Path: AC/ACCoord
% Euler angles given ECI information. Since version 2 (ACT) -------------------------------------------------------------------------- Form: e = EulNED( r, qECIToB, e ) -------------------------------------------------------------------------- ------ Inputs ------ r (3,1) ECI Position vector qECIToB (4,1) Quaternion from ECI to B e (3,1) Euler angles [phi;theta;psi] ------- Outputs ------- e (3,1) Euler angles [phi;theta;psi] -------------------------------------------------------------------------- Reference: Stevens, B.L., Lewis, F.L. , Aircraft Control and Simulation, John Wiley & Sons, 1992, p. 38. --------------------------------------------------------------------------
AC: ACCoord/ECIToNED Common: Quaternion/Q2Eul Common: Quaternion/QMult Common: Quaternion/QPose
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