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PX4-Autopilot/EKF/matlab/scripts/Inertial Nav EKF/NormQuat.m
T
2018-05-03 22:25:36 -04:00

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Matlab

% normalise the quaternion
function quaternion = normQuat(quaternion)
quatMag = sqrt(quaternion(1)^2 + quaternion(2)^2 + quaternion(3)^2 + quaternion(4)^2);
quaternion(1:4) = quaternion / quatMag;