Reconfigurable fault-tolerant control using GIMC structure

被引:43
作者
Campos-Delgado, DU [1 ]
Zhou, KM
机构
[1] Zona Univ, Fac Ciencias, UASLP, San Luis Potosi 78290, Mexico
[2] Louisiana State Univ, Dept Elect & Comp Engn, Baton Rouge, LA 70803 USA
基金
美国国家航空航天局;
关键词
H-infinity control; fault-tolerant control; gyroscope; robust control;
D O I
10.1109/TAC.2003.811263
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
In this note, a fault-tolerant control strategy is proposed from a robust control perspective by applying the recently introduced generalized internal mode control architecture. This fault-tolerant control design consists of two parts: a nominal performance controller and a robustness controller, and works in such way that when a sensor failure is detected, the controller. structure is reconfigured by adding a robustness loop to compensate the fault. This note shows how to design such controllers for a single-input two-output gyroscope system so that the performance with the nominal controller may be maintained in the case of sensor failure and/or model uncertainties.
引用
收藏
页码:832 / 838
页数:7
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