This attitude guidance module computes the orbital Hill reference frame states.
The orbit can be any type of Keplerian motion, including circular, elliptical or hyperbolic.
This is also known as Hill Pointing software. The LVLH coordinate system is defined by
the unit vectors {i_r, i_theta, i_h}, with radial vector i_r, angular momentum vector
i_h = r^ x v^, and azimuthal vector i_theta 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.