The alleviation of the effects of gusts on tilt rotor aircraft by means of active control systems was investigated. The gust generator, the derivation of the equations of motion of the rotor wing combination, the correlation of these equations with the results of wind tunnel model tests, the use of the equations to design various gust alleviating active control systems, and the testing and evaluation of these control systems by means of wind tunnel model tests were developed.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    A Wind-Tunnel Investigation of Tilt-Rotor Gust Alleviation Systems


    Beteiligte:
    Ham, N. D. (Autor:in) / Whitaker, H. P. (Autor:in)

    Erscheinungsdatum :

    01.01.1978


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch






    Adaptive Gust Alleviation for a Tilt-Rotor UAV Operating in Turbulent Airwakes

    Horn, Joseph / Cooper, Jared / Schierman, John et al. | AIAA | 2008



    Adaptive Gust Alleviation for a Tilt-Rotor UAV Operating in Turbulent Airwakes

    Horn, J. / Cooper, J. / Schierman, J. et al. | British Library Conference Proceedings | 2008