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See this multi-body gravity example script that uses Spice. http://hanspeterschaub.info/basilisk/_modules/scenarioOrbitMultiBody.html#run It talks about setting However, it won't do it relative to a rotating planet fixed frame to the best of my knowledge. There you'd have to do some post-processing. |
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I've set a simulation creating the Earth through the Spice interface.
Does anybody know if it is possible to get the spacecraft state with respect to the Earth fixed rotating frame (IAU_Earth) or it is only possible to get the state relative to the inertial frame (r_BN_N) ?
The only thing that I've found is that the
SpicePlanetStateMsgPayload
hasJ20002Pfix
as one of the outputs but I if I try to make the matrix vector multiplication for each saved inertial position vector to get the ones in the planet fixed frame it takes a lot of time. For this reason I was wondering if there is any message or any way that I've not found yet that directly gives the r_BP_P position of the spacecraft.Thank you in advance!
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