Maximum capability of aero-space vehicle can be determined quickly and accurately using steepest-ascent optimization procedure developed at Raytheon Co; performance of specific re-entry vehicle was calculated using computer; procedure generates sequence of improved control histories, culminating in one which extremalizes prescribed terminal quantity called pay-off, while satisfying specified set of terminal and in-flight constraints; procedure yields not only vehicle's performance limits but, in addition, sequence of successively improved trajectories together with their control histories.


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    Titel :

    Optimum earth re-entry corridors


    Weitere Titelangaben:

    NASA CR


    Beteiligte:
    Muzyka, A. (Autor:in) / Blanton, H.E. (Autor:in)


    Erscheinungsdatum :

    1966


    Format / Umfang :

    98 pages


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Optimum earth re-entry corridors

    Blanton, H. E. / Muzyka, A. | NTRS | 1966


    Optimum earth re-entry corridors

    Muzyka, Ann / Blanton, H. Elmore | TIBKAT | 1966


    Optimum Earth Re-Entry Corridors

    H. E. Blanton / A. Muzyka | NTIS | 1966