Fixed-Time Zero-Sum Pursuit-Evasion Game Control of Multisatellite via Adaptive Dynamic Programming

被引:0
|
作者
Zhang, Zhixuan [1 ]
Zhang, Kun [2 ]
Xie, Xiangpeng [1 ]
Sun, Jiayue [3 ]
机构
[1] Nanjing Univ Posts & Telecommun, Inst Adv Technol, Nanjing 210003, Peoples R China
[2] Beihang Univ, Sch Astronaut, Beijing 100191, Peoples R China
[3] Northeastern Univ, Sch Informat Sci & Engn, Shenyang 110004, Peoples R China
基金
中国国家自然科学基金;
关键词
Satellites; Games; Game theory; Optimal control; Orbits; Aerodynamics; Mathematical models; Adaptive dynamic programming (ADP); fixed-time stability; Nash equilibrium; satellite capture; zero-sum pursuit-evasion game; SPACECRAFT;
D O I
10.1109/TAES.2024.3351810
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
Inspired by the combination of zero-sum game and fixed-time convergence, this study investigates the optimal control strategy for a multisatellite fixed-time pursuit-evasion zero-sum game. A novel fixed-time adaptive dynamic programming approach is proposed to achieve satellite pursuit within a fixed time frame. The optimal control strategy for achieving Nash equilibrium of pursuit and target satellites' states is obtained. The derivation of the capture conditions in the game involves the construction of a Lyapunov function. Furthermore, a neural network weight update law is designed to eliminate the persistent excitation condition. In addition, this article employs a single network architecture, which simplifies the computing cost and complexity of the design process. Finally, the effectiveness of the proposed method is demonstrated through two simulation examples.
引用
收藏
页码:2224 / 2235
页数:12
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