Fixed-Time Zero-Sum Pursuit–Evasion Game Control of Multisatellite via Adaptive Dynamic Programming. Zhang, Z., Zhang, K., Xie, X., & Sun, J. IEEE Transactions on Aerospace and Electronic Systems, 60(2):2224–2235, April, 2024. ![Fixed-Time Zero-Sum Pursuit–Evasion Game Control of Multisatellite via Adaptive Dynamic Programming [link]](https://bibbase.org/img/filetypes/link.svg "link")
Paper doi abstract bibtex This paper contributes to the design of an evader controller for the pursuit–evasion problem, where both agents are described by single integrator dynamics. The proposed evader controller only requires a slight knowledge of the pursuer control law and state. The control law guarantees the evasion of the pursuer under a proper design of the evader controller parameters. Moreover, the synthesis of the evader controller is constructive and simple–to–tune since it is in terms of a linear matrix inequality. The stability analysis of the tracking error dynamics is based on a Lyapunov–like function approach. The effectiveness of the proposed evader control design is illustrated through some simulation results.
@article{zhang_fixed-time_2024,
title = {Fixed-{Time} {Zero}-{Sum} {Pursuit}–{Evasion} {Game} {Control} of {Multisatellite} via {Adaptive} {Dynamic} {Programming}},
volume = {60},
copyright = {https://ieeexplore.ieee.org/Xplorehelp/downloads/license-information/IEEE.html},
issn = {0018-9251, 1557-9603, 2371-9877},
url = {https://ieeexplore.ieee.org/document/10384730/},
doi = {10.1109/TAES.2024.3351810},
abstract = {This paper contributes to the design of an evader controller for the pursuit–evasion problem, where both agents are described by single integrator dynamics. The proposed evader controller only requires a slight knowledge of the pursuer control law and state. The control law guarantees the evasion of the pursuer under a proper design of the evader controller parameters. Moreover, the synthesis of the evader controller is constructive and simple–to–tune since it is in terms of a linear matrix inequality. The stability analysis of the tracking error dynamics is based on a Lyapunov–like function approach. The effectiveness of the proposed evader control design is illustrated through some simulation results.},
language = {en},
number = {2},
urldate = {2024-12-18},
journal = {IEEE Transactions on Aerospace and Electronic Systems},
author = {Zhang, Zhixuan and Zhang, Kun and Xie, Xiangpeng and Sun, Jiayue},
month = apr,
year = {2024},
pages = {2224--2235},
}
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