比例导航
计算机科学
导弹制导
导弹
视线
控制理论(社会学)
趋同(经济学)
Lyapunov稳定性
法学
控制(管理)
航空航天工程
工程类
人工智能
政治学
经济增长
经济
作者
Pengpeng Yan,Yonghua Fan,Ruifan Liu,Mingang Wang
标识
DOI:10.1177/1729881420929140
摘要
The target-encirclement guidance problem for many-to-one missile-target engagement scenario is studied, where the missiles evenly distribute on a target-centered circle during the homing guidance. The proposed distributed target-encirclement guidance law can achieve simultaneous attack of multiple missiles in different line-of-sight directions. Firstly, the decentralization protocols of desired line-of-sight angles are constructed based on the information of neighboring missiles. Secondly, a biased proportional navigation guidance law that can arbitrarily designate the impact angle is cited. The missiles can achieve all-aspect attack on the target in an encirclement manner by combining the biased proportional navigation guidance law and dynamic virtual targets strategy. Thirdly, the consensus protocol of simultaneous attack is designed, which can guarantee that all missiles’ time-to-go estimates achieve consensus asymptotically, and the convergence of the closed-loop system is proved strictly via the Lyapunov stability theory. Finally, numerical simulation results demonstrate the performance and feasibility of the proposed distributed target-encirclement guidance law in different engagement situations.
科研通智能强力驱动
Strongly Powered by AbleSci AI