Simultaneous attack of a stationary target using multiple missiles: a consensus-based approach

• 作 者: Jialing ZHOU Jianying YANG Zhongkui LI
• 机 构: State Key Laboratory for Turbulence and Complex Systems, Department of Mechanics and Engineering Sci
• 出 处: Science China(Information Sciences)
• 发表日期: 2017年07期
• 关键词: consensus stationary navigation missile simultaneous undirected guidance coopera

This paper considers the simultaneous attack problem of multiple missiles against a stationary target. Built upon the classic proportional navigation structure, we propose a consensus-based approach to design the cooperative guidance law. Specifically, we present time-varying navigation ratios for the missiles,which exchange the time-to-go estimates between neighboring missiles via a communication network. For the cases where the communication topology is undirected or in the leader–follower structure with a missile acting as the leader whose navigation ratio cannot be tuned, we show that the proposed cooperative guidance law can solve the simultaneous attack problem. The effectiveness of the theoretical results is finally illustrated by numerical simulations.

This paper considers the simultaneous attack problem of multiple missiles against a stationary target. We propose a consensus-based approach to design the comaging guidance law. Specifically, we present time-varying navigation ratios for the missiles, which exchange the time-to-go estimates between neighboring missiles via a communication network. For the cases where the communication topology is undirected or in the leader-follower structure with a missile act as the leader whose navigation ratio can not be tuned, we show that the proposed cooperative guidance law can solve the simultaneous attack problem. The effectiveness of the theoretical results is finally illustrated by numerical simulations.