Steepest-ascent method would be more usable if requirements for guessing desired increase in performance parameter and/or certain weighting factors were eliminated; method described eliminates guessing of these parameters; computer program is used to determine optimum trajectories for wide variety of rocket-powered vehicles in several mission options; convergence of iteration is good, and program can be used by engineers who are not familiar with calculus of variations.


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    Titel :

    New approach to steepest-ascent trajectory optimization


    Weitere Titelangaben:

    AIAA J


    Beteiligte:
    Stancil, R.T. (Autor:in)

    Erschienen in:

    AIAA Journal ; 2 , n 8


    Erscheinungsdatum :

    1964


    Format / Umfang :

    6 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :





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