计算机科学
视线
控制理论(社会学)
邻里(数学)
人工智能
数学
航空航天工程
控制(管理)
工程类
数学分析
作者
Zhaohui Liu,Yuezu Lv,Jialing Zhou,Liang Hu
标识
DOI:10.1177/1729881419894808
摘要
This article investigates the simultaneous attack problem of multiple missiles against a manoeuvring target with delayed information transmission in three-dimensional space. Based on the kinetic model of the missiles, the problem is divided into three demands: the velocity components normal to line-of-sight converge to zero in finite time, the component of motion states along line-of-sight should achieve consensus and converge to zero. The guidance law is designed for each demand and by theoretical proof, the upper bound of delay which can tolerate is presented and the consensus error of the relative distances can converge to a small neighbourhood of zero. And simulation example presented also demonstrates the validity of the theoretical result.
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