Computes the solution to the attitude determination problem using
   Schuster's single frame method. Uses sun angles, dihedral angles
   and chordwidths. 
   Requires the corresponding sun vectors and nadir vectors. 

   The 4th and 5th inputs can either be leading and trailing edge times
   or chordwidths and mid-scan dihedral angles, respectively. The last 
   input must be set to either 'time' or 'angl'. The default is 'time'.
   [ra, dec, rd] = SFShustr( usun, unadir, sa, tle_cw, tte_da, cant, eradius,
                             spinrate, threshold, dihedral, type )

   usun         (3,n)     Unit sun vector
   unadir       (3,n)     Unit nadir vectors
   sa           (1,n)     The angle between the sun line and the spin axis
   tle_cw       (1,n)     Leading edge times (sec) or chordwidths (rad)
   tte_da       (1,n)     Trailing edge time (sec) or mid-scan dihedral angles (rad)
   cant                   Cant angle (rad)
   eradius      (1,n)     Angular radius of the rearth (rad)
   spinrate               Spin rate (rad/sec)
   threshold              Threshold chord width (rad)
   dihedral               Dihedral angle of hsa (rad)
   type                   'time' = leading and trail edge times entered (default)
                          'angl' = chordwidths and dihedral angles entered

   ra                     Right ascension of the spin axis
   dec                    Declination of the spin axis
   rd           (2,n)     [Right Ascension;Declination] vector

	References:	Shuster, M.D., Efficient Algorithms for Spin-Axis Attitude
               Determination, The Journal of the Astronautical Sciences,
               Vol. XXXI, No. 2, April-June, 1983, pp. 237-249.


Common: Graphics/NewFig
Common: Graphics/XLabelS
Common: Graphics/YLabelS
Math: Linear/Unit