Package fr.cnes.sirius.patrius.propagation.analytical

Interface Summary

Interface	Description
AdapterPropagator.DifferentialEffect	Interface for orbit differential effects.

Class Summary

Class	Description
AbstractLyddanePropagator	Abstract Lyddane propagator.
AdapterPropagator	Orbit propagator that adapts an underlying propagator, adding differential effects.
AnalyticalEphemerisModeHandler	This class stores sequentially generated orbital parameters for later retrieval.
EcksteinHechlerPropagator	This class propagates a SpacecraftState using the analytical Eckstein-Hechler model.
J2DifferentialEffect	Analytical model for J2 effect.
J2SecularPropagator	J2 secular propagator.
KeplerianPropagator	Simple keplerian orbit propagator.
LiuMeanOsculatingConverter	Liu mean - osculating elements converter.
LyddaneLongPeriodPropagator	Lyddane long period propagator.
LyddaneSecularPropagator	Lyddane secular propagator.

Enum Summary

Enum	Description
AbstractLyddanePropagator.LyddaneParametersType	Lyddane parameters types.
AbstractLyddanePropagator.SubModel	Enumerate that indicates how we deal with eccentricity DEFAULT : Used only for the first call of propagateOrbit in computeSecular to compute ecc model LOW_ECC : Used to keep low ecc model if computed during first call HIGH_ECC : Used to keep high ecc model if computed during first call