Abstract The large elliptical orbit is a large-eccentricity orbit with the apogee altitude several times higher than the earth’s radius. Because of its orbital characteristics, the satellite has a slow operating velocity and long duration on the side of the apogee. With wide coverage area, it can complete various space and earth observation missions.


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    Titel :

    Orbit Design of Spacecraft on Elliptical Orbit


    Beteiligte:
    Liu, Fucheng (Autor:in) / Lu, Shan (Autor:in) / Sun, Yue (Autor:in)


    Erscheinungsdatum :

    15.08.2018


    Format / Umfang :

    45 pages





    Medientyp :

    Aufsatz/Kapitel (Buch)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




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