OK - that shows conclusively that the aircraft had a yaw oscillation. Did you notice that - you did not mention it in your description. Anyway, both the IMU yaw and magnetic yaw recorded the oscillation. The IMU source was the z-axis rate gyro, that clearly shows the rotations. The direct cause is also clear - computing the difference between the CW and CCW prop rotation rates gives us a measure of the total motor angular momentum which will turn the aircraft both due to the change in angular momentum and the difference in prop drag. The graph below is somewhat busy, but that's necessary to show the relationship between all the plotted values, and it's simple enough if you refer to the legend.
![2018-07-04_[20-54-22]_06.png 2018-07-04_[20-54-22]_06.png](https://mavicpilots.com/data/attachments/42/42495-24acd36e2f146ecca6a69d9839b57784.jpg?hash=JKzTbi8Ubs)
The motor speed changes correlate perfectly with the yaw oscillations. Since they were not commanded by rudder input, the FC was directing them which, to me, looks like a gain issue. However, this still is not the direct cause of the lateral motion and crash, which was caused by the stick inputs.