Uses of Package
org.orekit.propagation.integration

Packages that use org.orekit.propagation.integration

Package	Description
org.orekit.estimation.leastsquares	The leastsquares package provides an implementation of a batch least squares estimator engine to perform an orbit determination.
org.orekit.estimation.measurements.modifiers	This package provides measurement modifier.
org.orekit.estimation.sequential	The sequential package provides an implementation of a Kalman Filter engine to perform an orbit determination.
org.orekit.propagation.conversion	This package provides tools to convert a given propagator or a set of SpacecraftState into another propagator.
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.numerical.cr3bp	Top level package for CR3BP Models used with a numerical propagator.
org.orekit.propagation.semianalytical.dsst	This package provides an implementation of the Draper Semi-analytical Satellite Theory (DSST).
org.orekit.utils	This package provides useful objects.

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

Class and Description
AbstractIntegratedPropagator Common handling of Propagator methods for both numerical and semi-analytical propagators.

Classes in org.orekit.propagation.integration used by org.orekit.estimation.measurements.modifiers

Class and Description
AbstractGradientConverter Converter for states and parameters arrays for both numerical and semi-analytical propagators.

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

Class and Description
AbstractIntegratedPropagator Common handling of Propagator methods for both numerical and semi-analytical propagators.

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

Class and Description
AdditionalEquations This interface allows users to add their own differential equations to a numerical propagator.

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).
AbstractJacobiansMapper Base class for jacobian mapper.
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.numerical.cr3bp

Class and Description
AdditionalEquations This interface allows users to add their own differential equations to a numerical propagator.

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).
AbstractJacobiansMapper Base class for jacobian mapper.
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.utils

Class and Description
AdditionalEquations This interface allows users to add their own differential equations to a numerical propagator.