On the aspect of getting the optimal flight performance, this paper discusses the trimming principle and solution for the aircraft with multiplecontrol effectors.
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。
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Conventional linear flight control systems do not satisfy nonlinear control requirement of aircraft with thrust vector, which is a multiplecontrol redundances and nonlinear MIMO system.