航空兵器2024，Vol.31Issue(1)：38-44,7.DOI:10.12132/ISSN.1673-5048.2023.0099
考虑通信拓扑切换的多导弹协同制导研究
Cooperative Multi-Missile Guidance Research Considering Communication Topology Switching
摘要
Abstract
A time-space cooperative guidance law based on switching strategy is proposed for the multi-missile co-operative strike problem under switching topology.The distributed guidance law is designed for the time constraint in combination with the consistency algorithm,and it is proved that the system converges in finite time based on Lyapunov theory and can achieve simultaneous strikes.For spatial constraints,the ballistic shaping guidance law is used to make each missile converge to the desired line of sight angle.The switching strategy is designed so that missiles can achieve both temporal and angular coordinated attacks.The simulation analysis verifies that the designed guidance law can a-chieve the flanking attack and angular constraint under the switching topology condition and the loss of one missile from the group.关键词
协同制导/切换拓扑/时间约束/角度约束/制导律/速度不可控Key words
cooperative guidance/switching topology/time constraint/angular constraint/guidance law/veloci-ty uncontrollability分类
军事科技引用本文复制引用
张世强,李群生,何金刚..考虑通信拓扑切换的多导弹协同制导研究[J].航空兵器,2024,31(1):38-44,7.基金项目
航空科学基金项目(20200001081010) （20200001081010）
