现代防御技术2024,Vol.52Issue(2) :104-114.DOI:10.3969/j.issn.1009-086x.2024.02.012

有向切换拓扑条件下针对机动目标的分布式协同制导方法

Distributed Cooperative Guidance Method for Maneuvering Targets Under Directed Switching Topologies

董晓飞 郝明瑞 任章
现代防御技术2024,Vol.52Issue(2) :104-114.DOI:10.3969/j.issn.1009-086x.2024.02.012

有向切换拓扑条件下针对机动目标的分布式协同制导方法

Distributed Cooperative Guidance Method for Maneuvering Targets Under Directed Switching Topologies

董晓飞 1郝明瑞 2任章3
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作者信息

  • 1. 北京机电工程研究所,北京 100074;复杂系统控制与智能协同全国重点实验室,北京 100074;北京航空航天大学 自动化科学与电气工程学院,北京 100083
  • 2. 北京机电工程研究所,北京 100074;复杂系统控制与智能协同全国重点实验室,北京 100074
  • 3. 北京航空航天大学 自动化科学与电气工程学院,北京 100083
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摘要

针对多飞行器对机动目标的协同制导问题,在视线坐标系下建立飞行器-目标相对运动模型,在此基础上将协同制导问题分为视线角协同以及命中时间协同2个子问题.基于扩张状态观测器分别在视线方向以及视线法向设计了分布式协同制导律.通过一致性分析证明了所设计的制导律在有向切换拓扑条件下的收敛性,并通过数值仿真的方式进一步验证了制导律的有效性.

Abstract

To address the cooperative guidance problem for multi-aircraft attacking maneuvering targets,this paper initially builds a relative model in the line-of-sight frame.Subsequently,the paper decomposes the cooperative guidance issue into two sub-issues:line-of-sight angle cooperation and impact time cooperation.Distributed cooperative guidance laws are developed based on extended state observers,strategically designed in both the line-of-sight and its normal direction.Consensus analysis is conducted to demonstrate the convergence of the proposed guidance laws under directed switching topologies.Numerical simulations are then employed to further substantiate the effectiveness of the guidance laws.

关键词

机动目标/分布式协同制导/扩张状态观测器/一致性/多飞行器

Key words

maneuvering target/distributed cooperative guidance/extended state observer/consensus/multi-aircraft

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出版年

2024
现代防御技术
北京电子工程总体研究所

现代防御技术

CSTPCD北大核心
影响因子:0.357
ISSN:1009-086X
参考文献量23
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