同时飞机平飞时比水平盘旋和俯冲拉起时的非线性强烈，这说明飞机机动飞行时产生的附加力对转子系统的非线性有明显的抑制作用。

The plane at the same time pulled strongly nonlinear than the hover and diver-hike. This shows that the response of the nonlinear rotor system has significantly inhibited by maneuver load.

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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。

This paper discussed the application of this method in the design of flight control system for the post stall maneuver.

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游标速度，在某些机动飞行过程中，特别是在进近和着陆时，飞机所应保持的预定速度。

BUG speed, a preselected speed to be observed during certain maneuvers, particularly the approach and landing sequence.

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