Integrated Design of Missile Guidance and Control: Active Disturbance Rejection Control Method

被引：0
|
作者：
Ran, Maopeng [1 ]
Chen, Yifen [2 ]
Wang, Qing [1 ]
Dong, Chaoyang [3 ]
Ma, Aojia [3 ]
机构：
[1] Beihang Univ, Sch Automat Sci & Elect Engn, Beijing 100191, Peoples R China
[2] Shanghai Acad Spaceflight Technol, Inst 8, Shanghai 201109, Peoples R China
[3] Beihang Univ, Sch Aeronaut Sci & Engn, Beijing 100191, Peoples R China
来源：
2014 IEEE CHINESE GUIDANCE, NAVIGATION AND CONTROL CONFERENCE (CGNCC) | 2014年
关键词：
D O I：
暂无
中图分类号：
TM [电工技术]; TN [电子技术、通信技术];
学科分类号：
0808 ; 0809 ;
摘要：
In this paper, we present an active disturbance rejection control (ADRC) based integrated guidance and control (IGC) law. The IGC law is designed using the backstepping technique, and the particle swarm optimization (PSO) algorithm is utilized to find the optimal selection of the controller parameters. Simulation results show that, with the application of the proposed IGC law, small miss distance can be achieved, and the system is robust against target maneuver and system uncertainties.
引用
收藏
页码：115 / 119
页数：5
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