Uses of Class
org.orekit.orbits.FieldKeplerianOrbit

Packages that use FieldKeplerianOrbit

Package	Description
org.orekit.orbits	This package provides classes to represent orbits.
org.orekit.propagation.analytical	Top level package for analytical propagators.

Uses of FieldKeplerianOrbit in org.orekit.orbits

Methods in org.orekit.orbits that return FieldKeplerianOrbit

Modifier and Type	Method and Description
FieldKeplerianOrbit<T>	FieldKeplerianOrbit.interpolate(FieldAbsoluteDate<T> date, Stream<FieldOrbit<T>> sample) Get an interpolated instance.
FieldKeplerianOrbit<T>	FieldKeplerianOrbit.shiftedBy(double dt) Get a time-shifted instance.
FieldKeplerianOrbit<T>	FieldKeplerianOrbit.shiftedBy(T dt) Get a time-shifted orbit.

Uses of FieldKeplerianOrbit in org.orekit.propagation.analytical

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

Modifier and Type	Method and Description
static <T extends CalculusFieldElement<T>> FieldKeplerianOrbit<T>	FieldBrouwerLyddanePropagator.computeMeanOrbit(FieldOrbit<T> osculating, double referenceRadius, double mu, double c20, double c30, double c40, double c50, double M2Value, double epsilon, int maxIterations) Conversion from osculating to mean orbit.
static <T extends CalculusFieldElement<T>> FieldKeplerianOrbit<T>	FieldBrouwerLyddanePropagator.computeMeanOrbit(FieldOrbit<T> osculating, UnnormalizedSphericalHarmonicsProvider provider, UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics harmonics, double M2Value) Conversion from osculating to mean orbit.
static <T extends CalculusFieldElement<T>> FieldKeplerianOrbit<T>	FieldBrouwerLyddanePropagator.computeMeanOrbit(FieldOrbit<T> osculating, UnnormalizedSphericalHarmonicsProvider provider, UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics harmonics, double M2Value, double epsilon, int maxIterations) Conversion from osculating to mean orbit.
FieldKeplerianOrbit<T>	FieldBrouwerLyddanePropagator.propagateOrbit(FieldAbsoluteDate<T> date, T[] parameters) Extrapolate an orbit up to a specific target date.