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 and 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 and 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 and 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.