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).
AdditionalEquations	This interface allows users to add their own differential equations to a numerical propagator.
FieldAbstractIntegratedPropagator.MainStateEquations<T extends CalculusFieldElement<T>>	Differential equations for the main state (orbit, attitude and mass).
FieldAdditionalEquations<T extends CalculusFieldElement<T>>	This interface allows users to add their own differential equations to a numerical propagator.

Class Summary

Class	Description
AbstractGradientConverter	Converter for states and parameters arrays.
AbstractIntegratedPropagator	Common handling of Propagator methods for both numerical and semi-analytical propagators.
AbstractJacobiansMapper	Base class for jacobian mapper.
FieldAbstractIntegratedPropagator<T extends CalculusFieldElement<T>>	Common handling of FieldPropagator methods for both numerical and semi-analytical propagators.
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.

Package org.orekit.propagation.integration Description

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