Adaptive variable structure control of flight control system

被引：0

作者：

Shi, Jun-Peng ^{[1
]}

Liu, Jian-Wei ^{[1
]}

Lan, Bi ^{[2
]}

Yang, Pu ^{[1
]}

机构：

[1] Nanjing Univ Aeronaut & Astronaut, Coll Automat Engn, Nanjing 211100, Jiangsu, Peoples R China

[2] Shanghai Aircraft Mfg Co Ltd China, Shanghai 200000, Peoples R China

来源：

2016 IEEE CHINESE GUIDANCE, NAVIGATION AND CONTROL CONFERENCE (CGNCC) | 2016年

关键词：

flight control system; fault tolerant control; sliding mode variable structure; adaptive control; SLIDING-MODE CONTROL; DESIGN;

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：

In this paper, a control method using sliding mode variable structure control combined with adaptive control is proposed. Based on Lyapunov stability theory, a sliding mode variable structure controller is designed to ensure that the closed-loop system is asymptotically stable in system faulty cases. Then, a modified control law is designed to cope with the situation that without knowing the upper bound of the perturbation. At last, The fault tolerant control is carried out on the fault of the system failure of the flight control system. Finally, simulation results demonstrate the feasibility and effectiveness of the proposed theory by using MATLAB software.

引用

页码：648 / 651

页数：4

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