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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

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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.
Distributed Cooperative Guidance Method for Maneuvering Targets Under Directed Switching Topologies
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.

maneuvering targetdistributed cooperative guidanceextended state observerconsensusmulti-aircraft

董晓飞、郝明瑞、任章

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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

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

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
年,卷(期):2024.52(2)
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