The secondary structures, which support aerodynamic fairings or skins, flight control surfaces and control mechanisms, consist of the leading edge, trailing edge, and wingtip.
2
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.
3
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.