System studied can control aircraft over very large ranges of flight conditions without resort to air data measurements; methods for predicting frequency, amplitude, and effect on performance of inherent limit cycle or "chatter".


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    Titel :

    On design of high-gain saturating control system for use as adaptive autopilot


    Weitere Titelangaben:

    NASA -- Tech Note


    Beteiligte:
    McLean, J.D. (Autor:in) / Schmidt, S.F. (Autor:in)


    Erscheinungsdatum :

    1960


    Format / Umfang :

    48 pages


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :



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