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.

 
  • 然后根據飛行姿態(tài)記錄,通過(guò)數據辨識,求得俯仰力矩系數斜率,俯仰阻尼力矩系數和馬格努斯力矩系數。
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