SToW:

Path: AC/ACCoord

% Convert from stability axes to wind axes.
--------------------------------------------------------------------------
   Form:
   b = SToW( beta, opt )
--------------------------------------------------------------------------

   ------
   Inputs
   ------
   beta        (1,1) Sideslip angle (rad)
   opt         (1,:) 'matrix' or 'quaternion'

   -------
   Outputs
   -------
   b           (3,3) Transformation matrix
               (4,1) Quaternion

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   Reference: Stevens, B.L., Lewis, F.L. , Aircraft Control and 
              Simulation, John Wiley & Sons, 1992, p. 63.
--------------------------------------------------------------------------

Children:

Common: Quaternion/Mat2Q

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