控制可重构飞机要求其基本飞行控制系统对舵面部分缺损故障具有强的鲁棒特性 ,在故障发生后保证飞机的稳定性 ,提供足够的时间进行故障的检测和隔离 ,为控制系统重构提供条件 .本文采用高速采样PI控制器设计输出反馈跟随系统 ,给出了控制器的设计方法 ,并分析了它对于控制舵面部分缺损故障的鲁棒特性 .仿真结果表明 ,这种控制器具有好的鲁棒特性 Controlling reconfigurable aircraft requires its basic flight control system to have strong robustness to partial defect failure on the control surface, to ensure aircraft stability after failure, to provide sufficient time for fault detection and isolation, to reconstruct the control system The paper presents the design method of the controller and analyzes its robustness to the control of partial defect of the control surface.The simulation results show that this controller has the following features Good robustness