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

Packages that use FieldTimeDerivativesEquations

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 FieldTimeDerivativesEquations in org.orekit.forces

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

Modifier and Type	Method and Description
default <T extends RealFieldElement<T>> void	ForceModel.addContribution(FieldSpacecraftState<T> s, FieldTimeDerivativesEquations<T> adder) Compute the contribution of the force model to the perturbing acceleration.

Uses of FieldTimeDerivativesEquations in org.orekit.forces.gravity

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

Modifier and Type	Method and Description
<T extends RealFieldElement<T>> void	NewtonianAttraction.addContribution(FieldSpacecraftState<T> s, FieldTimeDerivativesEquations<T> adder) Compute the contribution of the force model to the perturbing acceleration.

Uses of FieldTimeDerivativesEquations in org.orekit.forces.maneuvers

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

Modifier and Type	Method and Description
<T extends RealFieldElement<T>> void	ConstantThrustManeuver.addContribution(FieldSpacecraftState<T> s, FieldTimeDerivativesEquations<T> adder) Compute the contribution of the force model to the perturbing acceleration.