Encircling Hostile Spacecraft Through Constellation Collaboration: A Differential Game Approach to Orbital Pursuit-Evasion

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Authors: Yuanshi Liu, Chenhui Qin, Jianbin Qiu, Wenqiang Ji
Cited by: 1
References: 31

Abstract

Recent advancements in large-scale constellation architectures provide a foundation for spacecraft clusters to effectively achieve the threat interception in the congested orbit. To address this issue, a containment-oriented collaborative interception framework for the multi-spacecraft system is designed. Firstly, a relative dynamics model capturing pursuer-evader interactions is established, anchored to the orbit threat as a reference point. An objective function incorporating a relative distance penalty term is formulated for the individual spacecraft. Subsequently, an integrated objective function is constructed and applied to all spacecraft. Secondly, the optimal interception strategies for the multi-spacecraft system are derived and simplified by identifying the sufficient conditions guaranteeing strategy uniqueness. Furthermore, the equivalence between the integrated model and the multi-agent model in terms of optimal interception strategies is rigorously proven, along with a computationally efficient solution. Finally, the effectiveness of the proposed interception strategy is validated through high-fidelity numerical simulations.

Fields of Study & Subjects

Spacecraft Dynamics and Control Guidance and Control Systems Space Satellite Systems and Control

Publication details

Journal / source
IEEE Transactions on Aerospace and Electronic Systems
Publisher
Institute of Electrical and Electronics Engineers (IEEE)
Volume
62
Pages
4118–4127
Publication date
1 January 2026