Swing-by trajectory about Jupiter compared in EME2000, ICRF and
Jupiter-centered inertial reference frame.
Case 1:
- Integration frame: EME2000
- Representation of the trajectory: AbsolutePVCoordinates
- No central body
- SingleBodyAbsoluteAttraction with Jupiter
- SingleBodyAbsoluteAttraction with the Sun and all remaining planets
- InertialForces between EME2000 and ICRF
Case 2:
- Integration frame: ICRF
- Representation of the trajectory: AbsolutePVCoordinates
- No central body
- SingleBodyAbsoluteAttraction with Jupiter
- SingleBodyAbsoluteAttraction with the Sun and all remaining planets
Case 3:
- Integration frame: Jupiter-centered inertial
- Representation of the trajectory: Cartesian orbit
- Central body: Jupiter
- ThirdBodyAttraction with the Sun and all remaining planets
All trajectories output in Jovian frame.