Time-varying Terminal Sliding Mode Based on Salvo Attack Cooperative Guidance Law for Unknown Uncertainty Upper Bounds

被引:0
作者
Wei Xiaoqian [1 ,2 ]
Yang Jianying [1 ,2 ]
机构
[1] Peking Univ, Dept Mech & Engn Sci, Coll Engn, State Key Lab Turbulence & Complex Syst, Beijing 100871, Peoples R China
[2] Natl Key Lab Sci & Technol Aerosp Intelligence Co, Beijing 100854, Peoples R China
来源
PROCEEDINGS OF THE 35TH CHINESE CONTROL CONFERENCE 2016 | 2016年
关键词
Terminal Sliding Mode; Salvo Attack; Unknown Uncertainty Upper Bounds;
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 new time-varying terminal sliding mode with unknown uncertainty bounds is designed to make multiple missiles-attack against the maneuvering target simultaneously. The new method in this paper can guarantee accurate time-to-go by distributed cooperation. Then, a new cooperative guidance law is designed for the nonlinear system based on the known uncertainty bound. Furthermore, it is extended to unknown uncertainty bound using the disturbance observer and the composite cooperative guidance law. The desired salvo attack time is achieved by selecting the parameter variables of sliding model and the adjacency matrix in the end. Numerical simulations with the comparisons demonstrate the effectiveness and the superiority of the proposed method.
引用
收藏
页码:5398 / 5403
页数:6
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