Electromechanical system developed at Hamilton Standard Div of United Aircraft Corp, for Hiller L model helicopter; system is 2 axis SAS which accepts signals from pitch and roll rate gyros, modifies and amplifies signals, and drives 2 linear actuators which add to pilot' s stick input to position helicopter cyclic control surfaces.


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    Titel :

    Light helicopter stability augmentation system


    Weitere Titelangaben:

    Electromechanical Components Systems Design


    Beteiligte:
    Latina, M.S. (Autor:in)


    Erscheinungsdatum :

    1963


    Format / Umfang :

    6 pages


    Medientyp :

    Standard


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :



    Synthesis design method of helicopter stability and control augmentation system

    Jiang, G. / An, J. / Dai, N. | British Library Online Contents | 1997


    Helicopter Yaw Axis Augmentation Investigation

    W. E. Clark / G. P. Intano | NTIS | 1976



    Optimization of a Helicopter Stability Augmentation System for Operation in a Ship Airwake

    Lee, D. / Horn, J. F. / American Helicopter Society | British Library Conference Proceedings | 2005