Uses of Interface
org.orekit.time.TimeInterpolator

Packages that use TimeInterpolator

Package	Description
org.orekit.attitudes	This package provides classes to represent simple attitudes.
org.orekit.files.sp3	This package provides a parser for orbit data stored in SP3 format.
org.orekit.orbits	This package provides classes to represent orbits.
org.orekit.propagation	Propagation
org.orekit.propagation.analytical	Top level package for analytical propagators.
org.orekit.propagation.conversion	This package provides tools to convert a given propagator or a set of SpacecraftState into another propagator.
org.orekit.time	This independent package provides classes to handle epochs, time scales, and to compare instants together.
org.orekit.utils	This package provides useful objects.

Uses of TimeInterpolator in org.orekit.attitudes

Classes in org.orekit.attitudes that implement TimeInterpolator

Modifier and Type	Class and Description
class	AttitudeInterpolator Class for attitude interpolation.

Methods in org.orekit.attitudes that return TimeInterpolator

Modifier and Type	Method and Description
TimeInterpolator<TimeStampedAngularCoordinates>	AttitudeInterpolator.getAngularInterpolator() Get time stamped angular coordinates interpolator.

Constructors in org.orekit.attitudes with parameters of type TimeInterpolator

Constructor and Description
AttitudeInterpolator(Frame referenceFrame, TimeInterpolator<TimeStampedAngularCoordinates> interpolator) Constructor.

Uses of TimeInterpolator in org.orekit.files.sp3

Classes in org.orekit.files.sp3 that implement TimeInterpolator

Modifier and Type	Class and Description
class	SP3CoordinateHermiteInterpolator Interpolator for SP3 coordinates.

Uses of TimeInterpolator in org.orekit.orbits

Classes in org.orekit.orbits that implement TimeInterpolator

Modifier and Type	Class and Description
class	AbstractOrbitInterpolator Abstract class for orbit interpolator.
class	OrbitBlender Orbit blender.
class	OrbitHermiteInterpolator Class using a Hermite interpolator to interpolate orbits.

Uses of TimeInterpolator in org.orekit.propagation

Classes in org.orekit.propagation that implement TimeInterpolator

Modifier and Type	Class and Description
class	AbstractStateCovarianceInterpolator Abstract class for orbit and state covariance interpolator.
class	SpacecraftStateInterpolator Generic class for spacecraft state interpolator.
class	StateCovarianceBlender State covariance blender.
class	StateCovarianceKeplerianHermiteInterpolator State covariance Keplerian quintic interpolator.

Methods in org.orekit.propagation that return TimeInterpolator

Modifier and Type	Method and Description
TimeInterpolator<Orbit>	AbstractStateCovarianceInterpolator.getOrbitInterpolator() Get orbit interpolator.

Methods in org.orekit.propagation that return types with arguments of type TimeInterpolator

Modifier and Type	Method and Description
Optional<TimeInterpolator<AbsolutePVCoordinates>>	SpacecraftStateInterpolator.getAbsPVAInterpolator() Get absolute position-velocity-acceleration interpolator.
Optional<TimeInterpolator<TimeStampedDouble>>	SpacecraftStateInterpolator.getAdditionalStateInterpolator() Get additional state interpolator.
Optional<TimeInterpolator<Attitude>>	SpacecraftStateInterpolator.getAttitudeInterpolator() Get attitude interpolator.
Optional<TimeInterpolator<TimeStampedDouble>>	SpacecraftStateInterpolator.getMassInterpolator() Get mass interpolator.
Optional<TimeInterpolator<Orbit>>	SpacecraftStateInterpolator.getOrbitInterpolator() Get orbit interpolator.
List<TimeInterpolator<? extends TimeStamped>>	SpacecraftStateInterpolator.getSubInterpolators() Get all lowest level interpolators implemented by this instance, otherwise return a list with this instance only.

Constructors in org.orekit.propagation with parameters of type TimeInterpolator

Constructor and Description
AbstractStateCovarianceInterpolator(int interpolationPoints, double extrapolationThreshold, TimeInterpolator<Orbit> orbitInterpolator, Frame outFrame, OrbitType outOrbitType, PositionAngleType outPositionAngleType) Constructor.
AbstractStateCovarianceInterpolator(int interpolationPoints, double extrapolationThreshold, TimeInterpolator<Orbit> orbitInterpolator, LOFType outLOF) Constructor.
SpacecraftStateInterpolator(Frame outputFrame, TimeInterpolator<Orbit> orbitInterpolator, TimeInterpolator<AbsolutePVCoordinates> absPVAInterpolator, TimeInterpolator<TimeStampedDouble> massInterpolator, TimeInterpolator<Attitude> attitudeInterpolator, TimeInterpolator<TimeStampedDouble> additionalStateInterpolator) Constructor with: Default number of interpolation points of DEFAULT_INTERPOLATION_POINTS Default extrapolation threshold of DEFAULT_EXTRAPOLATION_THRESHOLD_SEC s
SpacecraftStateInterpolator(Frame outputFrame, TimeInterpolator<Orbit> orbitInterpolator, TimeInterpolator<AbsolutePVCoordinates> absPVAInterpolator, TimeInterpolator<TimeStampedDouble> massInterpolator, TimeInterpolator<Attitude> attitudeInterpolator, TimeInterpolator<TimeStampedDouble> additionalStateInterpolator) Constructor with: Default number of interpolation points of DEFAULT_INTERPOLATION_POINTS Default extrapolation threshold of DEFAULT_EXTRAPOLATION_THRESHOLD_SEC s
SpacecraftStateInterpolator(Frame outputFrame, TimeInterpolator<Orbit> orbitInterpolator, TimeInterpolator<AbsolutePVCoordinates> absPVAInterpolator, TimeInterpolator<TimeStampedDouble> massInterpolator, TimeInterpolator<Attitude> attitudeInterpolator, TimeInterpolator<TimeStampedDouble> additionalStateInterpolator) Constructor with: Default number of interpolation points of DEFAULT_INTERPOLATION_POINTS Default extrapolation threshold of DEFAULT_EXTRAPOLATION_THRESHOLD_SEC s
SpacecraftStateInterpolator(Frame outputFrame, TimeInterpolator<Orbit> orbitInterpolator, TimeInterpolator<AbsolutePVCoordinates> absPVAInterpolator, TimeInterpolator<TimeStampedDouble> massInterpolator, TimeInterpolator<Attitude> attitudeInterpolator, TimeInterpolator<TimeStampedDouble> additionalStateInterpolator) Constructor with: Default number of interpolation points of DEFAULT_INTERPOLATION_POINTS Default extrapolation threshold of DEFAULT_EXTRAPOLATION_THRESHOLD_SEC s
SpacecraftStateInterpolator(Frame outputFrame, TimeInterpolator<Orbit> orbitInterpolator, TimeInterpolator<AbsolutePVCoordinates> absPVAInterpolator, TimeInterpolator<TimeStampedDouble> massInterpolator, TimeInterpolator<Attitude> attitudeInterpolator, TimeInterpolator<TimeStampedDouble> additionalStateInterpolator) Constructor with: Default number of interpolation points of DEFAULT_INTERPOLATION_POINTS Default extrapolation threshold of DEFAULT_EXTRAPOLATION_THRESHOLD_SEC s
SpacecraftStateInterpolator(int interpolationPoints, double extrapolationThreshold, Frame outputFrame, TimeInterpolator<Orbit> orbitInterpolator, TimeInterpolator<AbsolutePVCoordinates> absPVAInterpolator, TimeInterpolator<TimeStampedDouble> massInterpolator, TimeInterpolator<Attitude> attitudeInterpolator, TimeInterpolator<TimeStampedDouble> additionalStateInterpolator) Constructor.
SpacecraftStateInterpolator(int interpolationPoints, double extrapolationThreshold, Frame outputFrame, TimeInterpolator<Orbit> orbitInterpolator, TimeInterpolator<AbsolutePVCoordinates> absPVAInterpolator, TimeInterpolator<TimeStampedDouble> massInterpolator, TimeInterpolator<Attitude> attitudeInterpolator, TimeInterpolator<TimeStampedDouble> additionalStateInterpolator) Constructor.
SpacecraftStateInterpolator(int interpolationPoints, double extrapolationThreshold, Frame outputFrame, TimeInterpolator<Orbit> orbitInterpolator, TimeInterpolator<AbsolutePVCoordinates> absPVAInterpolator, TimeInterpolator<TimeStampedDouble> massInterpolator, TimeInterpolator<Attitude> attitudeInterpolator, TimeInterpolator<TimeStampedDouble> additionalStateInterpolator) Constructor.
SpacecraftStateInterpolator(int interpolationPoints, double extrapolationThreshold, Frame outputFrame, TimeInterpolator<Orbit> orbitInterpolator, TimeInterpolator<AbsolutePVCoordinates> absPVAInterpolator, TimeInterpolator<TimeStampedDouble> massInterpolator, TimeInterpolator<Attitude> attitudeInterpolator, TimeInterpolator<TimeStampedDouble> additionalStateInterpolator) Constructor.
SpacecraftStateInterpolator(int interpolationPoints, double extrapolationThreshold, Frame outputFrame, TimeInterpolator<Orbit> orbitInterpolator, TimeInterpolator<AbsolutePVCoordinates> absPVAInterpolator, TimeInterpolator<TimeStampedDouble> massInterpolator, TimeInterpolator<Attitude> attitudeInterpolator, TimeInterpolator<TimeStampedDouble> additionalStateInterpolator) Constructor.
StateCovarianceBlender(org.hipparchus.analysis.polynomials.SmoothStepFactory.SmoothStepFunction blendingFunction, TimeInterpolator<Orbit> orbitInterpolator, Frame outFrame, OrbitType outOrbitType, PositionAngleType outPositionAngleType) Constructor.
StateCovarianceBlender(org.hipparchus.analysis.polynomials.SmoothStepFactory.SmoothStepFunction blendingFunction, TimeInterpolator<Orbit> orbitInterpolator, LOFType outLOF) Constructor.
StateCovarianceKeplerianHermiteInterpolator(int interpolationPoints, double extrapolationThreshold, TimeInterpolator<Orbit> orbitInterpolator, CartesianDerivativesFilter filter, Frame outFrame, OrbitType outOrbitType, PositionAngleType outPositionAngleType) Constructor using an output frame.
StateCovarianceKeplerianHermiteInterpolator(int interpolationPoints, double extrapolationThreshold, TimeInterpolator<Orbit> orbitInterpolator, CartesianDerivativesFilter filter, LOFType outLOF) Constructor using an output local orbital frame.
StateCovarianceKeplerianHermiteInterpolator(int interpolationPoints, TimeInterpolator<Orbit> orbitInterpolator, CartesianDerivativesFilter filter, Frame outFrame, OrbitType outOrbitType, PositionAngleType outPositionAngleType) Constructor using an output frame and : Default extrapolation threshold value (DEFAULT_EXTRAPOLATION_THRESHOLD_SEC s) 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).
StateCovarianceKeplerianHermiteInterpolator(int interpolationPoints, TimeInterpolator<Orbit> orbitInterpolator, CartesianDerivativesFilter filter, LOFType outLOF) Constructor using an output local orbital frame and : 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).
StateCovarianceKeplerianHermiteInterpolator(int interpolationPoints, TimeInterpolator<Orbit> orbitInterpolator, Frame outFrame, OrbitType outOrbitType, PositionAngleType outPositionAngleType) Constructor using an output frame and : Default number of interpolation points of DEFAULT_INTERPOLATION_POINTS 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).
StateCovarianceKeplerianHermiteInterpolator(int interpolationPoints, TimeInterpolator<Orbit> orbitInterpolator, LOFType outLOF) Constructor using an output local orbital frame and : 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).
StateCovarianceKeplerianHermiteInterpolator(TimeInterpolator<Orbit> orbitInterpolator, Frame outFrame, OrbitType outOrbitType, PositionAngleType outPositionAngleType) Constructor using an output frame and : 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).
StateCovarianceKeplerianHermiteInterpolator(TimeInterpolator<Orbit> orbitInterpolator, LOFType outLOF) Constructor using an output local orbital frame and : 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).

Uses of TimeInterpolator in org.orekit.propagation.analytical

Methods in org.orekit.propagation.analytical that return TimeInterpolator

Modifier and Type	Method and Description
TimeInterpolator<SpacecraftState>	Ephemeris.getStateInterpolator() Get state interpolator.

Methods in org.orekit.propagation.analytical that return types with arguments of type TimeInterpolator

Modifier and Type	Method and Description
Optional<TimeInterpolator<TimeStampedPair<Orbit,StateCovariance>>>	Ephemeris.getCovarianceInterpolator() Get covariance interpolator.

Methods in org.orekit.propagation.analytical with parameters of type TimeInterpolator

Modifier and Type	Method and Description
static void	Ephemeris.checkInputConsistency(List<SpacecraftState> states, TimeInterpolator<SpacecraftState> stateInterpolator, List<StateCovariance> covariances, TimeInterpolator<TimeStampedPair<Orbit,StateCovariance>> covarianceInterpolator) Check input consistency between states, covariances and their associated interpolators.
static void	Ephemeris.checkInputConsistency(List<SpacecraftState> states, TimeInterpolator<SpacecraftState> stateInterpolator, List<StateCovariance> covariances, TimeInterpolator<TimeStampedPair<Orbit,StateCovariance>> covarianceInterpolator) Check input consistency between states, covariances and their associated interpolators.

Constructors in org.orekit.propagation.analytical with parameters of type TimeInterpolator

Constructor and Description
Ephemeris(List<SpacecraftState> states, TimeInterpolator<SpacecraftState> stateInterpolator) Constructor with tabulated states.
Ephemeris(List<SpacecraftState> states, TimeInterpolator<SpacecraftState> stateInterpolator, AttitudeProvider attitudeProvider) Constructor with tabulated states.
Ephemeris(List<SpacecraftState> states, TimeInterpolator<SpacecraftState> stateInterpolator, List<StateCovariance> covariances, TimeInterpolator<TimeStampedPair<Orbit,StateCovariance>> covarianceInterpolator) Constructor with tabulated states and associated covariances.
Ephemeris(List<SpacecraftState> states, TimeInterpolator<SpacecraftState> stateInterpolator, List<StateCovariance> covariances, TimeInterpolator<TimeStampedPair<Orbit,StateCovariance>> covarianceInterpolator) Constructor with tabulated states and associated covariances.
Ephemeris(List<SpacecraftState> states, TimeInterpolator<SpacecraftState> stateInterpolator, List<StateCovariance> covariances, TimeInterpolator<TimeStampedPair<Orbit,StateCovariance>> covarianceInterpolator, AttitudeProvider attitudeProvider) Constructor with tabulated states and associated covariances.
Ephemeris(List<SpacecraftState> states, TimeInterpolator<SpacecraftState> stateInterpolator, List<StateCovariance> covariances, TimeInterpolator<TimeStampedPair<Orbit,StateCovariance>> covarianceInterpolator, AttitudeProvider attitudeProvider) Constructor with tabulated states and associated covariances.

Uses of TimeInterpolator in org.orekit.propagation.conversion

Constructors in org.orekit.propagation.conversion with parameters of type TimeInterpolator

Constructor and Description
EphemerisPropagatorBuilder(List<SpacecraftState> states, TimeInterpolator<SpacecraftState> stateInterpolator) Constructor using the default attitude provider.
EphemerisPropagatorBuilder(List<SpacecraftState> states, TimeInterpolator<SpacecraftState> stateInterpolator, AttitudeProvider attitudeProvider) Constructor.
EphemerisPropagatorBuilder(List<SpacecraftState> states, TimeInterpolator<SpacecraftState> stateInterpolator, List<StateCovariance> covariances, TimeInterpolator<TimeStampedPair<Orbit,StateCovariance>> covarianceInterpolator) Constructor with covariances and default attitude provider.
EphemerisPropagatorBuilder(List<SpacecraftState> states, TimeInterpolator<SpacecraftState> stateInterpolator, List<StateCovariance> covariances, TimeInterpolator<TimeStampedPair<Orbit,StateCovariance>> covarianceInterpolator) Constructor with covariances and default attitude provider.
EphemerisPropagatorBuilder(List<SpacecraftState> states, TimeInterpolator<SpacecraftState> stateInterpolator, List<StateCovariance> covariances, TimeInterpolator<TimeStampedPair<Orbit,StateCovariance>> covarianceInterpolator, AttitudeProvider attitudeProvider) Constructor.
EphemerisPropagatorBuilder(List<SpacecraftState> states, TimeInterpolator<SpacecraftState> stateInterpolator, List<StateCovariance> covariances, TimeInterpolator<TimeStampedPair<Orbit,StateCovariance>> covarianceInterpolator, AttitudeProvider attitudeProvider) Constructor.

Uses of TimeInterpolator in org.orekit.time

Classes in org.orekit.time that implement TimeInterpolator

Modifier and Type	Class and Description
class	AbstractTimeInterpolator<T extends TimeStamped> Abstract class for time interpolator.
class	TimeStampedDoubleHermiteInterpolator Hermite interpolator of time stamped double value.

Methods in org.orekit.time that return types with arguments of type TimeInterpolator

Modifier and Type	Method and Description
List<TimeInterpolator<? extends TimeStamped>>	AbstractTimeInterpolator.getSubInterpolators() Get all lowest level interpolators implemented by this instance, otherwise return a list with this instance only.
List<TimeInterpolator<? extends TimeStamped>>	TimeInterpolator.getSubInterpolators() Get all lowest level interpolators implemented by this instance, otherwise return a list with this instance only.

Methods in org.orekit.time with parameters of type TimeInterpolator

Modifier and Type	Method and Description
protected void	AbstractTimeInterpolator.addOptionalSubInterpolatorIfDefined(TimeInterpolator<? extends TimeStamped> subInterpolator, List<TimeInterpolator<? extends TimeStamped>> subInterpolators) Add all lowest level sub interpolators to the sub interpolator list.
static void	AbstractTimeInterpolator.checkInterpolatorCompatibilityWithSampleSize(TimeInterpolator<? extends TimeStamped> interpolator, int sampleSize) Method checking if given interpolator is compatible with given sample size.

Method parameters in org.orekit.time with type arguments of type TimeInterpolator

Modifier and Type	Method and Description
protected void	AbstractTimeInterpolator.addOptionalSubInterpolatorIfDefined(TimeInterpolator<? extends TimeStamped> subInterpolator, List<TimeInterpolator<? extends TimeStamped>> subInterpolators) Add all lowest level sub interpolators to the sub interpolator list.

Uses of TimeInterpolator in org.orekit.utils

Classes in org.orekit.utils that implement TimeInterpolator

Modifier and Type	Class and Description
class	AbsolutePVCoordinatesHermiteInterpolator Class using a Hermite interpolator to interpolate absolute position-velocity-acceleration coordinates.
class	TimeStampedAngularCoordinatesHermiteInterpolator Class using Hermite interpolator to interpolate time stamped angular coordinates.
class	TimeStampedPVCoordinatesHermiteInterpolator Class using a Hermite interpolator to interpolate time stamped position-velocity-acceleration coordinates.