Index (OREKIT 12.2 API)

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

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: Deprecated.
Use AbsoluteDate(Instant, UTCScale) or AbsoluteDate(Instant) instead
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.
AbstractAnalyticalPropagatorBuilder - Class in org.orekit.propagation.conversion: Abstract class for propagator builders of analytical models (except for ephemeris i.e.
AbstractAnalyticalPropagatorBuilder(Orbit, PositionAngleType, double, boolean, AttitudeProvider, double) - Constructor for class org.orekit.propagation.conversion.AbstractAnalyticalPropagatorBuilder: 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: Bridge between measurements and least squares problems.
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 non-central 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.
AbstractCartesianAdjointDerivativesProvider - Class in org.orekit.control.indirect.adjoint: Abstract class defining common things for Cartesian adjoint dynamics between standard and Field versions.
AbstractCartesianAdjointDerivativesProvider(CartesianCost) - Constructor for class org.orekit.control.indirect.adjoint.AbstractCartesianAdjointDerivativesProvider: Constructor.
AbstractCartesianAdjointEquationTerm - Class in org.orekit.control.indirect.adjoint: Abstract class to define terms in the adjoint equations and Hamiltonian for Cartesian coordinates.
AbstractCartesianAdjointEquationTerm() - Constructor for class org.orekit.control.indirect.adjoint.AbstractCartesianAdjointEquationTerm
AbstractCartesianAdjointGravitationalTerm - Class in org.orekit.control.indirect.adjoint: Abstract class for common computations regarding adjoint dynamics and gravity for Cartesian coordinates.
AbstractCartesianAdjointGravitationalTerm(double) - Constructor for class org.orekit.control.indirect.adjoint.AbstractCartesianAdjointGravitationalTerm: Constructor.
AbstractCartesianAdjointNewtonianTerm - Class in org.orekit.control.indirect.adjoint: Abstract class for common computations regarding adjoint dynamics and Newtonian gravity for Cartesian coordinates.
AbstractCartesianAdjointNewtonianTerm(double) - Constructor for class org.orekit.control.indirect.adjoint.AbstractCartesianAdjointNewtonianTerm: Constructor.
AbstractCartesianAdjointNonCentralBodyTerm - Class in org.orekit.control.indirect.adjoint: Abstract class defining the contributions of a point-mass, single body gravity in the adjoint equations for Cartesian coordinates.
AbstractCartesianAdjointNonCentralBodyTerm(double, ExtendedPositionProvider) - Constructor for class org.orekit.control.indirect.adjoint.AbstractCartesianAdjointNonCentralBodyTerm: Constructor.
AbstractCartesianEnergy - Class in org.orekit.control.indirect.adjoint.cost: Abstract class for energy cost with Cartesian coordinates.
AbstractCartesianEnergy(String, double) - Constructor for class org.orekit.control.indirect.adjoint.cost.AbstractCartesianEnergy: 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: Deprecated.
as of 12.2
AbstractDetector(EventDetectionSettings, 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.
AbstractFixedBoundaryCartesianSingleShooting - Class in org.orekit.control.indirect.shooting: Abstract class for indirect single shooting methods with Cartesian coordinates for fixed time fixed boundary.
AbstractFixedBoundaryCartesianSingleShooting(ShootingPropagationSettings, FixedTimeBoundaryOrbits, CartesianBoundaryConditionChecker) - Constructor for class org.orekit.control.indirect.shooting.AbstractFixedBoundaryCartesianSingleShooting: Constructor with boundary conditions as orbits.
AbstractFixedBoundaryCartesianSingleShooting(ShootingPropagationSettings, FixedTimeCartesianBoundaryStates, CartesianBoundaryConditionChecker) - Constructor for class org.orekit.control.indirect.shooting.AbstractFixedBoundaryCartesianSingleShooting: Constructor with boundary conditions as orbits.
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 C_i^j and the S_i^j 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 U_i^j and V_i^j 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 C_i^j and the S_i^j 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 U_i^j and V_i^j 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.
AbstractIndirectShooting - Class in org.orekit.control.indirect.shooting: Abstract class for indirect shooting methods with numerical propagation.
AbstractIndirectShooting(ShootingPropagationSettings) - Constructor for class org.orekit.control.indirect.shooting.AbstractIndirectShooting: 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.
AbstractPropagatorBuilder(Orbit, PositionAngleType, double, boolean, AttitudeProvider, double) - 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.
AbstractSolarLightFluxModel - Class in org.orekit.forces.radiation: Abstract class for the definition of the solar flux model with a single occulting body of spherical shape.
AbstractSolarLightFluxModel(double, ExtendedPositionProvider, double, EventDetectionSettings) - Constructor for class org.orekit.forces.radiation.AbstractSolarLightFluxModel: Constructor.
AbstractSolarLightFluxModel(ExtendedPositionProvider, double, EventDetectionSettings) - Constructor for class org.orekit.forces.radiation.AbstractSolarLightFluxModel: Constructor with default value for reference flux.
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.
AbstractVariableStepIntegratorBuilder - Class in org.orekit.propagation.conversion: Abstract class for integrator builder using variable step size.
AbstractVariableStepIntegratorBuilder(double, double, double) - Constructor for class org.orekit.propagation.conversion.AbstractVariableStepIntegratorBuilder: Constructor.
AbstractVariableStepIntegratorBuilder(double, double, double, double) - Constructor for class org.orekit.propagation.conversion.AbstractVariableStepIntegratorBuilder: Constructor with expected velocity error.
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: Meta-data for Attitude Comprehensive Message.
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.
AdamsBashforthFieldIntegratorBuilder(int, double, 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.
AdamsBashforthIntegratorBuilder(int, double, 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.
AdamsMoultonFieldIntegratorBuilder(int, double, 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.
AdamsMoultonIntegratorBuilder(int, double, 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.
addImpulseManeuver(ImpulseManeuver) - Method in class org.orekit.propagation.conversion.AbstractAnalyticalPropagatorBuilder: Add impulse maneuver.
addImpulseManeuver(ImpulseManeuver) - Method in class org.orekit.propagation.conversion.NumericalPropagatorBuilder: Add impulse maneuver.
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.
AdjointDynamicsProvider - Interface in org.orekit.control.indirect.shooting.propagation: Interface for adjoint derivatives provider (both standard and Field).
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: Builder class for AggregatedPVCoordinatesProvider.
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.
AlignedAndConstrained - Class in org.orekit.attitudes: Attitude provider with one satellite vector aligned and another one constrained to two targets.
AlignedAndConstrained(Vector3D, TargetProvider, Vector3D, TargetProvider, ExtendedPositionProvider, OneAxisEllipsoid) - Constructor for class org.orekit.attitudes.AlignedAndConstrained: Simple constructor.
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.
AnalyticalSolarPositionProvider - Class in org.orekit.bodies: Class computing low-fidelity positions for the Sun.
AnalyticalSolarPositionProvider() - Constructor for class org.orekit.bodies.AnalyticalSolarPositionProvider: Constructor with default data context.
AnalyticalSolarPositionProvider(DataContext) - Constructor for class org.orekit.bodies.AnalyticalSolarPositionProvider: Constructor.
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 tropospheric 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 H_f.
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: Keys for covariance history container entries.
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.Switch - Class in org.orekit.attitudes: Switch specification.
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: Keys for attitude state history container entries.
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 gn_h, ge_h, gn_w and ge_w.
AzimuthalGradientCoefficients(double, double, double, double) - Constructor for class org.orekit.models.earth.troposphere.AzimuthalGradientCoefficients: Simple constructor.
AzimuthalGradientProvider - Interface in org.orekit.models.earth.troposphere: Provider for AzimuthalGradientCoefficients and FieldAzimuthalGradientCoefficients.
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: Deprecated.
as of 12.1, replaced by BaseRangeRateTroposphericDelayModifier(TroposphericModel)
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.
as of 12.1, replaced by BaseRangeTroposphericDelayModifier(TroposphericModel)
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: Bridge between measurements and least squares problems.
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: Deprecated.
as of 12.1, replaced by BistaticRangeRateTroposphericDelayModifier(TroposphericModel)
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: Deprecated.
as of 12.1 replaced by BistaticRangeTroposphericDelayModifier(TroposphericModel)
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.
BoundedCartesianEnergy - Class in org.orekit.control.indirect.adjoint.cost: Class for bounded energy cost with Cartesian coordinates.
BoundedCartesianEnergy(String, double, double) - Constructor for class org.orekit.control.indirect.adjoint.cost.BoundedCartesianEnergy: Constructor.
BoundedCartesianEnergy(String, double, double, EventDetectionSettings) - Constructor for class org.orekit.control.indirect.adjoint.cost.BoundedCartesianEnergy: Constructor.
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: Build a parser for Attitude Comprehensive Messages.
buildAcmWriter() - Method in class org.orekit.files.ccsds.ndm.WriterBuilder: Build a writer for Attitude Comprehensive Messages.
buildAdditionalDerivativesProvider() - Method in interface org.orekit.control.indirect.shooting.propagation.AdjointDynamicsProvider: Builds adjoint derivatives provider.
buildAdditionalDerivativesProvider() - Method in class org.orekit.control.indirect.shooting.propagation.CartesianAdjointDynamicsProvider: Builds adjoint derivatives provider.
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.
buildFieldAdditionalDerivativesProvider(Field<T>) - Method in interface org.orekit.control.indirect.shooting.propagation.AdjointDynamicsProvider: Builds Field adjoint derivatives provider.
buildFieldAdditionalDerivativesProvider(Field<T>) - Method in class org.orekit.control.indirect.shooting.propagation.CartesianAdjointDynamicsProvider: Builds Field adjoint derivatives provider.
buildFieldGradientCartesianVector(T[]) - Static method in class org.orekit.control.indirect.adjoint.AbstractCartesianAdjointEquationTerm: Build a Cartesian vector whose components are independent variables for automatic differentiation at order 1.
buildFieldPropagator(FieldSpacecraftState<Gradient>) - Method in class org.orekit.control.indirect.shooting.AbstractFixedBoundaryCartesianSingleShooting: Create Gradient numerical propagator.
buildFieldPropagator(FieldSpacecraftState<Gradient>) - Method in class org.orekit.control.indirect.shooting.AbstractIndirectShooting: Create Gradient numerical propagator.
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.
buildGradientCartesianVector(double[]) - Static method in class org.orekit.control.indirect.adjoint.AbstractCartesianAdjointEquationTerm: Build a Cartesian vector whose components are independent variables for automatic differentiation at order 1.
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.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.
buildIntegrator(AbsolutePVCoordinates) - Method in interface org.orekit.propagation.conversion.ODEIntegratorBuilder: Build a first order integrator.
buildIntegrator(FieldAbsolutePVCoordinates<T>) - Method in interface org.orekit.propagation.conversion.FieldODEIntegratorBuilder: Build a first order integrator.
buildLeastSquaresModel(PropagatorBuilder[], List<ObservedMeasurement<?>>, ParameterDriversList, ModelObserver) - Method in class org.orekit.propagation.conversion.AbstractAnalyticalPropagatorBuilder: 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.EphemerisPropagatorBuilder: 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.
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.
buildPropagator(SpacecraftState) - Method in class org.orekit.control.indirect.shooting.AbstractFixedBoundaryCartesianSingleShooting: Create numerical propagator.
buildPropagator(SpacecraftState) - Method in class org.orekit.control.indirect.shooting.AbstractIndirectShooting: Create numerical 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: Caching wrapper for NormalizedSphericalHarmonicsProvider.
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.
CartesianAdjointDerivativesProvider - Class in org.orekit.control.indirect.adjoint: Class defining the adjoint dynamics, as defined in the Pontryagin Maximum Principle, in the case where Cartesian coordinates in an inertial frame are the dependent variable.
CartesianAdjointDerivativesProvider(CartesianCost, CartesianAdjointEquationTerm...) - Constructor for class org.orekit.control.indirect.adjoint.CartesianAdjointDerivativesProvider: Constructor.
CartesianAdjointDynamicsProvider - Class in org.orekit.control.indirect.shooting.propagation: Class for Cartesian adjoint derivatives provider (both standard and Field).
CartesianAdjointDynamicsProvider(CartesianCost, CartesianAdjointEquationTerm...) - Constructor for class org.orekit.control.indirect.shooting.propagation.CartesianAdjointDynamicsProvider: Constructor.
CartesianAdjointEquationTerm - Interface in org.orekit.control.indirect.adjoint: Interface to define terms in the adjoint equations and Hamiltonian for Cartesian coordinates.
CartesianAdjointInertialTerm - Class in org.orekit.control.indirect.adjoint: Class defining inertial forces' contributions in the adjoint equations for Cartesian coordinates.
CartesianAdjointInertialTerm(Frame) - Constructor for class org.orekit.control.indirect.adjoint.CartesianAdjointInertialTerm: Constructor.
CartesianAdjointJ2Term - Class in org.orekit.control.indirect.adjoint: Class defining a (constant) J2 contributions in the adjoint equations for Cartesian coordinates.
CartesianAdjointJ2Term(double, double, double, Frame) - Constructor for class org.orekit.control.indirect.adjoint.CartesianAdjointJ2Term: Constructor.
CartesianAdjointKeplerianTerm - Class in org.orekit.control.indirect.adjoint: Class defining the Keplerian contributions in the adjoint equations for Cartesian coordinates.
CartesianAdjointKeplerianTerm(double) - Constructor for class org.orekit.control.indirect.adjoint.CartesianAdjointKeplerianTerm: Constructor.
CartesianAdjointSingleBodyTerm - Class in org.orekit.control.indirect.adjoint: Class defining the contributions of a point-mass, single body gravity in the adjoint equations for Cartesian coordinates.
CartesianAdjointSingleBodyTerm(double, ExtendedPositionProvider) - Constructor for class org.orekit.control.indirect.adjoint.CartesianAdjointSingleBodyTerm: Constructor.
CartesianAdjointThirdBodyTerm - Class in org.orekit.control.indirect.adjoint: Class defining the contributions of a point-mass, third body in the adjoint equations for Cartesian coordinates.
CartesianAdjointThirdBodyTerm(double, ExtendedPositionProvider) - Constructor for class org.orekit.control.indirect.adjoint.CartesianAdjointThirdBodyTerm: Constructor.
CartesianBoundaryConditionChecker - Interface in org.orekit.control.indirect.shooting.boundary: Interface defining convergence criterion when the terminal condition is on a Cartesian state.
cartesianBuilder(OneAxisEllipsoid) - Static method in class org.orekit.utils.WaypointPVBuilder: Construct a waypoint builder interpolating points using a linear cartesian interpolation.
CartesianCost - Interface in org.orekit.control.indirect.adjoint.cost: Interface to definite cost function in the frame of Pontryagin's Maximum Principle using Cartesian coordinates.
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: Keys for OPM/OMM/OCM Cartesian covariance entries.
CartesianCovarianceUtils - Class in org.orekit.utils: Utility class for conversions related to Cartesian covariance matrices.
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: ProcessingState for CDM header.
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.
changeReferenceFrame(Frame, RealMatrix, AbsoluteDate, Frame) - Static method in class org.orekit.utils.CartesianCovarianceUtils: Convert input position-velocity covariance matrix between reference frames.
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 S_j(k, h) and the C_j(k, h) series and their partial derivatives with respect to k and h.
CjSjCoefficient(double, double) - Constructor for class org.orekit.propagation.semianalytical.dsst.utilities.CjSjCoefficient: C_j(k, h) and S_j(k, h) constructor.
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.
ClassicalRungeKuttaIntegrationSettings - Class in org.orekit.control.indirect.shooting.propagation: Integration settings using the classical Runge-Kutta 4 scheme.
ClassicalRungeKuttaIntegrationSettings(double) - Constructor for class org.orekit.control.indirect.shooting.propagation.ClassicalRungeKuttaIntegrationSettings: Constructor.
ClassicalRungeKuttaIntegratorBuilder - Class in org.orekit.propagation.conversion: Builder for ClassicalRungeKuttaIntegrator.
ClassicalRungeKuttaIntegratorBuilder(double) - Constructor for class org.orekit.propagation.conversion.ClassicalRungeKuttaIntegratorBuilder: Build a new instance.
CLASSIFICATION - 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.
clearImpulseManeuvers() - Method in class org.orekit.propagation.conversion.AbstractAnalyticalPropagatorBuilder: Remove all impulse maneuvers.
clearImpulseManeuvers() - Method in class org.orekit.propagation.conversion.NumericalPropagatorBuilder: Remove all impulse maneuvers.
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.
clone() - Method in class org.orekit.propagation.conversion.AbstractPropagatorBuilder
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 class org.orekit.control.indirect.adjoint.FieldCartesianAdjointDerivativesProvider: Compute the derivatives related to the additional state (and optionally main state increments).
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.control.indirect.adjoint.CartesianAdjointDerivativesProvider: 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: Deprecated.
as of 12.1, replaced by CombinedObservationData(double, double, CombinationType, MeasurementType, List)
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.
computeAccelerationInJ2Frame(FieldVector3D<T>, double, double, T) - Static method in class org.orekit.forces.gravity.J2OnlyPerturbation: Compute acceleration in J2 frame.
computeAccelerationInJ2Frame(Vector3D, double, double, double) - Static method in class org.orekit.forces.gravity.J2OnlyPerturbation: Compute acceleration in J2 frame.
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 G_s and H_s 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 G_s and H_s 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 Q_n,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 Q_n,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 V_n,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.
ConicallyShadowedLightFluxModel - Class in org.orekit.forces.radiation: Class defining a flux model from a single occulted body, casting a shadow on a spherical occulting body.
ConicallyShadowedLightFluxModel(double, double, ExtendedPositionProvider, double) - Constructor for class org.orekit.forces.radiation.ConicallyShadowedLightFluxModel: Constructor with default event detection settings.
ConicallyShadowedLightFluxModel(double, double, ExtendedPositionProvider, double, EventDetectionSettings) - Constructor for class org.orekit.forces.radiation.ConicallyShadowedLightFluxModel: Constructor.
ConicallyShadowedLightFluxModel(double, ExtendedPositionProvider, double) - Constructor for class org.orekit.forces.radiation.ConicallyShadowedLightFluxModel: Constructor with default value for reference flux.
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: Constant provider for AzimuthalGradientCoefficients and