The study will provide a new theoretical approach to investigate aircraft agility, the direct force control and post-stall maneuver of modern combat aircraft.
为飞机敏捷性、直接力控制和过失速机动问题提供了一种理论研究方法。
This paper discussed the application of this method in the design of flight control system for the post stall 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。
The control laws of the inner closed loop system and post stall maneuver are obtained through using symbol operations design.
使用符号运算方法设计了系统闭环控制律和大攻角下的过失速控制律。
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