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.
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.
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