Uses of Interface org.orekit.propagation.numerical.TimeDerivativesEquations (ORbit Extrapolation KIT 9.3 API)

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.