A direct optimization method intended to be used primarily for preliminary design of low-thrust interplanetary trajectories, including those with multiple gravity assists, is presented.


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    Titel :

    Preliminary Design of Low-Thrust Interplanetary Missions


    Beteiligte:
    Flanagan, S. (Autor:in) / Sims, J. (Autor:in)

    Erscheinungsdatum :

    16.08.1999


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch




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