Uses of Interface
fr.cnes.sirius.patrius.propagation.numerical.AdditionalEquations

Packages that use AdditionalEquations

Package	Description
fr.cnes.sirius.patrius.assembly.models
fr.cnes.sirius.patrius.assembly.properties
fr.cnes.sirius.patrius.propagation
fr.cnes.sirius.patrius.propagation.numerical
fr.cnes.sirius.patrius.propagation.numerical.multi

Uses of AdditionalEquations in fr.cnes.sirius.patrius.assembly.models

Methods in fr.cnes.sirius.patrius.assembly.models that return AdditionalEquations

Modifier and Type	Method and Description
AdditionalEquations	InertiaSimpleModel.getAdditionalEquation(String partName) Get the mass equation related to the part.
AdditionalEquations	MassModel.getAdditionalEquation(String name) Get the mass equation related to the part.
AdditionalEquations	InertiaComputedModel.getAdditionalEquation(String name) Get the mass equation related to the part.

Uses of AdditionalEquations in fr.cnes.sirius.patrius.assembly.properties

Classes in fr.cnes.sirius.patrius.assembly.properties that implement AdditionalEquations

Modifier and Type	Class and Description
class	MassEquation This class represents the mass equation with a name in the form "MASS_".

Uses of AdditionalEquations in fr.cnes.sirius.patrius.propagation

Methods in fr.cnes.sirius.patrius.propagation that return AdditionalEquations

Modifier and Type	Method and Description
AdditionalEquations	SimpleMassModel.getAdditionalEquation(String name) Get the mass equation related to the part.
AdditionalEquations	MassProvider.getAdditionalEquation(String name) Get the mass equation related to the part.

Uses of AdditionalEquations in fr.cnes.sirius.patrius.propagation.numerical

Classes in fr.cnes.sirius.patrius.propagation.numerical that implement AdditionalEquations

Modifier and Type	Class and Description
class	AttitudeEquation This interface allows users to add their own attitude differential equations to a numerical propagator.
class	PartialDerivativesEquations Set of additional equations computing the partial derivatives of the state (orbit) with respect to initial state and force models parameters.

Methods in fr.cnes.sirius.patrius.propagation.numerical that return AdditionalEquations

Modifier and Type	Method and Description
AdditionalEquations	AdditionalEquationsAndTolerances.getEquations() Get the additional equations.

Methods in fr.cnes.sirius.patrius.propagation.numerical with parameters of type AdditionalEquations

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

Constructors in fr.cnes.sirius.patrius.propagation.numerical with parameters of type AdditionalEquations

Constructor and Description
AdditionalEquationsAndTolerances(AdditionalEquations equationsIn) Simple constructor.

Uses of AdditionalEquations in fr.cnes.sirius.patrius.propagation.numerical.multi

Classes in fr.cnes.sirius.patrius.propagation.numerical.multi that implement AdditionalEquations

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

Methods in fr.cnes.sirius.patrius.propagation.numerical.multi with parameters of type AdditionalEquations

Modifier and Type	Method and Description
void	MultiNumericalPropagator.addAdditionalEquations(AdditionalEquations addEqu, String satId) Add a set of user-specified equations to be integrated along with the orbit propagation.