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).
AdditionalDerivativesProvider	Provider for additional derivatives.
FieldAbstractIntegratedPropagator.MainStateEquations<T extends CalculusFieldElement<T>>	Differential equations for the main state (orbit, attitude and mass).
FieldAdditionalDerivativesProvider<T extends CalculusFieldElement<T>>	Provider for additional derivatives.

Class Summary

Class	Description
AbstractGradientConverter	Converter for states and parameters arrays.
AbstractIntegratedPropagator	Common handling of Propagator methods for both numerical and semi-analytical propagators.
CombinedDerivatives	Container for additional derivatives.
FieldAbstractIntegratedPropagator<T extends CalculusFieldElement<T>>	Common handling of FieldPropagator methods for both numerical and semi-analytical propagators.
FieldCombinedDerivatives<T extends CalculusFieldElement<T>>	Container for additional derivatives.
FieldIntegratedEphemeris<T extends CalculusFieldElement<T>>	This class stores sequentially generated orbital parameters for later retrieval.
FieldStateMapper<T extends CalculusFieldElement<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.