Inclined geosynchronous orbits with small inclinations can enhance safeguard capability and reduce propellant consumption of high-orbit satellites. This paper focuses on the orbit plane control of inclined geosynchronous satellite. Firstly, the dynamic model of inclination vector perturbation is established. The daily average variation of inclination vector is derived and the inclination out-of-tolerance index is computed. Then, an orbit plane control strategy of inclined geosynchronous satellite is developed, combining the active control and passive drift so as to meet the orbit plane control requirement in the entire working life. The velocity increment of active control is minimized by use of particle swarm optimization (PSO) algorithm for the purpose of reducing propellant consumption. Finally, the effectiveness of the orbit plane control strategy proposed in this paper is verified by numerical simulations.


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    Title :

    Orbit Plane Control of Inclined Geosynchronous Satellite Based on Particle Swarm Optimization


    Additional title:

    Lect. Notes Electrical Eng.


    Contributors:
    Yan, Liang (editor) / Duan, Haibin (editor) / Deng, Yimin (editor) / Wang, Xinglong (author) / Wang, Ran (author) / Wang, Jiaming (author)

    Conference:

    International Conference on Guidance, Navigation and Control ; 2024 ; Changsha, China August 09, 2024 - August 11, 2024



    Publication date :

    2025-03-02


    Size :

    10 pages





    Type of media :

    Article/Chapter (Book)


    Type of material :

    Electronic Resource


    Language :

    English




    Orbit Plane Control Strategies for Inclined Geosynchronous Satellite Constellation

    Kechichian, J. A. / American Astronautical Society| American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 1996




    INCLINED GEOSYNCHRONOUS ORBIT SPACECRAFT CONSTELLATIONS

    TURNER ANDREW E | European Patent Office | 2017

    Free access

    INCLINED GEOSYNCHRONOUS ORBIT SPACECRAFT CONSTELLATIONS

    TURNER ANDREW E | European Patent Office | 2017

    Free access