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

Packages that use AdditionalEquations

Package	Description
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.

Uses of AdditionalEquations in org.orekit.propagation.conversion

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

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

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

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

Uses of AdditionalEquations in org.orekit.propagation.integration

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

Modifier and Type	Method and Description
void	AbstractIntegratedPropagator.addAdditionalEquations(AdditionalEquations additional) Add a set of user-specified equations to be integrated along with the orbit propagation.

Uses of AdditionalEquations in org.orekit.propagation.numerical

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

Modifier and Type	Class and Description
class	AbsolutePartialDerivativesEquations Set of additional equations computing the partial derivatives of the state (orbit) with respect to initial state and force models parameters.
class	EpochDerivativesEquations This class is a copy of AbsolutePartialDerivativesEquations The computation of the derivatives of the acceleration due to a ThirdBodyAttraction has been added.
class	PartialDerivativesEquations Set of additional equations computing the partial derivatives of the state (orbit) with respect to initial state and force models parameters.

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

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

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

Methods in org.orekit.propagation.numerical.cr3bp with parameters of type AdditionalEquations

Modifier and Type	Method and Description
protected SpacecraftState	CR3BPMultipleShooter.getAugmentedInitialState(SpacecraftState initialState, AdditionalEquations additionalEquation) Compute the additional state from the additionalEquations.

Constructor parameters in org.orekit.propagation.numerical.cr3bp with type arguments of type AdditionalEquations

Constructor and Description
CR3BPMultipleShooter(List<SpacecraftState> initialGuessList, List<NumericalPropagator> propagatorList, List<AdditionalEquations> additionalEquations, double arcDuration, double tolerance) Simple Constructor.

Uses of AdditionalEquations in org.orekit.propagation.semianalytical.dsst

Classes in org.orekit.propagation.semianalytical.dsst that implement AdditionalEquations

Modifier and Type	Class and Description
class	DSSTPartialDerivativesEquations Set of additional equations computing the partial derivatives of the state (orbit) with respect to initial state and force models parameters.

Uses of AdditionalEquations in org.orekit.utils

Methods in org.orekit.utils with parameters of type AdditionalEquations

Modifier and Type	Method and Description
protected SpacecraftState	MultipleShooter.getAugmentedInitialState(SpacecraftState initialState, AdditionalEquations additionalEquation) Compute the additional state from the additionalEquations.
protected abstract SpacecraftState	AbstractMultipleShooting.getAugmentedInitialState(SpacecraftState initialState, AdditionalEquations additionalEquations2) Compute the additional state from the additionalEquations.

Constructor parameters in org.orekit.utils with type arguments of type AdditionalEquations

Constructor and Description
AbstractMultipleShooting(List<SpacecraftState> initialGuessList, List<NumericalPropagator> propagatorList, List<AdditionalEquations> additionalEquations, double arcDuration, double tolerance, String additionalName) Simple Constructor.
MultipleShooter(List<SpacecraftState> initialGuessList, List<NumericalPropagator> propagatorList, List<AdditionalEquations> additionalEquations, double arcDuration, double tolerance) Simple Constructor.