Three-Dimensional Cooperative Mid-Course Guidance Law Against the Maneuvering Target

被引:8
|
作者
Wu, Zihao [1 ]
Fang, Yangwang [2 ]
Fu, Wenxing [2 ]
Wang, Zhikai [1 ]
Ma, Wenhui [3 ]
机构
[1] Northwestern Polytech Univ, Sch Astronaut, Xian 710072, Peoples R China
[2] Northwestern Polytech Univ, Unmanned Syst Res Inst, Xian 710072, Peoples R China
[3] Northwestern Polytech Univ, Sch Automat, Xian 710072, Peoples R China
来源
IEEE ACCESS | 2020年 / 8卷
基金
中国国家自然科学基金;
关键词
Cooperative mid-course guidance law; trajectory shaping guidance law; maneuvering target; IMPACT-TIME; ANGLE; MISSILES;
D O I
10.1109/ACCESS.2020.2968593
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
Because of the limitation of the long-range detection capability of airborne sensors, it is very difficult for a single interceptor to achieve accurate mid-course guidance, especially for the long and medium range interceptors, and the maneuvering or invisible targets. As one of the solutions, the strategy of multi-interceptor cooperative intercepting can overcome the shortages of single-interceptor. Unfortunately, the existing mid-course guidance laws can't meet the requirements of cooperative intercepting strategy. To solve the problem, a novel cooperative mid-course guidance law is proposed in this paper by combining the traditional trajectory shaping guidance law and the cooperative parameter. Firstly, the cooperative mid-course guidance law is designed, and consensus of cooperative parameter characteristics is proved then. Secondly, the general expression of cooperative parameter and its convergence speed is analyzed. Finally, numeral simulations demonstrate the effectiveness and advantages of the proposed cooperative mid-course guidance law.
引用
收藏
页码:18841 / 18851
页数:11
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