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Delta-V-Based Cooperative Strategies for Orbital Two-Pursuer One-Evader Pursuit–Evasion GamesOA

中文摘要

This paper investigates the application of the Nash equilibrium solution method within 2-versus-1 impulsive orbital pursuit–evasion(P-E)scenarios,involving 2 pursuers and an evader.Through the integration of game theory and coordinated strategies between the pursuers,the initial 2-pursuer 1-evader game((P_(1),P_(2))-E)is transformed into a composite 1-pursuer 1-evader game(P_(2)-(P_(1)-E)).To address the core challenge of the P-E game,we utilize the MinMax bilateral optimization algorithm to determine optimal strategies in each game iteration,ensuring fairness and equal opportunities for all involved parties.Within the composite P-E framework,the second pursuer(P_(2))assumes responsibility for executing a coordinated pursuit strategy,including the evaluation and tracking of the anticipated outcome of P_(1)−E.Subsequently,the evader formulates an optimal counterplay by reverse engineering the potential role assignments and strategies of the pursuers.In order to explore the intricate aspects of these scenarios,our study harnesses Monte Carlo statistical methods,offering insights into critical factors such as initial positions,impulse intervals,and magnitudes of delta-V within orbital settings,all of which substantially influence game outcomes.Ultimately,this research not only advances our understanding of multiagent orbital P-E dynamics but also establishes a foundation for more informed and effective strategic planning in practical space missions.It aims to ensure mission success and responsible resource allocation in the domain of space exploration.

Sihan Xu;Liran Zhao;Weichen Zhang;Zhaohui Dang

School of Astronautics,Northwestern Polytechnical University,Xi’an 710072,ChinaSchool of Astronautics,Northwestern Polytechnical University,Xi’an 710072,ChinaSchool of Electrical and Computer Engineering,National University of Singapore,117583 SingaporeSchool of Astronautics,Northwestern Polytechnical University,Xi’an 710072,China National Key Laboratory of Aerospace Flight Dynamics,Northwestern Polytechnical University,Xi’an 710072,China

航空航天

delta vminmax bilateral optimization algorithmorbital pursuit evasion p e scenariosinvolvingnash equilibrium solution methodcooperative strategiesintegration game theorycoordinated strategiesorbital pursuit evasion

《Space(Science & Technology)》 2025 (1)

P.563-581,19

supported by the National Key R&D Program of China:Gravitational Wave Detection Project(Nos.2021YFC22026,2021YFC2202601,2021YFC2202603)the National Natural Science Foundation of China(No.12172288).

10.34133/space.0222

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