A Tracking Differentiator Based Backstepping Control of Missile System

被引：0
|
作者：
Zhang, Wenguang [1 ]
Yang, Lili [1 ]
Lei, Junwei [1 ]
机构：
[1] Naval Aeronaut & Astronaut Univ, Dept Control, Yantai 264001, Peoples R China
来源：
PROCEEDINGS OF THE 2017 4TH INTERNATIONAL CONFERENCE ON MACHINERY, MATERIALS AND COMPUTER (MACMC 2017) | 2017年 / 150卷
关键词：
Tracking differentiator; stability; Backstepping; Missile; Control system;
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：
To avoid the complex calculation of derivative in the backstepping design procedure, a novel kind of tracking differentiator was adopt to solve the derivative of ideal angle speed of the pitch channel missile system. Also, the ideal angle speed should be bounded or the stability of the system can not be guaranteed. And a Lyapunov function was chosen to prove the stability of the whole system. At last, the detailed numerical simulation was done to show the rightness and effectiveness of the proposed method.
引用
收藏
页码：700 / 703
页数：4
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