Method whereby bending models of flexible boosters can be stabilized while still retaining adequate stability and response in attitude control mode, involves addition to system of auxiliary feedback loops which function from measured bending mode data; methods for measuring data indicated; advantages of scheme are that it can be applied to systems where filtering methods are useless, and that it is relatively free of complexities inherent in other systems.


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    Titel :

    Control scheme for attitude control of large flexible boosters


    Weitere Titelangaben:

    SAE -- Paper


    Beteiligte:
    Kopp, R.E. (Autor:in) / White, R.J. (Autor:in)

    Kongress:

    SAE Meeting ; 1961 Boosters



    Erscheinungsdatum :

    1961


    Format / Umfang :

    7 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    A Control Scheme for Attitude Control of Large Flexible Boosters

    Kopp, Richard E. / White, Richard J. | SAE Technical Papers | 1961





    Minimax control of large launch boosters

    Graham, K. D. | NTRS | 1966