Path: AC/ACCoord
% Convert from the body axes to stability axes. Since version 2 (ACT) -------------------------------------------------------------------------- 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] -------------------------------------------------------------------------- Reference: Stevens, B.L., Lewis, F.L. , Aircraft Control and Simulation, John Wiley & Sons, 1992, p. 63. --------------------------------------------------------------------------
AC: ACCoord/AlphBeta Math: Linear/Mag
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