Micro/nano satellites have become the protagonists in most formation flying missions currently, there is an urgent demand to find an approach to quickly calculate multiple-impulsive scheme on board for relative orbital transfer, while considering the optimality of total impulsive consumption. This paper presents an optimal control approach based on multiple impulses for in-plane satellite formation reconfiguration in near circular orbit. A new type of relative orbit motion equation is established based on the initial small deviation in the cylindrical coordinates system in this paper, which is suitable to calculate the solution of relative orbital maneuver by means of multiple impulses. The formation reconfiguration problem is investigated on account of the relative orbit motion, and the orbital motion equations with initial deviations are presented. The formation reconfiguration problem in orbital plane is discussed and analyzed selectively. An optimal three-impulsive approach for relative orbital transfer in plane is obtained by analysis solution based on graphical and numerical way, which is achieved by the combination method from four-impulsive solution. And the method is proved to be effectivity and optimality.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Research on Three-Impulsive Approach for Satellite Formation Reconfiguration in Near Circular Orbit


    Beteiligte:
    Liu, Xingchuan (Autor:in) / Chen, Danhe (Autor:in) / Wu, Kunxu (Autor:in) / Liao, Wenhe (Autor:in) / Zhang, Xiang (Autor:in)


    Erscheinungsdatum :

    16.07.2021


    Format / Umfang :

    3445712 byte




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




    A New Approach to Optimal Impulsive Transfer Near Circular Orbit

    Carter, Thomas E. / Humi, Mayer | AIAA | 2014


    Reconfiguration of Small-Satellite General Circular Orbit Formations (AIAA 2018-2219)

    LaRue, Robert / Johnson, Kirk | British Library Conference Proceedings | 2018


    A New Approach to Optimal Impulsive Transfer Near Circular Orbit (AIAA 2014-4111)

    Carter, T.E. / Humi, M. / American Institute of Aeronautics and Astronautics; American Astronautical Society | British Library Conference Proceedings | 2014


    Near-circular orbit satellite electric propulsion orbit injection method

    ZHAO SHUGE / LIU QI / LI XIAOYU et al. | Europäisches Patentamt | 2023

    Freier Zugriff