fr.cnes.sirius.patrius.propagation.analytical

Interface AdapterPropagator.DifferentialEffect

All Known Implementing Classes:

J2DifferentialEffect, SmallManeuverAnalyticalModel

Enclosing class:

AdapterPropagator

public static interface AdapterPropagator.DifferentialEffect

Interface for orbit differential effects.

Method Summary

Modifier and Type	Method and Description
SpacecraftState	apply(SpacecraftState original) Apply the effect to a spacecraft state.

Method Detail

apply

SpacecraftState apply(SpacecraftState original)
               throws PatriusException

Apply the effect to a spacecraft state.

Applying the effect may be a no-op in some cases. A typical example is maneuvers, for which the state is changed only for time after the maneuver occurrence.

Parameters:

original - original state without the effect

Returns:

updated state at the same date, taking the effect into account if meaningful

Throws:

PatriusException - if effect cannot be computed