Through the processing of the altitute angle data, the static pitching moment stability coefficient, the damping moment stability coefficent and the Magnus moment stability coefficient can be obtained.

• 然后根据飞行姿态记录,通过数据辨识,求得俯仰力矩系数斜率,俯仰阻尼力矩系数和马格努斯力矩系数。