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Saddle Point of Orbital Pursuit-Evasion Game Under -Perturbed Dynamics
THE orbital pursuit–evasion (PE) problem of two spacecraft is typically modeled as a two-
player zero-sum differential game [1], where one of the players is called the pursuer and the …
player zero-sum differential game [1], where one of the players is called the pursuer and the …
A dimension-reduction solution of free-time differential games for spacecraft pursuit-evasion
This paper presents a dimension-reduction method for solving the free-time pursuit-evasion
game between two spacecraft near circular orbits. Theoretically, finding the saddle-point …
game between two spacecraft near circular orbits. Theoretically, finding the saddle-point …
An escape strategy in orbital pursuit-evasion games with incomplete information
The orbital pursuit-evasion game is typically formulated as a complete-information game,
which assumes the payoff functions of the two players are common knowledge. However …
which assumes the payoff functions of the two players are common knowledge. However …
Solving pursuit/evasion game along elliptical orbit by providing precise gradient
B Pang, C Wen, H Han, D Qiao - Journal of Guidance, Control, and …, 2024 - arc.aiaa.org
DIFFERENTIAL game refers to a game of two players in a time-continuous system in an
attempt to optimize the players, independent or conflicting goals. The differential game was …
attempt to optimize the players, independent or conflicting goals. The differential game was …
Autonomous game control for spacecraft rendezvous via adaptive perception and interaction
M Wang, HN Wu - IEEE Transactions on Aerospace and …, 2022 - ieeexplore.ieee.org
This article studies the autonomous game control problem for spacecraft rendezvous by
using the adaptive perception and interaction. The rendezvous mission involves two …
using the adaptive perception and interaction. The rendezvous mission involves two …
Numerical solution for elliptical orbit pursuit-evasion game via deep neural networks and pseudospectral method
C Zhang, Y Zhu, L Yang, X Zeng… - Proceedings of the …, 2023 - journals.sagepub.com
This paper presents an efficient and stable DNNs-based Radau pseudospectral method for
the free-time elliptical orbit pursuit-evasion game based on the equivalent reconstruction of …
the free-time elliptical orbit pursuit-evasion game based on the equivalent reconstruction of …
[HTML][HTML] Application of the hp-adaptive pseudospectral method in spacecraft orbit pursuit-evasion game
Z Zhang, Y Zhang, B Wang - Advances in Space Research, 2024 - Elsevier
In this paper, a Cartesian model of the orbit pursuit-evasion game under J2 perturbations is
constructed, and a step-by-step solution method applicable to this problem, namely the Hp …
constructed, and a step-by-step solution method applicable to this problem, namely the Hp …
[HTML][HTML] Incomplete information pursuit-evasion game control for a space non-cooperative target
Z Wang, B Gong, Y Yuan, X Ding - Aerospace, 2021 - mdpi.com
Aiming to solve the optimal control problem for the pursuit-evasion game with a space non-
cooperative target under the condition of incomplete information, a new method …
cooperative target under the condition of incomplete information, a new method …
[HTML][HTML] Pursuer's control strategy for orbital pursuit-evasion-defense game with continuous low thrust propulsion
J Zhou, L Zhao, J Cheng, S Wang, Y Wang - Applied Sciences, 2019 - mdpi.com
This paper studies the orbital pursuit-evasion-defense problem with the continuous low
thrust propulsion. A control strategy for the pursuer is proposed based on the fuzzy …
thrust propulsion. A control strategy for the pursuer is proposed based on the fuzzy …
Attitude Takeover Control of Failed Spacecraft via Leader–Followers Adaptive Cooperative Game
HN Wu, M Wang - Journal of Aerospace Information Systems, 2023 - arc.aiaa.org
In this paper, the problem of microsatellites-based adaptive cooperative game attitude
takeover control for a failed spacecraft is investigated. Specifically, a manned microsatellite …
takeover control for a failed spacecraft is investigated. Specifically, a manned microsatellite …