Abstract This paper deals with the problems on the spacecraft motion in the Earth’s atmosphere taking into account the Earth’s atmospheric drag as well as on the extra-atmospheric part of the trajectory, where resistance is absent. An analytical solution of these problems by the method of fast expansions is proposed.


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    Titel :

    Application of the fast expansion method for spacecraft trajectory calculation


    Beteiligte:

    Erschienen in:

    Erscheinungsdatum :

    2015-04-01


    Format / Umfang :

    7 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




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