ConeInt:

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   Computes the solution to the attitude determination problem using
   the cone intercept method. Only uses sun angles and chordwidths.
   Requires the corresponding sun vectors and nadir vectors. 
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   Form:
   [ra,dec,rd] = ConeInt( usun, unadir, sa, tle, tte, cant, eradius,
                          spinrate, threshold )
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   ------
   Inputs
   ------
   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                    Leading edge times
   tte                    Trailing edge time
   cant                   Cant angle (rad)
   eradius      (1,n)     Angular radius of the rearth (rad)
   spinrate               Spin rate (rad/sec)
   threshold              Threshold chord width (rad)

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

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Children:

AeroUtils: Coord/U2RADec
Common: Graphics/NewFig