Package fr.cnes.sirius.patrius.propagation

Interface Summary

Interface	Description
AdditionalStateProvider	This interface represents providers for additional state data beyond SpacecraftState.
BoundedPropagator	This interface is intended for ephemerides valid only during a time range.
MassProvider	Interface for spacecraft models that provide the mass.
MeanOsculatingElementsProvider	Interface for mean/osculating elements converter.
MultiPropagator	This interface is copied from Propagator and adapted to multi propagation.
Propagator	This interface provides a way to propagate an orbit at any time.

Class Summary

Class	Description
AbstractPropagator	Common handling of Propagator methods for analytical propagators.
AnalyticalIntegratedEphemeris	This class stores sequentially generated orbital parameters for later retrieval.
PVCoordinatePropagator	This class is an analytical propagator which propagates states from the input PV, Attitude, and additional state provider.
SimpleAdditionalStateProvider	This class is a simple implementation of additionalStateProvider.
SimpleMassModel	Simple implementation of MassProvider.
SpacecraftState	This class is the representation of a complete state holding orbit, attitude for forces and events computation and additional states informations at a given date.

Enum Summary

Enum	Description
ParametersType	Enum class for elements type (mean or osculating).