Distributed Cooperative Strategy Design Against A Maneuvering Target With Acceleration

被引：0
|
作者：
Hu Zilun [1 ,2 ]
Yang Jianying [1 ,2 ]
机构：
[1] Peking Univ, Coll Engn, Dept Mech & Engn Sci, Beijing 100871, Peoples R China
[2] Natl Key Lab Sci & Technol Aerosp Intelligence Co, Beijing 100871, Peoples R China
来源：
PROCEEDINGS OF THE 35TH CHINESE CONTROL CONFERENCE 2016 | 2016年
关键词：
Aircraft control; Distributed guidance law; Consensus protocol; IMPACT TIME; GUIDANCE;
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：
This paper concerns on the simultaneous attack problem with multiple missiles against a maneuvering target with acceleration. A new distributed guidance protocol based on the local information of each missile and its neighboring missiles is proposed. The asymptotical convergence of the consensus error of the range-to-go and the range rate of each missile ensures the simultaneous attack, which was investigated through a Lyapunov analysis.
引用
收藏
页码：10619 / 10624
页数：6
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