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

Packages that use TimeDerivativesEquations

Package	Description
fr.cnes.sirius.patrius.assembly.properties
fr.cnes.sirius.patrius.forces
fr.cnes.sirius.patrius.forces.drag
fr.cnes.sirius.patrius.forces.gravity
fr.cnes.sirius.patrius.forces.gravity.tides
fr.cnes.sirius.patrius.forces.gravity.variations
fr.cnes.sirius.patrius.forces.maneuvers
fr.cnes.sirius.patrius.forces.radiation
fr.cnes.sirius.patrius.forces.relativistic
fr.cnes.sirius.patrius.propagation.numerical

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

Methods in fr.cnes.sirius.patrius.assembly.properties with parameters of type TimeDerivativesEquations

Modifier and Type	Method and Description
void	MassEquation.computeDerivatives(SpacecraftState s, TimeDerivativesEquations adder) Compute the derivatives related to the additional state parameters.

Uses of TimeDerivativesEquations in fr.cnes.sirius.patrius.forces

Methods in fr.cnes.sirius.patrius.forces with parameters of type TimeDerivativesEquations

Modifier and Type	Method and Description
void	EmpiricalForce.addContribution(SpacecraftState state, TimeDerivativesEquations adder) Compute the contribution of the force model to the perturbing acceleration.
void	ForceModel.addContribution(SpacecraftState s, TimeDerivativesEquations adder) Compute the contribution of the force model to the perturbing acceleration.

Uses of TimeDerivativesEquations in fr.cnes.sirius.patrius.forces.drag

Methods in fr.cnes.sirius.patrius.forces.drag with parameters of type TimeDerivativesEquations

Modifier and Type	Method and Description
void	DragForce.addContribution(SpacecraftState s, TimeDerivativesEquations adder) Compute the contribution of the drag to the perturbing acceleration.

Uses of TimeDerivativesEquations in fr.cnes.sirius.patrius.forces.gravity

Methods in fr.cnes.sirius.patrius.forces.gravity with parameters of type TimeDerivativesEquations

Modifier and Type	Method and Description
void	BalminoAttractionModel.addContribution(SpacecraftState state, TimeDerivativesEquations adder) Compute the contribution of the force model to the perturbing acceleration.
void	ThirdBodyAttraction.addContribution(SpacecraftState s, TimeDerivativesEquations adder) Compute the contribution of the force model to the perturbing acceleration.
void	CunninghamAttractionModel.addContribution(SpacecraftState state, TimeDerivativesEquations adder) Compute the contribution of the force model to the perturbing acceleration.
void	NewtonianAttraction.addContribution(SpacecraftState s, TimeDerivativesEquations adder) Compute the contribution of the force model to the perturbing acceleration.
void	DrozinerAttractionModel.addContribution(SpacecraftState state, TimeDerivativesEquations adder) Compute the contribution of the force model to the perturbing acceleration.

Uses of TimeDerivativesEquations in fr.cnes.sirius.patrius.forces.gravity.tides

Methods in fr.cnes.sirius.patrius.forces.gravity.tides with parameters of type TimeDerivativesEquations

Modifier and Type	Method and Description
void	AbstractTides.addContribution(SpacecraftState s, TimeDerivativesEquations adder) Compute the contribution of the force model to the perturbing acceleration.

Uses of TimeDerivativesEquations in fr.cnes.sirius.patrius.forces.gravity.variations

Methods in fr.cnes.sirius.patrius.forces.gravity.variations with parameters of type TimeDerivativesEquations

Modifier and Type	Method and Description
void	VariablePotentialAttractionModel.addContribution(SpacecraftState s, TimeDerivativesEquations adder) Compute the contribution of the force model to the perturbing acceleration.

Uses of TimeDerivativesEquations in fr.cnes.sirius.patrius.forces.maneuvers

Methods in fr.cnes.sirius.patrius.forces.maneuvers with parameters of type TimeDerivativesEquations

Modifier and Type	Method and Description
void	ConstantThrustError.addContribution(SpacecraftState s, TimeDerivativesEquations adder) Compute the contribution of the constant thrust error model to the perturbing acceleration.
void	ContinuousThrustManeuver.addContribution(SpacecraftState s, TimeDerivativesEquations adder) Compute the contribution of the force model to the perturbing acceleration.

Uses of TimeDerivativesEquations in fr.cnes.sirius.patrius.forces.radiation

Methods in fr.cnes.sirius.patrius.forces.radiation with parameters of type TimeDerivativesEquations

Modifier and Type	Method and Description
void	SolarRadiationPressureCircular.addContribution(SpacecraftState s, TimeDerivativesEquations adder) Compute the contribution of the force model to the perturbing acceleration.
void	RediffusedRadiationPressure.addContribution(SpacecraftState s, TimeDerivativesEquations adder) Compute the contribution of the force model to the perturbing acceleration.
void	SolarRadiationPressureEllipsoid.addContribution(SpacecraftState s, TimeDerivativesEquations adder) Compute the contribution of the force model to the perturbing acceleration.

Uses of TimeDerivativesEquations in fr.cnes.sirius.patrius.forces.relativistic

Methods in fr.cnes.sirius.patrius.forces.relativistic with parameters of type TimeDerivativesEquations

Modifier and Type	Method and Description
void	CoriolisRelativisticEffect.addContribution(SpacecraftState s, TimeDerivativesEquations adder) Compute the contribution of the force model to the perturbing acceleration.
void	LenseThirringRelativisticEffect.addContribution(SpacecraftState s, TimeDerivativesEquations adder) Compute the contribution of the force model to the perturbing acceleration.
void	SchwarzschildRelativisticEffect.addContribution(SpacecraftState s, TimeDerivativesEquations adder) Compute the contribution of the force model to the perturbing acceleration.

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

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

Modifier and Type	Method and Description
void	PartialDerivativesEquations.computeDerivatives(SpacecraftState s, TimeDerivativesEquations adder) Compute the derivatives related to the additional state parameters.
void	AdditionalEquations.computeDerivatives(SpacecraftState s, TimeDerivativesEquations adder) Compute the derivatives related to the additional state parameters.