The effectiveness of some departure/spin resistance system, including angle-of-attack boundary control system, aileron-rudder-interconnect system (ARI) and stability-axis yaw damper, is discussed.

 
  • 在此基础上探 讨了各类飞控系统控制律的效果及其相应参数的选择,其中包括迎角 边界控制系统、ARI系统和稳定轴偏航阻尼器等。
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