The problem of control laws, allowing the formation and maintenance of the required halo-orbit, is considered. The motion of the electric propulsion spacecraft is considered in the vicinity of the collinear libration points of the Earth-Moon system. The gravitational effects of the Earth, the Moon and the Sun are taken into account. The results are based on the simplified linearized models of the gravitational potential.


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    Titel :

    Halo-orbit formation in the Earth-Moon system by the electric propulsion spacecraft


    Beteiligte:
    Starinova, Olga (Autor:in) / Kupczov, Vyacheslav (Autor:in) / Gao, Changsheng (Autor:in) / Hu, Yudon (Autor:in) / Fain, Maksim (Autor:in) / Khabibullin, Roman (Autor:in) / Sivasundaram, Seenith (Herausgeber:in)

    Kongress:

    ICNPAA 2018 WORLD CONGRESS: 12th International Conference on Mathematical Problems in Engineering, Aerospace and Sciences ; 2018 ; Yerevan, Armenia


    Erschienen in:

    Erscheinungsdatum :

    04.12.2018


    Format / Umfang :

    8 pages





    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




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