Uses of Class
org.orekit.time.TimeStampedPair

Packages that use TimeStampedPair

Package	Description
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.

Uses of TimeStampedPair in org.orekit.propagation

Methods in org.orekit.propagation that return TimeStampedPair

Modifier and Type	Method and Description
protected TimeStampedPair<Orbit,StateCovariance>	AbstractStateCovarianceInterpolator.expressCovarianceInDesiredOutput(Orbit interpolatedOrbit, StateCovariance covarianceInOrbitFrame) Express covariance in output configuration defined at this instance construction.
TimeStampedPair<Orbit,StateCovariance>	AbstractStateCovarianceInterpolator.interpolate(AbstractTimeInterpolator.InterpolationData interpolationData) Interpolate orbit and associated covariance.

Method parameters in org.orekit.propagation with type arguments of type TimeStampedPair

Modifier and Type	Method and Description
protected StateCovariance	StateCovarianceBlender.computeInterpolatedCovarianceInOrbitFrame(List<TimeStampedPair<Orbit,StateCovariance>> uncertainStates, Orbit interpolatedOrbit) Compute the interpolated covariance expressed in the interpolated orbit frame.
protected StateCovariance	StateCovarianceKeplerianHermiteInterpolator.computeInterpolatedCovarianceInOrbitFrame(List<TimeStampedPair<Orbit,StateCovariance>> uncertainStates, Orbit interpolatedOrbit) Compute the interpolated covariance expressed in the interpolated orbit frame.
protected abstract StateCovariance	AbstractStateCovarianceInterpolator.computeInterpolatedCovarianceInOrbitFrame(List<TimeStampedPair<Orbit,StateCovariance>> uncertainStates, Orbit interpolatedOrbit) Compute the interpolated covariance expressed in the interpolated orbit frame.
protected Orbit	AbstractStateCovarianceInterpolator.interpolateOrbit(AbsoluteDate interpolationDate, List<TimeStampedPair<Orbit,StateCovariance>> neighborList) Interpolate orbit at given interpolation date.

Uses of TimeStampedPair in org.orekit.propagation.analytical

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

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

Method parameters in org.orekit.propagation.analytical with type arguments of type TimeStampedPair

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.

Constructor parameters in org.orekit.propagation.analytical with type arguments of type TimeStampedPair

Constructor and Description
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.

Uses of TimeStampedPair in org.orekit.propagation.conversion

Constructor parameters in org.orekit.propagation.conversion with type arguments of type TimeStampedPair

Constructor and Description
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.