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。

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So maneuver reentry trajectory design problem was transferred into the more complex optimum control problem with terminal constraints and inner state constraints.

这就增加了内点约束，从而使机动再入弹道设计问题成为具有内点约束和终端约束更复杂的最优控制问题。

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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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As an engineer and explorer, one of his first challenges was to design and build cost-effective submarines that were lighter and easier to maneuver.

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