Package | Description |
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fr.cnes.sirius.patrius.forces | |
fr.cnes.sirius.patrius.frames |
Modifier and Type | Method and Description |
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Vector3D |
EmpiricalForce.computeAcceleration(PVCoordinates pv,
LocalOrbitalFrame localFrameValidation,
Vector3D vectorS,
Frame frame,
SpacecraftState state)
Method to compute the acceleration.
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Constructor and Description |
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SynodicFrame(LocalOrbitalFrame parentLOF,
String name,
double normalizedCenterPosition)
Constructor.
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