高超音速
稳健性(进化)
约束(计算机辅助设计)
控制理论(社会学)
非线性系统
计算机科学
法学
工程类
控制(管理)
航空航天工程
人工智能
机械工程
政治学
生物化学
化学
物理
量子力学
基因
作者
Shuangxi Liu,Binbin Yan,Tong Zhang,X. Zhang,Jie Yan
标识
DOI:10.1016/j.ast.2022.107651
摘要
This paper studies the problem of multiple interceptors with low velocity, weak maneuverability, and limited overload constraint to cooperatively intercept hypersonic vehicles under a nonlinear interception model. First, a coverage-based cooperative guidance (CBCG) law is proposed based on three concepts, i.e., interceptor reachable area, interceptor feasible area, and hypersonic vehicle escape area. Then, the relationship among the initial location of the interceptors, the parameters of the CBCG law, and the coverage area of the interceptor for intercepting the hypersonic vehicle is analyzed. Next, an allocation algorithm is designed to assign the coverage area and the initial locations of multiple interceptors. Finally, simulations are performed for intercepting the hypersonic vehicle with different maneuverabilities and maneuvering modes, and the proposed CBCG law is compared with the proportional navigation guidance (PNG) and sliding mode control guidance (SMCG) laws. The simulation results show that the proposed CBCG law can ensure that at least one interceptor can accurately intercept the hypersonic vehicle, giving full play of the scale advantage of low-cost interceptors. And the guidance robustness can be guaranteed in the presence of measurement errors.
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