Multi-satellite Capture Configuration with Continuous Thrust
Author:
Funder
National Natural Science Foundation of China
Military Science and Technology Commission
Publisher
Springer Science and Business Media LLC
Link
https://link.springer.com/content/pdf/10.1007/s42423-024-00161-3.pdf
Reference18 articles.
1. Liao T, Li S, Chen X, Zhu M (2023) Numerical solution of spacecraft pursuit-evasion-capture game based on progressive shooting method. Proc Inst Mech Eng Part G J Aerosp Eng. https://doi.org/10.1177/09544100231164269
2. Luo Y, Zhu H, Li Z (2020) Survey on spacecraft orbital pursuit-evasion differential games (in Chinese). Scientia Sinica Technologica 50(12):1533–1545. https://doi.org/10.1360/SST-2019-0174
3. Zy Li, Zhu H, Yang Z, Luo YZ (2019) A dimension-reduction solution of free-time differential games for spacecraft pursuit-evasion. Acta Astronautica 163:201–210. https://doi.org/10.1016/j.actaastro.2019.01.011
4. Liao T (2021) Research on control and solving method of pursuit-evasion game for spacecraft (in Chinese) [Master’s Thesis]. Harbin Institute of Technology, Harbin
5. Zeng X, Cai W, Yang L, Zhu Y (2018) On the orbital pursuit-evasion games with low constant thrust-to-mass ratio. In: 2018 Chinese automation congress (CAC), pp 1655–1660. https://ieeexplore.ieee.org/document/8623543/
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