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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    Title :

    Satellite Trajectory Planning for Space Debris Collision Avoidance


    Additional title:

    Lect. Notes Electrical Eng.


    Contributors:
    Fu, Wenxing (editor) / Gu, Mancang (editor) / Niu, Yifeng (editor) / Yang, Zhiyuan (author) / Wang, Honglun (author) / Liu, Yiheng (author) / Zhang, Menghua (author) / Wu, JianFa (author)

    Conference:

    International Conference on Autonomous Unmanned Systems ; 2022 ; Xi'an, China September 23, 2022 - September 25, 2022



    Publication date :

    2023-03-10


    Size :

    10 pages





    Type of media :

    Article/Chapter (Book)


    Type of material :

    Electronic Resource


    Language :

    English




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