Reliable Robust Sampled-Data H∞ Output Tracking Control with Application to Flight Control

被引:6
作者
Wang, Yueying [1 ]
Zhou, Pingfang [1 ]
Wang, Quanbao [1 ]
Duan, Dengping [1 ]
机构
[1] Shanghai Jiao Tong Univ, Sch Aeronaut & Astronaut, Shanghai 200240, Peoples R China
来源
INFORMATION TECHNOLOGY AND CONTROL | 2014年 / 43卷 / 02期
基金
中国国家自然科学基金;
关键词
probabilistic actuator failures; output tracking; sampled-data control; convex polytope; flight control; parameter uncertainty; NONLINEAR-SYSTEMS; DISTURBANCES; FEEDBACK; FAULTS; MOTOR; DELAY;
D O I
10.5755/j01.itc.43.2.4821
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 paper is concerned with the problem of robust H-infinity output tracking control for uncertain sampleddata systems with probabilistic actuator failures. By assuming that each actuator fault takes values randomly in a finite set, a new actuator-failure-mode is proposed. Lyapunov-Krasovskii functional combined with the input delay approach as well as the free-weighting matrix approach are employed to establish the H-infinity performance, and the controller design is cast into a convex optimization problem with linear matrix inequality (LMI) constraints. The designed reliable controller can guarantee that the output of the closed-loop sampled-data system tracks the reference signal without steady-state error. An airship model is considered in this paper and its simulation results are given.
引用
收藏
页码:175 / 182
页数:8
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