Package org.orekit.propagation.integration

Utilities for integration-based propagators (both numerical and semi-analytical).

Interface Summary

Interface	Description
AbstractIntegratedPropagator.MainStateEquations	Differential equations for the main state (orbit, attitude and mass).
AdditionalEquations	This interface allows users to add their own differential equations to a numerical propagator.
FieldAbstractIntegratedPropagator.MainStateEquations<T extends org.hipparchus.RealFieldElement<T>>	Differential equations for the main state (orbit, attitude and mass).
FieldAdditionalEquations<T extends org.hipparchus.RealFieldElement<T>>	This interface allows users to add their own differential equations to a numerical propagator.
FieldModeHandler<T extends org.hipparchus.RealFieldElement<T>>	Common interface for all propagator mode handlers initialization.
ModeHandler	Common interface for all propagator mode handlers initialization.

Class Summary

Class	Description
AbstractIntegratedPropagator	Common handling of Propagator methods for both numerical and semi-analytical propagators.
FieldAbstractIntegratedPropagator<T extends org.hipparchus.RealFieldElement<T>>	Common handling of FieldPropagator methods for both numerical and semi-analytical propagators.
FieldIntegratedEphemeris<T extends org.hipparchus.RealFieldElement<T>>	This class stores sequentially generated orbital parameters for later retrieval.
FieldStateMapper<T extends org.hipparchus.RealFieldElement<T>>	This class maps between raw double elements and FieldSpacecraftState instances.
IntegratedEphemeris	This class stores sequentially generated orbital parameters for later retrieval.
StateMapper	This class maps between raw double elements and SpacecraftState instances.