When the aircraft attitude angle control, based on the quaternion and Euler angle of the coordinates of the conversion relationship between the Euler angle control method and quaternion control method conversion between.

234567\C2Eular.m
......\C2EularXYZ.m
......\C2Q.m
......\Cal_Coi.m
......\CrossX.m
......\Eular2C.m
......\Q2C.m
......\Q2Eular.m
......\QuaternionError.m
234567

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