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

Packages that use AdditionalDerivativesProvider

Package	Description
org.orekit.control.indirect.adjoint	This package provides routines to model the adjoint dynamics as in the Pontryagin Maximum Principle, as used in indirect control.
org.orekit.control.indirect.shooting.propagation	This package provides classes relative to the propagation part of indirect shooting.
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.control.indirect.adjoint

Classes in org.orekit.control.indirect.adjoint that implement AdditionalDerivativesProvider

Modifier and Type	Class	Description
class	CartesianAdjointDerivativesProvider	Class defining the adjoint dynamics, as defined in the Pontryagin Maximum Principle, in the case where Cartesian coordinates in an inertial frame are the dependent variable.

Uses of AdditionalDerivativesProvider in org.orekit.control.indirect.shooting.propagation

Methods in org.orekit.control.indirect.shooting.propagation that return AdditionalDerivativesProvider

Modifier and Type	Method	Description
AdditionalDerivativesProvider	AdjointDynamicsProvider.buildAdditionalDerivativesProvider()	Builds adjoint derivatives provider.

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

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

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