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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