Accurate solutions of minimal time Earth-Mars and Earth-Venus heliocentric trajectories are calculated with a shooting-Newton method. The flight times are less and the steering histories are diferent than those presented in [1], thus contradicting the optimality claims in [1].


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    Titel :

    Computation of Optimal Earth-Mars and Earth-Venus Trajectories


    Beteiligte:

    Erschienen in:

    Erscheinungsdatum :

    1977-09-01


    Format / Umfang :

    373223 byte




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



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