This attitude guidance module computes the velocity pointing reference frame state.
The orbit can be any type of Keplerian motion, including circular, elliptical or hyperbolic.
The velocity coordinate system is defined by the unit vectors {i_n, i_v, i_h},
with velocity vector i_v, angular momentum vector i_h = r^ x v^, and normal vector i_n
to complete the triad.
This method is called whenever some key parameters are changedand any new local variables are required to be recalculated. Thiscan be called by the software chains if a configuration of somevalues are updated.