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

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	Description
`default <T extends org.hipparchus.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	Description
`<T extends org.hipparchus.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	Description
`<T extends org.hipparchus.RealFieldElement<T>> void`	ConstantThrustManeuver.`addContribution(FieldSpacecraftState<T> s, FieldTimeDerivativesEquations<T> adder)`	Compute the contribution of the force model to the perturbing acceleration.