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

Packages that use TimeDerivativesEquations

Package	Description
org.orekit.forces	This package provides the interface for force models that will be used by the NumericalPropagator, as well as some classical spacecraft models for surface forces (spherical, box and solar array ...).
org.orekit.forces.drag
org.orekit.forces.gravity	This package provides all gravity-related forces.
org.orekit.forces.maneuvers	This package provides models of simple maneuvers.
org.orekit.forces.radiation

Uses of TimeDerivativesEquations in org.orekit.forces

Methods in org.orekit.forces with parameters of type TimeDerivativesEquations

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

Uses of TimeDerivativesEquations in org.orekit.forces.drag

Methods in org.orekit.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 org.orekit.forces.gravity

Methods in org.orekit.forces.gravity with parameters of type TimeDerivativesEquations

Modifier and Type	Method and Description
void	SolidTides.addContribution(SpacecraftState s, TimeDerivativesEquations adder) Compute the contribution of the force model to the perturbing acceleration.
void	CunninghamAttractionModel.addContribution(SpacecraftState s, TimeDerivativesEquations adder) Compute the contribution of the force model to the perturbing acceleration.
void	Relativity.addContribution(SpacecraftState s, TimeDerivativesEquations adder)
void	ThirdBodyAttraction.addContribution(SpacecraftState s, TimeDerivativesEquations adder) Compute the contribution of the force model to the perturbing acceleration.
void	OceanTides.addContribution(SpacecraftState s, TimeDerivativesEquations adder) Compute the contribution of the force model to the perturbing acceleration.
void	DrozinerAttractionModel.addContribution(SpacecraftState s, TimeDerivativesEquations adder) Compute the contribution of the force model to the perturbing acceleration.
void	HolmesFeatherstoneAttractionModel.addContribution(SpacecraftState s, 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.

Uses of TimeDerivativesEquations in org.orekit.forces.maneuvers

Methods in org.orekit.forces.maneuvers with parameters of type TimeDerivativesEquations

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

Uses of TimeDerivativesEquations in org.orekit.forces.radiation

Methods in org.orekit.forces.radiation with parameters of type TimeDerivativesEquations

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