约束(计算机辅助设计)
网络拓扑
组分(热力学)
导弹
奇点
趋同(经济学)
导弹制导
计算机科学
领域(数学)
弹道
视野
控制理论(社会学)
拓扑(电路)
法学
数学优化
数学
工程类
人工智能
航空航天工程
控制(管理)
计算机网络
数学分析
经济
天文
物理
组合数学
热力学
纯数学
经济增长
政治学
几何学
作者
Honglong Kang,Pengyu Wang,Shenmin Song
标识
DOI:10.1177/09544100231153265
摘要
In this paper, a generalized three-dimensional (3D) cooperative guidance law with seeker’s field-of-view (FOV) constraints is designed for multiple missiles to achieve salvo attack against a stationary target. The proposed generalized guidance law is composed of two parts: a proportional navigation guidance (PNG) component for target capture and a biased feedback component for simultaneous arrival. Two novel auxiliary functions are integrated into the biased feedback component to guarantee the satisfaction of FOV constraint. Furthermore, a time-varying lower bound that contains the impact time error is utilized to avoid the guidance command singularity. The proposed guidance law can be easily applied to various missile communication topologies, including centralized connected, distributed connected, and no-connected topologies. The convergence of impact time error, FOV constraint satisfaction, and command non-singularity of the proposed guidance law are theoretically analyzed and proved. Extensive numerical simulations with comparative studies are conducted to demonstrate the effectiveness and advantages of the proposed guidance law.
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