Uses of Package
org.orekit.propagation.integration

Packages that use org.orekit.propagation.integration

Package	Description
org.orekit.propagation.integration	Utilities for integration-based propagators (both numerical and semi-analytical).
org.orekit.propagation.numerical	Top level package for numerical propagators.
org.orekit.propagation.semianalytical.dsst	This package provides an implementation of the Draper Semi-analytical Satellite Theory (DSST).

Classes in org.orekit.propagation.integration used by org.orekit.propagation.integration

Class	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	Differential equations for the main state (orbit, attitude and mass).
FieldAdditionalEquations	This interface allows users to add their own differential equations to a numerical propagator.
FieldStateMapper	This class maps between raw double elements and FieldSpacecraftState instances.
StateMapper	This class maps between raw double elements and SpacecraftState instances.

Classes in org.orekit.propagation.integration used by org.orekit.propagation.numerical

Class	Description
AbstractIntegratedPropagator	Common handling of Propagator methods for both numerical and semi-analytical propagators.
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	Common handling of FieldPropagator methods for both numerical and semi-analytical propagators.
FieldAbstractIntegratedPropagator.MainStateEquations	Differential equations for the main state (orbit, attitude and mass).
FieldStateMapper	This class maps between raw double elements and FieldSpacecraftState instances.
StateMapper	This class maps between raw double elements and SpacecraftState instances.

Classes in org.orekit.propagation.integration used by org.orekit.propagation.semianalytical.dsst

Class	Description
AbstractIntegratedPropagator	Common handling of Propagator methods for both numerical and semi-analytical propagators.
AbstractIntegratedPropagator.MainStateEquations	Differential equations for the main state (orbit, attitude and mass).
StateMapper	This class maps between raw double elements and SpacecraftState instances.