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.gravity	This package provides all gravity-related forces.
org.orekit.forces.maneuvers	This package provides models of simple maneuvers.

Uses of TimeDerivativesEquations in org.orekit.forces

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

Modifier and Type	Method	Description
default 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.gravity

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

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