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px4-firmware/EKF/matlab/scripts/Inertial Nav EKF/yaw_input_321.c

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matlab: Fix derivation for 321 Euler rotation sequence
2017-07-20 21:48:54 -03:00
A0[0][0] = q0*q3*2.0+q1*q2*2.0;
matlab: Add scripts to calculate rotation conversions for 321 or 312 Euler sequences
2017-07-20 21:10:03 -03:00
A0[1][0] = q0*q0+q1*q1-q2*q2-q3*q3;