Package org.orekit.propagation.integration

Utilities for integration-based propagators (both numerical and semi-analytical).

See: Description

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 org.hipparchus.CalculusFieldElement<T>>	Differential equations for the main state (orbit, attitude and mass).
FieldAdditionalDerivativesProvider<T extends org.hipparchus.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 org.hipparchus.CalculusFieldElement<T>>	Common handling of FieldPropagator methods for both numerical and semi-analytical propagators.
FieldCombinedDerivatives<T extends org.hipparchus.CalculusFieldElement<T>>	Container for additional derivatives.
FieldIntegratedEphemeris<T extends org.hipparchus.CalculusFieldElement<T>>	This class stores sequentially generated orbital parameters for later retrieval.
FieldStateMapper<T extends org.hipparchus.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.

Package org.orekit.propagation.integration Description

Utilities for integration-based propagators (both numerical and semi-analytical).