Cooperative Differential Games Guidance Laws with Multiple Constraints for Intercepting Maneuvering and Varying-speed Targets

被引:0
作者
Gao, Qunchang [1 ]
Yuan, Yuan [1 ]
Yuan, Huanhuan [1 ]
Wang, Mengbi [2 ]
机构
[1] School of Astronautics, Northwestern Polytechnical University, Xi’an
[2] Department of Precision Instrument, Tsinghua University, Beijing
来源
Yuhang Xuebao/Journal of Astronautics | 2024年 / 45卷 / 12期
关键词
Cooperative guidance; Differential games; Extended state observer; Intercept angle constraints; Varying speed target; ϵ-Nash equilibrium;
D O I
10.3873/j.issn.1000-1328.2024.12.008
中图分类号
学科分类号
摘要
A novel cooperative differential game guidance law is proposed to address the problem of effective coordinated attack on maneuvering and varying speed targets in the terminal guidance. Firstly,a guidance model for intercepting maneuvering and varying speed targets is established. Utilizing the theory of differential games,energy consumption constraints,the intercept angle constraints and miss distance are considered as performance index. Based on optimal control methods,a cooperative game guidance law with arbitrary-order linear dynamics is derived. Considering the possible external disturbance of the missile,a time-varying gain extended state observer is designed to estimate disturbances,compensating for them in the game strategy to achieve ϵ-Nash equilibrium in multi-missile games,with the upper bound of ϵ is calculated. Furthermore,to validate the effectiveness of the proposed guidance law,an analytical cooperative guidance law for a two-to-one scenario with ideal dynamics and constant axial acceleration is provided,and the effectiveness is validated by numerical simulations. © 2024 Chinese Society of Astronautics. All rights reserved.
引用
收藏
页码:1944 / 1958
页数:14
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