Abstract
In view of the increasingly space environment's threat to the safety of satellites on orbit, this paper carries out the research on satellite trajectory planning method for avoiding space debris (non-confrontation) on the basis of the satellite's mission requirements and dynamic characteristics. In order to make the satellites have the ability to avoid space debris and return to the predetermined orbit, this paper proposes a space debris avoidance framework based on the combination of improved Lyapunov Guidance Vector Field (LGVF) and Interfered Fluid Dynamic System (IFDS) algorithm. Further, the receding-horizon optimization (RHO) and particle swarm optimization (PSO) strategy are adopted to optimize the parameters of IFDS algorithm, which realize that the satellite returns to the predetermined orbit as soon as possible after avoiding space debris with a small offset under low fuel consumption. Finally, the feasibility and effectiveness of the proposed method are verified by numerical simulations.
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Acknowledgement
The authors would like to express their acknowledgment for the support from the National Natural Science Foundation of China (No. U21B6001) and China Postdoctoral Science Foundation (No. 2022M713006).
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© 2023 Beijing HIWING Sci. and Tech. Info Inst
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Yang, Z., Wang, H., Liu, Y., Zhang, M., Wu, J. (2023). Satellite Trajectory Planning for Space Debris Collision Avoidance. In: Fu, W., Gu, M., Niu, Y. (eds) Proceedings of 2022 International Conference on Autonomous Unmanned Systems (ICAUS 2022). ICAUS 2022. Lecture Notes in Electrical Engineering, vol 1010. Springer, Singapore. https://doi.org/10.1007/978-981-99-0479-2_258
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DOI: https://doi.org/10.1007/978-981-99-0479-2_258
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Publisher Name: Springer, Singapore
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Online ISBN: 978-981-99-0479-2
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