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