Analysis of boost trajectory optimizations illustrates advantages of indirect methods of calculus of variations; method for boost vehicle evaluations during design studies includes provisions to account for effects of planetary rotation, aerodynamic forces, variable atmosphere and time variant thrust; techniques employed on digital computer and numerical examples illustrating character of extremals for satellite launchings and minimal sensitivity of extremals to guidance and control errors.


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    Titel :

    Rocket boost vehicle mission optimizations


    Weitere Titelangaben:

    ARS J


    Beteiligte:
    Stancil, R.T. (Autor:in) / Kulakowski, L.J. (Autor:in)

    Erschienen in:

    ARS Journal ; 31 , n 7


    Erscheinungsdatum :

    1961


    Format / Umfang :

    9 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


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