Uses of Class
org.orekit.orbits.FieldCircularOrbit
Packages that use FieldCircularOrbit
Package
Description
This package provides classes to represent orbits.
Top level package for analytical propagators.
-
Uses of FieldCircularOrbit in org.orekit.orbits
Methods in org.orekit.orbits that return FieldCircularOrbitModifier and TypeMethodDescriptionCreate a new object representing the same physical orbital state, but attached to a different reference frame.FieldCircularOrbit.shiftedBy(double dt) Get a time-shifted orbit.FieldCircularOrbit.shiftedBy(TimeOffset dt) Get a time-shifted orbit.Get a time-shifted orbit.FieldCircularOrbit.withCachedPositionAngleType(PositionAngleType positionAngleType) Creates a new instance with the provided type used for caching.FieldCircularOrbit.withKeplerianRates()Creates a new instance such thatPositionAngleBased.hasNonKeplerianRates()is false. -
Uses of FieldCircularOrbit in org.orekit.propagation.analytical
Methods in org.orekit.propagation.analytical that return FieldCircularOrbitModifier and TypeMethodDescriptionstatic <T extends CalculusFieldElement<T>>
FieldCircularOrbit<T> FieldEcksteinHechlerPropagator.computeMeanOrbit(FieldOrbit<T> osculating, double referenceRadius, double mu, double c20, double c30, double c40, double c50, double c60, double epsilon, int maxIterations) Conversion from osculating to mean orbit.static <T extends CalculusFieldElement<T>>
FieldCircularOrbit<T> FieldEcksteinHechlerPropagator.computeMeanOrbit(FieldOrbit<T> osculating, double referenceRadius, double mu, double c20, double c30, double c40, double c50, double c60, OsculatingToMeanConverter converter) Conversion from osculating to mean orbit.static <T extends CalculusFieldElement<T>>
FieldCircularOrbit<T> FieldEcksteinHechlerPropagator.computeMeanOrbit(FieldOrbit<T> osculating, UnnormalizedSphericalHarmonicsProvider provider, UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics harmonics) Conversion from osculating to mean orbit.static <T extends CalculusFieldElement<T>>
FieldCircularOrbit<T> FieldEcksteinHechlerPropagator.computeMeanOrbit(FieldOrbit<T> osculating, UnnormalizedSphericalHarmonicsProvider provider, UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics harmonics, double epsilon, int maxIterations) Conversion from osculating to mean orbit.FieldEcksteinHechlerPropagator.getOsculatingCircularOrbit(FieldAbsoluteDate<T> date) Get the osculating circular orbit from the EH model.