结果表明利用该方法设计的飞行控制系统在跟踪参考输入信号时具有较好的自适应跟踪性能和鲁棒性能。

The result showed that the flight control system designed by this method has fine adaptive tracking performance and robustness when following the reference input signals.

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同时，在选择参考输入信号的时候，本文采用一种称为虚拟模型参考自适应的智能选取参考输入信号的方法。

And we use a wise method to select the system's reference inputs, which is called Virtual Model reference Adaptive Control.

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在更一般、更实际的执行器故障模型的基础上，根据区域极点配置理论。给出了系统输出信号渐近跟踪参考输入信号的可靠跟踪控制器存在的充分条件。

Based on a more practical and general fault model of the actuator, a sufficient condition about reliable tracking control is obtained by the region pole assignment theory.

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