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

Packages that use AdditionalEquations

fr.cnes.sirius.patrius.assembly.models
fr.cnes.sirius.patrius.assembly.properties
fr.cnes.sirius.patrius.propagation.numerical.multi
org.orekit.propagation	This package provides tools to propagate orbital states with different methods.
org.orekit.propagation.numerical

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

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

AdditionalEquations	InertiaSimpleModel.getAdditionalEquation(String partName) Get the mass equation related to the part.
AdditionalEquations	InertiaComputedModel.getAdditionalEquation(String name) Get the mass equation related to the part.
AdditionalEquations	MassModel.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

class

MassEquation This class represents the mass equation with a name in the form "MASS_".

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

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

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

Uses of AdditionalEquations in org.orekit.propagation

Methods in org.orekit.propagation that return AdditionalEquations

AdditionalEquations	MassProvider.getAdditionalEquation(String name) Get the mass equation related to the part.
AdditionalEquations	SimpleMassModel.getAdditionalEquation(String name) Get the mass equation related to the part.

Uses of AdditionalEquations in org.orekit.propagation.numerical

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

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 org.orekit.propagation.numerical with parameters of type AdditionalEquations

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