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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    Title :

    Preliminary Design of Low-Thrust Interplanetary Missions


    Contributors:
    Flanagan, S. (author) / Sims, J. (author)

    Publication date :

    1999-08-16


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English




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