Uses of Interface
org.orekit.propagation.integration.AdditionalDerivativesProvider

Packages that use AdditionalDerivativesProvider

Package	Description
org.orekit.forces.maneuvers.jacobians	Generators for columns of Jacobian matrices related to maneuver parameters.
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.

Uses of AdditionalDerivativesProvider in org.orekit.forces.maneuvers.jacobians

Classes in org.orekit.forces.maneuvers.jacobians that implement AdditionalDerivativesProvider

Modifier and Type	Class and Description
class	MassDepletionDelay Generator for effect of delaying mass depletion when delaying a maneuver.

Uses of AdditionalDerivativesProvider in org.orekit.propagation.conversion

Methods in org.orekit.propagation.conversion that return types with arguments of type AdditionalDerivativesProvider

Modifier and Type	Method and Description
protected List<AdditionalDerivativesProvider>	AbstractPropagatorBuilder.getAdditionalDerivativesProviders() Get the list of additional equations.

Methods in org.orekit.propagation.conversion with parameters of type AdditionalDerivativesProvider

Modifier and Type	Method and Description
void	AbstractPropagatorBuilder.addAdditionalDerivativesProvider(AdditionalDerivativesProvider provider) Add a set of user-specified equations to be integrated along with the orbit propagation (author Shiva Iyer).

Uses of AdditionalDerivativesProvider in org.orekit.propagation.integration

Methods in org.orekit.propagation.integration that return types with arguments of type AdditionalDerivativesProvider

Modifier and Type	Method and Description
List<AdditionalDerivativesProvider>	AbstractIntegratedPropagator.getAdditionalDerivativesProviders() Get an unmodifiable list of providers for additional derivatives.

Methods in org.orekit.propagation.integration with parameters of type AdditionalDerivativesProvider

Modifier and Type	Method and Description
void	AbstractIntegratedPropagator.addAdditionalDerivativesProvider(AdditionalDerivativesProvider provider) Add a provider for user-specified state derivatives to be integrated along with the orbit propagation.

Uses of AdditionalDerivativesProvider in org.orekit.propagation.numerical

Classes in org.orekit.propagation.numerical that implement AdditionalDerivativesProvider

Modifier and Type	Class and Description
class	EpochDerivativesEquations Computes derivatives of the acceleration, including ThirdBodyAttraction.

Uses of AdditionalDerivativesProvider in org.orekit.propagation.numerical.cr3bp

Classes in org.orekit.propagation.numerical.cr3bp that implement AdditionalDerivativesProvider

Modifier and Type	Class and Description
class	STMEquations Class calculating the state transition matrix coefficient for CR3BP Computation.