This paper discussed the application of this method in the design of flight control system for the poststall maneuver.
针对过失速机动飞机探讨了非线性动态逆方法在飞行控制系统设计中的应用。
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This paper investigates the large Angle attitude poststall maneuver control for the agile turn phase of an air-to-air missile that has high off-boresight capability and head reverse maneuverability.