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Added warning, needs more work on the rotation matrix output
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@@ -413,6 +413,8 @@ int attitude_estimator_ekf_thread_main(int argc, char *argv[])
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/* send out */
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att.timestamp = raw.timestamp;
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// XXX Apply the same transformation to the rotation matrix
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att.roll = euler[0] - ekf_params.roll_off;
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att.pitch = euler[1] - ekf_params.pitch_off;
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att.yaw = euler[2] - ekf_params.yaw_off;
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