Package org.orekit.propagation.integration

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.
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.
IntegratedEphemeris	This class stores sequentially generated orbital parameters for later retrieval.
StateMapper	This class maps between raw double elements and SpacecraftState instances.