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在飞控系统发生故障时，利用可重构飞控系统实现故障重构。本文将低、高增益反馈控制方法和分段线性控制技术相结合，提出一种新的可重构飞控系统鲁棒控制结构，通过对反馈控制律设计，同时考虑操纵面偏转速率饱和限制，从而设计出一种鲁棒重构控制系统。计算结果表明：该方法能有效地完成飞控系统故障重构。
In flight control system failure, the use of reconfigurable flight control system fault reconstruction. In this paper, the low and high gain feedback control method and the piecewise linear control technology are combined to propose a new robust control structure of reconfigurable flight control system. By designing the feedback control law and taking into account the saturation limit of the deflection rate of the control surface, Thus a robust reconfigurable control system is designed. The calculation results show that this method can effectively accomplish the fault reconfiguration of flight control system.