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飞机余度舵机系统鲁棒故障诊断
引用本文:张若青,沈现军,裘丽华. 飞机余度舵机系统鲁棒故障诊断[J]. 控制理论与应用, 2001, 18(2): 205-209
作者姓名:张若青  沈现军  裘丽华
作者单位:北京航空航天大学自动控制系
基金项目:国家自然科学基金! (5 96 75 0 2 0 )资助项目
摘    要:提出一种利用特征结构配置与状态反馈解耦相结合设计观测器的方法,实现余度伺服系统的鲁棒故障诊断,利用特征结构方法,可以实现残差与结构性干扰解耦;利用对偶原理,进行解耦观测器设计,可使残差不受交联作用影响,利用这两种方法中参数设计的自由度,使其互相逼近,做到在干扰解耦的基础上,故障最大程度地实现通道解耦,该方法不仅适用于突变故障,而且也适用于渐变故障和多故障的诊断。

关 键 词:飞机 余度舵机系统 鲁棒故障诊断 状态反馈 干扰解耦
文章编号:1000-8152(2001)02-0205-05
收稿时间:1999-08-30
修稿时间:1999-08-30

Robust Fault Diagnosis for Redundant Servo System
ZHANG Ruo-qing,SHEN Xian-jun and QIU Li-hua. Robust Fault Diagnosis for Redundant Servo System[J]. Control Theory & Applications, 2001, 18(2): 205-209
Authors:ZHANG Ruo-qing  SHEN Xian-jun  QIU Li-hua
Affiliation:Department of Automatiic Control, Beijing University of Aeronautics and Astronautics, Beijing, 100083, P.R.China;Department of Automatiic Control, Beijing University of Aeronautics and Astronautics, Beijing, 100083, P.R.China;Department of Automatiic Control, Beijing University of Aeronautics and Astronautics, Beijing, 100083, P.R.China
Abstract:Present a scheme of designing observer to achieve robust fault diagnosis of redundant servo system, combining eigenstructure assignment with dual theory and state feedback. By using eigenstructure assignment, the residual is de coupled from structured disturbance; By using dual theory and state feedback, the residual is de coupled from interaction of other channels. On the basis of disturbance de coupling, utilized the design freedom of observer's parameters, the fault is isolated to the greatest extent. Finally, the simulations of two redundant servo systems show the effectiveness of the scheme.
Keywords:robust fault diagnosis  eigenstructure assignment  disturbance de couple  state feedback  fault de couple
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