Tabulated attitude laws in local orbital frames
We would like to propagate a spacecraft state with a tabulated attitude
law specified in an orbital frame.
One option would have been to use TabulatedProvider, but it seems to
only accept attitude tables given in an inertial frame. It is not always
possible to convert an attitude in an orbital frame to one in an
inertial frame if the underlying dynamics is dependant on the attitude.
Therefore, it would be desirable to make TabulatedProvider compatible with non-inertial frame, or provide a specific class for local orbital frame tabulated attitude laws.
(from redmine: issue id 227, created on 2015-12-14, closed on 2016-02-10)