次要结构由机翼前缘，后缘和翼尖构成，主要用来减小空气阻力，支撑蒙皮，协助飞行操纵面和操纵机构。
The secondary structures, which support aerodynamic fairings or skins, flight control surfaces and control mechanisms, consist of the leading edge, trailing edge, and wingtip.
从飞行性能最优的角度，对多操纵面飞机的配平原则与算法进行了研究。
On the aspect of getting the optimal flight performance, this paper discusses the trimming principle and solution for the aircraft with multiple control effectors.
研究了当飞机常规操纵舵面失效时，通过调节飞机发动机推力大小来操纵飞机的飞行问题。
In this paper, the concept of emergency flight control system which USES the engine throttle to manipulate the aircraft in case of control surface failure is discussed.
同时考虑操纵面偏转角度饱和及偏转速率饱和对系统的影响，设计出一种变结构可重构飞行控制系统。
The limitations on surface's deflection and deflection rate are addressed to develop the variable structure reconfigurable flight control system.
同时考虑操纵面偏转角度饱和及偏转速率饱和对系统的影响，设计出一种变结构可重构飞行控制系统。
The limitations on surface's deflection and deflection rate are addressed to develop the variable structure reconfigurable flight control system.
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