.ParametricAcceleration
Compute acceleration.
acceleration(SpacecraftState, double[]) - Method in class org.orekit.forces.empirical.TimeSpanParametricAcceleration
Compute acceleration.
acceleration(SpacecraftState, double[]) - Method in interface org.orekit.forces.ForceModel
Compute acceleration.
acceleration(SpacecraftState, double[]) - Method in class org.orekit.forces.gravity.DeSitterRelativity
Compute acceleration.
acceleration(SpacecraftState, double[]) - Method in class org.orekit.forces.gravity.HolmesFeatherstoneAttractionModel
Compute acceleration.
acceleration(SpacecraftState, double[]) - Method in class org.orekit.forces.gravity.J2OnlyPerturbation
Compute acceleration.
acceleration(SpacecraftState, double[]) - Method in class org.orekit.forces.gravity.LenseThirringRelativity
Compute acceleration.
acceleration(SpacecraftState, double[]) - Method in class org.orekit.forces.gravity.NewtonianAttraction
Compute acceleration.
acceleration(SpacecraftState, double[]) - Method in class org.orekit.forces.gravity.OceanTides
Compute acceleration.
acceleration(SpacecraftState, double[]) - Method in class org.orekit.forces.gravity.Relativity
Compute acceleration.
acceleration(SpacecraftState, double[]) - Method in class org.orekit.forces.gravity.SingleBodyAbsoluteAttraction
Compute acceleration.
acceleration(SpacecraftState, double[]) - Method in class org.orekit.forces.gravity.SingleBodyRelativeAttraction
Compute acceleration.
acceleration(SpacecraftState, double[]) - Method in class org.orekit.forces.gravity.SolidTides
Compute acceleration.
acceleration(SpacecraftState, double[]) - Method in class org.orekit.forces.gravity.ThirdBodyAttraction
Compute acceleration.
acceleration(SpacecraftState, double[]) - Method in class org.orekit.forces.inertia.InertialForces
Compute acceleration.
acceleration(SpacecraftState, double[]) - Method in class org.orekit.forces.maneuvers.Maneuver
 
acceleration(SpacecraftState, double[]) - Method in class org.orekit.forces.radiation.ECOM2
Compute acceleration.
acceleration(SpacecraftState, double[]) - Method in class org.orekit.forces.radiation.KnockeRediffusedForceModel
Compute acceleration.
acceleration(SpacecraftState, double[]) - Method in class org.orekit.forces.radiation.RadiationPressureModel
Compute acceleration.
acceleration(SpacecraftState, double[]) - 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_SUFFIX - Static variable in class org.orekit.estimation.measurements.GroundStation
Suffix for ground clock drift parameters name.
AccelerationModel - Interface in org.orekit.forces.empirical
Acceleration model used by empirical force.
accept(boolean) - Method in interface org.orekit.files.ccsds.utils.lexical.ParseToken.BooleanConsumer
Consume a boolean.
accept(char) - Method in interface org.orekit.files.ccsds.utils.lexical.ParseToken.CharConsumer
Consume a character.
accept(char, double) - Method in interface org.orekit.files.ccsds.utils.lexical.ParseToken.LabeledDoubleConsumer
Consume an indexed double.
accept(double) - Method in interface org.orekit.files.ccsds.utils.lexical.ParseToken.DoubleConsumer
Consume a double.
accept(double[]) - Method in interface org.orekit.files.ccsds.utils.lexical.ParseToken.DoubleArrayConsumer
Consume an array of doubles.
accept(int) - Method in interface org.orekit.files.ccsds.utils.lexical.ParseToken.IntConsumer
Consume an integer.
accept(int[]) - Method in interface org.orekit.files.ccsds.utils.lexical.ParseToken.IntegerArrayConsumer
Consume an array of integers.
accept(int, double) - Method in interface org.orekit.files.ccsds.utils.lexical.ParseToken.IndexedDoubleConsumer
Consume an indexed double.
accept(int, double[]) - Method in interface org.orekit.files.ccsds.utils.lexical.ParseToken.IndexedDoubleArrayConsumer
Consume an indexed double array.
accept(int, int) - Method in interface org.orekit.files.ccsds.utils.lexical.ParseToken.IndexedIntConsumer
Consume an integer.
accept(int, int, double) - Method in interface org.orekit.files.ccsds.utils.lexical.ParseToken.DoublyIndexedDoubleConsumer
Consume a doubly indexed double.
accept(int, String) - Method in interface org.orekit.files.ccsds.utils.lexical.ParseToken.IndexedStringConsumer
Consume an indexed string.
accept(String) - Method in interface org.orekit.files.ccsds.utils.lexical.ParseToken.StringConsumer
Consume a string.
accept(List<String>) - Method in interface org.orekit.files.ccsds.utils.lexical.ParseToken.StringListConsumer
Consume a list of strings.
accept(List<BodyFacade>) - Method in interface org.orekit.files.ccsds.utils.lexical.ParseToken.CenterListConsumer
Consume a body center.
accept(List<Unit>) - Method in interface org.orekit.files.ccsds.utils.lexical.ParseToken.UnitListConsumer
Consume a list of units.
accept(List<T>) - Method in interface org.orekit.files.ccsds.utils.lexical.ParseToken.EnumListConsumer
Consume an enum.
accept(RotationOrder) - Method in interface org.orekit.files.ccsds.utils.lexical.ParseToken.RotationOrderConsumer
Consume a data.
accept(Vector3D) - Method in interface org.orekit.files.ccsds.utils.lexical.ParseToken.VectorConsumer
Consume a vector.
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.
accept(BodyFacade) - Method in interface org.orekit.files.ccsds.utils.lexical.ParseToken.CenterConsumer
Consume a body center.
accept(FrameFacade) - Method in interface org.orekit.files.ccsds.utils.lexical.ParseToken.FrameConsumer
Consume a frame.
accept(TimeSystem) - Method in interface org.orekit.files.ccsds.utils.lexical.ParseToken.TimeSystemConsumer
Consume a time system.
accept(Maneuvrable) - Method in interface org.orekit.files.ccsds.utils.lexical.ParseToken.ManeuvrableConsumer
Consume a Maneuvrable.
accept(MessageParser<T>) - Method in class org.orekit.files.ccsds.utils.lexical.KvnLexicalAnalyzer
Parse a CCSDS Message.
accept(MessageParser<T>) - Method in interface org.orekit.files.ccsds.utils.lexical.LexicalAnalyzer
Parse a CCSDS Message.
accept(MessageParser<T>) - Method in class org.orekit.files.ccsds.utils.lexical.XmlLexicalAnalyzer
Parse a CCSDS Message.
accept(AbsoluteDate) - Method in interface org.orekit.files.ccsds.utils.lexical.ParseToken.DateConsumer
Consume a date.
accept(T) - Method in interface org.orekit.files.ccsds.utils.lexical.ParseToken.EnumConsumer
Consume an enum.
acceptComments() - Method in class org.orekit.files.ccsds.section.CommentsContainer
Check if container is still accepting comments.
acceptStep(FieldAbstractAnalyticalPropagator.FieldBasicStepInterpolator, FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.analytical.FieldAbstractAnalyticalPropagator
Accept a step, triggering events and step handlers.
acceptStep(OrekitStepInterpolator, AbsoluteDate) - Method in class org.orekit.propagation.analytical.AbstractAnalyticalPropagator
Accept a step, triggering events and step handlers.
AccuracyProvider - Interface in org.orekit.gnss.metric.messages.common
This interface represents an accuracy providerused to validate RTCM ephemeris messages.
AccurateFormatter - Class in org.orekit.utils
Formatter used to produce strings from data with high accuracy.
Acm - Class in org.orekit.files.ccsds.ndm.adm.acm
This class gathers the informations present in the Attitude Comprehensive Message (ACM).
Acm(AdmHeader, List<Segment<AcmMetadata, AcmData>>, IERSConventions, DataContext) - Constructor for class org.orekit.files.ccsds.ndm.adm.acm.Acm
Simple constructor.
ACM_DATA_ELEMENTS - org.orekit.files.ccsds.ndm.adm.acm.AcmMetadataKey
List of elements of information data blocks included in this message.
AcmData - Class in org.orekit.files.ccsds.ndm.adm.acm
Data container for Attitude Comprehensive Messages.
AcmData(List<AttitudeStateHistory>, AttitudePhysicalProperties, List<AttitudeCovarianceHistory>, List<AttitudeManeuver>, AttitudeDetermination, UserDefined) - Constructor for class org.orekit.files.ccsds.ndm.adm.acm.AcmData
Simple constructor.
AcmDataSubStructureKey - Enum in org.orekit.files.ccsds.ndm.adm.acm
Keywords for ACM data sub-structure.
AcmElements - Enum in org.orekit.files.ccsds.ndm.adm.acm
Data elements types used in CCSDS Attitude Comprehensive Messages.
AcmMetadata - Class in org.orekit.files.ccsds.ndm.adm.acm
AcmMetadata(DataContext) - Constructor for class org.orekit.files.ccsds.ndm.adm.acm.AcmMetadata
Create a new meta-data.
AcmMetadataKey - Enum in org.orekit.files.ccsds.ndm.adm.acm
Keys for ACM container entries.
AcmParser - Class in org.orekit.files.ccsds.ndm.adm.acm
A parser for the CCSDS ACM (Attitude Comprehensive Message).
AcmParser(IERSConventions, boolean, DataContext, ParsedUnitsBehavior, Function<ParseToken, List<ParseToken>>[]) - Constructor for class org.orekit.files.ccsds.ndm.adm.acm.AcmParser
Complete constructor.
AcmSatelliteEphemeris - Class in org.orekit.files.ccsds.ndm.adm.acm
ACM ephemeris blocks for a single satellite.
AcmSatelliteEphemeris(String, List<AttitudeStateHistory>) - Constructor for class org.orekit.files.ccsds.ndm.adm.acm.AcmSatelliteEphemeris
Create a container for the set of ephemeris blocks in the file that pertain to a single satellite.
AcmWriter - Class in org.orekit.files.ccsds.ndm.adm.acm
Writer for CCSDS Attitude Comprehensive Message.
AcmWriter(IERSConventions, DataContext) - Constructor for class org.orekit.files.ccsds.ndm.adm.acm.AcmWriter
Complete constructor.
ACTUAL_OD_SPAN - org.orekit.files.ccsds.ndm.cdm.ODParametersKey
Based on the observations available and the RECOMMENDED_OD_SPAN, the actual time span used for the OD of the object.
ACTUAL_OD_SPAN - org.orekit.files.ccsds.ndm.odm.ocm.OrbitDeterminationKey
Actual time span used for the OD of the object.
ACTUATOR - org.orekit.files.ccsds.definitions.SpacecraftBodyFrame.BaseEquipment
Actuator: could denote reaction wheels, solar arrays, thrusters, etc..
ACTUATOR_USED - org.orekit.files.ccsds.ndm.adm.acm.AttitudeManeuverKey
Actuator used.
ad - org.orekit.files.ccsds.ndm.adm.acm.AcmDataSubStructureKey
Orbit determination section.
AD - org.orekit.files.ccsds.ndm.adm.acm.AcmDataSubStructureKey
Attitude determination section.
AD - org.orekit.files.ccsds.ndm.adm.acm.AcmElements
Attitude determination.
AD_ID - org.orekit.files.ccsds.ndm.adm.acm.AttitudeDeterminationKey
Identification number.
AD_METHOD - org.orekit.files.ccsds.ndm.adm.acm.AttitudeDeterminationKey
Attitude determination method.
AD_PREV_ID - org.orekit.files.ccsds.ndm.adm.acm.AttitudeDeterminationKey
Identification of previous attitude determination.
AdamsBashforthFieldIntegratorBuilder<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.conversion
Builder for AdamsBashforthFieldIntegrator.
AdamsBashforthFieldIntegratorBuilder(int, double, double, double) - Constructor for class org.orekit.propagation.conversion.AdamsBashforthFieldIntegratorBuilder
Build a new instance.
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.
AdamsMoultonFieldIntegratorBuilder<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.conversion
Builder for AdamsMoultonFieldIntegrator.
AdamsMoultonFieldIntegratorBuilder(int, double, double, double) - Constructor for class org.orekit.propagation.conversion.AdamsMoultonFieldIntegratorBuilder
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.
AdaptableInterval - Interface in org.orekit.propagation.events
This interface represents an event checking interval that depends on state.
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.
ADBARV - org.orekit.files.ccsds.ndm.odm.ocm.OrbitElementsType
Spherical 6-element set (α,δ,β,A,r,v).
add(double, OrekitFixedStepHandler) - Method in class org.orekit.propagation.sampling.StepHandlerMultiplexer
Add a handler for fixed size step.
add(FieldOrekitStepHandler<T>) - Method in class org.orekit.propagation.sampling.FieldStepHandlerMultiplexer
Add a handler for variable size step.
add(OrekitStepHandler) - Method in class org.orekit.propagation.sampling.StepHandlerMultiplexer
Add a handler for variable size step.
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.
add(T, FieldOrekitFixedStepHandler<T>) - Method in class org.orekit.propagation.sampling.FieldStepHandlerMultiplexer
Add a handler for fixed size step.
addAccelerationModelValidAfter(AccelerationModel, AbsoluteDate) - Method in class org.orekit.forces.empirical.TimeSpanParametricAcceleration
Add a AccelerationModel entry valid after a limit date.
addAccelerationModelValidBefore(AccelerationModel, AbsoluteDate) - Method in class org.orekit.forces.empirical.TimeSpanParametricAcceleration
Add an AccelerationModel entry valid before a limit date.
addAdditionalDerivativesProvider(AdditionalDerivativesProvider) - 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).
addAdditionalDerivativesProvider(AdditionalDerivativesProvider) - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
Add a provider for user-specified state derivatives to be integrated along with the orbit propagation.
addAdditionalDerivativesProvider(FieldAdditionalDerivativesProvider<T>) - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator
Add a provider for user-specified state derivatives to be integrated along with the orbit propagation.
addAdditionalState(String, double...) - Method in class org.orekit.propagation.SpacecraftState
Add an additional state.
addAdditionalState(String, T...) - Method in class org.orekit.propagation.FieldSpacecraftState
Add an additional state.
addAdditionalStateDerivative(String, double...) - Method in class org.orekit.propagation.SpacecraftState
Add an additional state derivative.
addAdditionalStateDerivative(String, T...) - Method in class org.orekit.propagation.FieldSpacecraftState
Add an additional state derivative.
addAdditionalStateProvider(AdditionalStateProvider) - Method in class org.orekit.propagation.AbstractPropagator
Add a set of user-specified state parameters to be computed along with the orbit propagation.
addAdditionalStateProvider(AdditionalStateProvider) - Method in interface org.orekit.propagation.Propagator
Add a set of user-specified state parameters to be computed along with the orbit propagation.
addAdditionalStateProvider(FieldAdditionalStateProvider<T>) - Method in class org.orekit.propagation.FieldAbstractPropagator
Add a set of user-specified state parameters to be computed along with the orbit propagation.
addAdditionalStateProvider(FieldAdditionalStateProvider<T>) - Method in interface org.orekit.propagation.FieldPropagator
Add a set of user-specified state parameters to be computed along with the orbit propagation.
addAnglesData(CRD.AnglesMeasurement) - Method in class org.orekit.files.ilrs.CRD.CRDDataBlock
Add an entry to the list of angles data.
addAntennaTypeValidAfter(String, AbsoluteDate) - Method in class org.orekit.files.sinex.Station
Add a antenna type entry valid after a limit date.
Using addAntennaTypeValidAfter(entry, t) will make entry valid in [t, +∞[ (note the closed bracket).
addAntennaTypeValidBefore(String, AbsoluteDate) - Method in class org.orekit.files.sinex.Station
Add a antenna type entry valid before a limit date.
Using addAntennaTypeValidBefore(entry, t) will make entry valid in ]-∞, t[ (note the open bracket).
addAppliedDCBS(AppliedDCBS) - Method in class org.orekit.files.rinex.clock.RinexClock
Add an applied differencial code bias corrections.
addAppliedDCBS(AppliedDCBS) - Method in class org.orekit.files.rinex.observation.RinexObservationHeader
Add applied differential code bias corrections.
addAppliedPCVS(AppliedPCVS) - Method in class org.orekit.files.rinex.clock.RinexClock
Add an applied phase center variations.
addAppliedPCVS(AppliedPCVS) - Method in class org.orekit.files.rinex.observation.RinexObservationHeader
Add antenna center variation corrections.
addBDGIMMessage(IonosphereBDGIMMessage) - Method in class org.orekit.files.rinex.navigation.RinexNavigation
Add an ionosphere BDGIM message.
addBeidouCivilianNavigationMessage(BeidouCivilianNavigationMessage) - Method in class org.orekit.files.rinex.navigation.RinexNavigation
Add a Beidou navigation message to the list.
addBeidouLegacyNavigationMessage(BeidouLegacyNavigationMessage) - Method in class org.orekit.files.rinex.navigation.RinexNavigation
Add a Beidou navigation message to the list.
addCalibrationData(CRD.Calibration) - Method in class org.orekit.files.ilrs.CRD.CRDDataBlock
Add an entry to the list of calibration data.
addCalibrationDetailData(CRD.CalibrationDetail) - Method in class org.orekit.files.ilrs.CRD.CRDDataBlock
Add an entry to the list of calibration detail data.
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.
addClockData(String, RinexClock.ClockDataLine) - Method in class org.orekit.files.rinex.clock.RinexClock
Add a clock data line to a specified receiver/satellite.
addClockDataType(RinexClock.ClockDataType) - Method in class org.orekit.files.rinex.clock.RinexClock
Add a clock data types.
addCodeBias(CodeBias) - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm05Data
Add a code bias value for the current satellite.
addComment(String) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata
Set comment for relative metadata.
addComment(String) - Method in class org.orekit.files.ccsds.ndm.NdmParser
Add comment.
addComment(String) - Method in class org.orekit.files.ccsds.section.CommentsContainer
Add comment.
addComment(String) - Method in class org.orekit.files.rinex.clock.RinexClock
Add a comment line.
addComment(String) - Method in class org.orekit.files.sp3.SP3Header
Add a comment.
addComment(RinexComment) - Method in class org.orekit.files.rinex.RinexFile
Add a comment.
addConfigurationRecord(CRDConfiguration.BaseConfiguration) - Method in class org.orekit.files.ilrs.CRDConfiguration
Add a configuration record, such as SystemConfiguation, LaserConfiguration, DetectorConfiguration, etc.
addConstraint(int, int, double) - Method in class org.orekit.utils.AbstractMultipleShooting
Add a constraint on one component of one patch point.
addContribution(BodiesElements, double[][], double[][]) - Method in class org.orekit.forces.gravity.potential.OceanTidesWave
Add the contribution of the wave to Stokes coefficients.
addContribution(FieldSpacecraftState<T>, FieldTimeDerivativesEquations<T>) - Method in interface org.orekit.forces.ForceModel
Compute the contribution of the force model to the perturbing acceleration.
addContribution(FieldSpacecraftState<T>, FieldTimeDerivativesEquations<T>) - Method in class org.orekit.forces.gravity.NewtonianAttraction
Compute the contribution of the force model to the perturbing acceleration.
addContribution(FieldSpacecraftState<T>, FieldTimeDerivativesEquations<T>) - Method in class org.orekit.forces.maneuvers.Maneuver
Compute the contribution of the force model to the perturbing acceleration.
addContribution(SpacecraftState, TimeDerivativesEquations) - Method in interface org.orekit.forces.ForceModel
Compute the contribution of the force model to the perturbing acceleration.
addContribution(SpacecraftState, TimeDerivativesEquations) - Method in class org.orekit.forces.gravity.NewtonianAttraction
Compute the contribution of the force model to the perturbing acceleration.
addContribution(SpacecraftState, TimeDerivativesEquations) - Method in class org.orekit.forces.maneuvers.Maneuver
Compute the contribution of the force model to the perturbing acceleration.
addCoordinate(SP3Coordinate) - Method in class org.orekit.files.sp3.SP3Segment
Adds a new P/V coordinate.
addCoordinate(SP3Coordinate, double) - Method in class org.orekit.files.sp3.SP3Ephemeris
Adds a new P/V coordinate.
addCovarianceMatrix(CartesianCovariance) - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemData
Add a covariance matrix.
addData(TimeStampedAngularCoordinates) - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemData
Add a data point.
addData(TimeStampedPVCoordinates, boolean) - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemData
Add a data point.
addDataBlock(CRD.CRDDataBlock) - Method in class org.orekit.files.ilrs.CRD
Add a data block to the current list of data blocks.
addDcb(SatelliteSystem, Dcb) - Method in class org.orekit.files.sinex.DcbStation
Add the DCB data corresponding to a satellite system.
addDcbLine(String, String, AbsoluteDate, AbsoluteDate, double) - Method in class org.orekit.files.sinex.Dcb
Add the content of a DCB line to the DCBSatellite object.
addDefaultCelestialBodyLoader(String) - Static method in class org.orekit.bodies.CelestialBodyFactory
Add the default loaders for all predefined celestial bodies.
addDefaultCelestialBodyLoader(String) - Method in class org.orekit.bodies.LazyLoadedCelestialBodies
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, String) - Method in class org.orekit.bodies.LazyLoadedCelestialBodies
Add the default loaders for celestial bodies.
addDefaultEOP1980HistoryLoaders(String, 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, String) - Method in class org.orekit.frames.LazyLoadedFrames
Add the default loaders EOP history (IAU 1980 precession/nutation).
addDefaultEOP1980HistoryLoaders(String, String, String, String, String, String, Supplier<TimeScale>) - Method in class org.orekit.frames.LazyLoadedEop
Add the default loaders EOP history (IAU 1980 precession/nutation).
addDefaultEOP2000HistoryLoaders(String, 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, String) - Method in class org.orekit.frames.LazyLoadedFrames
Add the default loaders for EOP history (IAU 2000/2006 precession/nutation).
addDefaultEOP2000HistoryLoaders(String, 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).
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
Deprecated.
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
Deprecated.
Add a DragSensitive entry valid before a limit date.
Using addDragSensitiveValidBefore(entry, t) will make entry valid in ]-∞, t[ (note the open bracket).
addEarthOrientationParameter(EarthOrientationParameterMessage) - Method in class org.orekit.files.rinex.navigation.RinexNavigation
Add an Earth orientation parameter.
addEffect(AdapterPropagator.DifferentialEffect) - Method in class org.orekit.propagation.analytical.AdapterPropagator
Add a differential effect.
addEntry(String, String) - Method in class org.orekit.files.ccsds.ndm.odm.UserDefined
Add a key/value entry.
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.
addEphemerisName(int, String) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Adds an ephemeris name to the list.
addEventDate(AbsoluteDate) - Method in class org.orekit.propagation.events.DateDetector
Add an event date.
addEventDate(FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.events.FieldDateDetector
Add an event date.
addEventDetector(D) - Method in class org.orekit.propagation.analytical.FieldAbstractAnalyticalPropagator
Add an event detector.
addEventDetector(D) - Method in interface org.orekit.propagation.FieldPropagator
Add an event detector.
addEventDetector(D) - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator
Add an event detector.
addEventDetector(EventDetector) - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
Add an event detector.
addEventDetector(T) - Method in class org.orekit.propagation.analytical.AbstractAnalyticalPropagator
Add an event detector.
addEventDetector(T) - Method in interface org.orekit.propagation.Propagator
Add an event detector.
addFilter(DataFilter) - Method in class org.orekit.data.FiltersManager
Add a data filter.
addForceModel(ForceModel) - Method in class org.orekit.propagation.conversion.NumericalPropagatorBuilder
Add a force model to the global perturbation model.
addForceModel(ForceModel) - Method in class org.orekit.propagation.numerical.FieldNumericalPropagator
Add a force model to the global perturbation model.
addForceModel(ForceModel) - Method in class org.orekit.propagation.numerical.NumericalPropagator
Add a force model.
addForceModel(DSSTForceModel) - Method in class org.orekit.propagation.conversion.DSSTPropagatorBuilder
Add a force model to the global perturbation model.
addForceModel(DSSTForceModel) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator
Add a force model to the global perturbation model.
addForceModel(DSSTForceModel) - Method in class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator
Add a force model to the global perturbation model.
addGalileoNavigationMessage(GalileoNavigationMessage) - Method in class org.orekit.files.rinex.navigation.RinexNavigation
Add a Galileo navigation message to the list.
addGlonassChannel(GlonassSatelliteChannel) - Method in class org.orekit.files.rinex.observation.RinexObservationHeader
Add GLONASS satellite/channel association.
addGlonassNavigationMessage(GLONASSNavigationMessage) - Method in class org.orekit.files.rinex.navigation.RinexNavigation
Add a Glonass navigation message to the list.
addGPSLegacyNavigationMessage(GPSCivilianNavigationMessage) - Method in class org.orekit.files.rinex.navigation.RinexNavigation
Add a GPS civilian navigation message to the list.
addGPSLegacyNavigationMessage(GPSLegacyNavigationMessage) - Method in class org.orekit.files.rinex.navigation.RinexNavigation
Add a GPS legacy navigation message to the list.
addGridPoint(AbsoluteDate, double[]) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.ShortPeriodicsInterpolatedCoefficient
Add a point to the interpolation grid.
addGridPoint(FieldAbsoluteDate<T>, T[]) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.FieldShortPeriodicsInterpolatedCoefficient
Add a point to the interpolation grid.
addHandler(EventHandler) - Method in class org.orekit.propagation.events.handlers.EventMultipleHandler
Add one handler to the managed handlers list.
addHandlers(EventHandler...) - Method in class org.orekit.propagation.events.handlers.EventMultipleHandler
Add several handlers to the managed handlers list.
addInput(T) - Method in class org.orekit.data.AbstractListCrawler
Add an input to the supported list.
addIRNSSNavigationMessage(IRNSSNavigationMessage) - Method in class org.orekit.files.rinex.navigation.RinexNavigation
Add a IRNSS navigation message to the list.
ADDITIONAL_STATE_NAME_ALREADY_IN_USE - org.orekit.errors.OrekitMessages
ADDITIONAL_STATE_NAME_ALREADY_IN_USE.
AdditionalCovarianceMetadata - Class in org.orekit.files.ccsds.ndm.cdm
Container for the additional covariance metadata (optional).
AdditionalCovarianceMetadata() - Constructor for class org.orekit.files.ccsds.ndm.cdm.AdditionalCovarianceMetadata
Simple constructor.
AdditionalCovarianceMetadataKey - Enum in org.orekit.files.ccsds.ndm.cdm
Keys for covariance metadatail y a entries.
AdditionalDerivativesProvider - Interface in org.orekit.propagation.integration
Provider for additional derivatives.
additionalParameters - org.orekit.files.ccsds.ndm.cdm.XmlSubStructureKey
Additional Parameter section.
AdditionalParameters - Class in org.orekit.files.ccsds.ndm.cdm
Container for additional parameters data block.
AdditionalParameters() - Constructor for class org.orekit.files.ccsds.ndm.cdm.AdditionalParameters
Simple constructor.
AdditionalParametersKey - Enum in org.orekit.files.ccsds.ndm.cdm
Keys for CDM additional parameters entries.
AdditionalParametersWriter - Class in org.orekit.files.ccsds.ndm.cdm
Writer for additional parameters data block for CCSDS Conjunction Data Messages.
AdditionalStateProvider - Interface in org.orekit.propagation
This interface allows to modify SpacecraftState and set up additional state data.
addKeplerContribution(double) - Method in interface org.orekit.propagation.numerical.TimeDerivativesEquations
Add the contribution of the Kepler evolution.
addKeplerContribution(PositionAngleType, double, double[]) - Method in class org.orekit.orbits.CartesianOrbit
Add the contribution of the Keplerian motion to parameters derivatives
addKeplerContribution(PositionAngleType, double, double[]) - Method in class org.orekit.orbits.CircularOrbit
Add the contribution of the Keplerian motion to parameters derivatives
addKeplerContribution(PositionAngleType, double, double[]) - Method in class org.orekit.orbits.EquinoctialOrbit
Add the contribution of the Keplerian motion to parameters derivatives
addKeplerContribution(PositionAngleType, double, double[]) - Method in class org.orekit.orbits.KeplerianOrbit
Add the contribution of the Keplerian motion to parameters derivatives
addKeplerContribution(PositionAngleType, double, double[]) - Method in class org.orekit.orbits.Orbit
Add the contribution of the Keplerian motion to parameters derivatives
addKeplerContribution(PositionAngleType, T, T[]) - Method in class org.orekit.orbits.FieldCartesianOrbit
Add the contribution of the Keplerian motion to parameters derivatives
addKeplerContribution(PositionAngleType, T, T[]) - Method in class org.orekit.orbits.FieldCircularOrbit
Add the contribution of the Keplerian motion to parameters derivatives
addKeplerContribution(PositionAngleType, T, T[]) - Method in class org.orekit.orbits.FieldEquinoctialOrbit
Add the contribution of the Keplerian motion to parameters derivatives
addKeplerContribution(PositionAngleType, T, T[]) - Method in class org.orekit.orbits.FieldKeplerianOrbit
Add the contribution of the Keplerian motion to parameters derivatives
addKeplerContribution(PositionAngleType, T, T[]) - Method in class org.orekit.orbits.FieldOrbit
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.
addKlobucharMessage(IonosphereKlobucharMessage) - Method in class org.orekit.files.rinex.navigation.RinexNavigation
Add an ionosphere Klobuchar message.
addManeuver(Maneuver) - Method in class org.orekit.files.ccsds.ndm.adm.apm.ApmData
Add a maneuver.
addMassDerivative(double) - Method in interface org.orekit.propagation.numerical.TimeDerivativesEquations
Add the contribution of the flow rate (dm/dt).
addMassDerivative(T) - Method in interface org.orekit.propagation.numerical.FieldTimeDerivativesEquations
Add the contribution of the flow rate (dm/dt).
addMeasurement(ObservedMeasurement<?>) - Method in class org.orekit.estimation.leastsquares.BatchLSEstimator
Add a measurement.
addMeteoData(CRD.MeteorologicalMeasurement) - Method in class org.orekit.files.ilrs.CRD.CRDDataBlock
Add an entry to the list of meteorological data.
addModifier(EstimationModifier<MultiplexedMeasurement>) - Method in class org.orekit.estimation.measurements.generation.MultiplexedMeasurementBuilder
Add a modifier.
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.
addNequickGMessage(IonosphereNequickGMessage) - Method in class org.orekit.files.rinex.navigation.RinexNavigation
Add an ionosphere Nequick-G message.
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>, String, int, AngularDerivativesFilter) - Method in class org.orekit.files.general.OrekitAttitudeEphemerisFile.OrekitSatelliteAttitudeEphemeris
Injects pre-computed satellite states into this attitude ephemeris file object, returning the generated OrekitAttitudeEphemerisFile.OrekitAttitudeEphemerisSegment 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(Observation) - Method in class org.orekit.files.ccsds.ndm.tdm.ObservationsBlock
Adds an observation data line.
addObservation(ObservationType, AbsoluteDate, double) - Method in class org.orekit.files.ccsds.ndm.tdm.ObservationsBlock
Adds an observation data line.
addObservationDataSet(ObservationDataSet) - Method in class org.orekit.files.rinex.observation.RinexObservation
Add an observations data set.
addObserver(int, String, MessageObserver) - Method in class org.orekit.gnss.metric.ntrip.NtripClient
Add an observer for an encoded messages.
addObserver(int, MessageObserver) - Method in class org.orekit.gnss.metric.ntrip.StreamMonitor
Add an observer for encoded messages.
addObserver(ParameterObserver) - Method in class org.orekit.utils.ParameterDriver
Add an observer for this driver.
addOccultingBody(OneAxisEllipsoid) - Method in class org.orekit.forces.radiation.AbstractRadiationForceModel
Add a new occulting body.
addOccultingBody(ExtendedPVCoordinatesProvider, double) - Method in class org.orekit.forces.radiation.AbstractRadiationForceModel
Add a new occulting body.
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(AngularCoordinates) - Method in class org.orekit.utils.TimeStampedAngularCoordinates
Add an offset from the instance.
addOffset(FieldAngularCoordinates<T>) - Method in class org.orekit.utils.FieldAngularCoordinates
Add an offset from the instance.
addOffset(FieldAngularCoordinates<T>) - Method in class org.orekit.utils.TimeStampedFieldAngularCoordinates
Add an offset from the instance.
addOptionalSubInterpolatorIfDefined(FieldTimeInterpolator<? extends FieldTimeStamped<S>, S>, List<FieldTimeInterpolator<? extends FieldTimeStamped<S>, S>>) - Method in class org.orekit.time.AbstractFieldTimeInterpolator
Add all lowest level sub interpolators to the sub interpolator list.
addOptionalSubInterpolatorIfDefined(TimeInterpolator<? extends TimeStamped>, List<TimeInterpolator<? extends TimeStamped>>) - Method in class org.orekit.time.AbstractTimeInterpolator
Add all lowest level sub interpolators to the sub interpolator list.
addParameterDriver(ParameterDriver) - Method in class org.orekit.estimation.measurements.AbstractMeasurement
Add a parameter driver.
addParticipant(int, String) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Adds a participant to the list.
addPhaseBias(PhaseBias) - Method in class org.orekit.gnss.metric.messages.ssr.igm.SsrIgm06Data
Add a phase bias value for the current satellite.
addPhaseShiftCorrection(PhaseShiftCorrection) - Method in class org.orekit.files.rinex.observation.RinexObservationHeader
Add phase shift correction used to generate phases consistent w/r to cycle shifts.
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(DSSTPropagatorBuilder, CovarianceMatrixProvider) - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanEstimatorBuilder
Add a propagation configuration.
addPropagationConfiguration(DSSTPropagatorBuilder, CovarianceMatrixProvider) - Method in class org.orekit.estimation.sequential.SemiAnalyticalUnscentedKalmanEstimatorBuilder
Add a propagation configuration.
addPropagationConfiguration(PropagatorBuilder, CovarianceMatrixProvider) - Method in class org.orekit.estimation.sequential.KalmanEstimatorBuilder
Add a propagation configuration.
addPropagationConfiguration(PropagatorBuilder, CovarianceMatrixProvider) - Method in class org.orekit.estimation.sequential.UnscentedKalmanEstimatorBuilder
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.
addPsdCorrectionValidAfter(PsdCorrection, AbsoluteDate) - Method in class org.orekit.files.sinex.Station
Add a Post-Seismic Deformation entry valid after a limit date.
Using addPsdCorrectionValidAfter(entry, t) will make entry valid in [t, +∞[ (note the closed bracket).
addPVProviderAfter(AbsoluteDate, PVCoordinatesProvider, boolean) - Method in class org.orekit.utils.AggregatedPVCoordinatesProvider.Builder
Add a PVCoordinatesProvider to the collection.
addPVProviderBefore(AbsoluteDate, PVCoordinatesProvider, boolean) - Method in class org.orekit.utils.AggregatedPVCoordinatesProvider.Builder
Add a PVCoordinatesProvider to the collection.
addQZSSCivilianNavigationMessage(QZSSCivilianNavigationMessage) - Method in class org.orekit.files.rinex.navigation.RinexNavigation
Add a QZSS navigation message to the list.
addQZSSLegacyNavigationMessage(QZSSLegacyNavigationMessage) - Method in class org.orekit.files.rinex.navigation.RinexNavigation
Add a QZSS navigation message to the list.
addRangeData(CRD.RangeMeasurement) - Method in class org.orekit.files.ilrs.CRD.CRDDataBlock
Add an entry to the list of range data.
addRangeSupplementData(CRD.RangeSupplement) - Method in class org.orekit.files.ilrs.CRD.CRDDataBlock
Add an entry to the list of range supplement data.
addReceiveDelay(int, double) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Adds a receive delay to the list.
addReceiver(RinexClock.Receiver) - Method in class org.orekit.files.rinex.clock.RinexClock
Add a new receiver to the list of stored receivers.
addReferenceClockList(List<RinexClock.ReferenceClock>, AbsoluteDate) - Method in class org.orekit.files.rinex.clock.RinexClock
Add a list of reference clocks which will be used after a specified date.
addResetter(Field<T>, FieldManeuverTriggersResetter<T>) - Method in class org.orekit.forces.maneuvers.trigger.AbstractManeuverTriggers
Add a resetter.
addResetter(Field<T>, FieldManeuverTriggersResetter<T>) - Method in interface org.orekit.forces.maneuvers.trigger.ManeuverTriggers
Add a resetter.
addResetter(ManeuverTriggersResetter) - Method in class org.orekit.forces.maneuvers.trigger.AbstractManeuverTriggers
Add a resetter.
addResetter(ManeuverTriggersResetter) - Method in interface org.orekit.forces.maneuvers.trigger.ManeuverTriggers
Add a resetter.
addSatellite(String) - Method in class org.orekit.files.general.OrekitAttitudeEphemerisFile
Adds a new satellite to this object.
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.rinex.clock.RinexClock
Add a new satellite with a given identifier to the list of stored satellites.
addSatellite(String) - Method in class org.orekit.files.sp3.SP3
Add a new satellite with a given identifier to the list of stored satellites.
addSatelliteCoordinate(String, CPF.CPFCoordinate) - Method in class org.orekit.files.ilrs.CPF
Add a new P/V coordinates to the satellite.
addSatelliteCoordinates(String, List<CPF.CPFCoordinate>) - Method in class org.orekit.files.ilrs.CPF
Adds a set of P/V coordinates to the satellite.
addSatelliteVelocityToCPFCoordinate(String, Vector3D) - Method in class org.orekit.files.ilrs.CPF
Add the velocity to the last CPF coordinate entry.
addSatId(String) - Method in class org.orekit.files.sp3.SP3Header
Add a satellite identifier.
addSBASNavigationMessage(SBASNavigationMessage) - Method in class org.orekit.files.rinex.navigation.RinexNavigation
Add a SBAS navigation message to the list.
addScaleFactorCorrection(SatelliteSystem, ScaleFactorCorrection) - Method in class org.orekit.files.rinex.observation.RinexObservationHeader
Add scale factor correction.
addScheduler(Scheduler<T>) - Method in class org.orekit.estimation.measurements.generation.Generator
Add a sequences generator for a specific measurement type.
addSensor(AttitudeDeterminationSensor) - Method in class org.orekit.files.ccsds.ndm.adm.acm.AttitudeDetermination
Add a sensor used.
addSessionStatisticsData(CRD.SessionStatistics) - Method in class org.orekit.files.ilrs.CRD.CRDDataBlock
Add an entry to the list of session statistics data.
addSolution(long[], double) - Method in class org.orekit.estimation.measurements.gnss.AbstractLambdaMethod
Add a new solution.
addSpanAtDate(AbsoluteDate) - Method in class org.orekit.utils.ParameterDriver
Create a new span in values and names time span map given a start date.
addSpans(AbsoluteDate, AbsoluteDate, double) - Method in class org.orekit.utils.ParameterDriver
Cut values and names time span map given orbit determination start and end and driver periodicity.
addStationEccentricitiesValidAfter(Vector3D, AbsoluteDate) - Method in class org.orekit.files.sinex.Station
Add a station eccentricity vector entry valid after a limit date.
Using addStationEccentricitiesValidAfter(entry, t) will make entry valid in [t, +∞[ (note the closed bracket).
addStationEccentricitiesValidBefore(Vector3D, AbsoluteDate) - Method in class org.orekit.files.sinex.Station
Add a station eccentricity vector entry valid before a limit date.
Using addStationEccentricitiesValidBefore(entry, t) will make entry valid in ]-∞, t[ (note the open bracket).
addSubscriber(GeneratedMeasurementSubscriber) - Method in class org.orekit.estimation.measurements.generation.Generator
Add a subscriber.
addSupportedParameters(List<ParameterDriver>) - Method in class org.orekit.propagation.conversion.AbstractPropagatorBuilder
Add supported parameters.
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.
addSystemObservationType(SatelliteSystem, ObservationType) - Method in class org.orekit.files.rinex.clock.RinexClock
Add an observation type for a specified satellite system.
addSystemTimeOffset(SystemTimeOffsetMessage) - Method in class org.orekit.files.rinex.navigation.RinexNavigation
Add a system time offset.
addTimeSystemCorrections(TimeSystemCorrection) - Method in class org.orekit.files.rinex.navigation.RinexNavigationHeader
Add a time system correction to the list.
addTransmitDelay(int, double) - Method in class org.orekit.files.ccsds.ndm.tdm.TdmMetadata
Adds a transmit delay to the list.
addTroposphericModelValidAfter(EstimatedModel, AbsoluteDate) - Method in class org.orekit.models.earth.troposphere.TimeSpanEstimatedModel
Add a EstimatedTroposphericModel entry valid after a limit date.
Using addTroposphericModelValidAfter(entry, t) will make entry valid in [t, +∞[ (note the closed bracket).
addTroposphericModelValidAfter(EstimatedTroposphericModel, AbsoluteDate) - Method in class org.orekit.models.earth.troposphere.TimeSpanEstimatedTroposphericModel
Deprecated.
Add a EstimatedTroposphericModel entry valid after a limit date.
Using addTroposphericModelValidAfter(entry, t) will make entry valid in [t, +∞[ (note the closed bracket).
addTroposphericModelValidBefore(EstimatedModel, AbsoluteDate) - Method in class org.orekit.models.earth.troposphere.TimeSpanEstimatedModel
Add an EstimatedTroposphericModel entry valid before a limit date.
Using addTroposphericValidBefore(entry, t) will make entry valid in ]-∞, t[ (note the open bracket).
addTroposphericModelValidBefore(EstimatedTroposphericModel, AbsoluteDate) - Method in class org.orekit.models.earth.troposphere.TimeSpanEstimatedTroposphericModel
Deprecated.
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, AbsoluteDate, boolean) - Method in class org.orekit.utils.TimeSpanMap
Add an entry valid after a limit date.
addValidAfter(T, FieldAbsoluteDate<D>) - Method in class org.orekit.utils.FieldTimeSpanMap
Add an entry valid after a limit date.
addValidBefore(T, AbsoluteDate, boolean) - Method in class org.orekit.utils.TimeSpanMap
Add an entry valid before a limit date.
addValidBefore(T, FieldAbsoluteDate<D>) - Method in class org.orekit.utils.FieldTimeSpanMap
Add an entry valid before a limit date.
addValidBetween(T, AbsoluteDate, AbsoluteDate) - Method in class org.orekit.utils.TimeSpanMap
Add an entry valid between two limit dates.
addWaveCoefficients(int, int, int, double, double, double, double, int, String) - Method in class org.orekit.forces.gravity.potential.OceanTidesReader
Add parsed coefficients.
addWaypoint(GeodeticPoint, AbsoluteDate) - Method in class org.orekit.utils.WaypointPVBuilder
Add a waypoint.
addWeightedPoint(AbsoluteDate, double, double) - Method in class org.orekit.utils.SecularAndHarmonic
Add a weighted fitting point.
ADM_MSG_LINK - org.orekit.files.ccsds.ndm.cdm.CdmMetadataKey
Unique identifier of Attitude Data Message(s) that are linked (relevant) to this Conjunction Data Message.
ADM_MSG_LINK - org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadataKey
Unique identifier of Attitude Data Message linked to this Orbit Data Message.
AdmCommonMetadataKey - Enum in org.orekit.files.ccsds.ndm.adm
Keys for APM and AEM entries.
AdmCommonMetadataWriter - Class in org.orekit.files.ccsds.ndm.adm
Writer for Common metadata for CCSDS Attitude Parameter/Ephemeris Messages.
AdmCommonMetadataWriter(AdmMetadata) - Constructor for class org.orekit.files.ccsds.ndm.adm.AdmCommonMetadataWriter
Simple constructor.
AdMethodType - Enum in org.orekit.files.ccsds.definitions
Type of attitude determination method used in CCSDS Attitude Comprehensive Messages.
AdmHeader - Class in org.orekit.files.ccsds.ndm.adm
Header of a CCSDS Attitude Data Message.
AdmHeader() - Constructor for class org.orekit.files.ccsds.ndm.adm.AdmHeader
Constructor.
AdmMetadata - Class in org.orekit.files.ccsds.ndm.adm
This class gathers the meta-data present in the Attitude Data Message (ADM).
AdmMetadata() - Constructor for class org.orekit.files.ccsds.ndm.adm.AdmMetadata
Simple constructor.
AdmMetadataKey - Enum in org.orekit.files.ccsds.ndm.adm
Keys for ADM container entries.
AdmParser<T extends NdmConstituent<AdmHeader,​?>,​P extends AbstractConstituentParser<AdmHeader,​T,​?>> - Class in org.orekit.files.ccsds.ndm.adm
Base class for Attitude Data Message parsers.
AdmParser(String, String, IERSConventions, boolean, DataContext, AbsoluteDate, ParsedUnitsBehavior, Function<ParseToken, List<ParseToken>>[]) - Constructor for class org.orekit.files.ccsds.ndm.adm.AdmParser
Complete constructor.
Aem - Class in org.orekit.files.ccsds.ndm.adm.aem
This class stores all the information of the Attitude Ephemeris Message (AEM) File parsed by AEMParser.
Aem(AdmHeader, List<AemSegment>, IERSConventions, DataContext) - Constructor for class org.orekit.files.ccsds.ndm.adm.aem.Aem
Simple constructor.
AemData - Class in org.orekit.files.ccsds.ndm.adm.aem
The Attitude Ephemerides data blocks class contain list of attitude data points.
AemData() - Constructor for class org.orekit.files.ccsds.ndm.adm.aem.AemData
Constructor.
AemMetadata - Class in org.orekit.files.ccsds.ndm.adm.aem
This class gathers the meta-data present in the Attitude Data Message (ADM).
AemMetadata(int) - Constructor for class org.orekit.files.ccsds.ndm.adm.aem.AemMetadata
Simple constructor.
AemMetadataKey - Enum in org.orekit.files.ccsds.ndm.adm.aem
Keys for AEM container entries.
AemParser - Class in org.orekit.files.ccsds.ndm.adm.aem
A parser for the CCSDS AEM (Attitude Ephemeris Message).
AemParser(IERSConventions, boolean, DataContext, AbsoluteDate, int, ParsedUnitsBehavior, Function<ParseToken, List<ParseToken>>[]) - Constructor for class org.orekit.files.ccsds.ndm.adm.aem.AemParser
Complete constructor.
AemSatelliteEphemeris - Class in org.orekit.files.ccsds.ndm.adm.aem
AEM ephemeris blocks for a single satellite.
AemSatelliteEphemeris(String, List<AemSegment>) - Constructor for class org.orekit.files.ccsds.ndm.adm.aem.AemSatelliteEphemeris
Create a container for the set of ephemeris blocks in the file that pertain to a single satellite.
AemSegment - Class in org.orekit.files.ccsds.ndm.adm.aem
This class stores the metadata and data for one attitude segment.
AemSegment(AemMetadata, AemData) - Constructor for class org.orekit.files.ccsds.ndm.adm.aem.AemSegment
Simple constructor.
AemWriter - Class in org.orekit.files.ccsds.ndm.adm.aem
A writer for Attitude Ephemeris Messsage (AEM) files.
AemWriter(IERSConventions, DataContext, AbsoluteDate) - Constructor for class org.orekit.files.ccsds.ndm.adm.aem.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.
AggregateBoundedAttitudeProvider - Class in org.orekit.attitudes
A BoundedAttitudeProvider that covers a larger time span from several constituent attitude providers that cover shorter time spans.
AggregateBoundedAttitudeProvider(Collection<? extends BoundedAttitudeProvider>) - Constructor for class org.orekit.attitudes.AggregateBoundedAttitudeProvider
Constructor.
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.
AggregateBoundedPropagator(NavigableMap<AbsoluteDate, ? extends BoundedPropagator>, AbsoluteDate, AbsoluteDate) - Constructor for class org.orekit.propagation.analytical.AggregateBoundedPropagator
Create a propagator from several constituent propagators.
AggregatedClockModel - Class in org.orekit.time
Offset clock model aggregating several other clock models.
AggregatedClockModel(TimeSpanMap<ClockModel>) - Constructor for class org.orekit.time.AggregatedClockModel
Simple constructor.
AggregatedPVCoordinatesProvider - Class in org.orekit.utils
Aggreate multiple PVCoordinatesProvider instances together This can be used to describe an aircraft or surface vehicle.
AggregatedPVCoordinatesProvider(TimeSpanMap<PVCoordinatesProvider>) - Constructor for class org.orekit.utils.AggregatedPVCoordinatesProvider
Class constructor.
AggregatedPVCoordinatesProvider(TimeSpanMap<PVCoordinatesProvider>, AbsoluteDate, AbsoluteDate) - Constructor for class org.orekit.utils.AggregatedPVCoordinatesProvider
Class constructor.
AggregatedPVCoordinatesProvider.Builder - Class in org.orekit.utils
AggregatedPVCoordinatesProvider.InvalidPVProvider - Class in org.orekit.utils
Implementation of PVCoordinatesProvider that throws an illegal state exception.
AGILeapSecondFilesLoader - Class in org.orekit.time
Loader for UTC-TAI extracted from LeapSecond file from AGI.
AGILeapSecondFilesLoader(String) - Constructor for class org.orekit.time.AGILeapSecondFilesLoader
Build a loader for LeapSecond.dat file from AGI.
AGILeapSecondFilesLoader(String, DataProvidersManager) - Constructor for class org.orekit.time.AGILeapSecondFilesLoader
Build a loader for LeapSecond.dat file from AGI.
AGILeapSecondFilesLoader.Parser - Class in org.orekit.time
Internal class performing the parsing.
AGOM - org.orekit.files.ccsds.ndm.odm.omm.OmmTleKey
SGP4-XP solar radiation pressure-like coefficient.
AKELLAALFRIEND_2000 - org.orekit.files.ccsds.definitions.PocMethodType
Akella and Alfriend - 2000 method.
ALBEDO_GRID_SIZE - org.orekit.files.ccsds.ndm.odm.ocm.PerturbationsKey
Albedo grid size.
ALBEDO_MODEL - org.orekit.files.ccsds.ndm.odm.ocm.PerturbationsKey
Albedo model.
ALFANO_2005 - org.orekit.files.ccsds.definitions.PocMethodType
Alfano 2005 method.
ALFANO_2005 - org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DPOCMethodType
Probability of collision computing method described in :"S.
ALFANO_MAX_PROBABILITY - org.orekit.files.ccsds.definitions.PocMethodType
Maximum conjunction probability method from Alfano.
ALFANO_PARAL_2007 - org.orekit.files.ccsds.definitions.PocMethodType
Adjoining parallelepipeds method from Alfano.
ALFANO_TUBES_2007 - org.orekit.files.ccsds.definitions.PocMethodType
Adjoining tubes method from Alfano.
ALFANO_VOXELS_2006 - org.orekit.files.ccsds.definitions.PocMethodType
Voxels method from Alfano.
Alfano2005 - Class in org.orekit.ssa.collision.shorttermencounter.probability.twod
Compute the probability of collision using the method described in :"S.
Alfano2005() - Constructor for class org.orekit.ssa.collision.shorttermencounter.probability.twod.Alfano2005
Empty constructor.
ALFRIEND_1999 - org.orekit.files.ccsds.definitions.PocMethodType
Alfriend 1999 method.
ALFRIEND_1999 - org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DPOCMethodType
Probability of collision computing method described in :"Kyle Alfriend, Maruthi Akella, Joseph Frisbee, James Foster, Deok-Jin Lee, and Matthew Wilkins.
ALFRIEND_1999_MAX - org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DPOCMethodType
Probability of collision computing method described in :"Kyle Alfriend, Maruthi Akella, Joseph Frisbee, James Foster, Deok-Jin Lee, and Matthew Wilkins.
Alfriend1999 - Class in org.orekit.ssa.collision.shorttermencounter.probability.twod
Compute the probability of collision using the method described in : "Kyle Alfriend, Maruthi Akella, Joseph Frisbee, James Foster, Deok-Jin Lee, and Matthew Wilkins.
Alfriend1999() - Constructor for class org.orekit.ssa.collision.shorttermencounter.probability.twod.Alfriend1999
Empty constructor.
Alfriend1999Max - Class in org.orekit.ssa.collision.shorttermencounter.probability.twod
Compute the probability of collision assuming the worst case described in : "Kyle Alfriend, Maruthi Akella, Joseph Frisbee, James Foster, Deok-Jin Lee, and Matthew Wilkins.
Alfriend1999Max() - Constructor for class org.orekit.ssa.collision.shorttermencounter.probability.twod.Alfriend1999Max
Empty constructor.
alias(String) - Method in class org.orekit.utils.units.Unit
Create an alias for a unit.
AlignmentDetector - Class in org.orekit.propagation.events
Finder for satellite/body alignment events in orbital plane.
AlignmentDetector(double, double, PVCoordinatesProvider, double) - Constructor for class org.orekit.propagation.events.AlignmentDetector
Build a new alignment detector.
AlignmentDetector(double, Orbit, PVCoordinatesProvider, double) - Constructor for class org.orekit.propagation.events.AlignmentDetector
Build a new alignment detector.
AlignmentDetector(Orbit, PVCoordinatesProvider, double) - Constructor for class org.orekit.propagation.events.AlignmentDetector
Build a new alignment detector.
AlignmentDetector(AdaptableInterval, double, int, EventHandler, PVCoordinatesProvider, double) - Constructor for class org.orekit.propagation.events.AlignmentDetector
Protected constructor with full parameters.
ALMOST_CRITICALLY_INCLINED_ORBIT - org.orekit.errors.OrekitMessages
ALMOST_CRITICALLY_INCLINED_ORBIT.
ALMOST_EQUATORIAL_ORBIT - org.orekit.errors.OrekitMessages
ALMOST_EQUATORIAL_ORBIT.
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.
ALT_COV_REF_FRAME - org.orekit.files.ccsds.ndm.cdm.CdmMetadataKey
Name of the reference frame in which the alternate covariance data are given.
ALT_COV_TYPE - org.orekit.files.ccsds.ndm.cdm.CdmMetadataKey
Flag indicating the type of alternate covariance information provided.
AltCovarianceType - Enum in org.orekit.files.ccsds.ndm.cdm
Flag indicating the type of alternate covariance information provided.
ALTERNATE_NAMES - org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadataKey
Alternate names fir this space object.
ALTITUDE_BELOW_ALLOWED_THRESHOLD - org.orekit.errors.OrekitMessages
ALTITUDE_BELOW_ALLOWED_THRESHOLD.
AltitudeDetector - Class in org.orekit.propagation.events
Finder for satellite altitude crossing events.
AltitudeDetector(double, double, double, BodyShape) - Constructor for class org.orekit.propagation.events.AltitudeDetector
Build a new altitude detector.
AltitudeDetector(double, double, BodyShape) - Constructor for class org.orekit.propagation.events.AltitudeDetector
Build a new altitude detector.
AltitudeDetector(double, BodyShape) - Constructor for class org.orekit.propagation.events.AltitudeDetector
Build a new altitude detector.
AltitudeDetector(AdaptableInterval, double, int, EventHandler, double, BodyShape) - Constructor for class org.orekit.propagation.events.AltitudeDetector
Protected constructor with full parameters.
AMBIGUITY_NAME - Static variable in class org.orekit.estimation.measurements.gnss.InterSatellitesPhase
Deprecated.
as of 12.1 not used anymore
AMBIGUITY_NAME - Static variable in class org.orekit.estimation.measurements.gnss.OneWayGNSSPhase
Deprecated.
as of 12.1 not used anymore
AMBIGUITY_NAME - Static variable in class org.orekit.estimation.measurements.gnss.Phase
Deprecated.
as of 12.1 not used anymore
AmbiguityAcceptance - Interface in org.orekit.estimation.measurements.gnss
Interface defining ambiguity acceptance tests.
AmbiguityCache - Class in org.orekit.estimation.measurements.gnss
Cache for AmbiguityDriver.
AmbiguityCache() - Constructor for class org.orekit.estimation.measurements.gnss.AmbiguityCache
Simple constructor.
AmbiguityDriver - Class in org.orekit.estimation.measurements.gnss
Specialized ParameterDriver for ambiguity.
AmbiguityDriver(String, String, double) - Constructor for class org.orekit.estimation.measurements.gnss.AmbiguityDriver
Simple constructor.
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.
AMPERE - Static variable in class org.orekit.utils.units.Unit
Ampere unit.
andCombine(Collection<? extends EventDetector>) - Static method in class org.orekit.propagation.events.BooleanDetector
Create a new event detector that is the logical AND of the given event detectors.
andCombine(Collection<? extends FieldEventDetector<T>>) - Static method in class org.orekit.propagation.events.FieldBooleanDetector
Create a new event detector that is the logical AND of the given event detectors.
andCombine(EventDetector...) - Static method in class org.orekit.propagation.events.BooleanDetector
Create a new event detector that is the logical AND of the given event detectors.
andCombine(FieldEventDetector<T>...) - Static method in class org.orekit.propagation.events.FieldBooleanDetector
Create a new event detector that is the logical AND of the given event detectors.
ANGLE - org.orekit.files.ccsds.ndm.adm.acm.AttitudeCovarianceType
Angles.
ANGLE_1 - org.orekit.files.ccsds.ndm.adm.aem.AttitudeEntryKey
Rotation about first axis.
ANGLE_1 - org.orekit.files.ccsds.ndm.adm.apm.EulerKey
First body rotation angle entry.
ANGLE_1 - org.orekit.files.ccsds.ndm.tdm.ObservationType
Data: ANGLE_1 in degrees and in [-180, +360[ [deg].
ANGLE_1_DOT - org.orekit.files.ccsds.ndm.adm.aem.AttitudeEntryKey
Rotation about first axis.
ANGLE_1_DOT - org.orekit.files.ccsds.ndm.adm.apm.EulerKey
First body rotation rate entry.
ANGLE_2 - org.orekit.files.ccsds.ndm.adm.aem.AttitudeEntryKey
Rotation about second axis.
ANGLE_2 - org.orekit.files.ccsds.ndm.adm.apm.EulerKey
Second body rotation angle entry.
ANGLE_2 - org.orekit.files.ccsds.ndm.tdm.ObservationType
Data: ANGLE_2 in degrees and in [-180, +360[ [deg].
ANGLE_2_DOT - org.orekit.files.ccsds.ndm.adm.aem.AttitudeEntryKey
Rotation about second axis.
ANGLE_2_DOT - org.orekit.files.ccsds.ndm.adm.apm.EulerKey
Second body rotation rate entry.
ANGLE_3 - org.orekit.files.ccsds.ndm.adm.aem.AttitudeEntryKey
Rotation about third axis.
ANGLE_3 - org.orekit.files.ccsds.ndm.adm.apm.EulerKey
Third body rotation angle entry.
ANGLE_3_DOT - org.orekit.files.ccsds.ndm.adm.aem.AttitudeEntryKey
Rotation about third axis.
ANGLE_3_DOT - org.orekit.files.ccsds.ndm.adm.apm.EulerKey
Third body rotation rate entry.
ANGLE_ANGVEL - org.orekit.files.ccsds.ndm.adm.acm.AttitudeCovarianceType
Angles and angular velocities.
ANGLE_GYROBIAS - org.orekit.files.ccsds.ndm.adm.acm.AttitudeCovarianceType
Angles and gyro biases.
ANGLE_TYPE - org.orekit.files.ccsds.ndm.tdm.TdmMetadataKey
Angle type entry.
ANGLE_TYPE_NOT_SUPPORTED - org.orekit.errors.OrekitMessages
ANGLE_TYPE_NOT_SUPPORTED.
angles(FieldSpacecraftState<T>) - Method in class org.orekit.utils.OccultationEngine
Compute the occultation angles as seen from a spacecraft.
angles(SpacecraftState) - Method in class org.orekit.utils.OccultationEngine
Compute the occultation angles as seen from a spacecraft.
AnglesMeasurement(AbsoluteDate, double, double, int, int, boolean, double, double) - Constructor for class org.orekit.files.ilrs.CRD.AnglesMeasurement
Constructor.
AngleType - Enum in org.orekit.files.ccsds.ndm.tdm
Antenna geometry represented in the angle date.
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(FieldRotation<U>) - Constructor for class org.orekit.utils.AngularCoordinates
Builds a AngularCoordinates from a FieldRotation<Derivative>.
AngularCoordinates(Rotation) - Constructor for class org.orekit.utils.AngularCoordinates
Builds angular coordinates with the given rotation, zero angular velocity, and zero angular acceleration.
AngularCoordinates(Rotation, Vector3D) - Constructor for class org.orekit.utils.AngularCoordinates
Builds a rotation/rotation rate pair.
AngularCoordinates(Rotation, Vector3D, Vector3D) - Constructor for class org.orekit.utils.AngularCoordinates
Builds a rotation/rotation rate/rotation acceleration triplet.
AngularCoordinates(PVCoordinates, PVCoordinates) - Constructor for class org.orekit.utils.AngularCoordinates
Build one of the rotations that transform one pv coordinates into another one.
AngularCoordinates(PVCoordinates, PVCoordinates, PVCoordinates, PVCoordinates, double) - Constructor for class org.orekit.utils.AngularCoordinates
Build the rotation that transforms a pair of pv coordinates into another one.
AngularDerivativesFilter - Enum in org.orekit.utils
Enumerate for selecting which derivatives to use in TimeStampedAngularCoordinates and TimeStampedFieldAngularCoordinates interpolation.
AngularIonosphericDelayModifier - Class in org.orekit.estimation.measurements.modifiers
Class modifying theoretical angular measurement with ionospheric delay.
AngularIonosphericDelayModifier(IonosphericModel, double) - Constructor for class org.orekit.estimation.measurements.modifiers.AngularIonosphericDelayModifier
Constructor.
AngularRaDec - Class in org.orekit.estimation.measurements
Class modeling a 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(AdaptableInterval, double, int, EventHandler, PVCoordinatesProvider, PVCoordinatesProvider, double) - Constructor for class org.orekit.propagation.events.AngularSeparationDetector
Protected constructor with full parameters.
AngularSeparationDetector(PVCoordinatesProvider, PVCoordinatesProvider, double) - Constructor for class org.orekit.propagation.events.AngularSeparationDetector
Build a new angular separation detector.
AngularSeparationFromSatelliteDetector - Class in org.orekit.propagation.events
Detects when two moving objects come close to each other, as seen from spacecraft.
AngularSeparationFromSatelliteDetector(AdaptableInterval, double, int, EventHandler, PVCoordinatesProvider, PVCoordinatesProvider, double) - Constructor for class org.orekit.propagation.events.AngularSeparationFromSatelliteDetector
Protected constructor with full parameters.
AngularSeparationFromSatelliteDetector(PVCoordinatesProvider, PVCoordinatesProvider, double) - Constructor for class org.orekit.propagation.events.AngularSeparationFromSatelliteDetector
Build a new angular detachment detector.
AngularTroposphericDelayModifier - Class in org.orekit.estimation.measurements.modifiers
Deprecated.
as of 12.1, AngularRadioRefractionModifier shall be used to handle tropospheric effect on angular measurements
AngularTroposphericDelayModifier(DiscreteTroposphericModel) - Constructor for class org.orekit.estimation.measurements.modifiers.AngularTroposphericDelayModifier
Deprecated.
as of 12.1, AngularRadioRefractionModifier shall be used to handle tropospheric effect on angular measurements
AngularTroposphericDelayModifier(TroposphericModel) - Constructor for class org.orekit.estimation.measurements.modifiers.AngularTroposphericDelayModifier
Deprecated.
as of 12.1, AngularRadioRefractionModifier shall be used to handle tropospheric effect on angular measurements
AngularVelocity - Class in org.orekit.files.ccsds.ndm.adm.apm
Container for Attitude Parameter Message data lines.
AngularVelocity() - Constructor for class org.orekit.files.ccsds.ndm.adm.apm.AngularVelocity
Simple constructor.
AngularVelocityKey - Enum in org.orekit.files.ccsds.ndm.adm.apm
Keys for APM angular velocity entries.
angVel - org.orekit.files.ccsds.ndm.adm.aem.AttitudeEntryKey
Angular velocity sub-sub-section.
ANGVEL - org.orekit.files.ccsds.ndm.adm.acm.RateElementsType
Angular velocity.
ANGVEL_FRAME - org.orekit.files.ccsds.ndm.adm.aem.AemMetadataKey
Reference frame for angular velocities.
ANGVEL_FRAME - org.orekit.files.ccsds.ndm.adm.apm.AngularVelocityKey
Frame in which angular velocity is defined.
ANGVEL_X - org.orekit.files.ccsds.ndm.adm.aem.AttitudeEntryKey
Angular velocity about X axis.
ANGVEL_X - org.orekit.files.ccsds.ndm.adm.apm.AngularVelocityKey
Angular velocity around X axis.
ANGVEL_Y - org.orekit.files.ccsds.ndm.adm.aem.AttitudeEntryKey
Angular velocity about Y axis.
ANGVEL_Y - org.orekit.files.ccsds.ndm.adm.apm.AngularVelocityKey
Angular velocity around Y axis.
ANGVEL_Z - org.orekit.files.ccsds.ndm.adm.aem.AttitudeEntryKey
Angular velocity about Z axis.
ANGVEL_Z - org.orekit.files.ccsds.ndm.adm.apm.AngularVelocityKey
Angular velocity around Z axis.
ANT_NB_TYPE - org.orekit.files.rinex.section.RinexLabels
Antenna number and type.
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.
ANTENNA_B_SIGHT_XYZ - org.orekit.files.rinex.section.RinexLabels
Antenna bore sight.
ANTENNA_DELTA_H_E_N - org.orekit.files.rinex.section.RinexLabels
Antenna reference point.
ANTENNA_DELTA_X_Y_Z - org.orekit.files.rinex.section.RinexLabels
Antenna reference point.
ANTENNA_PHASE_CENTER - org.orekit.files.rinex.section.RinexLabels
Antenna phase center.
ANTENNA_ZERODIR_AZI - org.orekit.files.rinex.section.RinexLabels
Antenna zero direction.
ANTENNA_ZERODIR_XYZ - org.orekit.files.rinex.section.RinexLabels
Antenna zero direction.
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 a DataProvidersManager.
AntexLoader(DataSource, TimeScale) - Constructor for class org.orekit.gnss.antenna.AntexLoader
Construct a loader by specifying the source of ANTEX auxiliary data files.
ANTICIPATED - org.orekit.files.ccsds.ndm.odm.ocm.ManBasis
Non-cooperative future maneuver that is anticipated (i.e.
anticipateNext(ProcessingState) - Method in class org.orekit.files.ccsds.utils.parsing.AbstractMessageParser
Anticipate what next processing state should be.
Apm - Class in org.orekit.files.ccsds.ndm.adm.apm
This class stores all the information of the Attitude Parameter Message (APM) File parsed by APMParser.
Apm(AdmHeader, List<Segment<AdmMetadata, ApmData>>, IERSConventions, DataContext) - Constructor for class org.orekit.files.ccsds.ndm.adm.apm.Apm
Simple constructor.
ApmData - Class in org.orekit.files.ccsds.ndm.adm.apm
Container for Attitude Parameter Message data.
ApmData(CommentsContainer, AbsoluteDate, ApmQuaternion, Euler, AngularVelocity, SpinStabilized, Inertia) - Constructor for class org.orekit.files.ccsds.ndm.adm.apm.ApmData
Simple constructor.
ApmParser - Class in org.orekit.files.ccsds.ndm.adm.apm
A parser for the CCSDS APM (Attitude Parameter Message).
ApmParser(IERSConventions, boolean, DataContext, AbsoluteDate, ParsedUnitsBehavior, Function<ParseToken, List<ParseToken>>[]) - Constructor for class org.orekit.files.ccsds.ndm.adm.apm.ApmParser
Complete constructor.
ApmQuaternion - Class in org.orekit.files.ccsds.ndm.adm.apm
Container for Attitude Parameter Message quaternion logical block.
ApmQuaternion() - Constructor for class org.orekit.files.ccsds.ndm.adm.apm.ApmQuaternion
Simple constructor.
ApmQuaternionKey - Enum in org.orekit.files.ccsds.ndm.adm.apm
Keys for APM quaternion entries.
ApmWriter - Class in org.orekit.files.ccsds.ndm.adm.apm
Writer for CCSDS Orbit Parameter Message.
ApmWriter(IERSConventions, DataContext, AbsoluteDate) - Constructor for class org.orekit.files.ccsds.ndm.adm.apm.ApmWriter
Complete constructor.
APOAPSIS_ALTITUDE - org.orekit.files.ccsds.ndm.cdm.AdditionalParametersKey
The distance of the furthest point in the objects orbit above the equatorial radius of the central body.
AppliedDCBS - Class in org.orekit.files.rinex
Corrections of Differential Code Biases (DCBs) applied.
AppliedDCBS(SatelliteSystem, String, String) - Constructor for class org.orekit.files.rinex.AppliedDCBS
Simple constructor.
AppliedPCVS - Class in org.orekit.files.rinex
Corrections of antenna phase center variations (PCVs) applied.
AppliedPCVS(SatelliteSystem, String, String) - Constructor for class org.orekit.files.rinex.AppliedPCVS
Simple constructor.
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(Orbit) - Method in class org.orekit.propagation.analytical.J2DifferentialEffect
Compute the effect of the maneuver on an orbit.
apply(SpacecraftState) - Method in class org.orekit.forces.maneuvers.SmallManeuverAnalyticalModel
Compute the effect of the maneuver on a spacecraft state.
apply(SpacecraftState) - Method in interface org.orekit.propagation.analytical.AdapterPropagator.DifferentialEffect
Apply the effect to a spacecraft state.
apply(SpacecraftState) - Method in class org.orekit.propagation.analytical.J2DifferentialEffect
Apply the effect to a spacecraft state.
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.
applyDynamicOutlierFilter(EstimatedMeasurement<T>, RealMatrix) - Static method in class org.orekit.estimation.sequential.KalmanEstimatorUtil
Set and apply a dynamic outlier filter on a measurement.
applyRelevantFilters(DataSource) - Method in class org.orekit.data.FiltersManager
Apply all the relevant data filters, taking care of layers.
applyResetters(FieldSpacecraftState<T>) - Method in class org.orekit.forces.maneuvers.trigger.AbstractManeuverTriggers
Apply resetters.
applyResetters(SpacecraftState) - Method in class org.orekit.forces.maneuvers.trigger.AbstractManeuverTriggers
Apply resetters.
applyTo(FieldPVCoordinates<T>) - Method in class org.orekit.utils.AngularCoordinates
Apply the rotation to a pv coordinates.
applyTo(FieldPVCoordinates<T>) - Method in class org.orekit.utils.FieldAngularCoordinates
Apply the rotation to a pv coordinates.
applyTo(PVCoordinates) - Method in class org.orekit.utils.AngularCoordinates
Apply the rotation to a pv coordinates.
applyTo(PVCoordinates) - Method in class org.orekit.utils.FieldAngularCoordinates
Apply the rotation to a pv coordinates.
applyTo(TimeStampedFieldPVCoordinates<T>) - Method in class org.orekit.utils.AngularCoordinates
Apply the rotation to a pv coordinates.
applyTo(TimeStampedFieldPVCoordinates<T>) - Method in class org.orekit.utils.FieldAngularCoordinates
Apply the rotation to a pv coordinates.
applyTo(TimeStampedPVCoordinates) - Method in class org.orekit.utils.AngularCoordinates
Apply the rotation to a pv coordinates.
applyTo(TimeStampedPVCoordinates) - Method in class org.orekit.utils.FieldAngularCoordinates
Apply the rotation to a pv coordinates.
APPROACH_ANGLE - org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadataKey
The approach angle computed between Objects 1 and 2 in the RTN coordinate frame relative to object 1.
APPROX_POSITION_XYZ - org.orekit.files.rinex.section.RinexLabels
Approximative position.
approximateAsPolynomialOnly(int, AbsoluteDate, int, int, AbsoluteDate, AbsoluteDate, double) - Method in class org.orekit.utils.SecularAndHarmonic
Approximate an already fitted model to polynomial only terms.
APRIL - org.orekit.time.Month
April.
ApsideDetectionAdaptableIntervalFactory - Class in org.orekit.propagation.events.intervals
Factory class for AdaptableInterval suitable for apside detection on eccentric orbits.
ApsideDetector - Class in org.orekit.propagation.events
Finder for apside crossing events.
ApsideDetector(double) - 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.
ApsideDetector(Orbit) - Constructor for class org.orekit.propagation.events.ApsideDetector
Build a new instance.
ApsideDetector(AdaptableInterval, double, int, EventHandler) - Constructor for class org.orekit.propagation.events.ApsideDetector
Public constructor with full parameters.
AR - org.orekit.files.rinex.clock.RinexClock.ClockDataType
Data analysis for receiver clocks.
ARBITRARY_EPOCH - Static variable in class org.orekit.time.AbsoluteDate
An arbitrary finite date.
ARC_MINUTE - Static variable in class org.orekit.utils.units.Unit
Arc minute unit.
ARC_SECOND - Static variable in class org.orekit.utils.units.Unit
Arc second unit.
ARC_SECONDS - org.orekit.data.PolynomialParser.Unit
Arc-seconds angles.
ARC_SECONDS_TO_RADIANS - Static variable in interface org.orekit.utils.Constants
Conversion factor from arc seconds to radians: 2*PI/(360*60*60).
ARC_SECONDS_TO_RADIANS - Static variable in class org.orekit.utils.units.UnitsConverter
Arcseconds to radians converter.
AREA_ALONG_OEB_INT - org.orekit.files.ccsds.ndm.cdm.AdditionalParametersKey
Cross-sectional area of Optimally Enclosing Box when viewed along the intermediate OEB direction.
AREA_ALONG_OEB_INT - org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalPropertiesKey
Cross-sectional area of Optimally Enclosing Box along Y-OEB.
AREA_ALONG_OEB_MAX - org.orekit.files.ccsds.ndm.cdm.AdditionalParametersKey
Cross-sectional area of Optimally Enclosing Box when viewed along the maximum OEB direction.
AREA_ALONG_OEB_MAX - org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalPropertiesKey
Cross-sectional area of Optimally Enclosing Box along X-OEB.
AREA_ALONG_OEB_MIN - org.orekit.files.ccsds.ndm.cdm.AdditionalParametersKey
Cross-sectional area of Optimally Enclosing Box when viewed along the minimum OEB direction.
AREA_ALONG_OEB_MIN - org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalPropertiesKey
Cross-sectional area of Optimally Enclosing Box along Z-OEB.
AREA_DRG - org.orekit.files.ccsds.ndm.cdm.AdditionalParametersKey
The effective area of the object exposed to atmospheric drag.
AREA_MAX_FOR_PC - org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalPropertiesKey
Maximum cross-sectional area for collision probability estimation purposes.
AREA_MIN_FOR_PC - org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalPropertiesKey
Minimum cross-sectional area for collision probability estimation purposes.
AREA_PC - org.orekit.files.ccsds.ndm.cdm.AdditionalParametersKey
The actual area of the object.
AREA_PC_MAX - org.orekit.files.ccsds.ndm.cdm.AdditionalParametersKey
Maximum area (or cross-section) of the object to be used in the calculation of the probability of collision.
AREA_PC_MIN - org.orekit.files.ccsds.ndm.cdm.AdditionalParametersKey
Minimum area (or cross-section) of the object to be used in the calculation of the probability of collision.
AREA_SRP - org.orekit.files.ccsds.ndm.cdm.AdditionalParametersKey
The effective area of the object exposed to solar radiation pressure.
AREA_TYP_FOR_PC - org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalPropertiesKey
Typical (50th percentile) cross-sectional area for collision probability estimation purposes.
areAdditionalDataAvailable() - Method in class org.orekit.gnss.metric.messages.rtcm.ephemeris.Rtcm1020Data
Get the flag indicating if additional parameters are in the message.
areFeesRequired() - Method in class org.orekit.gnss.metric.ntrip.DataStreamRecord
Check if fees are required.
areFeesRequired() - Method in class org.orekit.gnss.metric.ntrip.NetworkRecord
Check if fees are required.
ARG_OF_PERICENTER - org.orekit.files.ccsds.ndm.odm.KeplerianElementsKey
Orbit argument of pericenter.
AS - org.orekit.files.rinex.clock.RinexClock.ClockDataType
Data analysis for satellite clocks.
asCelestialBodyFrame() - Method in class org.orekit.files.ccsds.definitions.FrameFacade
Get the associated celestial body frame.
asFrame() - Method in class org.orekit.files.ccsds.definitions.FrameFacade
Get the associated frame tree node.
AskneNordiusModel - Class in org.orekit.models.earth.troposphere
The Askne Nordius model.
AskneNordiusModel(TroposphereMappingFunction) - Constructor for class org.orekit.models.earth.troposphere.AskneNordiusModel
Create a new Askne Nordius model.
asOrbitRelativeFrame() - Method in class org.orekit.files.ccsds.definitions.FrameFacade
Get the associated orbit relative frame.
asSpacecraftBodyFrame() - Method in class org.orekit.files.ccsds.definitions.FrameFacade
Get the associated spacecraft body frame.
AST - org.orekit.files.ccsds.definitions.SpacecraftBodyFrame.BaseEquipment
Autonomous Star Tracker.
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.
ATMOSPHERIC_MODEL - org.orekit.files.ccsds.ndm.cdm.CdmMetadataKey
Name of atmospheric model.
ATMOSPHERIC_MODEL - org.orekit.files.ccsds.ndm.odm.ocm.PerturbationsKey
Name of atmospheric model.
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.
att - org.orekit.files.ccsds.ndm.adm.acm.AcmDataSubStructureKey
Trajectory state time history section.
ATT - org.orekit.files.ccsds.ndm.adm.acm.AcmDataSubStructureKey
Attitude state time history section.
ATT - org.orekit.files.ccsds.ndm.adm.acm.AcmElements
Attitude state time history.
ATT_ACTUATOR_TYPE - org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalPropertiesKey
Type of actuator for attitude control.
ATT_BASIS - org.orekit.files.ccsds.ndm.adm.acm.AttitudeStateHistoryMetadataKey
Basis of this attitude state time history data.
ATT_BASIS_ID - org.orekit.files.ccsds.ndm.adm.acm.AttitudeStateHistoryMetadataKey
Identification number of the attitude determination or simulation upon which this attitude is based.
ATT_CONTROL - org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalPropertiesKey
Accuracy of attitude control.
ATT_CONTROL_MODE - org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalPropertiesKey
Attitude control mode.
ATT_ID - org.orekit.files.ccsds.ndm.adm.acm.AttitudeStateHistoryMetadataKey
Attitude identification number.
ATT_KNOWLEDGE - org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalPropertiesKey
Accuracy of attitude knowledge.
ATT_LINE - Static variable in class org.orekit.files.ccsds.ndm.adm.acm.Acm
Attitude line element for XML messages.
ATT_POINTING - org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalPropertiesKey
Overall accuracy of spacecraft to maintain attitude.
ATT_PREV_ID - org.orekit.files.ccsds.ndm.adm.acm.AttitudeStateHistoryMetadataKey
Identification number of previous attitude.
ATT_TYPE - org.orekit.files.ccsds.ndm.adm.acm.AttitudeStateHistoryMetadataKey
Attitude element set type.
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.
ATTEMPT_TO_GENERATE_MALFORMED_FILE - org.orekit.errors.OrekitMessages
ATTEMPT_TO_GENERATE_MALFORMED_FILE.
Attitude - Class in org.orekit.attitudes
This class handles attitude definition at a given date.
Attitude(Frame, TimeStampedAngularCoordinates) - Constructor for class org.orekit.attitudes.Attitude
Creates a new instance.
Attitude(AbsoluteDate, Frame, Rotation, Vector3D, Vector3D) - Constructor for class org.orekit.attitudes.Attitude
Creates a new instance.
Attitude(AbsoluteDate, Frame, AngularCoordinates) - Constructor for class org.orekit.attitudes.Attitude
Creates a new instance.
ATTITUDE_DIR - org.orekit.files.ccsds.ndm.adm.aem.AemMetadataKey
Rotation direction entry.
ATTITUDE_POINTING_LAW_DOES_NOT_POINT_TO_GROUND - org.orekit.errors.OrekitMessages
ATTITUDE_POINTING_LAW_DOES_NOT_POINT_TO_GROUND.
ATTITUDE_SOURCE - org.orekit.files.ccsds.ndm.adm.acm.AttitudeDeterminationKey
Source of attitude estimate.
ATTITUDE_STATES - org.orekit.files.ccsds.ndm.adm.acm.AttitudeDeterminationKey
Attitude states.
ATTITUDE_TYPE - org.orekit.files.ccsds.ndm.adm.aem.AemMetadataKey
Format of the data line entry.
AttitudeBuilder - Interface in org.orekit.attitudes
This interface represents a builder for attitude.
AttitudeCovariance - Class in org.orekit.files.ccsds.ndm.adm.acm
Covariance entry.
AttitudeCovariance(AttitudeCovarianceType, AbsoluteDate, String[], int) - Constructor for class org.orekit.files.ccsds.ndm.adm.acm.AttitudeCovariance
Simple constructor.
AttitudeCovarianceHistory - Class in org.orekit.files.ccsds.ndm.adm.acm
Covariance history.
AttitudeCovarianceHistory(AttitudeCovarianceHistoryMetadata, List<AttitudeCovariance>) - Constructor for class org.orekit.files.ccsds.ndm.adm.acm.AttitudeCovarianceHistory
Simple constructor.
AttitudeCovarianceHistoryMetadata - Class in org.orekit.files.ccsds.ndm.adm.acm
Metadata for covariance history.
AttitudeCovarianceHistoryMetadata() - Constructor for class org.orekit.files.ccsds.ndm.adm.acm.AttitudeCovarianceHistoryMetadata
Empty constructor.
AttitudeCovarianceHistoryMetadataKey - Enum in org.orekit.files.ccsds.ndm.adm.acm
AttitudeCovarianceType - Enum in org.orekit.files.ccsds.ndm.adm.acm
Attitude covariance set type used in CCSDS Attitude Comprehensive Messages.
AttitudeDetermination - Class in org.orekit.files.ccsds.ndm.adm.acm
Attitude determination data.
AttitudeDetermination() - Constructor for class org.orekit.files.ccsds.ndm.adm.acm.AttitudeDetermination
Simple constructor.
AttitudeDeterminationKey - Enum in org.orekit.files.ccsds.ndm.adm.acm
Keys for attitude determination data entries.
AttitudeDeterminationSensor - Class in org.orekit.files.ccsds.ndm.adm.acm
Attitude determination sensor data.
AttitudeDeterminationSensor() - Constructor for class org.orekit.files.ccsds.ndm.adm.acm.AttitudeDeterminationSensor
Simple constructor.
AttitudeDeterminationSensorKey - Enum in org.orekit.files.ccsds.ndm.adm.acm
Keys for attitude determination data sensor entries.
AttitudeElementsType - Enum in org.orekit.files.ccsds.ndm.adm.acm
Attitude element set type used in CCSDS Attitude Comprehensive Messages.
AttitudeEndpoints - Class in org.orekit.files.ccsds.ndm.adm
Endpoints for attitude definition.
AttitudeEndpoints() - Constructor for class org.orekit.files.ccsds.ndm.adm.AttitudeEndpoints
Empty constructor.
AttitudeEntryKey - Enum in org.orekit.files.ccsds.ndm.adm.aem
Keys for attitude entries in XML messages.
AttitudeEphemerisFile<C extends TimeStampedAngularCoordinates,​S extends AttitudeEphemerisFile.AttitudeEphemerisSegment<C>> - Interface in org.orekit.files.general
An interface for accessing the data stored in an attitude ephemeris file.
AttitudeEphemerisFile.AttitudeEphemerisSegment<C extends TimeStampedAngularCoordinates> - Interface in org.orekit.files.general
A segment of an attitude ephemeris for a satellite.
AttitudeEphemerisFile.SatelliteAttitudeEphemeris<C extends TimeStampedAngularCoordinates,​S extends AttitudeEphemerisFile.AttitudeEphemerisSegment<C>> - Interface in org.orekit.files.general
Contains the information about a single satellite from an AttitudeEphemerisFile.
AttitudeEphemerisFileParser<T extends AttitudeEphemerisFile<?,​?>> - Interface in org.orekit.files.general
Parse an ephemeris file.
AttitudeEphemerisFileWriter - Interface in org.orekit.files.general
An interface for writing out ephemeris files to disk.
AttitudeInterpolator - Class in org.orekit.attitudes
Class for attitude interpolation.
AttitudeInterpolator(Frame, TimeInterpolator<TimeStampedAngularCoordinates>) - Constructor for class org.orekit.attitudes.AttitudeInterpolator
Constructor.
AttitudeManeuver - Class in org.orekit.files.ccsds.ndm.adm.acm
Maneuver entry.
AttitudeManeuver() - Constructor for class org.orekit.files.ccsds.ndm.adm.acm.AttitudeManeuver
Build an uninitialized maneuver.
AttitudeManeuverKey - Enum in org.orekit.files.ccsds.ndm.adm.acm
Keys for attitude maneuver entries.
AttitudePhysicalProperties - Class in org.orekit.files.ccsds.ndm.adm.acm
Spacecraft physical properties.
AttitudePhysicalProperties(AbsoluteDate) - Constructor for class org.orekit.files.ccsds.ndm.adm.acm.AttitudePhysicalProperties
Simple constructor.
AttitudePhysicalPropertiesKey - Enum in org.orekit.files.ccsds.ndm.adm.acm
Keys for physical properties data entries.
attitudeProvider(AttitudeProvider) - Method in class org.orekit.propagation.analytical.gnss.GLONASSAnalyticalPropagatorBuilder
Sets the attitude provider.
attitudeProvider(AttitudeProvider) - Method in class org.orekit.propagation.analytical.gnss.GNSSPropagatorBuilder
Sets the attitude provider.
attitudeProvider(AttitudeProvider) - Method in class org.orekit.propagation.analytical.gnss.SBASPropagatorBuilder
Sets the attitude provider.
attitudeProvider(AttitudeProvider) - Method in class org.orekit.propagation.numerical.GLONASSNumericalPropagatorBuilder
Sets the attitude provider.
AttitudeProvider - Interface in org.orekit.attitudes
This interface represents an attitude provider model set.
AttitudeProviderModifier - Interface in org.orekit.attitudes
This interface represents an attitude provider that modifies/wraps another underlying provider.
AttitudesSequence - Class in org.orekit.attitudes
This classes manages a sequence of different attitude providers that are activated in turn according to switching events.
AttitudesSequence() - Constructor for class org.orekit.attitudes.AttitudesSequence
Constructor for an initially empty sequence.
AttitudesSequence.SwitchHandler - Interface in org.orekit.attitudes
Interface for attitude switch notifications.
AttitudeState - Class in org.orekit.files.ccsds.ndm.adm.acm
Attitude state entry.
AttitudeState(AttitudeElementsType, RateElementsType, AbsoluteDate, String[], int) - Constructor for class org.orekit.files.ccsds.ndm.adm.acm.AttitudeState
Simple constructor.
AttitudeStateHistory - Class in org.orekit.files.ccsds.ndm.adm.acm
Attitude state history.
AttitudeStateHistory(AttitudeStateHistoryMetadata, List<AttitudeState>) - Constructor for class org.orekit.files.ccsds.ndm.adm.acm.AttitudeStateHistory
Simple constructor.
AttitudeStateHistoryMetadata - Class in org.orekit.files.ccsds.ndm.adm.acm
Metadata for attitude state history.
AttitudeStateHistoryMetadata() - Constructor for class org.orekit.files.ccsds.ndm.adm.acm.AttitudeStateHistoryMetadata
Simple constructor.
AttitudeStateHistoryMetadataKey - Enum in org.orekit.files.ccsds.ndm.adm.acm
AttitudeType - Enum in org.orekit.files.ccsds.ndm.adm
Enumerate for ADM attitude type.
AttitudeWriter - Class in org.orekit.files.ccsds.ndm.adm.aem
An AttitudeEphemerisFileWriter generating AEM files.
AttitudeWriter(AemWriter, AdmHeader, AemMetadata, FileFormat, String, double, int) - Constructor for class org.orekit.files.ccsds.ndm.adm.aem.AttitudeWriter
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.
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.AbstractBodyAttraction
Suffix for parameter name for attraction coefficient enabling Jacobian processing.
ATTRACTION_COEFFICIENT_SUFFIX - Static variable in class org.orekit.forces.gravity.DeSitterRelativity
Suffix for parameter name for attraction coefficient enabling Jacobian processing.
AUGUST - org.orekit.time.Month
August.
Authentication - Enum in org.orekit.gnss.metric.ntrip
Enumerate for authentication method in DataStreamRecord.
AuxiliaryElements - Class in org.orekit.propagation.semianalytical.dsst.utilities
Container class for common parameters used by all DSST forces.
AuxiliaryElements(Orbit, int) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.AuxiliaryElements
Simple constructor.
AVERAGE - org.orekit.models.earth.atmosphere.data.MarshallSolarActivityFutureEstimation.StrengthLevel
Average level of activity.
AveragedCircularWithMeanAngle - Class in org.orekit.propagation.conversion.averaging.elements
Immutable class containing values of averaged circular elements from any applicable theory (with MEAN as PositionAngleType).
AveragedCircularWithMeanAngle(double, double, double, double, double, double) - Constructor for class org.orekit.propagation.conversion.averaging.elements.AveragedCircularWithMeanAngle
Constructor.
AveragedEquinoctialWithMeanAngle - Class in org.orekit.propagation.conversion.averaging.elements
Immutable class containing values of averaged equinoctial elements from any applicable theory (with MEAN as PositionAngleType).
AveragedEquinoctialWithMeanAngle(double, double, double, double, double, double) - Constructor for class org.orekit.propagation.conversion.averaging.elements.AveragedEquinoctialWithMeanAngle
Constructor.
AveragedKeplerianWithMeanAngle - Class in org.orekit.propagation.conversion.averaging.elements
Immutable class containing values of averaged Keplerian elements from any applicable theory (with MEAN as PositionAngleType).
AveragedKeplerianWithMeanAngle(double, double, double, double, double, double) - Constructor for class org.orekit.propagation.conversion.averaging.elements.AveragedKeplerianWithMeanAngle
Constructor.
AveragedOrbitalElements - Interface in org.orekit.propagation.conversion.averaging.elements
Interface for storing averaged orbital elements.
AveragedOrbitalState - Interface in org.orekit.propagation.conversion.averaging
Interface representing averaged orbital elements at a specific instant.
AVG_MANEUVER_FREQ - org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalPropertiesKey
Average number of orbit or attitude maneuvers per year.
AZEL - org.orekit.files.ccsds.ndm.tdm.AngleType
Azimuth, elevation.
AzimuthalGradientCoefficients - Class in org.orekit.models.earth.troposphere
Container for the azimuthal gradient coefficients gnh, geh, gnw and gew.
AzimuthalGradientCoefficients(double, double, double, double) - Constructor for class org.orekit.models.earth.troposphere.AzimuthalGradientCoefficients
Simple constructor.
AzimuthalGradientProvider - Interface in org.orekit.models.earth.troposphere
azimuthBetweenPoints(FieldGeodeticPoint<T>, FieldGeodeticPoint<T>) - Method in class org.orekit.bodies.OneAxisEllipsoid
Compute the azimuth angle from local north between the two points.
azimuthBetweenPoints(GeodeticPoint, GeodeticPoint) - Method in class org.orekit.bodies.OneAxisEllipsoid
Compute the azimuth angle from local north between the two points.

B

B - org.orekit.gnss.SignalCode
Galileo B I/NAV and B C/NAV / IRNSS B RS / GLONASS L1OCp and LO2Cp codes.
B_STAR - Static variable in class org.orekit.propagation.analytical.tle.FieldTLE
Parameter name for B* coefficient.
B_STAR - Static variable in class org.orekit.propagation.analytical.tle.TLE
Parameter name for B* coefficient.
B01 - org.orekit.gnss.Frequency
Beidou B1 (1561.098 MHz).
B02 - org.orekit.gnss.Frequency
Beidou B2 (1207.14 MHz).
B03 - org.orekit.gnss.Frequency
Beidou B3 (1268.52 MHz).
B08 - org.orekit.gnss.Frequency
Beidou B2 (B2a + B2b) (1191.795MHz).
B1A - org.orekit.gnss.Frequency
Beidou B1A (1575.42 MHz).
B1C - org.orekit.gnss.Frequency
Beidou B1C (1575.42 MHz).
B2A - org.orekit.gnss.Frequency
Beidou B2a (1176.45 MHz).
B2A - Static variable in class org.orekit.files.ccsds.ndm.adm.AttitudeEndpoints
Constant for A ← B direction.
B2B - org.orekit.gnss.Frequency
Beidou B2b (1207.14 MHz).
B3A - org.orekit.gnss.Frequency
Beidou B3A (1268.52 MHz).
BACKUP - org.orekit.files.ccsds.ndm.odm.ocm.OpsStatus
Backup object.
BAR - Static variable in class org.orekit.utils.units.Unit
Bar unit.
BaseConfiguration() - Constructor for class org.orekit.files.ilrs.CRDConfiguration.BaseConfiguration
Empty constructor.
BaseRangeIonosphericDelayModifier - Class in org.orekit.estimation.measurements.modifiers
Base class modifying theoretical range measurement with ionospheric delay.
BaseRangeIonosphericDelayModifier(IonosphericModel, double) - Constructor for class org.orekit.estimation.measurements.modifiers.BaseRangeIonosphericDelayModifier
Constructor.
BaseRangeRateIonosphericDelayModifier - Class in org.orekit.estimation.measurements.modifiers
Base class modifying theoretical range-rate measurement with ionospheric delay.
BaseRangeRateIonosphericDelayModifier(IonosphericModel, double) - Constructor for class org.orekit.estimation.measurements.modifiers.BaseRangeRateIonosphericDelayModifier
Constructor.
BaseRangeRateTroposphericDelayModifier - Class in org.orekit.estimation.measurements.modifiers
Baselass modifying theoretical range-rate measurements with tropospheric delay.
BaseRangeRateTroposphericDelayModifier(DiscreteTroposphericModel) - Constructor for class org.orekit.estimation.measurements.modifiers.BaseRangeRateTroposphericDelayModifier
BaseRangeRateTroposphericDelayModifier(TroposphericModel) - Constructor for class org.orekit.estimation.measurements.modifiers.BaseRangeRateTroposphericDelayModifier
Constructor.
BaseRangeTroposphericDelayModifier - Class in org.orekit.estimation.measurements.modifiers
Base class modifying theoretical range measurements with tropospheric delay.
BaseRangeTroposphericDelayModifier(DiscreteTroposphericModel) - Constructor for class org.orekit.estimation.measurements.modifiers.BaseRangeTroposphericDelayModifier
Deprecated.
BaseRangeTroposphericDelayModifier(TroposphericModel) - Constructor for class org.orekit.estimation.measurements.modifiers.BaseRangeTroposphericDelayModifier
Constructor.
BASIC - org.orekit.gnss.metric.ntrip.Authentication
Basic.
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.
BasicConstantThrustPropulsionModel(double, double, Vector3D, Control3DVectorCostType, String) - Constructor for class org.orekit.forces.maneuvers.propulsion.BasicConstantThrustPropulsionModel
Generic 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
Propagate an orbit without any fancy features.
basicPropagate(AbsoluteDate) - Method in class org.orekit.propagation.integration.IntegratedEphemeris
Propagate an orbit without any fancy features.
basicPropagate(FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.analytical.FieldAbstractAnalyticalPropagator
Propagate an orbit without any fancy features.
basicPropagate(FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.integration.FieldIntegratedEphemeris
Propagate an orbit without any fancy features.
BATCH - org.orekit.files.ccsds.definitions.AdMethodType
Batch least squares.
BatchLSEstimator - Class in org.orekit.estimation.leastsquares
Least squares estimator for orbit determination.
BatchLSEstimator(LeastSquaresOptimizer, PropagatorBuilder...) - Constructor for class org.orekit.estimation.leastsquares.BatchLSEstimator
Simple constructor.
BatchLSModel - Class in org.orekit.estimation.leastsquares
BatchLSModel(PropagatorBuilder[], 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.
BCT - org.orekit.files.sp3.SP3OrbitType
broadcast.
BDS - org.orekit.files.rinex.navigation.IonosphericCorrectionType
Beidou α/β.
BDS - org.orekit.gnss.metric.ntrip.NavigationSystem
Beidou.
BDSBAS - org.orekit.files.rinex.navigation.SbasId
BeiDou Satellite-based Augmentation System.
BDT - org.orekit.gnss.ObservationTimeScale
Beidou time scale.
BDTScale - Class in org.orekit.time
Beidou system time scale.
beforeIntegration(FieldSpacecraftState<T>, FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.integration.FieldAbstractIntegratedPropagator
Method called just before integration.
beforeIntegration(FieldSpacecraftState<T>, FieldAbsoluteDate<T>) - Method in class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator
Method called just before integration.
beforeIntegration(SpacecraftState, AbsoluteDate) - Method in class org.orekit.propagation.integration.AbstractIntegratedPropagator
Method called just before integration.
beforeIntegration(SpacecraftState, AbsoluteDate) - Method in class org.orekit.propagation.numerical.NumericalPropagator
Method called just before integration.
beforeIntegration(SpacecraftState, AbsoluteDate) - Method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator
Method called just before integration.
BEIDOU - org.orekit.gnss.SatelliteSystem
Beidou system.
BEIDOU - org.orekit.gnss.TimeSystem
Beidou.
BEIDOU_2G - org.orekit.gnss.antenna.SatelliteType
BeiDou-2 GEO.
BEIDOU_2I - org.orekit.gnss.antenna.SatelliteType
BeiDou-2 IGSO.
BEIDOU_2M - org.orekit.gnss.antenna.SatelliteType
BeiDou-2 MEO.
BEIDOU_3G_CAST - org.orekit.gnss.antenna.SatelliteType
BeiDou-3.
BEIDOU_3I - org.orekit.gnss.antenna.SatelliteType
BeiDou-3 IGSO.
BEIDOU_3M_CAST - org.orekit.gnss.antenna.SatelliteType
BeiDou-3.
BEIDOU_3M_SECM - org.orekit.gnss.antenna.SatelliteType
BeiDou-3.
BEIDOU_3SI_CAST - org.orekit.gnss.antenna.SatelliteType
BeiDou-3.
BEIDOU_3SI_SECM - org.orekit.gnss.antenna.SatelliteType
BeiDou-3.
BEIDOU_3SM_CAST - org.orekit.gnss.antenna.SatelliteType
BeiDou-3.
BEIDOU_AV - Static variable in interface org.orekit.propagation.analytical.gnss.data.GNSSConstants
Value of the earth's rotation rate in rad/s for Beidou user.
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.data.GNSSConstants
Earth's universal gravitational parameter for Beidou user in m³/s².
BEIDOU_WEEK_NB - Static variable in interface org.orekit.propagation.analytical.gnss.data.GNSSConstants
Number of weeks in the Beidou cycle.
BeidouAlmanac - Class in org.orekit.propagation.analytical.gnss.data
Class for BeiDou almanac.
BeidouAlmanac() - Constructor for class org.orekit.propagation.analytical.gnss.data.BeidouAlmanac
Build a new almanac.
BeidouCivilianNavigationMessage - Class in org.orekit.propagation.analytical.gnss.data
Container for data contained in a Beidou civilian navigation message.
BeidouCivilianNavigationMessage(Frequency) - Constructor for class org.orekit.propagation.analytical.gnss.data.BeidouCivilianNavigationMessage
Constructor.
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.
BeidouLegacyNavigationMessage - Class in org.orekit.propagation.analytical.gnss.data
Container for data contained in a BeiDou navigation message.
BeidouLegacyNavigationMessage() - Constructor for class org.orekit.propagation.analytical.gnss.data.BeidouLegacyNavigationMessage
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.
BeidouSatelliteType - Enum in org.orekit.propagation.analytical.gnss.data
Enumerate for Beidou satellite type.
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.FieldTLEPropagator
sqrt (1 - e2).
beta0 - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator
sqrt (1 - e2).
beta02 - Variable in class org.orekit.propagation.analytical.tle.FieldTLEPropagator
1 - e2.
beta02 - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator
1 - e2.
BetaAngleDetector - Class in org.orekit.propagation.events
Finder for beta angle crossing events.
BetaAngleDetector(double) - Constructor for class org.orekit.propagation.events.BetaAngleDetector
Solar beta angle constructor.
BetaAngleDetector(double, PVCoordinatesProvider, Frame) - Constructor for class org.orekit.propagation.events.BetaAngleDetector
Class constructor.
BetaAngleDetector(AdaptableInterval, double, int, EventHandler, double, PVCoordinatesProvider, Frame) - Constructor for class org.orekit.propagation.events.BetaAngleDetector
Protected constructor with full parameters.
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.
BIG_TRUNCATION_TOLERANCE - Static variable in class org.orekit.propagation.semianalytical.dsst.forces.DSSTThirdBody
Truncation tolerance for big, eccentric orbits.
BINEX - org.orekit.gnss.metric.ntrip.DataFormat
BINEX.
BistaticRange - Class in org.orekit.estimation.measurements
Class modeling a bistatic range measurement using an emitter ground station and a receiver ground station.
BistaticRange(GroundStation, GroundStation, AbsoluteDate, double, double, double, ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.BistaticRange
Simple constructor.
BistaticRangeBuilder - Class in org.orekit.estimation.measurements.generation
Builder for BistaticRange measurements.
BistaticRangeBuilder(CorrelatedRandomVectorGenerator, GroundStation, GroundStation, double, double, ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.generation.BistaticRangeBuilder
Simple constructor.
BistaticRangeIonosphericDelayModifier - Class in org.orekit.estimation.measurements.modifiers
Class modifying theoretical bistatic range measurement with ionospheric delay.
BistaticRangeIonosphericDelayModifier(IonosphericModel, double) - Constructor for class org.orekit.estimation.measurements.modifiers.BistaticRangeIonosphericDelayModifier
Constructor.
BistaticRangeRate - Class in org.orekit.estimation.measurements
Class modeling a bistatic range rate measurement using an emitter ground station and a receiver ground station.
BistaticRangeRate(GroundStation, GroundStation, AbsoluteDate, double, double, double, ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.BistaticRangeRate
Simple constructor.
BistaticRangeRateBuilder - Class in org.orekit.estimation.measurements.generation
Builder for BistaticRangeRate measurements.
BistaticRangeRateBuilder(CorrelatedRandomVectorGenerator, GroundStation, GroundStation, double, double, ObservableSatellite) - Constructor for class org.orekit.estimation.measurements.generation.BistaticRangeRateBuilder
Simple constructor.
BistaticRangeRateIonosphericDelayModifier - Class in org.orekit.estimation.measurements.modifiers
Class modifying theoretical bistatic range-rate measurement with ionospheric delay.
BistaticRangeRateIonosphericDelayModifier(IonosphericModel, double) - Constructor for class org.orekit.estimation.measurements.modifiers.BistaticRangeRateIonosphericDelayModifier
Constructor.
BistaticRangeRateTroposphericDelayModifier - Class in org.orekit.estimation.measurements.modifiers
Class modifying theoretical bistatic range-rate measurements with tropospheric delay.
BistaticRangeRateTroposphericDelayModifier(DiscreteTroposphericModel) - Constructor for class org.orekit.estimation.measurements.modifiers.BistaticRangeRateTroposphericDelayModifier
BistaticRangeRateTroposphericDelayModifier(TroposphericModel) - Constructor for class org.orekit.estimation.measurements.modifiers.BistaticRangeRateTroposphericDelayModifier
Constructor.
BistaticRangeTroposphericDelayModifier - Class in org.orekit.estimation.measurements.modifiers
Class modifying theoretical bistatic range measurement with tropospheric delay.
BistaticRangeTroposphericDelayModifier(DiscreteTroposphericModel) - Constructor for class org.orekit.estimation.measurements.modifiers.BistaticRangeTroposphericDelayModifier
BistaticRangeTroposphericDelayModifier(TroposphericModel) - Constructor for class org.orekit.estimation.measurements.modifiers.BistaticRangeTroposphericDelayModifier
Constructor.
BIT_1 - org.orekit.gnss.metric.parser.DataType
1 bit.
BIT_10 - org.orekit.gnss.metric.parser.DataType
10 bits.
BIT_12 - org.orekit.gnss.metric.parser.DataType
12 bits.
BIT_2 - org.orekit.gnss.metric.parser.DataType
2 bits.
BIT_24 - org.orekit.gnss.metric.parser.DataType
24 bits.
BIT_3 - org.orekit.gnss.metric.parser.DataType
3 bits.
BIT_32 - org.orekit.gnss.metric.parser.DataType
32 bits.
BIT_4 - org.orekit.gnss.metric.parser.DataType
4 bits.
BIT_6 - org.orekit.gnss.metric.parser.DataType
6 bits.
BIT_7 - org.orekit.gnss.metric.parser.DataType
7 bits.
BIT_8 - org.orekit.gnss.metric.parser.DataType
8 bits.
blendArithmeticallyWith(FieldPVCoordinates<T>, T) - Method in class org.orekit.utils.FieldPVCoordinates
blendArithmeticallyWith(PVCoordinates, double) - Method in class org.orekit.utils.PVCoordinates
BLOCK_I - org.orekit.gnss.antenna.SatelliteType
GPS Block I : SVN 01-11.
BLOCK_II - org.orekit.gnss.antenna.SatelliteType
GPS Block II : SVN 13-21.
BLOCK_IIA - org.orekit.gnss.antenna.SatelliteType
GPS Block IIA : SVN 22-40.
BLOCK_IIF - org.orekit.gnss.antenna.SatelliteType
GPS Block IIF : SVN 62-73.
BLOCK_IIIA - org.orekit.gnss.antenna.SatelliteType
GPS Block IIIA : SVN 74-81.
BLOCK_IIR_A - org.orekit.gnss.antenna.SatelliteType
GPS Block IIR : SVN 41, 43-46, 51, 54, 56.
BLOCK_IIR_B - org.orekit.gnss.antenna.SatelliteType
GPS Block IIR : SVN 47, 59-61.
BLOCK_IIR_M - org.orekit.gnss.antenna.SatelliteType
GPS Block IIR-M : SVN 48-50, 52-53, 55, 57-58.
BlockWriter() - Constructor for class org.orekit.files.ccsds.ndm.odm.ocm.StreamingOcmWriter.BlockWriter
Empty 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.
body - org.orekit.files.ccsds.section.XmlStructureKey
Body structure.
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.
BodyFacade - Class in org.orekit.files.ccsds.definitions
Facade in front of several center bodies in CCSDS messages.
BodyFacade(String, CelestialBody) - Constructor for class org.orekit.files.ccsds.definitions.BodyFacade
Simple constructor.
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.
BooleanDetector(List<EventDetector>, BooleanDetector.Operator, AdaptableInterval, double, int, EventHandler) - Constructor for class org.orekit.propagation.events.BooleanDetector
Private constructor with all the parameters.
booleanValue(EncodedMessage) - Method in interface org.orekit.gnss.metric.parser.DataField
Get the value of the field as a boolean.
BoundedAttitudeProvider - Interface in org.orekit.attitudes
This interface is intended for attitude ephemerides valid only during a time range.
BoundedPropagator - Interface in org.orekit.propagation
This interface is intended for ephemerides valid only during a time range.
BOX - org.orekit.files.ccsds.ndm.cdm.ScreenVolumeShape
Box.
BoxAndSolarArraySpacecraft - Class in org.orekit.forces
Class representing the features of a classical satellite with a convex body shape.
BoxAndSolarArraySpacecraft(double, double, double, ExtendedPVCoordinatesProvider, double, Vector3D, double, double, double, double) - Constructor for class org.orekit.forces.BoxAndSolarArraySpacecraft
Build a spacecraft model with best lighting of solar array.
BoxAndSolarArraySpacecraft(List<Panel>) - Constructor for class org.orekit.forces.BoxAndSolarArraySpacecraft
Build a spacecraft model.
BrouwerLyddaneOrbitalState - Class in org.orekit.propagation.conversion.averaging
Class representing an averaged orbital state as in the Brouwer-Lyddane theory.
BrouwerLyddaneOrbitalState(AbsoluteDate, AveragedKeplerianWithMeanAngle, Frame, UnnormalizedSphericalHarmonicsProvider) - Constructor for class org.orekit.propagation.conversion.averaging.BrouwerLyddaneOrbitalState
Constructor.
BrouwerLyddanePropagator - Class in org.orekit.propagation.analytical
This class propagates a SpacecraftState using the analytical Brouwer-Lyddane model (from J2 to J5 zonal harmonics).
BrouwerLyddanePropagator(Orbit, double, double, double, double, double, double, double) - Constructor for class org.orekit.propagation.analytical.BrouwerLyddanePropagator
Build a propagator from orbit and potential.
BrouwerLyddanePropagator(Orbit, double, double, double, double, double, double, double, double) - Constructor for class org.orekit.propagation.analytical.BrouwerLyddanePropagator
Build a propagator from orbit, mass and potential.
BrouwerLyddanePropagator(Orbit, double, UnnormalizedSphericalHarmonicsProvider, double) - Constructor for class org.orekit.propagation.analytical.BrouwerLyddanePropagator
Build a propagator from orbit, mass and potential provider.
BrouwerLyddanePropagator(Orbit, AttitudeProvider, double, double, double, double, double, double, double) - Constructor for class org.orekit.propagation.analytical.BrouwerLyddanePropagator
Build a propagator from orbit, attitude provider and potential.
BrouwerLyddanePropagator(Orbit, AttitudeProvider, double, double, double, double, double, double, double, double) - Constructor for class org.orekit.propagation.analytical.BrouwerLyddanePropagator
Build a propagator from orbit, attitude provider, mass and potential.
BrouwerLyddanePropagator(Orbit, AttitudeProvider, double, double, double, double, double, double, double, PropagationType, double) - Constructor for class org.orekit.propagation.analytical.BrouwerLyddanePropagator
Build a propagator from orbit, attitude provider, mass and potential.
BrouwerLyddanePropagator(Orbit, AttitudeProvider, double, double, double, double, double, double, double, PropagationType, double, double, int) - Constructor for class org.orekit.propagation.analytical.BrouwerLyddanePropagator
Build a propagator from orbit, attitude provider, mass and potential.
BrouwerLyddanePropagator(Orbit, AttitudeProvider, double, UnnormalizedSphericalHarmonicsProvider, double) - Constructor for class org.orekit.propagation.analytical.BrouwerLyddanePropagator
Build a propagator from orbit, attitude provider, mass and potential provider.
BrouwerLyddanePropagator(Orbit, AttitudeProvider, double, UnnormalizedSphericalHarmonicsProvider, UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics, double) - Constructor for class org.orekit.propagation.analytical.BrouwerLyddanePropagator
Private helper constructor.
BrouwerLyddanePropagator(Orbit, AttitudeProvider, double, UnnormalizedSphericalHarmonicsProvider, UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics, PropagationType, double) - Constructor for class org.orekit.propagation.analytical.BrouwerLyddanePropagator
Private helper constructor.
BrouwerLyddanePropagator(Orbit, AttitudeProvider, double, UnnormalizedSphericalHarmonicsProvider, PropagationType, double) - Constructor for class org.orekit.propagation.analytical.BrouwerLyddanePropagator
Build a propagator from orbit, attitude provider, mass and potential provider.
BrouwerLyddanePropagator(Orbit, AttitudeProvider, UnnormalizedSphericalHarmonicsProvider, double) - Constructor for class org.orekit.propagation.analytical.BrouwerLyddanePropagator
Build a propagator from orbit, attitude provider and potential provider.
BrouwerLyddanePropagator(Orbit, UnnormalizedSphericalHarmonicsProvider, double) - Constructor for class org.orekit.propagation.analytical.BrouwerLyddanePropagator
Build a propagator from orbit and potential provider.
BrouwerLyddanePropagator(Orbit, UnnormalizedSphericalHarmonicsProvider, PropagationType, double) - Constructor for class org.orekit.propagation.analytical.BrouwerLyddanePropagator
Build a propagator from orbit and potential provider.
BrouwerLyddanePropagatorBuilder - Class in org.orekit.propagation.conversion
Builder for Brouwer-Lyddane propagator.
BrouwerLyddanePropagatorBuilder(Orbit, double, double, TideSystem, double, double, double, double, OrbitType, PositionAngleType, double, double) - Constructor for class org.orekit.propagation.conversion.BrouwerLyddanePropagatorBuilder
Build a new instance.
BrouwerLyddanePropagatorBuilder(Orbit, UnnormalizedSphericalHarmonicsProvider, PositionAngleType, double, double) - Constructor for class org.orekit.propagation.conversion.BrouwerLyddanePropagatorBuilder
Build a new instance.
BrouwerLyddanePropagatorBuilder(Orbit, UnnormalizedSphericalHarmonicsProvider, PositionAngleType, double, AttitudeProvider, double) - Constructor for class org.orekit.propagation.conversion.BrouwerLyddanePropagatorBuilder
Build a new instance.
BSTAR - org.orekit.files.ccsds.ndm.odm.omm.OmmTleKey
SGP/SGP4 drag-like coefficient.
BTERM - org.orekit.files.ccsds.ndm.odm.omm.OmmTleKey
SGP4-XP drag-like coefficient.
build() - Method in class org.orekit.estimation.sequential.KalmanEstimatorBuilder
Construct a KalmanEstimator from the data in this builder.
build() - Method in class org.orekit.estimation.sequential.SemiAnalyticalKalmanEstimatorBuilder
Construct a KalmanEstimator from the data in this builder.
build() - Method in class org.orekit.estimation.sequential.SemiAnalyticalUnscentedKalmanEstimatorBuilder
Construct a SemiAnalyticalUnscentedKalmanEstimator from the data in this builder.
build() - Method in class org.orekit.estimation.sequential.UnscentedKalmanEstimatorBuilder
Construct a UnscentedKalmanEstimator from the data in this builder.
build() - Method in class org.orekit.files.ccsds.ndm.adm.acm.AcmParser
Build the file from parsed entries.
build() - Method in class org.orekit.files.ccsds.ndm.adm.aem.AemParser
Build the file from parsed entries.
build() - Method in class org.orekit.files.ccsds.ndm.adm.apm.ApmParser
Build the file from parsed entries.
build() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmParser
Build the file from parsed entries.
build() - Method in class org.orekit.files.ccsds.ndm.NdmParser
Build the file from parsed entries.
build() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmParser
Build the file from parsed entries.
build() - Method in class org.orekit.files.ccsds.ndm.odm.oem.OemParser
Build the file from parsed entries.
build() - Method in class org.orekit.files.ccsds.ndm.odm.omm.OmmParser
Build the file from parsed entries.
build() - Method in class org.orekit.files.ccsds.ndm.odm.opm.OpmParser
Build the file from parsed entries.
build() - Method in class org.orekit.files.ccsds.ndm.tdm.TdmParser
Build the file from parsed entries.
build() - Method in interface org.orekit.files.ccsds.utils.lexical.MessageParser
Build the file from parsed entries.
build() - Method in class org.orekit.propagation.analytical.gnss.GLONASSAnalyticalPropagatorBuilder
Finalizes the build.
build() - Method in class org.orekit.propagation.analytical.gnss.GNSSPropagatorBuilder
Finalizes the build.
build() - Method in class org.orekit.propagation.analytical.gnss.SBASPropagatorBuilder
Finalizes the build.
build() - Method in class org.orekit.propagation.numerical.GLONASSNumericalPropagatorBuilder
Finalizes the build.
build() - Method in class org.orekit.utils.AggregatedPVCoordinatesProvider.Builder
Build the aggregated PVCoordinatesProvider.
build() - Method in class org.orekit.utils.WaypointPVBuilder
Build a PVCoordinatesProvider from the waypoints added to this builder.
build(boolean, boolean, RotationOrder, boolean, AbsoluteDate, double...) - Method in enum org.orekit.files.ccsds.ndm.adm.AttitudeType
Get the angular coordinates corresponding to the attitude data.
build(Frame, FieldPVCoordinatesProvider<T>, TimeStampedFieldAngularCoordinates<T>) - Method in interface org.orekit.attitudes.AttitudeBuilder
Build a filtered attitude.
build(Frame, FieldPVCoordinatesProvider<T>, TimeStampedFieldAngularCoordinates<T>) - Method in class org.orekit.attitudes.FixedFrameBuilder
Build a filtered attitude.
build(Frame, FieldPVCoordinatesProvider<T>, TimeStampedFieldAngularCoordinates<T>) - Method in class org.orekit.files.ccsds.ndm.adm.AttitudeEndpoints
Build a filtered attitude.
build(Frame, PVCoordinatesProvider, TimeStampedAngularCoordinates) - Method in interface org.orekit.attitudes.AttitudeBuilder
Build a filtered attitude.
build(Frame, PVCoordinatesProvider, TimeStampedAngularCoordinates) - Method in class org.orekit.attitudes.FixedFrameBuilder
Build a filtered attitude.
build(Frame, PVCoordinatesProvider, TimeStampedAngularCoordinates) - Method in class org.orekit.files.ccsds.ndm.adm.AttitudeEndpoints
Build a filtered attitude.
build(AbsoluteDate, Map<ObservableSatellite, OrekitStepInterpolator>) - Method in class org.orekit.estimation.measurements.generation.AngularAzElBuilder
Generate a single measurement.
build(AbsoluteDate, Map<ObservableSatellite, OrekitStepInterpolator>) - Method in class org.orekit.estimation.measurements.generation.AngularRaDecBuilder
Generate a single measurement.
build(AbsoluteDate, Map<ObservableSatellite, OrekitStepInterpolator>) - Method in class org.orekit.estimation.measurements.generation.BistaticRangeBuilder
Generate a single measurement.
build(AbsoluteDate, Map<ObservableSatellite, OrekitStepInterpolator>) - Method in class org.orekit.estimation.measurements.generation.BistaticRangeRateBuilder
Generate a single measurement.
build(AbsoluteDate, Map<ObservableSatellite, OrekitStepInterpolator>) - Method in class org.orekit.estimation.measurements.generation.FDOABuilder
Generate a single measurement.
build(AbsoluteDate, Map<ObservableSatellite, OrekitStepInterpolator>) - Method in class org.orekit.estimation.measurements.generation.InterSatellitesOneWayRangeRateBuilder
Generate a single measurement.
build(AbsoluteDate, Map<ObservableSatellite, OrekitStepInterpolator>) - Method in class org.orekit.estimation.measurements.generation.InterSatellitesPhaseBuilder
Generate a single measurement.
build(AbsoluteDate, Map<ObservableSatellite, OrekitStepInterpolator>) - Method in class org.orekit.estimation.measurements.generation.InterSatellitesRangeBuilder
Generate a single measurement.
build(AbsoluteDate, Map<ObservableSatellite, OrekitStepInterpolator>) - Method in interface org.orekit.estimation.measurements.generation.MeasurementBuilder
Generate a single measurement.
build(AbsoluteDate, Map<ObservableSatellite, OrekitStepInterpolator>) - Method in class org.orekit.estimation.measurements.generation.MultiplexedMeasurementBuilder
Generate a single measurement.
build(AbsoluteDate, Map<ObservableSatellite, OrekitStepInterpolator>) - Method in class org.orekit.estimation.measurements.generation.OneWayGNSSPhaseBuilder
Generate a single measurement.
build(AbsoluteDate, Map<ObservableSatellite, OrekitStepInterpolator>) - Method in class org.orekit.estimation.measurements.generation.OneWayGNSSRangeBuilder
Generate a single measurement.
build(AbsoluteDate, Map<ObservableSatellite, OrekitStepInterpolator>) - Method in class org.orekit.estimation.measurements.generation.OneWayGNSSRangeRateBuilder
Generate a single measurement.
build(AbsoluteDate, Map<ObservableSatellite, OrekitStepInterpolator>) - Method in class org.orekit.estimation.measurements.generation.PositionBuilder
Generate a single measurement.
build(AbsoluteDate, Map<ObservableSatellite, OrekitStepInterpolator>) - Method in class org.orekit.estimation.measurements.generation.PVBuilder
Generate a single measurement.
build(AbsoluteDate, Map<ObservableSatellite, OrekitStepInterpolator>) - Method in class org.orekit.estimation.measurements.generation.RangeBuilder
Generate a single measurement.
build(AbsoluteDate, Map<ObservableSatellite, OrekitStepInterpolator>) - Method in class org.orekit.estimation.measurements.generation.RangeRateBuilder
Generate a single measurement.
build(AbsoluteDate, Map<ObservableSatellite, OrekitStepInterpolator>) - Method in class org.orekit.estimation.measurements.generation.TDOABuilder
Generate a single measurement.
build(AbsoluteDate, Map<ObservableSatellite, OrekitStepInterpolator>) - Method in class org.orekit.estimation.measurements.generation.TurnAroundRangeBuilder
Generate a single measurement.
build(AbsoluteDate, Map<ObservableSatellite, OrekitStepInterpolator>) - Method in class org.orekit.estimation.measurements.gnss.PhaseBuilder
Generate a single measurement.
build(AbsoluteDate, SpacecraftState[]) - Method in interface org.orekit.estimation.measurements.generation.MeasurementBuilder
Generate a single measurement.
buildAcmParser() - Method in class org.orekit.files.ccsds.ndm.ParserBuilder
buildAcmWriter() - Method in class org.orekit.files.ccsds.ndm.WriterBuilder
buildAemParser() - Method in class org.orekit.files.ccsds.ndm.ParserBuilder
Build a parser for Attitude Ephemeris Messages.
buildAemWriter() - Method in class org.orekit.files.ccsds.ndm.WriterBuilder
Build a writer for Attitude Ephemeris Messages.
buildApmParser() - Method in class org.orekit.files.ccsds.ndm.ParserBuilder
Build a parser for Attitude Parameters Messages.
buildApmWriter() - Method in class org.orekit.files.ccsds.ndm.WriterBuilder
Build a writer for Attitude Parameters Messages.
buildAttitudeProvider(AbsoluteDate, AbsoluteDate, ExtendedPVCoordinatesProvider, Frame, int) - Method in enum org.orekit.gnss.antenna.SatelliteType
Build an attitude provider suitable for this satellite type.
buildBasicGradientSpacecraftState(SpacecraftState, int, AttitudeProvider) - Static method in class org.orekit.propagation.integration.AbstractGradientConverter
Process a state into a Gradient version without force model parameter.
buildBox(double, double, double, double, double, double, double) - Static method in class org.orekit.forces.BoxAndSolarArraySpacecraft
Build the panels of a simple parallelepipedic box.
buildCdmParser() - Method in class org.orekit.files.ccsds.ndm.ParserBuilder
Build a parser for Conjunction Data Messages.
buildCdmWriter() - Method in class org.orekit.files.ccsds.ndm.WriterBuilder
Build a writer for Conjunction Data Messages.
Builder() - Constructor for class org.orekit.utils.AggregatedPVCoordinatesProvider.Builder
Create a builder using the AggregatedPVCoordinatesProvider.InvalidPVProvider as the initial provider.
Builder(PVCoordinatesProvider) - Constructor for class org.orekit.utils.AggregatedPVCoordinatesProvider.Builder
Create a builder using the provided initial provider.
buildFlatArray(Flattener, double) - Static method in class org.orekit.forces.gravity.potential.PotentialCoefficientsReader
Build a coefficients array in flat form.
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(LOF, 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(Field<T>, Orbit, OrbitType) - Method in class org.orekit.propagation.conversion.AbstractFieldIntegratorBuilder
Build a first order integrator.
buildIntegrator(Field<T>, Orbit, OrbitType) - Method in class org.orekit.propagation.conversion.AbstractVariableStepFieldIntegratorBuilder
Build a first order integrator.
buildIntegrator(Field<T>, Orbit, OrbitType) - Method in class org.orekit.propagation.conversion.AdamsBashforthFieldIntegratorBuilder
Build a first order integrator.
buildIntegrator(Field<T>, Orbit, OrbitType) - Method in class org.orekit.propagation.conversion.AdamsMoultonFieldIntegratorBuilder
Build a first order integrator.
buildIntegrator(Field<T>, Orbit, OrbitType) - Method in class org.orekit.propagation.conversion.ClassicalRungeKuttaFieldIntegratorBuilder
Build a first order integrator.
buildIntegrator(Field<T>, Orbit, OrbitType) - Method in class org.orekit.propagation.conversion.DormandPrince54FieldIntegratorBuilder
Build a first order integrator.
buildIntegrator(Field<T>, Orbit, OrbitType) - Method in class org.orekit.propagation.conversion.DormandPrince853FieldIntegratorBuilder
Build a first order integrator.
buildIntegrator(Field<T>, Orbit, OrbitType) - Method in class org.orekit.propagation.conversion.EulerFieldIntegratorBuilder
Build a first order integrator.
buildIntegrator(Field<T>, Orbit, OrbitType) - Method in interface org.orekit.propagation.conversion.FieldODEIntegratorBuilder
Build a first order integrator.
buildIntegrator(Field<T>, Orbit, OrbitType) - Method in class org.orekit.propagation.conversion.GillFieldIntegratorBuilder
Build a first order integrator.
buildIntegrator(Field<T>, Orbit, OrbitType) - Method in class org.orekit.propagation.conversion.HighamHall54FieldIntegratorBuilder
Build a first order integrator.
buildIntegrator(Field<T>, Orbit, OrbitType) - Method in class org.orekit.propagation.conversion.LutherFieldIntegratorBuilder
Build a first order integrator.
buildIntegrator(Field<T>, Orbit, OrbitType) - Method in class org.orekit.propagation.conversion.MidpointFieldIntegratorBuilder
Build a first order integrator.
buildIntegrator(Field<T>, Orbit, OrbitType) - Method in class org.orekit.propagation.conversion.ThreeEighthesFieldIntegratorBuilder
Build a first order integrator.
buildIntegrator(FieldOrbit<T>, OrbitType) - Method in class org.orekit.propagation.conversion.AbstractFieldIntegratorBuilder
Build a first order integrator.
buildIntegrator(FieldOrbit<T>, OrbitType) - Method in interface org.orekit.propagation.conversion.FieldODEIntegratorBuilder
Build a first order integrator.
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.
buildLeastSquaresModel(PropagatorBuilder[], List<ObservedMeasurement<?>>, ParameterDriversList, ModelObserver) - Method in class org.orekit.propagation.conversion.BrouwerLyddanePropagatorBuilder
Build a new batch least squares model.
buildLeastSquaresModel(PropagatorBuilder[], List<ObservedMeasurement<?>>, ParameterDriversList, ModelObserver) - Method in class org.orekit.propagation.conversion.DSSTPropagatorBuilder
Build a new batch least squares model.
buildLeastSquaresModel(PropagatorBuilder[], List<ObservedMeasurement<?>>, ParameterDriversList, ModelObserver) - Method in class org.orekit.propagation.conversion.EcksteinHechlerPropagatorBuilder
Build a new batch least squares model.
buildLeastSquaresModel(PropagatorBuilder[], List<ObservedMeasurement<?>>, ParameterDriversList, ModelObserver) - Method in class org.orekit.propagation.conversion.EphemerisPropagatorBuilder
Build a new batch least squares model.
buildLeastSquaresModel(PropagatorBuilder[], List<ObservedMeasurement<?>>, ParameterDriversList, ModelObserver) - Method in class org.orekit.propagation.conversion.KeplerianPropagatorBuilder
Build a new batch least squares model.
buildLeastSquaresModel(PropagatorBuilder[], List<ObservedMeasurement<?>>, ParameterDriversList, ModelObserver) - Method in class org.orekit.propagation.conversion.NumericalPropagatorBuilder
Build a new batch least squares model.
buildLeastSquaresModel(PropagatorBuilder[], List<ObservedMeasurement<?>>, ParameterDriversList, ModelObserver) - Method in interface org.orekit.propagation.conversion.PropagatorBuilder
Build a new batch least squares model.
buildLeastSquaresModel(PropagatorBuilder[], List<ObservedMeasurement<?>>, ParameterDriversList, ModelObserver) - Method in class org.orekit.propagation.conversion.TLEPropagatorBuilder
Build a new batch least squares model.
buildNdmParser() - Method in class org.orekit.files.ccsds.ndm.ParserBuilder
Build a parser for Navigation Data Messages.
buildNdmWriter() - Method in class org.orekit.files.ccsds.ndm.WriterBuilder
Build a writer for Navigation Data Messages.
buildOcmParser() - Method in class org.orekit.files.ccsds.ndm.ParserBuilder
Build a parser for Orbit Comprehensive Messages.
buildOcmWriter() - Method in class org.orekit.files.ccsds.ndm.WriterBuilder
Build a writer for Orbit Comprehensive Messages.
buildOemParser() - Method in class org.orekit.files.ccsds.ndm.ParserBuilder
Build a parser for Orbit Ephemeris Messages.
buildOemWriter() - Method in class org.orekit.files.ccsds.ndm.WriterBuilder
Build a writer for Orbit Ephemeris Messages.
buildOmmParser() - Method in class org.orekit.files.ccsds.ndm.ParserBuilder
Build a parser for Orbit Mean elements Messages.
buildOmmWriter() - Method in class org.orekit.files.ccsds.ndm.WriterBuilder
Build a writer for Orbit Mean elements Messages.
buildOpmParser() - Method in class org.orekit.files.ccsds.ndm.ParserBuilder
Build a parser for Orbit Parameters Messages.
buildOpmWriter() - Method in class org.orekit.files.ccsds.ndm.WriterBuilder
Build a writer for Orbit Parameters Messages.
buildPanels(double, double, double, ExtendedPVCoordinatesProvider, double, Vector3D, double, double, double, double) - Static method in class org.orekit.forces.BoxAndSolarArraySpacecraft
Build the panels of a simple parallelepiped box plus one solar array panel.
buildPropagator() - Method in interface org.orekit.propagation.conversion.PropagatorBuilder
Build a propagator from current value of selected normalized parameters.
buildPropagator(double[]) - Method in class org.orekit.propagation.conversion.BrouwerLyddanePropagatorBuilder
Build a propagator.
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.EphemerisPropagatorBuilder
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.
buildReferenceSlot(O) - Method in class org.orekit.orbits.WalkerConstellation
Create the reference slot, which is satellite 0 in plane 0.
buildRegularSlots(O) - Method in class org.orekit.orbits.WalkerConstellation
Create the regular slots.
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).
buildSlot(WalkerConstellationSlot<O>, int, double) - Method in class org.orekit.orbits.WalkerConstellation
Create one offset slot from an already existing slot.
buildTdmParser() - Method in class org.orekit.files.ccsds.ndm.ParserBuilder
Build a parser for Tracking Data Messages.
buildTdmWriter() - Method in class org.orekit.files.ccsds.ndm.WriterBuilder
Build a writer for Tracking Data Messages.
buildTermsList(String) - Static method in class org.orekit.utils.units.Parser
Build the list of terms corresponding to a units specification.
buildTokens(boolean, boolean, String, String, Map<String, String>, int, String) - Method in class org.orekit.files.ccsds.ndm.adm.RotationXmlTokenBuilder
Create a list of parse tokens.
buildTokens(boolean, boolean, String, String, Map<String, String>, int, String) - Method in class org.orekit.files.ccsds.utils.lexical.MessageVersionXmlTokenBuilder
Create a list of parse tokens.
buildTokens(boolean, boolean, String, String, Map<String, String>, int, String) - Method in class org.orekit.files.ccsds.utils.lexical.RegularXmlTokenBuilder
Create a list of parse tokens.
buildTokens(boolean, boolean, String, String, Map<String, String>, int, String) - Method in class org.orekit.files.ccsds.utils.lexical.UserDefinedXmlTokenBuilder
Create a list of parse tokens.
buildTokens(boolean, boolean, String, String, Map<String, String>, int, String) - Method in interface org.orekit.files.ccsds.utils.lexical.XmlTokenBuilder
Create a list of parse tokens.
buildUncachedITRF(EOPHistory, UTCScale) - Static method in class org.orekit.frames.FramesFactory
Build an uncached International Terrestrial Reference Frame with specific EOP history.
buildUncachedITRF(UT1Scale) - Method in class org.orekit.frames.AbstractFrames
 
buildUncachedITRF(UT1Scale) - Method in interface org.orekit.frames.Frames
Build an uncached International Terrestrial Reference Frame with specific EOP history.
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.
BUS_MODEL - org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalPropertiesKey
Bus model name.
BWLS - org.orekit.files.ccsds.definitions.OdMethodType
Batch Weighted Least Squares.
ByteArrayEncodedMessage - Class in org.orekit.gnss.metric.parser
Encoded message as a byte array.
ByteArrayEncodedMessage(byte[]) - Constructor for class org.orekit.gnss.metric.parser.ByteArrayEncodedMessage
Simple constructor.

C

C - org.orekit.gnss.SignalCode
GPS C/A / GLONASS C/A / Galileo C / SBAS C/A / QZSS C/A / QZSS C/B / IRNSS C RS(P) codes.
C_2FASX4 - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants
C_2FASX4.
C_3FASX6 - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants
C_3FASX6.
C_FASX2 - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants
C_FASX2.
C_G22 - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants
C_G22.
C_G32 - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants
C_G32.
C_G44 - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants
C_G44.
C_G52 - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants
C_G52.
C_G54 - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants
C_G54.
C0 - org.orekit.gnss.ObservationType
Pseudorange for Rinex3.
C01 - org.orekit.gnss.Frequency
In the ANTEX files, both C01 and C02 refer to Beidou B1 signal (1561.098 MHz).
C02 - org.orekit.gnss.Frequency
In the ANTEX files, both C01 and C02 refer to Beidou B1 signal (1561.098 MHz).
C05 - org.orekit.gnss.Frequency
In the ANTEX files, C05 appears without much reference for consistency with Rinex 4 tables, we assume it is B2a (1176.45 MHz).
C06 - org.orekit.gnss.Frequency
In the ANTEX files, C06 appears without much reference, we assume it is B2 (1207.14 MHz).
C07 - org.orekit.gnss.Frequency
In the ANTEX files, C07 seems to refer to a signal close to E06, probably B3...
C08 - org.orekit.gnss.Frequency
In the ANTEX files, C08 appears without much reference for consistency with Rinex 4 tables, we assume it is B2 (B2a+B2b) (1191.795 MHz).
c1 - Variable in class org.orekit.propagation.analytical.tle.FieldTLEPropagator
C1 from SPTRCK #3.
c1 - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator
C1 from SPTRCK #3.
C1 - org.orekit.gnss.ObservationType
Pseudorange GPS L1 / GLONASS G1 / Galileo E2-L1-E1 / SBAS L1 for Rinex2.
C1A - org.orekit.gnss.ObservationType
Pseudorange Galileo E1 A / Beidou B1A for Rinex3.
C1B - org.orekit.gnss.ObservationType
Pseudorange Galileo E1 I/NAV OS/CS/SoL / QZSS geo signal for Rinex3.
C1C - org.orekit.gnss.ObservationType
Pseudorange GPS L1 C/A / GLONASS G1 C/A / Galileo E1 C / SBAS L1 C/A / QZSS L1 C/A for Rinex3.
C1D - org.orekit.gnss.ObservationType
Pseudorange Beidou B1 Data for Rinex3.
C1E - org.orekit.gnss.ObservationType
Pseudorange QZSS L1 C/B for Rinex4.
C1I - org.orekit.gnss.ObservationType
Pseudorange Beidou B1 I for Rinex3.02.
C1L - org.orekit.gnss.ObservationType
Pseudorange GPS L1 L1C(P) / QZSS L1 L1C(P) for Rinex3, Beidou B1A for Rinex3.03.
C1L - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants
C1L.
C1M - org.orekit.gnss.ObservationType
Pseudorange GPS L1 M for Rinex3.
C1P - org.orekit.gnss.ObservationType
Pseudorange GPS L1 P(AS off) / GLONASS G1 P / Beidou C1 Pilot for Rinex3.
C1Q - org.orekit.gnss.ObservationType
Pseudorange Beidou B1 Q for Rinex3.02.
C1S - org.orekit.gnss.ObservationType
Pseudorange GPS L1 L1C(D) / QZSS L1 L1C(D) for Rinex3, Beidou B1A for Rinex3.03.
C1SS - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants
C1SS.
C1W - org.orekit.gnss.ObservationType
Pseudorange GPS L1 Z-tracking and similar (AS on) for Rinex3.
C1X - org.orekit.gnss.ObservationType
Pseudorange GPS L1 L1C (D+P) / Galileo E1 B+C / QZSS L1 L1C(D+P) / Beidou B1 Data+Pilot for Rinex3.
C1Y - org.orekit.gnss.ObservationType
Pseudorange GPS L1 Y for Rinex3.
C1Z - org.orekit.gnss.ObservationType
Pseudorange Galileo E1 C1Z A+B+C / QZSS L1 L1-SAIF for Rinex3, Beidou B1A for Rinex3.03.
c2 - Variable in class org.orekit.propagation.analytical.tle.FieldTLEPropagator
C2 from SPTRCK #3.
c2 - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator
C2 from SPTRCK #3.
C2 - org.orekit.gnss.ObservationType
Pseudorange GPS L2 / GLONASS G2 / Beidou B02 for Rinex2.
C2C - org.orekit.gnss.ObservationType
Pseudorange GPS L2 C/A / GLONASS G2 C/A for Rinex3.
C2D - org.orekit.gnss.ObservationType
Pseudorange GPS L1(C/A)+(P2-P1) (semi-codeless) for Rinex3.
C2I - org.orekit.gnss.ObservationType
Pseudorange Beidou B1 I for Rinex3.03.
C2L - org.orekit.gnss.ObservationType
Pseudorange GPS L2 L2C(L) / QZSS L2 L2C(2) for Rinex3.
C2M - org.orekit.gnss.ObservationType
Pseudorange GPS L2 M for Rinex3.
C2P - org.orekit.gnss.ObservationType
Pseudorange GPS L2 P(AS off) / GLONASS G2 P for Rinex3.
C2Q - org.orekit.gnss.ObservationType
Pseudorange Beidou B1 Q for Rinex3.03.
C2S - org.orekit.gnss.ObservationType
Pseudorange GPS L2 L2C(M) / QZSS L2 L2C(M) for Rinex3.
C2W - org.orekit.gnss.ObservationType
Pseudorange GPS L2 Z-tracking and similar (AS on) for Rinex3.
C2X - org.orekit.gnss.ObservationType
Pseudorange GPS L2 L2C (M+L) / QZSS L2 L2C(M+L) for Rinex3, Beidou B1 I+Q for Rinex3.03.
C2Y - org.orekit.gnss.ObservationType
Pseudorange GPS L2 Y for Rinex3.
C3I - org.orekit.gnss.ObservationType
Pseudorange GLONASS G3 I for Rinex3.
C3Q - org.orekit.gnss.ObservationType
Pseudorange GLONASS G3 Q for Rinex3.
C3X - org.orekit.gnss.ObservationType
Pseudorange GLONASS G3 I+Q for Rinex3.
c4 - Variable in class org.orekit.propagation.analytical.tle.FieldTLEPropagator
C4 from SPTRCK #3.
c4 - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator
C4 from SPTRCK #3.
C4A - org.orekit.gnss.ObservationType
Pseudorange GLONASS G1a L1OCd for Rinex3.
C4B - org.orekit.gnss.ObservationType
Pseudorange GLONASS G1a L1OCp for Rinex3.
C4X - org.orekit.gnss.ObservationType
Pseudorange GLONASS G1a L1OCd+L1OCd for Rinex3.
C5 - org.orekit.gnss.ObservationType
Pseudorange GPS L5 / Galileo E5a / SBAS L5 for Rinex2.
C5A - org.orekit.gnss.ObservationType
Pseudorange IRNSS L5 A for Rinex3.
C5B - org.orekit.gnss.ObservationType
Pseudorange IRNSS L5 B for Rinex3.
C5C - org.orekit.gnss.ObservationType
Pseudorange IRNSS L5 C for Rinex3.
C5D - org.orekit.gnss.ObservationType
Pseudorange QZSS L5 D / Beidou B2a Data for Rinex3.
C5I - org.orekit.gnss.ObservationType
Pseudorange GPS L5 I/ Galileo E5a F/NAV OS / SBAS L5 I / QZSS L5 I for Rinex3.
C5P - org.orekit.gnss.ObservationType
Pseudorange QZSS L5 P / Beidou B2a Pilot for Rinex3.
C5Q - org.orekit.gnss.ObservationType
Pseudorange GPS L5 Q/ Galileo E5a Q / SBAS L5 Q / QZSS L5 Q for Rinex3.
C5X - org.orekit.gnss.ObservationType
Pseudorange GPS L5 I+Q/ Galileo E5a I+Q / SBAS L5 I+Q / QZSS L5 I+Q / IRNSS L5 B+C / Beidou B2a Data+Pilot for Rinex3.
C5Z - org.orekit.gnss.ObservationType
Pseudorange QZSS L5 D+P for Rinex3.
C6 - org.orekit.gnss.ObservationType
Pseudorange Galileo E6 / Beidou B03 for Rinex2.
C6A - org.orekit.gnss.ObservationType
Pseudorange Galileo E6 A PRS / GLONASS G2a L2CSI / Beidou B3A for Rinex3.
C6B - org.orekit.gnss.ObservationType
Pseudorange Galileo E6 B C/NAV CS / GLONASS G2a L2OCp for Rinex3.
C6C - org.orekit.gnss.ObservationType
Pseudorange Galileo E6 C no data for Rinex3.
C6D - org.orekit.gnss.ObservationType
Pseudorange Beidou B3A for Rinex3.
C6E - org.orekit.gnss.ObservationType
Pseudorange QZSS L6E for Rinex3.
C6I - org.orekit.gnss.ObservationType
Pseudorange Beidou B3 I for Rinex3.
C6L - org.orekit.gnss.ObservationType
Pseudorange QZSS LEX(6) L for Rinex3.
C6P - org.orekit.gnss.ObservationType
Pseudorange Beidou B3A for Rinex3.
C6Q - org.orekit.gnss.ObservationType
Pseudorange Beidou B3 Q for Rinex3.
C6S - org.orekit.gnss.ObservationType
Pseudorange QZSS LEX(6) S for Rinex3.
C6X - org.orekit.gnss.ObservationType
Pseudorange Galileo E6 B+C / QZSS LEX(6) S+L / Beidou B3 I+Q / GLONASS G2a L2CSI+L2OCp for Rinex3.
C6Z - org.orekit.gnss.ObservationType
Pseudorange Galileo E6 A+B+C / QZSS L6(D+E) / Beidou B3A for Rinex3.
C7 - org.orekit.gnss.ObservationType
Pseudorange Galileo E5b / Beidou B02 for Rinex2.
C7D - org.orekit.gnss.ObservationType
Pseudorange Beidou B2b Data for Rinex3.
C7I - org.orekit.gnss.ObservationType
Pseudorange Galileo E5b I I/NAV OS/CS/SoL / Beidou B2 I for Rinex3.
C7P - org.orekit.gnss.ObservationType
Pseudorange Beidou B2b Pilot for Rinex3.
C7Q - org.orekit.gnss.ObservationType
Pseudorange Galileo Q no data / Beidou B2 Q for Rinex3.
C7X - org.orekit.gnss.ObservationType
Pseudorange Galileo E5b I+Q / Beidou B2 I+Q for Rinex3.
C7Z - org.orekit.gnss.ObservationType
Pseudorange Beidou B2b Data+Pilot for Rinex3.
C8 - org.orekit.gnss.ObservationType
Pseudorange Galileo E5a+b for Rinex2.
C8D - org.orekit.gnss.ObservationType
Pseudorange Beidou B2(B2a+B2b) Data for Rinex3.
C8I - org.orekit.gnss.ObservationType
Pseudorange Galileo E5(E5a+E5b) I for Rinex3.
C8P - org.orekit.gnss.ObservationType
Pseudorange Beidou B2(B2a+B2b) Pilot for Rinex3.
C8Q - org.orekit.gnss.ObservationType
Pseudorange Galileo E5(E5a+E5b) Q for Rinex3.
C8X - org.orekit.gnss.ObservationType
Pseudorange Galileo E5(E5a+E5b) I+Q / Beidou B2(B2a+B2b) Data+Pilot for Rinex3.
C9A - org.orekit.gnss.ObservationType
Pseudorange IRNSS S A for Rinex3.
C9B - org.orekit.gnss.ObservationType
Pseudorange IRNSS S B for Rinex3.
C9C - org.orekit.gnss.ObservationType
Pseudorange IRNSS S C for Rinex3.
C9X - org.orekit.gnss.ObservationType
Pseudorange IRNSS S B+C for Rinex3.
CA - org.orekit.gnss.ObservationType
Pseudorange GPS L1 C/A / GLONASS G1 C/A for Rinex2.
CachedNormalizedSphericalHarmonicsProvider - Class in org.orekit.forces.gravity.potential
CachedNormalizedSphericalHarmonicsProvider(NormalizedSphericalHarmonicsProvider, double, int, int, double, double) - Constructor for class org.orekit.forces.gravity.potential.CachedNormalizedSphericalHarmonicsProvider
Simple constructor.
cachesTidalCorrection() - Method in class org.orekit.frames.EOPHistory
Check if the instance caches tidal corrections.
calculateBetaAngle(FieldSpacecraftState<T>, FieldPVCoordinatesProvider<T>) - Static method in class org.orekit.propagation.events.FieldBetaAngleDetector
Calculate the beta angle between the orbit plane and the celestial body.
calculateBetaAngle(FieldSpacecraftState<T>, FieldPVCoordinatesProvider<T>, Frame) - Static method in class org.orekit.propagation.events.FieldBetaAngleDetector
Calculate the beta angle between the orbit plane and the celestial body.
calculateBetaAngle(SpacecraftState, PVCoordinatesProvider) - Static method in class org.orekit.propagation.events.BetaAngleDetector
Calculate the beta angle between the orbit plane and the celestial body.
calculateBetaAngle(SpacecraftState, PVCoordinatesProvider, Frame) - Static method in class org.orekit.propagation.events.BetaAngleDetector
Calculate the beta angle between the orbit plane and the celestial body.
CALCULATED - org.orekit.files.ccsds.ndm.cdm.CovarianceMethod
Calculated covariance.
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.
calculatePointAlongArc(double) - Method in class org.orekit.bodies.LoxodromeArc
Calculate a point at a specific percentage along the arc.
Calibration(AbsoluteDate, int, String, int, int, double, double, double, double, double, double, double, int, int, int, int, double) - Constructor for class org.orekit.files.ilrs.CRD.Calibration
Constructor.
CalibrationDetail(AbsoluteDate, int, String, int, int, double, double, double, double, double, double, double, int, int, int, int, double) - Constructor for class org.orekit.files.ilrs.CRD.CalibrationDetail
Constructor.
CalibrationTargetConfiguration() - Constructor for class org.orekit.files.ilrs.CRDConfiguration.CalibrationTargetConfiguration
Empty constructor.
canAdd(int, int) - Method in class org.orekit.forces.gravity.potential.OceanTidesReader
Check if coefficients can be added.
CANDIDATE - org.orekit.files.ccsds.ndm.odm.ocm.ManBasis
Proposed operational or hypothetical future maneuver.
CANNOT_CHANGE_COVARIANCE_TYPE_IF_DEFINED_IN_LOF - org.orekit.errors.OrekitMessages
CANNOT_CHANGE_COVARIANCE_TYPE_IF_DEFINED_IN_LOF.
CANNOT_CHANGE_COVARIANCE_TYPE_IF_DEFINED_IN_NON_INERTIAL_FRAME - org.orekit.errors.OrekitMessages
CANNOT_CHANGE_COVARIANCE_TYPE_IF_DEFINED_IN_NON_INERTIAL_FRAME.
CANNOT_COMPUTE_AIMING_AT_SINGULAR_POINT - org.orekit.errors.OrekitMessages
CANNOT_COMPUTE_AIMING_AT_SINGULAR_POINT.
CANNOT_COMPUTE_LAGRANGIAN - org.orekit.errors.OrekitMessages
CANNOT_COMPUTE_LAGRANGIAN.
CANNOT_ESTIMATE_PRECESSION_WITHOUT_PROPER_DERIVATIVES - org.orekit.errors.OrekitMessages
CANNOT_ESTIMATE_PRECESSION_WITHOUT_PROPER_DERIVATIVES.
CANNOT_FIND_SATELLITE_IN_SYSTEM - org.orekit.errors.OrekitMessages
CANNOT_FIND_SATELLITE_IN_SYSTEM.
CANNOT_PARSE_BOTH_TAU_AND_GAMMA - org.orekit.errors.OrekitMessages
CANNOT_PARSE_BOTH_TAU_AND_GAMMA.
CANNOT_PARSE_GNSS_DATA - org.orekit.errors.OrekitMessages
CANNOT_PARSE_GNSS_DATA.
CANNOT_PARSE_SOURCETABLE - org.orekit.errors.OrekitMessages
CANNOT_PARSE_SOURCETABLE.
CANNOT_START_PROPAGATION_FROM_INFINITY - org.orekit.errors.OrekitMessages
CANNOT_START_PROPAGATION_FROM_INFINITY.
CANONICAL_I_J - Static variable in class org.orekit.estimation.measurements.gnss.Dipole
Canonical dipole, with primary vector set to Vector3D.PLUS_I and secondary vector set to Vector3D.PLUS_J.
CanonicalSaastamoinenModel - Class in org.orekit.models.earth.troposphere
The canonical Saastamoinen model.
CanonicalSaastamoinenModel() - Constructor for class org.orekit.models.earth.troposphere.CanonicalSaastamoinenModel
Create a new Saastamoinen model for the troposphere using the given environmental conditions and table from the reference book.
canReceiveNMEA() - Method in class org.orekit.gnss.metric.ntrip.CasterRecord
Check if caster can receive NMEA messages.
CARRIER_PHASE - org.orekit.gnss.MeasurementType
Carrier-phase measurement.
CARRIER_POWER - org.orekit.files.ccsds.ndm.tdm.ObservationType
Data: Carrier power [dBW].
CarrierPhase - Enum in org.orekit.gnss.metric.ntrip
Enumerate for carrier phase in DataStreamRecord.
CARTESIAN - org.orekit.orbits.OrbitType
Type for orbital representation in CartesianOrbit and FieldCartesianOrbit parameters.
cartesianBuilder(OneAxisEllipsoid) - Static method in class org.orekit.utils.WaypointPVBuilder
Construct a waypoint builder interpolating points using a linear cartesian interpolation.
CartesianCovariance - Class in org.orekit.files.ccsds.ndm.odm
Container for OPM/OMM/OCM Cartesian covariance matrix.
CartesianCovariance(Supplier<FrameFacade>) - Constructor for class org.orekit.files.ccsds.ndm.odm.CartesianCovariance
Create an empty data set.
CartesianCovarianceKey - Enum in org.orekit.files.ccsds.ndm.odm
CartesianCovarianceWriter - Class in org.orekit.files.ccsds.ndm.odm
Writer for covariance matrix data.
CartesianCovarianceWriter(String, String, CartesianCovariance) - Constructor for class org.orekit.files.ccsds.ndm.odm.CartesianCovarianceWriter
Create a writer.
CartesianDerivativesFilter - Enum in org.orekit.utils
Enumerate for selecting which derivatives to use in TimeStampedPVCoordinates and TimeStampedFieldPVCoordinates interpolation.
CartesianOrbit - Class in org.orekit.orbits
This class holds Cartesian orbital parameters.
CartesianOrbit(Orbit) - Constructor for class org.orekit.orbits.CartesianOrbit
Constructor from any kind of orbital parameters.
CartesianOrbit(PVCoordinates, Frame, AbsoluteDate, double) - Constructor for class org.orekit.orbits.CartesianOrbit
Constructor from Cartesian parameters.
CartesianOrbit(TimeStampedPVCoordinates, Frame, double) - Constructor for class org.orekit.orbits.CartesianOrbit
Constructor from Cartesian parameters.
CARTP - org.orekit.files.ccsds.ndm.odm.ocm.OrbitElementsType
Cartesian 3-element position (X, Y, Z).
CARTPV - org.orekit.files.ccsds.ndm.odm.ocm.OrbitElementsType
Cartesian 6-element position and velocity (X, Y, Z, XD, YD, ZD).
CARTPVA - org.orekit.files.ccsds.ndm.odm.ocm.OrbitElementsType
Cartesian 9-element position, velocity and acceleration (X, Y, Z, XD, YD, ZD, XDD, YDD, ZDD).
CAS - org.orekit.gnss.metric.ntrip.RecordType
Casters.
CasterRecord - Class in org.orekit.gnss.metric.ntrip
Caster record in source table.
CasterRecord(String) - Constructor for class org.orekit.gnss.metric.ntrip.CasterRecord
Build a caster record by parsing a source table line.
CATALOG_NAME - org.orekit.files.ccsds.ndm.adm.acm.AcmMetadataKey
Specification of satellite catalog source.
CATALOG_NAME - org.orekit.files.ccsds.ndm.cdm.CdmMetadataKey
Satellite catalog used for the object.
CATALOG_NAME - org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadataKey
Specification of satellite catalog source.
CB - org.orekit.gnss.ObservationType
Pseudorange GPS L1C for Rinex2.
CC - org.orekit.gnss.ObservationType
Pseudorange GPS L2C for Rinex2.
CCSDS_ACM_VERS - Static variable in class org.orekit.files.ccsds.ndm.adm.acm.AcmWriter
Version number implemented.
CCSDS_AEM_VERS - Static variable in class org.orekit.files.ccsds.ndm.adm.aem.AemWriter
Version number implemented.
CCSDS_APM_VERS - Static variable in class org.orekit.files.ccsds.ndm.adm.apm.ApmWriter
Version number implemented.
CCSDS_CDM_VERS - Static variable in class org.orekit.files.ccsds.ndm.cdm.CdmWriter
Version number implemented.
CCSDS_DATE_INVALID_LENGTH_TIME_FIELD - org.orekit.errors.OrekitMessages
CCSDS_DATE_INVALID_LENGTH_TIME_FIELD.
CCSDS_DATE_INVALID_PREAMBLE_FIELD - org.orekit.errors.OrekitMessages
CCSDS_DATE_INVALID_PREAMBLE_FIELD.
CCSDS_DATE_MISSING_AGENCY_EPOCH - org.orekit.errors.OrekitMessages
CCSDS_DATE_MISSING_AGENCY_EPOCH.
CCSDS_DIFFERENT_LVLH_DEFINITION - org.orekit.errors.OrekitMessages
CCSDS_DIFFERENT_LVLH_DEFINITION.
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_INCOMPATIBLE_KEYS_BOTH_USED - org.orekit.errors.OrekitMessages
CCSDS_INCOMPATIBLE_KEYS_BOTH_USED.
CCSDS_INCOMPLETE_DATA - org.orekit.errors.OrekitMessages
CCSDS_INCOMPLETE_DATA.
CCSDS_INCONSISTENT_NUMBER_OF_ATTITUDE_STATES - org.orekit.errors.OrekitMessages
CCSDS_INCONSISTENT_NUMBER_OF_ATTITUDE_STATES.
CCSDS_INCONSISTENT_TIME_SYSTEMS - org.orekit.errors.OrekitMessages
CCSDS_INCONSISTENT_TIME_SYSTEMS.
CCSDS_INVALID_FRAME - org.orekit.errors.OrekitMessages
CCSDS_INVALID_FRAME.
CCSDS_INVALID_ROTATION_SEQUENCE - org.orekit.errors.OrekitMessages
CCSDS_INVALID_ROTATION_SEQUENCE.
CCSDS_KEYWORD_NOT_ALLOWED_IN_VERSION - org.orekit.errors.OrekitMessages
CCSDS_KEYWORD_NOT_ALLOWED_IN_VERSION.
CCSDS_MANEUVER_MISSING_TIME - org.orekit.errors.OrekitMessages
CCSDS_MANEUVER_MISSING_TIME.
CCSDS_MANEUVER_UNITS_WRONG_NB_COMPONENTS - org.orekit.errors.OrekitMessages
CCSDS_MANEUVER_UNITS_WRONG_NB_COMPONENTS.
CCSDS_MISSING_KEYWORD - org.orekit.errors.OrekitMessages
CCSDS_MISSING_KEYWORD.
CCSDS_MISSING_SENSOR_INDEX - org.orekit.errors.OrekitMessages
CCSDS_MISSING_SENSOR_INDEX.
CCSDS_OCM_VERS - Static variable in class org.orekit.files.ccsds.ndm.odm.ocm.OcmWriter
Version number implemented.
CCSDS_OEM_VERS - Static variable in class org.orekit.files.ccsds.ndm.odm.oem.OemWriter
Version number implemented.
CCSDS_OMM_VERS - Static variable in class org.orekit.files.ccsds.ndm.odm.omm.OmmWriter
Version number implemented.
CCSDS_OPM_VERS - Static variable in class org.orekit.files.ccsds.ndm.odm.opm.OpmWriter
Version number implemented.
CCSDS_SENSOR_INDEX_ALREADY_USED - org.orekit.errors.OrekitMessages
CCSDS_SENSOR_INDEX_ALREADY_USED.
CCSDS_TDM_KEYWORD_NOT_FOUND - org.orekit.errors.OrekitMessages
CCSDS_TDM_KEYWORD_NOT_FOUND.
CCSDS_TDM_MISSING_RANGE_UNITS_CONVERTER - org.orekit.errors.OrekitMessages
CCSDS_TDM_MISSING_RANGE_UNITS_CONVERTER.
CCSDS_TDM_VERS - Static variable in class org.orekit.files.ccsds.ndm.tdm.TdmWriter
Version number implemented.
CCSDS_TIME_SYSTEM_NOT_IMPLEMENTED - org.orekit.errors.OrekitMessages
CCSDS_TIME_SYSTEM_NOT_IMPLEMENTED.
CCSDS_TIME_SYSTEM_NOT_READ_YET - org.orekit.errors.OrekitMessages
CCSDS_TIME_SYSTEM_NOT_READ_YET.
CCSDS_UNEXPECTED_KEYWORD - org.orekit.errors.OrekitMessages
CCSDS_UNEXPECTED_KEYWORD.
CCSDS_UNKNOWN_ATTITUDE_TYPE - org.orekit.errors.OrekitMessages
CCSDS_UNKNOWN_ATTITUDE_TYPE.
CCSDS_UNKNOWN_CONVENTIONS - org.orekit.errors.OrekitMessages
CCSDS_UNKNOWN_CONVENTIONS.
CCSDS_UNKNOWN_GM - org.orekit.errors.OrekitMessages
CCSDS_UNKNOWN_GM.
CCSDS_UNKNOWN_SPACECRAFT_MASS - org.orekit.errors.OrekitMessages
CCSDS_UNKNOWN_SPACECRAFT_MASS.
CCSDS_UNSUPPORTED_ELEMENT_SET_TYPE - org.orekit.errors.OrekitMessages
CCSDS_UNSUPPORTED_ELEMENT_SET_TYPE.
CCSDS_UNSUPPORTED_RETROGRADE_EQUINOCTIAL - org.orekit.errors.OrekitMessages
CCSDS_UNSUPPORTED_RETROGRADE_EQUINOCTIAL.
CD - org.orekit.gnss.ObservationType
Pseudorange GLONASS G2 for Rinex2.
CD_AREA_OVER_MASS - org.orekit.files.ccsds.ndm.cdm.AdditionalParametersKey
The object’s Cd x A/m used to propagate the state vector and covariance to TCA.
Cdm - Class in org.orekit.files.ccsds.ndm.cdm
This class stores all the information of the Conjunction Data Message (CDM) File parsed by CdmParser.
Cdm(CdmHeader, List<CdmSegment>, IERSConventions, DataContext) - Constructor for class org.orekit.files.ccsds.ndm.cdm.Cdm
Simple constructor.
CDM_MSG_LINK - org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadataKey
Unique identifier of Conjunction Data Message linked to this Orbit Data Message.
CdmData - Class in org.orekit.files.ccsds.ndm.cdm
Container for Conjunction Data Message data.
CdmData(CommentsContainer, ODParameters, AdditionalParameters, StateVector, RTNCovariance) - Constructor for class org.orekit.files.ccsds.ndm.cdm.CdmData
Constructor with RTN covariance.
CdmData(CommentsContainer, ODParameters, AdditionalParameters, StateVector, RTNCovariance, AdditionalCovarianceMetadata) - Constructor for class org.orekit.files.ccsds.ndm.cdm.CdmData
Constructor with RTN covariance.
CdmData(CommentsContainer, ODParameters, AdditionalParameters, StateVector, RTNCovariance, SigmaEigenvectorsCovariance, AdditionalCovarianceMetadata) - Constructor for class org.orekit.files.ccsds.ndm.cdm.CdmData
Constructor with RTN and sigma/eigenvector covariance.
CdmData(CommentsContainer, ODParameters, AdditionalParameters, StateVector, RTNCovariance, XYZCovariance, AdditionalCovarianceMetadata) - Constructor for class org.orekit.files.ccsds.ndm.cdm.CdmData
Constructor with RTN and XYZ covariance.
CdmHeader - Class in org.orekit.files.ccsds.ndm.cdm
Header of a CCSDS Conjunction Data Message.
CdmHeader() - Constructor for class org.orekit.files.ccsds.ndm.cdm.CdmHeader
Constructor.
CdmHeaderKey - Enum in org.orekit.files.ccsds.ndm.cdm
Keywords allowed in CdmHeader.
CdmHeaderProcessingState - Class in org.orekit.files.ccsds.ndm.cdm
CdmHeaderProcessingState(CdmParser) - Constructor for class org.orekit.files.ccsds.ndm.cdm.CdmHeaderProcessingState
Simple constructor.
CdmMessageWriter - Class in org.orekit.files.ccsds.ndm.cdm
Cdm message writer.
CdmMessageWriter(String, String, double, ContextBinding) - Constructor for class org.orekit.files.ccsds.ndm.cdm.CdmMessageWriter
Constructor used to create a new NDM writer configured with the necessary parameters to successfully fill in all required fields that aren't part of a standard object.
CdmMetadata - Class in org.orekit.files.ccsds.ndm.cdm
This class gathers the meta-data present in the Conjunction Data Message (CDM).
CdmMetadata() - Constructor for class org.orekit.files.ccsds.ndm.cdm.CdmMetadata
Simple constructor.
CdmMetadata(DataContext) - Constructor for class org.orekit.files.ccsds.ndm.cdm.CdmMetadata
Simple constructor.
CdmMetadataKey - Enum in org.orekit.files.ccsds.ndm.cdm
Keys for CDM container entries.
CdmMetadataWriter - Class in org.orekit.files.ccsds.ndm.cdm
Writer for Metadata for CCSDS Conjunction Data Messages.
CdmMetadataWriter(CdmMetadata) - Constructor for class org.orekit.files.ccsds.ndm.cdm.CdmMetadataWriter
Simple constructor.
CdmParser - Class in org.orekit.files.ccsds.ndm.cdm
Base class for Conjunction Data Message parsers.
CdmParser(IERSConventions, boolean, DataContext, ParsedUnitsBehavior, Function<ParseToken, List<ParseToken>>[]) - Constructor for class org.orekit.files.ccsds.ndm.cdm.CdmParser
Complete constructor.
CdmRelativeMetadata - Class in org.orekit.files.ccsds.ndm.cdm
This class gathers the relative meta-data present in the Conjunction Data Message (CDM).
CdmRelativeMetadata() - Constructor for class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata
Simple constructor.
CdmRelativeMetadataKey - Enum in org.orekit.files.ccsds.ndm.cdm
Keys for CDM container entries.
CdmSegment - Class in org.orekit.files.ccsds.ndm.cdm
This class stores the metadata and data for one object.
CdmSegment(CdmMetadata, CdmData) - Constructor for class org.orekit.files.ccsds.ndm.cdm.CdmSegment
Simple constructor.
CdmWriter - Class in org.orekit.files.ccsds.ndm.cdm
Writer for CCSDS Conjunction Data Message.
CdmWriter(IERSConventions, DataContext) - Constructor for class org.orekit.files.ccsds.ndm.cdm.CdmWriter
Complete constructor.
CDRG_DRG - org.orekit.files.ccsds.ndm.cdm.RTNCovarianceKey
Object covariance matrix [7,7].
CDRG_DRG - org.orekit.files.ccsds.ndm.cdm.XYZCovarianceKey
Object covariance matrix [7,7].
CDRG_N - org.orekit.files.ccsds.ndm.cdm.RTNCovarianceKey
Object covariance matrix [7,3].
CDRG_NDOT - org.orekit.files.ccsds.ndm.cdm.RTNCovarianceKey
Object covariance matrix [7,6].
CDRG_R - org.orekit.files.ccsds.ndm.cdm.RTNCovarianceKey
Object covariance matrix [7,1].
CDRG_RDOT - org.orekit.files.ccsds.ndm.cdm.RTNCovarianceKey
Object covariance matrix [7,4].
CDRG_T - org.orekit.files.ccsds.ndm.cdm.RTNCovarianceKey
Object covariance matrix [7,2].
CDRG_TDOT - org.orekit.files.ccsds.ndm.cdm.RTNCovarianceKey
Object covariance matrix [7,5].
CDRG_X - org.orekit.files.ccsds.ndm.cdm.XYZCovarianceKey
Object covariance matrix [7,1].
CDRG_XDOT - org.orekit.files.ccsds.ndm.cdm.XYZCovarianceKey
Object covariance matrix [7,4].
CDRG_Y - org.orekit.files.ccsds.ndm.cdm.XYZCovarianceKey
Object covariance matrix [7,2].
CDRG_YDOT - org.orekit.files.ccsds.ndm.cdm.XYZCovarianceKey
Object covariance matrix [7,5].
CDRG_Z - org.orekit.files.ccsds.ndm.cdm.XYZCovarianceKey
Object covariance matrix [7,3].
CDRG_ZDOT - org.orekit.files.ccsds.ndm.cdm.XYZCovarianceKey
Object covariance matrix [7,6].
CELESTIAL_SOURCE - org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadataKey
Source and version of celestial body (e.g.
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.
CelestialBodyFrame - Enum in org.orekit.files.ccsds.definitions
Frames used in CCSDS Orbit Data Messages.
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.
CellInterpolator - Class in org.orekit.models.earth.weather
Interpolator within a grid cell.
CENTER_NAME - org.orekit.files.ccsds.ndm.adm.AdmMetadataKey
Center name entry.
CENTER_NAME - org.orekit.files.ccsds.ndm.odm.CommonMetadataKey
Center name entry.
CENTER_NAME - org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadataKey
Origin of the reference frame of the trajectory.
CENTER_OF_MASS_XYZ - org.orekit.files.rinex.section.RinexLabels
Center of mass.
CenterName - Enum in org.orekit.files.ccsds.definitions
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.
CENTRAL_BODY_ROTATION - org.orekit.files.ccsds.ndm.odm.ocm.PerturbationsKey
Central body angular rotation rate.
CHAN_1997 - org.orekit.files.ccsds.definitions.PocMethodType
Chan 1997 method.
CHAN_1997 - org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DPOCMethodType
Probability of collision computing method described in :
"Chan,K.
CHAN_2003 - org.orekit.files.ccsds.definitions.PocMethodType
Chan 2003 method.
Chan1997 - Class in org.orekit.ssa.collision.shorttermencounter.probability.twod
Compute the probability of collision using the method described in :
"Chan, K.
Chan1997() - Constructor for class org.orekit.ssa.collision.shorttermencounter.probability.twod.Chan1997
Empty constructor.
change(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.FieldAbstractStateModifier
Change main state.
change(SpacecraftState) - Method in class org.orekit.propagation.AbstractStateModifier
Change main state.
CHANGE_IN_TWO_RECEIVER_ONE_SATELLITE_CARRIER_PHASE - org.orekit.files.sp3.DataUsed
Change in 2-receiver/1-satellite carrier phase.
CHANGE_IN_TWO_RECEIVER_ONE_SATELLITE_CODE_PHASE - org.orekit.files.sp3.DataUsed
Change in 2-receiver/1-satellite code phase.
CHANGE_IN_TWO_RECEIVER_TWO_SATELLITE_CARRIER_PHASE - org.orekit.files.sp3.DataUsed
Change in 2-receiver/2-satellite carrier phase.
CHANGE_IN_TWO_RECEIVER_TWO_SATELLITE_CODE_PHASE - org.orekit.files.sp3.DataUsed
Change in 2-receiver/2-satellite code phase.
CHANGE_IN_UNDIFFERENTIATED_CARRIER_PHASE - org.orekit.files.sp3.DataUsed
Change in undifferenciated carrier phase.
CHANGE_IN_UNDIFFERENTIATED_CODE_PHASE - org.orekit.files.sp3.DataUsed
Change in undifferenciated code phase.
changeCovarianceFrame(FieldOrbit<T>, Frame) - Method in class org.orekit.propagation.FieldStateCovariance
Get the covariance in the output frame.
changeCovarianceFrame(FieldOrbit<T>, LOF) - Method in class org.orekit.propagation.FieldStateCovariance
Get the covariance in a given local orbital frame.
changeCovarianceFrame(Orbit, Frame) - Method in class org.orekit.propagation.StateCovariance
Get the covariance in the output frame.
changeCovarianceFrame(Orbit, LOF) - Method in class org.orekit.propagation.StateCovariance
Get the covariance in a given local orbital frame.
changeCovarianceType(FieldOrbit<T>, OrbitType, PositionAngleType) - Method in class org.orekit.propagation.FieldStateCovariance
Get the covariance matrix in another orbit type.
changeCovarianceType(Orbit, OrbitType, PositionAngleType) - Method in class org.orekit.propagation.StateCovariance
Get the covariance matrix in another orbit type.
changeFrame(SP3, Frame) - Static method in class org.orekit.files.sp3.SP3
Change the frame of an SP3 file.
ChaoMappingFunction - Class in org.orekit.models.earth.troposphere
Chao mapping function for radio wavelengths.
ChaoMappingFunction() - Constructor for class org.orekit.models.earth.troposphere.ChaoMappingFunction
Builds a new instance.
checkAllowed(double, Object, String, double, double) - Method in class org.orekit.files.ccsds.section.CommentsContainer
Complain if a key is not allowed.
checkDatesConsistency(AbsoluteDate, AbsoluteDate, double) - Static method in class org.orekit.time.TimeStampedPair
Check date consistency.
checkDimension(int, ParameterDriversList, ParameterDriversList, ParameterDriversList) - Static method in class org.orekit.estimation.sequential.KalmanEstimatorUtil
Check dimension.
checkEOPContinuity(double) - Method in class org.orekit.frames.EOPHistory
Check Earth orientation parameters continuity.
checkException() - Method in class org.orekit.gnss.metric.ntrip.NtripClient
Check if any of the streaming thread has thrown an exception.
checkExternalFrame(Enum<?>, Enum<?>) - Method in class org.orekit.files.ccsds.ndm.adm.AttitudeEndpoints
Check external frame is properly initialized.
checkFrameAndOrbitTypeConsistency(Frame, OrbitType) - Static method in class org.orekit.propagation.StateCovariance
Check constructor's inputs consistency.
checkInputConsistency(List<SpacecraftState>, TimeInterpolator<SpacecraftState>, List<StateCovariance>, TimeInterpolator<TimeStampedPair<Orbit, StateCovariance>>) - Static method in class org.orekit.propagation.analytical.Ephemeris
Check input consistency between states, covariances and their associated interpolators.
checkInterpolatorCompatibilityWithSampleSize(FieldTimeInterpolator<? extends FieldTimeStamped<T>, T>, int) - Static method in class org.orekit.time.AbstractFieldTimeInterpolator
Method checking if given interpolator is compatible with given sample size.
checkInterpolatorCompatibilityWithSampleSize(TimeInterpolator<? extends TimeStamped>, int) - Static method in class org.orekit.time.AbstractTimeInterpolator
Method checking if given interpolator is compatible with given sample size.
checkMandatoryEntriesExceptExternalFrame(double, Enum<?>, Enum<?>, Enum<?>) - Method in class org.orekit.files.ccsds.ndm.adm.AttitudeEndpoints
Check is mandatory entries except external frame have been initialized.
checkNotNaN(double, String) - Method in class org.orekit.files.ccsds.section.CommentsContainer
Complain if a field is NaN.
checkNotNegative(int, String) - Method in class org.orekit.files.ccsds.section.CommentsContainer
Complain if a field is negative.
checkNotNull(Object, Enum<?>) - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata
Complain if a field is null.
checkNotNull(Object, String) - Method in class org.orekit.files.ccsds.section.CommentsContainer
Complain if a field is null.
checkOrbitsConsistency(Collection<Orbit>) - Static method in class org.orekit.orbits.AbstractOrbitInterpolator
Check orbits consistency by comparing their gravitational parameters µ.
checkParity(int, int) - Static method in class org.orekit.gnss.rflink.gps.SubFrame
Check parity.
checkSampleAndInterpolatorConsistency(List<SpacecraftState>, boolean, boolean) - Static method in class org.orekit.propagation.SpacecraftStateInterpolator
Check that an interpolator exist for given sample state definition.
checkScreenVolumeConditions() - Method in class org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadata
Check screen volume conditions.
checkStatesAndCovariancesConsistency(List<SpacecraftState>, List<StateCovariance>) - Static method in class org.orekit.propagation.analytical.Ephemeris
Check that given states and covariances are consistent.
checkStatesDefinitionsConsistency(List<SpacecraftState>) - Static method in class org.orekit.propagation.SpacecraftStateInterpolator
Check that all state are either orbit defined or based on absolute position-velocity-acceleration.
checkStep(double) - Method in class org.orekit.propagation.conversion.AbstractFixedStepFieldIntegratorBuilder
Check that given step size is not equal to 0.
checkTimeSystems() - Method in class org.orekit.files.ccsds.ndm.odm.oem.Oem
Check that, according to the CCSDS standard, every OEMBlock has the same time system.
checkUnit(Unit) - Method in enum org.orekit.files.ccsds.ndm.odm.ocm.ManeuverFieldType
Check if parsed unit is compatible with field type.
ChronologicalComparator - Class in org.orekit.time
Comparator for TimeStamped instance.
ChronologicalComparator() - Constructor for class org.orekit.time.ChronologicalComparator
Simple constructor.
CIPM2007 - Class in org.orekit.models.earth.weather.water
Official model CIPM-2007 (identical to CIPM-1981/91) from Comité International des Poids et Mesures.
CIPM2007() - Constructor for class org.orekit.models.earth.weather.water.CIPM2007
 
CIRCULAR - org.orekit.orbits.OrbitType
Type for orbital representation in CircularOrbit and FieldCircularOrbit parameters.
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.
CircularLatitudeArgumentUtility - Class in org.orekit.orbits
Utility methods for converting between different latitude arguments used by CircularOrbit.
CircularOrbit - Class in org.orekit.orbits
This class handles circular orbital parameters.
CircularOrbit(double, double, double, double, double, double, double, double, double, double, double, double, PositionAngleType, Frame, AbsoluteDate, double) - Constructor for class org.orekit.orbits.CircularOrbit
Creates a new instance with derivatives and with cached position angle same as value inputted.
CircularOrbit(double, double, double, double, double, double, double, double, double, double, double, double, PositionAngleType, PositionAngleType, Frame, AbsoluteDate, double) - Constructor for class org.orekit.orbits.CircularOrbit
Creates a new instance.
CircularOrbit(double, double, double, double, double, double, PositionAngleType, Frame, AbsoluteDate, double) - Constructor for class org.orekit.orbits.CircularOrbit
Creates a new instance without derivatives and with cached position angle same as value inputted.
CircularOrbit(double, double, double, double, double, double, PositionAngleType, PositionAngleType, Frame, AbsoluteDate, double) - Constructor for class org.orekit.orbits.CircularOrbit
Creates a new instance.
CircularOrbit(Orbit) - Constructor for class org.orekit.orbits.CircularOrbit
Constructor from any kind of orbital parameters.
CircularOrbit(PVCoordinates, Frame, AbsoluteDate, double) - Constructor for class org.orekit.orbits.CircularOrbit
Constructor from Cartesian parameters.
CircularOrbit(TimeStampedPVCoordinates, Frame, double) - Constructor for class org.orekit.orbits.CircularOrbit
Constructor from Cartesian parameters.
CIRF_CONVENTIONS_1996_ACCURATE_EOP - org.orekit.frames.Predefined
CIRF frame, IERS 1996 conventions, with accurate EOP interpolation.
CIRF_CONVENTIONS_1996_SIMPLE_EOP - org.orekit.frames.Predefined
CIRF frame, IERS 1996 conventions, with simple EOP interpolation.
CIRF_CONVENTIONS_2003_ACCURATE_EOP - org.orekit.frames.Predefined
CIRF frame, IERS 2003 conventions, with accurate EOP interpolation.
CIRF_CONVENTIONS_2003_SIMPLE_EOP - org.orekit.frames.Predefined
CIRF frame, IERS 2003 conventions, with simple EOP interpolation.
CIRF_CONVENTIONS_2010_ACCURATE_EOP - org.orekit.frames.Predefined
CIRF frame, IERS 2010 conventions, with accurate EOP interpolation.
CIRF_CONVENTIONS_2010_SIMPLE_EOP - org.orekit.frames.Predefined
CIRF frame, IERS 2010 conventions, with simple EOP interpolation.
CIVIL_DAWN_DUSK_ELEVATION - Static variable in class org.orekit.propagation.events.GroundAtNightDetector
Sun elevation at civil dawn/dusk (6° below horizon).
CivilianNavigationMessage - Class in org.orekit.propagation.analytical.gnss.data
Container for data contained in a GPS/QZNSS civilian navigation message.
CivilianNavigationMessage(boolean, double, double, int) - Constructor for class org.orekit.propagation.analytical.gnss.data.CivilianNavigationMessage
Constructor.
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.
CK2 - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants
CK2.
CK4 - Static variable in class org.orekit.propagation.analytical.tle.TLEConstants
CK4.
ClassicalRungeKuttaFieldIntegratorBuilder<T extends CalculusFieldElement<T>> - Class in org.orekit.propagation.conversion
Builder for ClassicalRungeKuttaFieldIntegrator.
ClassicalRungeKuttaFieldIntegratorBuilder(double) - Constructor for class org.orekit.propagation.conversion.ClassicalRungeKuttaFieldIntegratorBuilder
Constructor.
ClassicalRungeKuttaFieldIntegratorBuilder(T) - Constructor for class org.orekit.propagation.conversion.ClassicalRungeKuttaFieldIntegratorBuilder
Constructor using a "fielded" step.
ClassicalRungeKuttaIntegratorBuilder - Class in org.orekit.propagation.conversion
Builder for ClassicalRungeKuttaIntegrator.
ClassicalRungeKuttaIntegratorBuilder(double) - Constructor for class org.orekit.propagation.conversion.ClassicalRungeKuttaIntegratorBuilder
Build a new instance.
CLASSIFICATION - org.orekit.files.ccsds.ndm.cdm.CdmHeaderKey
User-defined free-text message classification or caveats of this CDM.
CLASSIFICATION - org.orekit.files.ccsds.section.HeaderKey
Classification.
CLASSIFICATION_TYPE - org.orekit.files.ccsds.ndm.odm.omm.OmmTleKey
Classifiation type.
ClasspathCrawler - Class in org.orekit.data
Provider for data files stored as resources in the classpath.
ClasspathCrawler(ClassLoader, String...) - Constructor for class org.orekit.data.ClasspathCrawler
Build a data classpath crawler.
ClasspathCrawler(String...) - Constructor for class org.orekit.data.ClasspathCrawler
Build a data classpath crawler.
clear() - Method in class org.orekit.propagation.events.handlers.FieldRecordAndContinue
Clear all stored events.
clear() - Method in class org.orekit.propagation.events.handlers.RecordAndContinue
Clear all stored events.
clear() - Method in class org.orekit.propagation.sampling.FieldStepHandlerMultiplexer
Remove all handlers managed by this multiplexer.
clear() - Method in class org.orekit.propagation.sampling.StepHandlerMultiplexer
Remove all handlers managed by this multiplexer.
clear() - Method in class org.orekit.utils.DoubleArrayDictionary
Remove all entries.
clear() - Method in class org.orekit.utils.FieldArrayDictionary
Remove all entries.
clearCelestialBodyCache() - Static method in class org.orekit.bodies.CelestialBodyFactory
Clear all loaded celestial bodies.
clearCelestialBodyCache() - Method in class org.orekit.bodies.LazyLoadedCelestialBodies
Clear all loaded celestial bodies.
clearCelestialBodyCache(String) - Static method in class org.orekit.bodies.CelestialBodyFactory
Clear the specified celestial body from the internal cache.
clearCelestialBodyCache(String) - Method in class org.orekit.bodies.LazyLoadedCelestialBodies
Clear the specified celestial body from the internal cache.
clearCelestialBodyLoaders() - Static method in class org.orekit.bodies.CelestialBodyFactory
Clear loaders for all celestial bodies.
clearCelestialBodyLoaders() - Method in class org.orekit.bodies.LazyLoadedCelestialBodies
Clear loaders for all celestial bodies.
clearCelestialBodyLoaders(String) - Static method in class org.orekit.bodies.CelestialBodyFactory
Clear loaders for one celestial body.
clearCelestialBodyLoaders(String) - Method in class org.orekit.bodies.LazyLoadedCelestialBodies
Clear loaders for one celestial body.
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.analytical.AbstractAnalyticalPropagator
Remove all events detectors.
clearEventsDetectors() - Method in class org.orekit.propagation.analytical.FieldAbstractAnalyticalPropagator
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.FiltersManager
Remove all data filters.
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.
clearStepHandlers() - Method in interface org.orekit.propagation.FieldPropagator
Remove all step handlers.
clearStepHandlers() - Method in interface org.orekit.propagation.Propagator
Remove all step handlers.
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_ACCELERATION_PREFIX - Static variable in class org.orekit.estimation.measurements.ObservableSatellite
Prefix for clock acceleration parameter driver, the propagator index will be appended to it.
CLOCK_ACCURACY_UNIT - Static variable in class org.orekit.files.sp3.SP3Utils
Clock accuracy unit.
CLOCK_ADDITIONAL_STATE - Static variable in class org.orekit.files.sp3.SP3Utils
Additional state name for clock.
CLOCK_BIAS - org.orekit.files.ccsds.ndm.tdm.ObservationType
Data: Clock bias [s].
CLOCK_CORRECTIONS - Static variable in class org.orekit.propagation.analytical.gnss.ClockCorrectionsProvider
Name of the additional state for satellite clock corrections.
CLOCK_DRIFT - org.orekit.files.ccsds.ndm.tdm.ObservationType
Data: Clock drift [s/s].
CLOCK_DRIFT_PREFIX - Static variable in class org.orekit.estimation.measurements.ObservableSatellite
Prefix for clock drift parameter driver, the propagator index will be appended to it.
CLOCK_FILE_UNSUPPORTED_VERSION - org.orekit.errors.OrekitMessages
CLOCK_FILE_UNSUPPORTED_VERSION.
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.
CLOCK_RATE_ACCURACY_UNIT - Static variable in class org.orekit.files.sp3.SP3Utils
Clock rate accuracy unit.
CLOCK_RATE_UNIT - Static variable in class org.orekit.files.sp3.SP3Utils
Clock rate unit.
CLOCK_UNIT - Static variable in class org.orekit.files.sp3.SP3Utils
Clock unit.
ClockCorrection - Class in org.orekit.gnss.metric.messages.common
Container for SSR clock correction data.
ClockCorrection(double, double, double) - Constructor for class org.orekit.gnss.metric.messages.common.ClockCorrection
Constructor.
ClockCorrectionsProvider - Class in org.orekit.propagation.analytical.gnss
Provider for clock corrections as additional states.
ClockCorrectionsProvider(GNSSClockElements) - Constructor for class org.orekit.propagation.analytical.gnss.ClockCorrectionsProvider
Simple constructor.
ClockDataLine(RinexClock.ClockDataType, String, DateComponents, TimeComponents, int, double, double, double, double, double, double) - Constructor for class org.orekit.files.rinex.clock.RinexClock.ClockDataLine
Constructor.
ClockModel - Interface in org.orekit.time
Offset clock model.
ClockOffset - Class in org.orekit.time
Container for time stamped clock offset.
ClockOffset(AbsoluteDate, double, double, double) - Constructor for class org.orekit.time.ClockOffset
Simple constructor.
ClockOffsetHermiteInterpolator - Class in org.orekit.time
bHermite interpolator of time stamped clock offsets.
ClockOffsetHermiteInterpolator(int) - Constructor for class org.orekit.time.ClockOffsetHermiteInterpolator
Constructor with default extrapolation threshold value (DEFAULT_EXTRAPOLATION_THRESHOLD_SEC s).
ClockOffsetHermiteInterpolator(int, double) - Constructor for class org.orekit.time.ClockOffsetHermiteInterpolator
Constructor.
ClockTimeScale - Class in org.orekit.time
Time scale with clock offset from another time scale.
ClockTimeScale(String, TimeScale, ClockModel) - Constructor for class org.orekit.time.ClockTimeScale
Simple constructor.
close() - Method in class org.orekit.data.LineOrientedFilteringReader
close() - Method in class org.orekit.files.ccsds.ndm.adm.aem.StreamingAemWriter
close() - Method in class org.orekit.files.ccsds.ndm.odm.ocm.StreamingOcmWriter
close() - Method in class org.orekit.files.ccsds.ndm.odm.oem.StreamingOemWriter
close() - Method in class org.orekit.files.ccsds.utils.generation.AbstractGenerator
Close the generator.
close() - Method in interface org.orekit.files.ccsds.utils.generation.Generator
Close the generator.
close() - Method in class org.orekit.files.rinex.observation.RinexObservationWriter
CM_COEFFICIENTS - Static variable in class org.orekit.propagation.semianalytical.dsst.forces.DSSTTesseral
Identifier for cMm coefficients.
CMR - org.orekit.gnss.metric.ntrip.DataFormat
CMR.
CMR_PLUS - org.orekit.gnss.metric.ntrip.DataFormat
CMR+.
CN_N - org.orekit.files.ccsds.ndm.cdm.RTNCovarianceKey
Object covariance matrix [3,3].
CN_R - org.orekit.files.ccsds.ndm.cdm.RTNCovarianceKey
Object covariance matrix [3,1].
CN_T - org.orekit.files.ccsds.ndm.cdm.RTNCovarianceKey
Object covariance matrix [3,2].
CNAV - Static variable in class org.orekit.propagation.analytical.gnss.data.CivilianNavigationMessage
Identifier for message type.
CNDOT_N - org.orekit.files.ccsds.ndm.cdm.RTNCovarianceKey
Object covariance matrix [6,3].
CNDOT_NDOT - org.orekit.files.ccsds.ndm.cdm.RTNCovarianceKey
Object covariance matrix [6,6].
CNDOT_R - org.orekit.files.ccsds.ndm.cdm.RTNCovarianceKey
Object covariance matrix [6,1].
CNDOT_RDOT - org.orekit.files.ccsds.ndm.cdm.RTNCovarianceKey
Object covariance matrix [6,4].
CNDOT_T - org.orekit.files.ccsds.ndm.cdm.RTNCovarianceKey
Object covariance matrix [6,2].
CNDOT_TDOT - org.orekit.files.ccsds.ndm.cdm.RTNCovarianceKey
Object covariance matrix [6,5].
CNV1 - Static variable in class org.orekit.propagation.analytical.gnss.data.BeidouCivilianNavigationMessage
Identifier for Beidou-3 B1C message type.
CNV2 - Static variable in class org.orekit.propagation.analytical.gnss.data.BeidouCivilianNavigationMessage
Identifier for Beidou-3 B2A message type.
CNV2 - Static variable in class org.orekit.propagation.analytical.gnss.data.CivilianNavigationMessage
Identifier for message type.
CNV3 - Static variable in class org.orekit.propagation.analytical.gnss.data.BeidouCivilianNavigationMessage
Identifier for Beidou-3 B2B message type.
co2AB - Variable in class org.orekit.propagation.semianalytical.dsst.forces.AbstractGaussianContributionContext
C / (2 * A * B) .
co2AB - Variable in class org.orekit.propagation.semianalytical.dsst.forces.FieldAbstractGaussianContributionContext
C / (2 * A * B) .
CodeBias - Class in org.orekit.gnss.metric.messages.common
Container for code bias data.
CodeBias(int, double) - Constructor for class org.orekit.gnss.metric.messages.common.CodeBias
Constructor.
CODELESS - org.orekit.gnss.SignalCode
Codeless.
coef - Variable in class org.orekit.propagation.analytical.tle.FieldTLEPropagator
coef for SGP C3 computation.
coef - Variable in class org.orekit.propagation.analytical.tle.TLEPropagator
coef for SGP C3 computation.
coef1 - Variable in class org.orekit.propagation.analytical.tle.FieldTLEPropagator
coef for SGP C5 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.
COHERENT - org.orekit.files.ccsds.ndm.tdm.RangeMode
Range tones coherent with uplink carrier.
COLLISION_MAX_PC_METHOD - org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadataKey
The method that was used to calculate the maximum collision probability.
COLLISION_MAX_PROBABILITY - org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadataKey
The maximum collision probability that Object1 and Object2 will collide.
COLLISION_PERCENTILE - org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadataKey
An array of 1 to n elements indicating the percentile(s) for which estimates of the collision probability are provided in the COLLISION_PROBABILITY variable.
COLLISION_PROBABILITY - org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadataKey
The probability (between 0.0 and 1.0) that Object1 and Object2 will collide.
COLLISION_PROBABILITY_METHOD - org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadataKey
The method that was used to calculate the collision probability.
COLUMN_DIM - Static variable in class org.orekit.propagation.AbstractStateCovarianceInterpolator
Default column dimension for position-velocity state covariance.
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(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 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(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.
COMBINED_RANGE_PHASE - org.orekit.gnss.MeasurementType
Combined pseudo-range carrier-phase measurement.
combinedDerivatives(FieldSpacecraftState<T>) - Method in interface org.orekit.propagation.integration.FieldAdditionalDerivativesProvider
Compute the derivatives related to the additional state (and optionally main state increments).
combinedDerivatives(SpacecraftState) - Method in class org.orekit.forces.maneuvers.jacobians.MassDepletionDelay
Compute the derivatives related to the additional state (and optionally main state increments).
combinedDerivatives(SpacecraftState) - Method in interface org.orekit.propagation.integration.AdditionalDerivativesProvider
Compute the derivatives related to the additional state (and optionally main state increments).
combinedDerivatives(SpacecraftState) - Method in class org.orekit.propagation.numerical.cr3bp.STMEquations
Compute the derivatives related to the additional state (and optionally main state increments).
combinedDerivatives(SpacecraftState) - Method in class org.orekit.propagation.numerical.EpochDerivativesEquations
Compute the derivatives related to the additional state (and optionally main state increments).
CombinedDerivatives - Class in org.orekit.propagation.integration
Container for additional derivatives.
CombinedDerivatives(double[], double[]) - Constructor for class org.orekit.propagation.integration.CombinedDerivatives
Simple constructor.
CombinedObservationData - Class in org.orekit.estimation.measurements.gnss
Combined observation data.
CombinedObservationData(double, double, CombinationType, MeasurementType, List<ObservationData>) - Constructor for class org.orekit.estimation.measurements.gnss.CombinedObservationData
Constructor.
CombinedObservationData(CombinationType, MeasurementType, double, double, List<ObservationData>) - Constructor for class org.orekit.estimation.measurements.gnss.CombinedObservationData
CombinedObservationDataSet - Class in org.orekit.estimation.measurements.gnss
Combined observation data set.
CombinedObservationDataSet(SatelliteSystem, int, AbsoluteDate, double, List<CombinedObservationData>) - Constructor for class org.orekit.estimation.measurements.gnss.CombinedObservationDataSet
Simple constructor.
COMMA_SEP - Static variable in exception org.orekit.errors.UnsupportedParameterException
Comma separator for printing list of supported parameter drivers.
COMMENT - org.orekit.files.ccsds.ndm.adm.acm.AttitudeCovarianceHistoryMetadataKey
Comment entry.
COMMENT - org.orekit.files.ccsds.ndm.adm.acm.AttitudeDeterminationKey
Comment entry.
COMMENT - org.orekit.files.ccsds.ndm.adm.acm.AttitudeManeuverKey
Comment entry.
COMMENT - org.orekit.files.ccsds.ndm.adm.acm.AttitudePhysicalPropertiesKey
Comment entry.
COMMENT - org.orekit.files.ccsds.ndm.adm.acm.AttitudeStateHistoryMetadataKey
Comment entry.
COMMENT - org.orekit.files.ccsds.ndm.adm.apm.AngularVelocityKey
Comment entry.
COMMENT - org.orekit.files.ccsds.ndm.adm.apm.ApmQuaternionKey
Comment entry.
COMMENT - org.orekit.files.ccsds.ndm.adm.apm.EulerKey
Comment entry.
COMMENT - org.orekit.files.ccsds.ndm.adm.apm.InertiaKey
Comment entry.
COMMENT - org.orekit.files.ccsds.ndm.adm.apm.ManeuverKey
Comment entry.
COMMENT - org.orekit.files.ccsds.ndm.adm.apm.SpinStabilizedKey
Comment entry.
COMMENT - org.orekit.files.ccsds.ndm.cdm.AdditionalCovarianceMetadataKey
Comment entry.
COMMENT - org.orekit.files.ccsds.ndm.cdm.AdditionalParametersKey
Comment entry.
COMMENT - org.orekit.files.ccsds.ndm.cdm.ODParametersKey
Comment entry.
COMMENT - org.orekit.files.ccsds.ndm.cdm.RTNCovarianceKey
Comment entry.
COMMENT - org.orekit.files.ccsds.ndm.cdm.SigmaEigenvectorsCovarianceKey
Comment entry.
COMMENT - org.orekit.files.ccsds.ndm.cdm.StateVectorKey
Comment entry.
COMMENT - org.orekit.files.ccsds.ndm.cdm.XmlSubStructureKey
General comment.
COMMENT - org.orekit.files.ccsds.ndm.cdm.XYZCovarianceKey
Comment entry.
COMMENT - org.orekit.files.ccsds.ndm.odm.CartesianCovarianceKey
Comment entry.
COMMENT - org.orekit.files.ccsds.ndm.odm.KeplerianElementsKey
Comment entry.
COMMENT - org.orekit.files.ccsds.ndm.odm.ocm.OrbitCovarianceHistoryMetadataKey
Comment entry.
COMMENT - org.orekit.files.ccsds.ndm.odm.ocm.OrbitDeterminationKey
Comment entry.
COMMENT - org.orekit.files.ccsds.ndm.odm.ocm.OrbitManeuverHistoryMetadataKey
Comment entry.
COMMENT - org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalPropertiesKey
Comment entry.
COMMENT - org.orekit.files.ccsds.ndm.odm.ocm.PerturbationsKey
Comment entry.
COMMENT - org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadataKey
Comment entry.
COMMENT - org.orekit.files.ccsds.ndm.odm.omm.OmmTleKey
Comment entry.
COMMENT - org.orekit.files.ccsds.ndm.odm.opm.ManeuverKey
Comment entry.
COMMENT - org.orekit.files.ccsds.ndm.odm.SpacecraftParametersKey
Comment entry.
COMMENT - org.orekit.files.ccsds.ndm.odm.StateVectorKey
Comment entry.
COMMENT - org.orekit.files.ccsds.ndm.tdm.TdmDataKey
Comment entry.
COMMENT - org.orekit.files.ccsds.section.HeaderKey
Header comment.
COMMENT - org.orekit.files.ccsds.section.MetadataKey
Comment entry.
COMMENT - org.orekit.files.rinex.section.RinexLabels
Comments.
CommentsContainer - Class in org.orekit.files.ccsds.section
Container for comments in various CCSDS messages.
CommentsContainer() - Constructor for class org.orekit.files.ccsds.section.CommentsContainer
Create a new meta-data.
CommonGnssData - Class in org.orekit.propagation.analytical.gnss.data
Container for common GNSS data contained in almanac and navigation messages.
CommonGnssData(double, double, int) - Constructor for class org.orekit.propagation.analytical.gnss.data.CommonGnssData
Constructor.
CommonMetadataKey - Enum in org.orekit.files.ccsds.ndm.odm
Keys for common ODM container entries.
CommonMetadataWriter - Class in org.orekit.files.ccsds.ndm.odm
Writer for Common metadata for CCSDS Orbit Parameter/Ephemeris/Mean Messages.
CommonMetadataWriter(OdmCommonMetadata, TimeConverter) - Constructor for class org.orekit.files.ccsds.ndm.odm.CommonMetadataWriter
Simple constructor.
CommonParametersWithDerivatives - Class in org.orekit.estimation.measurements
Common intermediate parameters used to estimate measurements where receiver is a ground station.
CommonParametersWithDerivatives(SpacecraftState, Map<String, Integer>, Gradient, SpacecraftState, TimeStampedFieldPVCoordinates<Gradient>) - Constructor for class org.orekit.estimation.measurements.CommonParametersWithDerivatives
Simple constructor.
CommonParametersWithoutDerivatives - Class in org.orekit.estimation.measurements
Common intermediate parameters used to estimate measurements.
CommonParametersWithoutDerivatives(SpacecraftState, double, SpacecraftState, TimeStampedPVCoordinates) - Constructor for class org.orekit.estimation.measurements.CommonParametersWithoutDerivatives
Simple constructor.
CommonPhysicalProperties - Class in org.orekit.files.ccsds.ndm
Container for common physical properties for both OrbitPhysicalProperties and AdditionalParameters.
CommonPhysicalProperties() - Constructor for class org.orekit.files.ccsds.ndm.CommonPhysicalProperties
Simple constructor.
ComparableMeasurement - Interface in org.orekit.estimation.measurements
Base interface for comparing measurements regardless of their type.
compare(IntegerLeastSquareSolution, IntegerLeastSquareSolution) - Method in class org.orekit.estimation.measurements.gnss.IntegerLeastSquareComparator
The comparison is based on the squared distance to the float solution.
compare(FieldTimeStamped<KK>, FieldTimeStamped<KK>) - Method in class org.orekit.time.FieldChronologicalComparator
Compare two time-stamped instances.
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(AbstractSolarActivityDataLoader.LineParameters) - Method in class org.orekit.models.earth.atmosphere.data.AbstractSolarActivityDataLoader.LineParameters
compareTo(AbstractSolarActivityDataLoader.LineParameters) - Method in class org.orekit.models.earth.atmosphere.data.CssiSpaceWeatherDataLoader.LineParameters
compareTo(AbstractSolarActivityDataLoader.LineParameters) - Method in class org.orekit.models.earth.atmosphere.data.MarshallSolarActivityFutureEstimationLoader.LineParameters
compareTo(CoefficientsFactory.NSKey) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.CoefficientsFactory.NSKey
compareTo(AbsoluteDate) - Method in class org.orekit.time.AbsoluteDate
Compare the instance with another date.
compareTo(DateComponents) - Method in class org.orekit.time.DateComponents
compareTo(DateTimeComponents) - Method in class org.orekit.time.DateTimeComponents
compareTo(FieldAbsoluteDate<T>) - Method in class org.orekit.time.FieldAbsoluteDate
Compare the instance with another date.
compareTo(TimeComponents) - Method in class org.orekit.time.TimeComponents
COMPASS - org.orekit.files.sp3.SP3FileType
COMPASS only file.
compile(PoissonSeries...) - Static method in class org.orekit.data.PoissonSeries
Join several nutation series, for fast simultaneous evaluation.
complain(String, boolean) - Method in class org.orekit.files.ccsds.utils.generation.AbstractGenerator
Complain about a missing value.
completed() - Method in class org.orekit.files.ccsds.ndm.odm.opm.Maneuver
Check if maneuver has been completed.
components(AbsoluteDate) - Method in class org.orekit.files.ccsds.definitions.TimeConverter
Generate calendar components.
compose(AbsoluteDate, KinematicTransform, KinematicTransform) - Static method in interface org.orekit.frames.KinematicTransform
Build a transform by combining two existing ones.
compose(AbsoluteDate, StaticTransform, StaticTransform) - Static method in interface org.orekit.frames.StaticTransform
Build a transform by combining two existing ones.
compose(FieldAbsoluteDate<T>, FieldKinematicTransform<T>, FieldKinematicTransform<T>) - Static method in interface org.orekit.frames.FieldKinematicTransform
Build a transform by combining two existing ones.
compose(FieldAbsoluteDate<T>, FieldStaticTransform<T>, FieldStaticTransform<T>) - Static method in interface org.orekit.frames.FieldStaticTransform
Build a transform by combining two existing ones.
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.
compositeRotation(FieldStaticTransform<T>, FieldStaticTransform<T>) - Static method in interface org.orekit.frames.FieldStaticTransform
Compute a composite rotation.
compositeRotation(StaticTransform, StaticTransform) - Static method in interface org.orekit.frames.StaticTransform
Compute a composite rotation.
compositeRotationRate(FieldKinematicTransform<T>, FieldKinematicTransform<T>) - Static method in interface org.orekit.frames.FieldKinematicTransform
Compute a composite rotation rate.
compositeRotationRate(KinematicTransform, KinematicTransform) - Static method in interface org.orekit.frames.KinematicTransform
Compute a composite rotation rate.
compositeTranslation(FieldStaticTransform<T>, FieldStaticTransform<T>) - Static method in interface org.orekit.frames.FieldStaticTransform
Compute a composite translation.
compositeTranslation(StaticTransform, StaticTransform) - Static method in interface org.orekit.frames.StaticTransform
Compute a composite translation.
compositeVelocity(FieldKinematicTransform<T>, FieldKinematicTransform<T>) - Static method in interface org.orekit.frames.FieldKinematicTransform
Compute a composite velocity.
compositeVelocity(KinematicTransform, KinematicTransform) - Static method in interface org.orekit.frames.KinematicTransform
Compute a composite velocity.
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.
compute(double, double, double, double, double) - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.AbstractAlfriend1999
Compute the probability of collision using arguments specific to the rotated encounter frame.
compute(double, double, double, double, double) - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.AbstractShortTermEncounter1DNumerical2DPOCMethod
Compute the probability of collision using arguments specific to the rotated encounter frame.
compute(double, double, double, double, double) - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.Alfano2005
Compute the probability of collision using arguments specific to the rotated encounter frame.
compute(double, double, double, double, double) - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.Chan1997
Compute the probability of collision using arguments specific to the rotated encounter frame.
compute(double, double, double, double, double) - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.Laas2015
Compute the probability of collision using arguments specific to the rotated encounter frame.
compute(double, double, double, double, double) - Method in interface org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DPOCMethod
Compute the probability of collision using arguments specific to the rotated encounter frame.
compute(double, double, double, double, double, UnivariateIntegrator, int) - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.AbstractShortTermEncounter1DNumerical2DPOCMethod
Compute the probability of collision using arguments specific to the rotated encounter frame and custom numerical configuration.
compute(double, double, double, double, double, UnivariateIntegrator, int) - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.Patera2005
Compute the probability of collision using arguments specific to the rotated encounter frame and custom numerical configuration.
compute(Cdm, double) - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.AbstractShortTermEncounter2DPOCMethod
Compute the probability of collision using a Conjunction Data Message (CDM).
compute(Cdm, double) - Method in interface org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DPOCMethod
Compute the probability of collision using a Conjunction Data Message (CDM).
compute(Cdm, double, double) - Method in interface org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DPOCMethod
Compute the probability of collision using a Conjunction Data Message (CDM).
compute(Cdm, double, double, UnivariateIntegrator, int, double) - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.AbstractShortTermEncounter1DNumerical2DPOCMethod
Compute the probability of collision using an Orekit Conjunction Data Message.
compute(Cdm, T) - Method in interface org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DPOCMethod
Compute the probability of collision using a Conjunction Data Message (CDM).
compute(Cdm, T, double) - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.AbstractShortTermEncounter2DPOCMethod
Compute the probability of collision using a Conjunction Data Message (CDM).
compute(Cdm, T, double) - Method in interface org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DPOCMethod
Compute the probability of collision using a Conjunction Data Message (CDM).
compute(Cdm, T, T) - Method in interface org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DPOCMethod
Compute the probability of collision using a Conjunction Data Message (CDM).
compute(Cdm, T, T, FieldUnivariateIntegrator<T>, int, double) - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.AbstractShortTermEncounter1DNumerical2DPOCMethod
Compute the probability of collision using an Orekit Conjunction Data Message.
compute(FieldOrbit<T>, FieldStateCovariance<T>, FieldOrbit<T>, FieldStateCovariance<T>, T) - Method in interface org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DPOCMethod
Compute the probability of collision using parameters necessary for creating a collision definition instance.
compute(FieldOrbit<T>, FieldStateCovariance<T>, FieldOrbit<T>, FieldStateCovariance<T>, T, double) - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.AbstractShortTermEncounter2DPOCMethod
Compute the probability of collision using parameters necessary for creating a collision definition instance.
compute(FieldOrbit<T>, FieldStateCovariance<T>, FieldOrbit<T>, FieldStateCovariance<T>, T, double) - Method in interface org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DPOCMethod
Compute the probability of collision using parameters necessary for creating a collision definition instance.
compute(FieldOrbit<T>, FieldStateCovariance<T>, T, FieldOrbit<T>, FieldStateCovariance<T>, T) - Method in interface org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DPOCMethod
Compute the probability of collision using parameters necessary for creating a collision definition instance.
compute(FieldOrbit<T>, FieldStateCovariance<T>, T, FieldOrbit<T>, FieldStateCovariance<T>, T, FieldUnivariateIntegrator<T>, int, double) - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.AbstractShortTermEncounter1DNumerical2DPOCMethod
Compute the probability of collision using parameters necessary for creating a collision definition instance.
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(Orbit, StateCovariance, double, Orbit, StateCovariance, double) - Method in interface org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DPOCMethod
Compute the probability of collision using parameters necessary for creating a collision definition instance.
compute(Orbit, StateCovariance, double, Orbit, StateCovariance, double, UnivariateIntegrator, int, double) - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.AbstractShortTermEncounter1DNumerical2DPOCMethod
Compute the probability of collision using parameters necessary for creating a collision definition instance.
compute(Orbit, StateCovariance, Orbit, StateCovariance, double) - Method in interface org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DPOCMethod
Compute the probability of collision using parameters necessary for creating a collision definition instance.
compute(Orbit, StateCovariance, Orbit, StateCovariance, double, double) - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.AbstractShortTermEncounter2DPOCMethod
Compute the probability of collision using parameters necessary for creating a collision definition instance.
compute(Orbit, StateCovariance, Orbit, StateCovariance, double, double) - Method in interface org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DPOCMethod
Compute the probability of collision using parameters necessary for creating a collision definition instance.
compute(FieldShortTermEncounter2DDefinition<T>) - Method in interface org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DPOCMethod
Compute the probability of collision using given collision definition.
compute(FieldShortTermEncounter2DDefinition<T>, double) - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.AbstractShortTermEncounter2DPOCMethod
Compute the probability of collision using given collision definition.
compute(FieldShortTermEncounter2DDefinition<T>, double) - Method in interface org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DPOCMethod
Compute the probability of collision using given collision definition.
compute(FieldShortTermEncounter2DDefinition<T>, FieldUnivariateIntegrator<T>, int, double) - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.AbstractShortTermEncounter1DNumerical2DPOCMethod
Compute the probability of collision using given collision definition.
compute(ShortTermEncounter2DDefinition) - Method in interface org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DPOCMethod
Compute the probability of collision using given collision definition.
compute(ShortTermEncounter2DDefinition, double) - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.AbstractShortTermEncounter2DPOCMethod
Compute the probability of collision using given collision definition.
compute(ShortTermEncounter2DDefinition, double) - Method in interface org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DPOCMethod
Compute the probability of collision using given collision definition.
compute(ShortTermEncounter2DDefinition, UnivariateIntegrator, int, double) - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.AbstractShortTermEncounter1DNumerical2DPOCMethod
Compute the probability of collision using a given collision definition.
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(T, T, T, T, T) - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.AbstractAlfriend1999
Compute the probability of collision using arguments specific to the rotated encounter frame.
compute(T, T, T, T, T) - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.AbstractShortTermEncounter1DNumerical2DPOCMethod
Compute the probability of collision using arguments specific to the rotated encounter frame.
compute(T, T, T, T, T) - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.Alfano2005
Compute the probability of collision using arguments specific to the rotated encounter frame.
compute(T, T, T, T, T) - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.Chan1997
Compute the probability of collision using arguments specific to the rotated encounter frame.
compute(T, T, T, T, T) - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.Laas2015
Compute the probability of collision using arguments specific to the rotated encounter frame.
compute(T, T, T, T, T) - Method in interface org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DPOCMethod
Compute the probability of collision using arguments specific to the rotated encounter frame.
compute(T, T, T, T, T, FieldUnivariateIntegrator<T>, int) - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.AbstractShortTermEncounter1DNumerical2DPOCMethod
Compute the probability of collision using arguments specific to the rotated encounter frame and custom numerical configuration.
compute(T, T, T, T, T, FieldUnivariateIntegrator<T>, int) - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.Patera2005
Compute the probability of collision using arguments specific to the rotated encounter frame and custom numerical configuration.
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.
computeAlbedo(AbsoluteDate, double) - Method in class org.orekit.forces.radiation.KnockeRediffusedForceModel
Compute Earth albedo.
computeAlbedo(FieldAbsoluteDate<T>, T) - Method in class org.orekit.forces.radiation.KnockeRediffusedForceModel
Compute Earth albedo.
computeC2Z(DSSTJ2SquaredClosedFormContext) - Method in class org.orekit.propagation.semianalytical.dsst.forces.ZeisModel
Get the value of the Zeis constant.
computeC2Z(FieldDSSTJ2SquaredClosedFormContext<T>) - Method in class org.orekit.propagation.semianalytical.dsst.forces.ZeisModel
Get the value of the Zeis constant.
computeCombinedCovarianceInEncounterFrame() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.FieldShortTermEncounter2DDefinition
Compute the combined covariance expressed in the encounter frame.
computeCombinedCovarianceInEncounterFrame() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DDefinition
Compute the combined covariance expressed in the encounter frame.
computeCombinedCovarianceInReferenceTNW() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.FieldShortTermEncounter2DDefinition
Takes both covariance matrices (expressed in their respective RTN local orbital frame) from reference and other collision object with which this instance was created and sum them in the reference collision object TNW local orbital frame.
computeCombinedCovarianceInReferenceTNW() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DDefinition
Takes both covariance matrices (expressed in their respective RTN local orbital frame) from reference and other collision object with which this instance was created and sum them in the reference collision object TNW local orbital frame.
computeCommonParametersWith(SpacecraftState[], boolean) - Method in class org.orekit.estimation.measurements.gnss.AbstractOnBoardMeasurement
Compute common estimation parameters.
computeCommonParametersWithDerivatives(SpacecraftState) - Method in class org.orekit.estimation.measurements.GroundReceiverMeasurement
Compute common estimation parameters.
computeCommonParametersWithout(SpacecraftState) - Method in class org.orekit.estimation.measurements.GroundReceiverMeasurement
Compute common estimation parameters.
computeCommonParametersWithout(SpacecraftState[], boolean) - Method in class org.orekit.estimation.measurements.gnss.AbstractOnBoardMeasurement
Compute common estimation parameters.
computeCoppolaEncounterDuration() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.FieldShortTermEncounter2DDefinition
Compute the Encounter duration (s) evaluated using Coppola's formula described in : "COPPOLA, Vincent, et al.
computeCoppolaEncounterDuration() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DDefinition
Compute the Encounter duration (s) evaluated using Coppola's formula described in : "COPPOLA, Vincent, et al.
computeDeltaPV(FieldSpacecraftState<T>) - Method in class org.orekit.propagation.events.FieldExtremumApproachDetector
Deprecated.
The output type of this method shall be modified in the future to improve code efficiency (though it will still give access to the relative position and velocity)
computeDeltaPV(SpacecraftState) - Method in class org.orekit.propagation.events.ExtremumApproachDetector
Deprecated.
The output type of this method shall be modified in the future to improve code efficiency (though it will still give access to the relative position and velocity)
computeDerivatives(FieldSpacecraftState<T>) - Method in interface org.orekit.propagation.integration.FieldAbstractIntegratedPropagator.MainStateEquations
Compute differential equations for main state.
computeDerivatives(SpacecraftState) - Method in interface org.orekit.propagation.integration.AbstractIntegratedPropagator.MainStateEquations
Compute differential equations for main state.
computeElementaryFlux(FieldSpacecraftState<T>, FieldVector3D<T>, FieldVector3D<T>, OneAxisEllipsoid, T) - Method in class org.orekit.forces.radiation.KnockeRediffusedForceModel
Compute elementary rediffused flux on satellite.
computeElementaryFlux(SpacecraftState, Vector3D, Vector3D, OneAxisEllipsoid, double) - Method in class org.orekit.forces.radiation.KnockeRediffusedForceModel
Compute elementary rediffused flux on satellite.
computeEmissivity(AbsoluteDate, double) - Method in class org.orekit.forces.radiation.KnockeRediffusedForceModel
Compute Earth emisivity.
computeEmissivity(FieldAbsoluteDate<T>, T) - Method in class org.orekit.forces.radiation.KnockeRediffusedForceModel
Compute Earth emisivity.
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.
computeHeightCorrection(double, double) - Static method in class org.orekit.models.earth.troposphere.TroposphericModelUtils
This method computes the height correction for the hydrostatic component of the mapping function.
computeHeightCorrection(T, T, Field<T>) - Static method in class org.orekit.models.earth.troposphere.TroposphericModelUtils
This method computes the height correction for the hydrostatic component of the mapping function.
computeInitValues(double) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenZonalLinear
Compute the roots for the Hansen coefficients and their derivatives.
computeInitValues(double, double, double) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenTesseralLinear
Compute the values for the first four coefficients and their derivatives by means of series.
computeInitValues(double, double, double) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.HansenThirdBodyLinear
Compute the initial values (see Collins, 4-255, 4-256 and 4.259)
computeInitValues(T) - Method in class org.orekit.propagation.semianalytical.dsst.utilities.hansen.FieldHansenZonalLinear
Compute the roots for the Hansen coefficients and their derivatives.
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)
computeInnovationVector(EstimatedMeasurement<?>) - Static method in class org.orekit.estimation.sequential.KalmanEstimatorUtil
Compute the unnormalized innovation vector from the given predicted measurement.
computeInnovationVector(EstimatedMeasurement<?>, double[]) - Static method in class org.orekit.estimation.sequential.KalmanEstimatorUtil
Compute the normalized innovation vector from the given predicted measurement.
computeInterpolatedCovarianceInOrbitFrame(List<TimeStampedPair<Orbit, StateCovariance>>, Orbit) - Method in class org.orekit.propagation.AbstractStateCovarianceInterpolator
Compute the interpolated covariance expressed in the interpolated orbit frame.
computeInterpolatedCovarianceInOrbitFrame(List<TimeStampedPair<Orbit, StateCovariance>>, Orbit) - Method in class org.orekit.propagation.StateCovarianceBlender
Compute the interpolated covariance expressed in the interpolated orbit frame.
computeInterpolatedCovarianceInOrbitFrame(List<TimeStampedPair<Orbit, StateCovariance>>, Orbit) - Method in class org.orekit.propagation.StateCovarianceKeplerianHermiteInterpolator
Compute the interpolated covariance expressed in the interpolated orbit frame.
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.
computeKeplerianDurationFromPreviousApoapsis(double, double) - Static method in class org.orekit.propagation.events.intervals.ApsideDetectionAdaptableIntervalFactory
Method computing time elapsed since last apoapsis, assuming Keplerian motion.
computeKeplerianDurationFromPreviousPeriapsis(double, double) - Static method in class org.orekit.propagation.events.intervals.ApsideDetectionAdaptableIntervalFactory
Method computing time elapsed since last periapsis, assuming Keplerian motion.
computeLimitVisibilityPoint(double, double, double) - Method in class org.orekit.frames.TopocentricFrame
Compute the limit visibility point for a satellite in a given direction.
computeLyapunov() - 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.
computeMahalanobisDistance() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.FieldShortTermEncounter2DDefinition
Compute the Mahalanobis distance computed with the other collision object projected onto the collision plane (commonly called B-Plane) and expressed in the rotated encounter frame (frame in which the combined covariance matrix is diagonalized, see FieldShortTermEncounter2DDefinition.computeEncounterPlaneRotationMatrix(double) for more details).
computeMahalanobisDistance() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DDefinition
Compute the Mahalanobis distance computed with the other collision object projected onto the collision plane (commonly called B-Plane) and expressed in the rotated encounter frame (frame in which the combined covariance matrix is diagonalized, see ShortTermEncounter2DDefinition.computeEncounterPlaneRotationMatrix(double) for more details).
computeMahalanobisDistance(double) - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.FieldShortTermEncounter2DDefinition
Compute the Mahalanobis distance computed with the other collision object projected onto the collision plane (commonly called B-Plane) and expressed in the rotated encounter frame (frame in which the combined covariance matrix is diagonalized, see FieldShortTermEncounter2DDefinition.computeEncounterPlaneRotationMatrix(double) for more details).
computeMahalanobisDistance(double) - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DDefinition
Compute the Mahalanobis distance computed with the other collision object projected onto the collision plane (commonly called B-Plane) and expressed in the rotated encounter frame (frame in which the combined covariance matrix is diagonalized, see ShortTermEncounter2DDefinition.computeEncounterPlaneRotationMatrix(double) for more details).
computeMeanEquinoctialSecondOrderTerms(DSSTJ2SquaredClosedFormContext) - Method in interface org.orekit.propagation.semianalytical.dsst.forces.J2SquaredModel
Compute the J2-squared second-order terms in equinoctial elements.
computeMeanEquinoctialSecondOrderTerms(DSSTJ2SquaredClosedFormContext) - Method in class org.orekit.propagation.semianalytical.dsst.forces.ZeisModel
Compute the J2-squared second-order terms in equinoctial elements.
computeMeanEquinoctialSecondOrderTerms(FieldDSSTJ2SquaredClosedFormContext<T>) - Method in interface org.orekit.propagation.semianalytical.dsst.forces.J2SquaredModel
Compute the J2-squared second-order terms in equinoctial elements.
computeMeanEquinoctialSecondOrderTerms(FieldDSSTJ2SquaredClosedFormContext<T>) - Method in class org.orekit.propagation.semianalytical.dsst.forces.ZeisModel
Compute the J2-squared second-order terms in equinoctial elements.
computeMeanOrbit(FieldOrbit<T>, double, double, double, double, double, double, double, double, int) - Static method in class org.orekit.propagation.analytical.FieldBrouwerLyddanePropagator
Conversion from osculating to mean orbit.
computeMeanOrbit(FieldOrbit<T>, double, double, double, double, double, double, double, double, int) - Static method in class org.orekit.propagation.analytical.FieldEcksteinHechlerPropagator
Conversion from osculating to mean orbit.
computeMeanOrbit(FieldOrbit<T>, UnnormalizedSphericalHarmonicsProvider, UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics) - Static method in class org.orekit.propagation.analytical.FieldEcksteinHechlerPropagator
Conversion from osculating to mean orbit.
computeMeanOrbit(FieldOrbit<T>, UnnormalizedSphericalHarmonicsProvider, UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics, double) - Static method in class org.orekit.propagation.analytical.FieldBrouwerLyddanePropagator
Conversion from osculating to mean orbit.
computeMeanOrbit(FieldOrbit<T>, UnnormalizedSphericalHarmonicsProvider, UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics, double, double, int) - Static method in class org.orekit.propagation.analytical.FieldBrouwerLyddanePropagator
Conversion from osculating to mean orbit.
computeMeanOrbit(FieldOrbit<T>, UnnormalizedSphericalHarmonicsProvider, UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics, double, int) - Static method in class org.orekit.propagation.analytical.FieldEcksteinHechlerPropagator
Conversion from osculating to mean orbit.
computeMeanOrbit(Orbit, double, double, double, double, double, double, double, double, int) - Static method in class org.orekit.propagation.analytical.BrouwerLyddanePropagator
Conversion from osculating to mean orbit.
computeMeanOrbit(Orbit, double, double, double, double, double, double, double, double, int) - Static method in class org.orekit.propagation.analytical.EcksteinHechlerPropagator
Conversion from osculating to mean orbit.
computeMeanOrbit(Orbit, UnnormalizedSphericalHarmonicsProvider, UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics) - Static method in class org.orekit.propagation.analytical.EcksteinHechlerPropagator
Conversion from osculating to mean orbit.
computeMeanOrbit(Orbit, UnnormalizedSphericalHarmonicsProvider, UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics, double) - Static method in class org.orekit.propagation.analytical.BrouwerLyddanePropagator
Conversion from osculating to mean orbit.
computeMeanOrbit(Orbit, UnnormalizedSphericalHarmonicsProvider, UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics, double, double, int) - Static method in class org.orekit.propagation.analytical.BrouwerLyddanePropagator
Conversion from osculating to mean orbit.
computeMeanOrbit(Orbit, UnnormalizedSphericalHarmonicsProvider, UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics, double, int) - Static method in class org.orekit.propagation.analytical.EcksteinHechlerPropagator
Conversion from osculating to mean orbit.
computeMeanState(FieldSpacecraftState<T>, AttitudeProvider, Collection<DSSTForceModel>) - Static method in class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator
Conversion from osculating to mean orbit.
computeMeanState(FieldSpacecraftState<T>, AttitudeProvider, Collection<DSSTForceModel>, double, int) - Static method in class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator
Conversion from osculating to mean orbit.
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.
computeMissDistance() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.FieldShortTermEncounter2DDefinition
Compute the miss distance at time of closest approach.
computeMissDistance() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DDefinition
Compute the miss distance at time of closest approach.
computeOsculatingState(FieldSpacecraftState<T>, AttitudeProvider, Collection<DSSTForceModel>) - Static method in class org.orekit.propagation.semianalytical.dsst.FieldDSSTPropagator
Conversion from mean to osculating orbit.
computeOsculatingState(SpacecraftState, AttitudeProvider, Collection<DSSTForceModel>) - Static method in class org.orekit.propagation.semianalytical.dsst.DSSTPropagator
Conversion from mean to osculating orbit.
computeOtherPositionInCollisionPlane() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.FieldShortTermEncounter2DDefinition
Compute the other collision object position projected onto the collision plane.
computeOtherPositionInCollisionPlane() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DDefinition
Compute the other collision object position projected onto the collision plane.
computeOtherPositionInRotatedCollisionPlane() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.FieldShortTermEncounter2DDefinition
Compute the other collision object position in the rotated collision plane.
computeOtherPositionInRotatedCollisionPlane() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DDefinition
Compute the other collision object position in the rotated collision plane.
computeOtherPositionInRotatedCollisionPlane(double) - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.FieldShortTermEncounter2DDefinition
Compute the other collision object position in the rotated collision plane.
computeOtherPositionInRotatedCollisionPlane(double) - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DDefinition
Compute the other collision object position in the rotated collision plane.
computeOtherRelativeToReferencePVInReferenceInertial() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.FieldShortTermEncounter2DDefinition
Compute the other collision position and velocity relative to the reference collision object.
computeOtherRelativeToReferencePVInReferenceInertial() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DDefinition
Compute the other collision position and velocity relative to the reference collision object.
computeProjectedAndDiagonalizedCombinedPositionalCovarianceMatrix() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.FieldShortTermEncounter2DDefinition
Compute the combined covariance matrix diagonalized and projected onto the collision plane.
computeProjectedAndDiagonalizedCombinedPositionalCovarianceMatrix() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DDefinition
Compute the combined covariance matrix diagonalized and projected onto the collision plane.
computeProjectedCombinedPositionalCovarianceMatrix() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.FieldShortTermEncounter2DDefinition
Compute the projected combined covariance matrix onto the collision plane.
computeProjectedCombinedPositionalCovarianceMatrix() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DDefinition
Compute the projected combined covariance matrix onto the collision plane.
computeProjectionMatrix() - Method in interface org.orekit.frames.encounter.EncounterLOF
Get the 2x3 projection matrix that projects values expressed in this encounter local orbital frame to the collision plane.
computeProjectionMatrix(Field<T>) - Method in interface org.orekit.frames.encounter.EncounterLOF
Get the 2x3 projection matrix that projects values expressed in this encounter local orbital frame to the collision plane defined by this same encounter local orbital frame.
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).
computeReferenceInertialToCollisionPlaneProjectionMatrix() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.FieldShortTermEncounter2DDefinition
Compute the projection matrix from the reference collision object inertial frame to the collision plane.
computeReferenceInertialToCollisionPlaneProjectionMatrix() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DDefinition
Compute the projection matrix from the reference collision object inertial frame to the collision plane.
computeSolarFlux(FieldVector3D<T>) - Method in class org.orekit.forces.radiation.KnockeRediffusedForceModel
Compute total solar flux impacting Earth.
computeSolarFlux(Vector3D) - Method in class org.orekit.forces.radiation.KnockeRediffusedForceModel
Compute total solar flux impacting Earth.
computeSquaredMahalanobisDistance() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.FieldShortTermEncounter2DDefinition
Compute the squared Mahalanobis distance computed with the other collision object projected onto the collision plane (commonly called B-Plane) and expressed in the rotated encounter frame (frame in which the combined covariance matrix is diagonalized, see FieldShortTermEncounter2DDefinition.computeEncounterPlaneRotationMatrix(double) for more details).
computeSquaredMahalanobisDistance() - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DDefinition
Compute the squared Mahalanobis distance computed with the other collision object projected onto the collision plane (commonly called B-Plane) and expressed in the rotated encounter frame (frame in which the combined covariance matrix is diagonalized, see ShortTermEncounter2DDefinition.computeEncounterPlaneRotationMatrix(double) for more details).
computeSquaredMahalanobisDistance(double) - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.FieldShortTermEncounter2DDefinition
Compute the squared Mahalanobis distance computed with the other collision object projected onto the collision plane (commonly called B-Plane) and expressed in the rotated encounter frame (frame in which the combined covariance matrix is diagonalized, see FieldShortTermEncounter2DDefinition.computeEncounterPlaneRotationMatrix(double) for more details).
computeSquaredMahalanobisDistance(double) - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DDefinition
Compute the squared Mahalanobis distance computed with the other collision object projected onto the collision plane (commonly called B-Plane) and expressed in the rotated encounter frame (frame in which the combined covariance matrix is diagonalized, see ShortTermEncounter2DDefinition.computeEncounterPlaneRotationMatrix(double) for more details).
computeSquaredMahalanobisDistance(double, double, double, double) - Static method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DDefinition
Compute the squared Mahalanobis distance.
computeSquaredMahalanobisDistance(FieldVector2D<T>, FieldMatrix<T>) - Static method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.FieldShortTermEncounter2DDefinition
Compute the squared Mahalanobis distance.
computeSquaredMahalanobisDistance(Vector2D, RealMatrix) - Static method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.ShortTermEncounter2DDefinition
Compute the squared Mahalanobis distance.
computeSquaredMahalanobisDistance(T, T, T, T) - Static method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.FieldShortTermEncounter2DDefinition
Compute the squared Mahalanobis distance.
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.
computeValue(double, double, double) - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.Alfriend1999Max
Compute the value of the probability of collision.
computeValue(T, T, T) - Method in class org.orekit.ssa.collision.shorttermencounter.probability.twod.Alfriend1999Max
Compute the value of the probability of collision.
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(FieldGeodeticPoint<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(FieldGeodeticPoint<T>, T[], FieldAbsoluteDate<T>) - Method in class org.orekit.models.earth.troposphere.ViennaOneModel
Deprecated.
This method allows the computation of the zenith hydrostatic and zenith wet delay.
computeZenithDelay(FieldGeodeticPoint<T>, T[], FieldAbsoluteDate<T>) - Method in class org.orekit.models.earth.troposphere.ViennaThreeModel
Deprecated.
This method allows the computation of the zenith hydrostatic and zenith wet delay.
computeZenithDelay(GeodeticPoint, 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(GeodeticPoint, double[], AbsoluteDate) - Method in class org.orekit.models.earth.troposphere.ViennaOneModel
Deprecated.
This method allows the computation of the zenith hydrostatic and zenith wet delay.
computeZenithDelay(GeodeticPoint, double[], AbsoluteDate) - Method in class org.orekit.models.earth.troposphere.ViennaThreeModel
Deprecated.
This method allows the computation of the zenith hydrostatic and zenith wet delay.
CONE - org.orekit.files.ccsds.ndm.odm.ocm.ShadowModel
Cone model, umbra only.
ConfigurableLowThrustManeuver - Class in org.orekit.forces.maneuvers
This class implements a configurable low thrust maneuver.
ConfigurableLowThrustManeuver(ThrustDirectionAndAttitudeProvider, ManeuverTriggers, double, double) - Constructor for class org.orekit.forces.maneuvers.ConfigurableLowThrustManeuver
Constructor.
configureHarvester(Propagator) - Method in class org.orekit.estimation.leastsquares.AbstractBatchLSModel
Configure the propagator to compute derivatives.
configureHarvester(Propagator) - Method in class org.orekit.estimation.leastsquares.BatchLSModel
Configure the propagator to compute derivatives.
configureHarvester(Propagator) - Method in class org.orekit.estimation.leastsquares.DSSTBatchLSModel
Configure the propagator to compute derivatives.
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.
configureOrbits(MatricesHarvester, Propagator) - Method in class org.orekit.estimation.leastsquares.AbstractBatchLSModel
Configure the current estimated orbits.
configureOrbits(MatricesHarvester, Propagator) - Method in class org.orekit.estimation.leastsquares.BatchLSModel
Configure the current estimated orbits.
configureOrbits(MatricesHarvester, Propagator) - Method in class org.orekit.estimation.leastsquares.DSSTBatchLSModel
Configure the current estimated orbits.
CONJUNCTION_ID - org.orekit.files.ccsds.ndm.cdm.CdmRelativeMetadataKey
The Originator’s ID that uniquely identifies the conjunction to which the message refers.
CONNECTION_ERROR - org.orekit.errors.OrekitMessages
CONNECTION_ERROR.
CONSIDER_N - org.orekit.files.ccsds.ndm.odm.ocm.OrbitDeterminationKey
Number of consider parameters.
CONSIDER_PARAMS - org.orekit.files.ccsds.ndm.odm.ocm.OrbitDeterminationKey
Description of consider parameters.
CONSTANT - org.orekit.files.ccsds.ndm.tdm.RangeMode
Range tones have constant frequency.
constantAfter() - Method in class org.orekit.utils.WaypointPVBuilder
Indicate the resulting PVCoordinatesProvider provide a constant location of the last waypoint after to the last time.
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.
ConstantAzimuthalGradientProvider - Class in org.orekit.models.earth.troposphere
ConstantAzimuthalGradientProvider(AzimuthalGradientCoefficients) - Constructor for class org.orekit.models.earth.troposphere.ConstantAzimuthalGradientProvider
Simple constructor.
constantBefore() - Method in class org.orekit.utils.WaypointPVBuilder
Indicate the resulting PVCoordinatesProvider provide a constant location of the first waypoint prior to the first time.
ConstantOffsetTimeScale - Class in org.orekit.time
Base class for time scales with constant offset with respecto to TAI.
ConstantOffsetTimeScale(String, double) - Constructor for class org.orekit.time.ConstantOffsetTimeScale
Simple constructor.
ConstantPressureTemperatureHumidityProvider - Class in org.orekit.models.earth.weather
Provider for constant weather parameters.
ConstantPressureTemperatureHumidityProvider(PressureTemperatureHumidity) - Constructor for class org.orekit.models.earth.weather.ConstantPressureTemperatureHumidityProvider
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.
ConstantPVCoordinatesProvider - Class in org.orekit.utils
Provider based on a single point.
ConstantPVCoordinatesProvider(Vector3D, Frame) - Constructor for class org.orekit.utils.ConstantPVCoordinatesProvider
Create the PVCoordinatesProvider from a fixed point in a frame.
ConstantPVCoordinatesProvider(GeodeticPoint, OneAxisEllipsoid) - Constructor for class org.orekit.utils.ConstantPVCoordinatesProvider
Create a the provider from a fixed lat/lon/alt on a central body.
ConstantPVCoordinatesProvider(PVCoordinates, Frame) - Constructor for class org.orekit.utils.ConstantPVCoordinatesProvider
Create the PVCoordinatesProvider from a fixed point in a frame.
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(AttitudeProvider, DateBasedManeuverTriggers, AbstractConstantThrustPropulsionModel) - Constructor for class org.orekit.forces.maneuvers.ConstantThrustManeuver
Simple constructor for a constant direction and constant thrust.
ConstantThrustManeuver(AbsoluteDate, double, double, double, Vector3D) - Constructor for class org.orekit.forces.maneuvers.ConstantThrustManeuver
Simple constructor for a constant direction and constant thrust.
ConstantThrustManeuver(AbsoluteDate, double, double, double, Vector3D, String) - Constructor for class org.orekit.forces.maneuvers.ConstantThrustManeuver
Simple constructor for a constant direction and constant thrust.
ConstantThrustManeuver(AbsoluteDate, double, double, double, AttitudeProvider, Vector3D) - Constructor for class org.orekit.forces.maneuvers.ConstantThrustManeuver
Simple constructor for a constant direction and constant thrust.
ConstantThrustManeuver(AbsoluteDate, double, double, double, AttitudeProvider, Vector3D, String) - Constructor for class org.orekit.forces.maneuvers.ConstantThrustManeuver
Simple constructor for a constant direction and constant thrust.
ConstantThrustManeuver(AbsoluteDate, double, double, double, AttitudeProvider, Vector3D, Control3DVectorCostType, 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.
ConstantTroposphericModel - Class in org.orekit.models.earth.troposphere
Defines a constant tropospheric model.
ConstantTroposphericModel(TroposphericDelay) - Constructor for class org.orekit.models.earth.troposphere.ConstantTroposphericModel
Simple constructor.
ConstantViennaAProvider - Class in org.orekit.models.earth.troposphere
Provider for constant Vienna A coefficients.
ConstantViennaAProvider(ViennaACoefficients) - Constructor for class org.orekit.models.earth.troposphere.ConstantViennaAProvider
Simple constructor.
CONSTELLATION - org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadataKey
Name of the constellation this space object belongs to.
containsSatellite(String) - Method in class org.orekit.files.sp3.SP3
Tests whether a satellite with the given id is contained in this orbit file.
ContextBinding - Class in org.orekit.files.ccsds.utils
Context for parsing/writing Navigation Data Message.
ContextBinding(Supplier<IERSConventions>, BooleanSupplier, Supplier<DataContext>, Supplier<ParsedUnitsBehavior>, Supplier<AbsoluteDate>, Supplier<TimeSystem>, DoubleSupplier, DoubleSupplier) - Constructor for class org.orekit.files.ccsds.utils.ContextBinding
Create a new context.
ContinueOnEvent - 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
Empty constructor.
CONTINUOUS - org.orekit.files.ccsds.definitions.DutyCycleType
Full/continuous thrust.
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.
Control3DVectorCostType - Enum in org.orekit.forces.maneuvers
Enumerate on types of cost for 3D control vector (thrust as a force or acceleration, including an impulse) at a given time.
convert() - Method in class org.orekit.propagation.conversion.OsculatingToMeanElementsConverter
Convert an osculating orbit into a mean orbit, in DSST sense.
convert(double) - Method in class org.orekit.utils.units.UnitsConverter
Convert a value.
convert(double[]) - Method in interface org.orekit.data.SimpleTimeStampedTableParser.RowConverter
Convert a row.
convert(List<SpacecraftState>, boolean, String...) - Method in class org.orekit.propagation.conversion.AbstractPropagatorConverter
Find the propagator that minimize the mean square error for a sample of states.
convert(List<SpacecraftState>, boolean, String...) - Method in interface org.orekit.propagation.conversion.PropagatorConverter
Find the propagator that minimize the mean square error for a sample of states.
convert(List<SpacecraftState>, boolean, List<String>) - Method in class org.orekit.propagation.conversion.AbstractPropagatorConverter
Find the propagator that minimize the mean square error for a sample of states.
convert(List<SpacecraftState>, boolean, List<String>) - Method in interface org.orekit.propagation.conversion.PropagatorConverter
Find the propagator that minimize the mean square error for a sample of states.
convert(FieldPressureTemperatureHumidity<T>, T) - Method in class org.orekit.models.earth.weather.HeightDependentPressureTemperatureHumidityConverter
Convert weather parameters.
convert(PressureTemperatureHumidity, double) - Method in class org.orekit.models.earth.weather.HeightDependentPressureTemperatureHumidityConverter
Convert weather parameters.
convert(Propagator, double, int, String...) - Method in class org.orekit.propagation.conversion.AbstractPropagatorConverter
Convert a propagator to another.
convert(Propagator, double, int, String...) - Method in interface org.orekit.propagation.conversion.PropagatorConverter
Convert a propagator into another one.
convert(Propagator, double, int, List<String>) - Method in class org.orekit.propagation.conversion.AbstractPropagatorConverter
Convert a propagator to another.
convert(Propagator, double, int, List<String>) - Method in interface org.orekit.propagation.conversion.PropagatorConverter
Convert a propagator into another one.
CONVERT_COMPATIBLE - org.orekit.files.ccsds.ndm.ParsedUnitsBehavior
Allow compatible units, performing conversion.
convert2DigitsYear(int) - Static method in class org.orekit.files.rinex.utils.parsing.RinexUtils
Convert a 2 digits year to a complete year.
convertIntervalDetector(Field<S>, ParameterDrivenDateIntervalDetector) - Method in class org.orekit.forces.maneuvers.trigger.DateBasedManeuverTriggers
Convert a primitive firing intervals detector into a field firing intervals detector.
convertIntervalDetector(Field<S>, T) - Method in class org.orekit.forces.maneuvers.trigger.IntervalEventTrigger
Convert a primitive firing intervals detector into a field firing intervals detector.
convertStartDetector(Field<S>, A) - Method in class org.orekit.forces.maneuvers.trigger.StartStopEventsTrigger
Convert a primitive firing start detector into a field firing start detector.
convertStopDetector(Field<S>, O) - Method in class org.orekit.forces.maneuvers.trigger.StartStopEventsTrigger
Convert a primitive firing stop detector into a field firing stop detector.
convertToAveraged(Orbit) - Method in interface org.orekit.propagation.conversion.averaging.converters.OsculatingToAveragedConverter
Convert osculating orbit to averaged orbital state according to underlying theory.
convertToAveraged(Orbit) - Method in class org.orekit.propagation.conversion.averaging.converters.OsculatingToBrouwerLyddaneConverter
Convert osculating orbit to averaged orbital state according to underlying theory.
convertToAveraged(Orbit) - Method in class org.orekit.propagation.conversion.averaging.converters.OsculatingToDSST6X0Converter
Convert osculating orbit to averaged orbital state according to underlying theory.
convertToAveraged(Orbit) - Method in class org.orekit.propagation.conversion.averaging.converters.OsculatingToEcksteinHechlerConverter
Convert osculating orbit to averaged orbital state according to underlying theory.
convertToAveraged(Orbit) - Method in class org.orekit.propagation.conversion.averaging.converters.OsculatingToSGP4Converter
Convert osculating orbit to averaged orbital state according to underlying theory.
convertToFieldOrbit(Field<T>, Orbit) - Method in enum org.orekit.orbits.OrbitType
Convert an orbit to the "Fielded" instance type.
convertType(FieldOrbit<T>) - Method in enum org.orekit.orbits.OrbitType
Convert an orbit to the instance type.
convertType(Orbit) - Method in enum org.orekit.orbits.OrbitType
Convert an orbit to the instance type.
copy() - Method in class org.orekit.propagation.conversion.BrouwerLyddanePropagatorBuilder
Create a new instance identical to this one.
copy() - Method in class org.orekit.propagation.conversion.DSSTPropagatorBuilder
Create a copy of a DSSTPropagatorBuilder object.
copy() - Method in class org.orekit.propagation.conversion.EcksteinHechlerPropagatorBuilder
Create a new instance identical to this one.
copy() - Method in class org.orekit.propagation.conversion.EphemerisPropagatorBuilder
Create a new instance identical to this one.
copy() - Method in class org.orekit.propagation.conversion.KeplerianPropagatorBuilder
Create a new instance identical to this one.
copy() - Method in class org.orekit.propagation.conversion.NumericalPropagatorBuilder
Create a copy of a NumericalPropagatorBuilder object.
copy() - Method in interface org.orekit.propagation.conversion.PropagatorBuilder
Create a new instance identical to this one.
copy() - Method in class org.orekit.propagation.conversion.TLEPropagatorBuilder
Create a new instance identical to this one.
copy(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.OcmMetadata
Copy the instance, making sure mandatory fields have been initialized.
copy(double) - Method in class org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistoryMetadata
Copy the instance, making sure mandatory fields have been initialized.
copyObservationData(ObservationData) - Method in class org.orekit.estimation.measurements.filtering.DualFrequencySmoother
Copy an ObservationData object.
copyObservationData(ObservationData) - Method in class org.orekit.estimation.measurements.filtering.SingleFrequencySmoother
Copy an ObservationData object.
correctedYaw(GNSSAttitudeContext) - Method in class org.orekit.gnss.attitude.BeidouGeo
Select the /** Compute GNSS attitude with midnight/noon yaw turn correction.
correctedYaw(GNSSAttitudeContext) - Method in class org.orekit.gnss.attitude.BeidouMeo
Select the /** Compute GNSS attitude with midnight/noon yaw turn correction.
correctedYaw(GNSSAttitudeContext) - Method in class org.orekit.gnss.attitude.Galileo
Select the /** Compute GNSS attitude with midnight/noon yaw turn correction.
correctedYaw(GNSSAttitudeContext) - Method in class org.orekit.gnss.attitude.GenericGNSS
Select the /** Compute GNSS attitude with midnight/noon yaw turn correction.
correctedYaw(GNSSAttitudeContext) - Method in class org.orekit.gnss.attitude.Glonass
Select the /** Compute GNSS attitude with midnight/noon yaw turn correction.
correctedYaw(GNSSAttitudeContext) - Method in class org.orekit.gnss.attitude.