Cooperative Guidance Law Design for Salvo Attacks with Impact Angle Constraint

被引:0
|
作者
Wang, Xianghua [1 ]
Yang, Qiwei [1 ]
机构
[1] Shandong Univ Sci & Technol, Coll Elect Engn & Automat, Qingdao 266590, Peoples R China
基金
中国博士后科学基金;
关键词
SLIDING-MODE CONTROL; TIME-CONTROL; CONSENSUS;
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 novel cooperative guidance law is proposed to make multiple missiles hit simultaneously the same target at a pre-specified impact angle. Firstly:, the normal acceleration which changes the velocity direction is designed such that all missiles will fly along the desired line of sight (LOS) after a given time which ensures the hit-to-kill interception; then the consensus variable is constructed using available information and can reach consensus under the proposed the tangential acceleration command which determines the velocity magnitude. Hence simultaneous hit-to-kill attack is achieved. Finally, some simulation studies are performed to verify the effectiveness of the proposed scheme.
引用
收藏
页码:3241 / 3246
页数:6
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