Problem of finding thrust program, or control, is considered as piecewise continuous function of time, so that, with fixed fuel supply, summit altitude of rocket in vertical flight is maximized; under assumptions that optimal control exists and that upper bound of thrust is at sufficiently high magnitude, it is proved that optimal control contains at most three subarcs; analysis extends previous results of A.Miele, G.Leitmann, and others to larger class of drag functions.


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    Titel :

    Goddard problem with bounded thrust


    Weitere Titelangaben:

    AIAA J


    Beteiligte:
    Munick, H. (Autor:in)

    Erschienen in:

    AIAA Journal ; 3 , n 7


    Erscheinungsdatum :

    1965


    Format / Umfang :

    3 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Goddard problem with bounded thrust

    MUNICK, H. | AIAA | 1965


    The reverse Goddard problem.

    Bejczy, A. K. | NTRS | 1969


    The reverse Goddard problem

    BEJCZY, A. | AIAA | 1969


    Goddard problem with constrained time of flight

    TSIOTRAS, PANAGIOTIS / KELLEY, HENRY J. | AIAA | 1992