Path: AC/ACCoord
% Compute body velocity from alpha, beta and vT. Since version 2 (ACT) -------------------------------------------------------------------------- Form: vB = VTToVB( vT, alpha, beta ) -------------------------------------------------------------------------- ------ Inputs ------ vT (1,1) Velocity alpha (1,1) Angle of attack (rad) beta (1,1) Sideslip angle (rad) ------- Outputs ------- vB (3,1) Velocity in the body frame -------------------------------------------------------------------------- Reference: Stevens, B.L., Lewis, F.L. , Aircraft Control and Simulation, John Wiley & Sons, 1992, p. 64. --------------------------------------------------------------------------
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