Hey all!
I have a question about the local orbit frames. I couldn’t really find a tutorial or anything for this, so I thought it would be best to ask the question here.
Suppose I have the spacecraft states of an estimated state (from OD), a reference state, and the ± 3 sigma bounds of the estimated state (SCest, SCref, SCstd_pos, SCstd_neg).
I want to transform these to a local orbital frame (NTW for example). How would I do this?
Thanks in advance,
Niek