Path: AC/ACCoord
% Convert from the body axes to stability axes.
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Form:
m = JacobVB( v )
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Inputs
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v (3,1) Velocity
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Outputs
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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.
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AC: ACCoord/AlphBeta Math: Linear/Mag
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