Fault-tolerant control via sliding-mode output feedback for uncertain linear systems with quantisation

被引:47
作者
Hao, Li-Ying [1 ]
Yang, Guang-Hong [1 ,2 ]
机构
[1] Northeastern Univ, Coll Informat Sci & Engn, Shenyang, Peoples R China
[2] Northeastern Univ, State Key Lab Synthet Automat Proc Ind, Shenyang, Peoples R China
关键词
actuators; asymptotic stability; closed loop systems; compensation; control system synthesis; fault tolerance; feedback; linear systems; matrix decomposition; uncertain systems; variable structure systems; vectors; sliding-mode output feedback; uncertain linear system; robust fault-tolerant control problem; compensator state signal; matrix full-rank factorisation technique; flexible design parameter; linear sliding surface; nonlinear discontinuous vector gain; sliding-mode controller design; static adjustment law; quantisation parameter; sliding-mode fault-tolerant strategy; closed-loop system; quantisation error; actuator fault; B747-100; 200 aircraft model; CONTROL DESIGN; STABILIZATION; ROBUST;
D O I
10.1049/iet-cta.2013.0380
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
This study studies the robust fault-tolerant control problem for uncertain linear systems via sliding-mode output feedback. It is assumed that measured output and compensator state signals are quantised before transmission. By employing the matrix full-rank factorisation technique with a flexible design parameter, a sufficient condition for the existence of a linear sliding surface and a compensator in the augmented space is given. Then the non-linear discontinuous vector gain of the sliding-mode controller is designed based on a static adjustment law of the quantisation parameters. It is shown that the proposed sliding-mode fault-tolerant strategy guarantees that the closed-loop system is asymptotically stable in the presence of quantisation errors and actuator faults including outage. Compared with the existing results, the derived results lead to less conservativeness and much wider scope of applicability. Finally, the effectiveness of the proposed design method is illustrated via a B747-100/200 aircraft model.
引用
收藏
页码:1992 / 2006
页数:15
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