JacobVB:

Path: AC/ACCoord

% Convert from the body axes to stability axes.
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   Form:
   m = JacobVB( v )
--------------------------------------------------------------------------

   ------
   Inputs
   ------
   v           (3,1) Velocity

   -------
   Outputs
   -------
   m           (3,3) Jacobian matrix
                     [Vx/alpha Vx/beta Vx/vT]
                     [Vy/alpha Vy/beta Vy/vT]
                     [Vz/alpha Vz/beta Vz/vT]

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

Children:

AC: ACCoord/AlphBeta
Math: Linear/Mag

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