Model reference sliding mode controller design for reconfigurable flight control

被引：0

作者：

Yang Zhijun ^{[1
]}

Qi Xiaohui ^{[1
]}

Shan Ganlin ^{[1
]}

He Wei ^{[1
]}

机构：

[1] Mech Engn Coll, Dept Opt & Elect Engn, Shijiazhuang 050003, Peoples R China

来源：

ISTM/2007: 7TH INTERNATIONAL SYMPOSIUM ON TEST AND MEASUREMENT, VOLS 1-7, CONFERENCE PROCEEDINGS | 2007年

关键词：

reconfigurable flight control; model reference; sliding mode control;

D O I：

暂无

中图分类号：

TP [自动化技术、计算机技术];

学科分类号：

0812 ;

摘要：

Based on the model reference control, a sliding mode controller is proposed for the reconfigurable flight control system in this paper: Using this controller, the controlled plant can track the reference model precisely. It is shown that this method provides better performance for the flight control system. Firstly, a Proportional-Integral type sliding surface is designed through LinearQuadratic Regulator method to make the sliding mode have good dynamic characteristics and to eliminate the steady state error: Secondly, the simple saturating control is adopted to avoid the chattering phenomena. The simulation results show that the flight control system with this controller not only doesn't require the procedure of fault detection and isolation, but also achieves the model tracking control.

引用

页码：5417 / 5420

页数：4