Access

    Access via TIB

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    An Optimal Actuator Placement Methodology for Active Control of Helicopter Airframe Vibrations




    Publication date :

    2001



    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English



    Classification :

    BKL:    55.50 Luftfahrzeugtechnik
    Local classification TIB:    770/7040



    An optimal actuator placement methodology for active control of helicopter airframe vibrations

    Heverly, D.E. II / Wang, K.W. / Smith, E.C. | Tema Archive | 2001


    OPTIMAL ACTUATOR PLACEMENT AND ACTIVE STRUCTURE DESIGN FOR CONTROL OF HELICOPTER AIRFRAME VIBRATIONS

    Heverly, D. E. / Wang, K. / Smith, E. et al. | British Library Conference Proceedings | 2002


    A distributed actuator approach for active control of helicopter airframe vibrations

    Heverly, II, David / Smith, Edward / Wang, K. | AIAA | 1999


    A Distributed Actuator Approach for Active Control of Helicopter Airframe Vibrations

    Heverly, D. / Smith, E. / Wang, K. | British Library Conference Proceedings | 1999


    Helicopter airframe

    FINK AXEL / STEINDL CHRISTOPH | European Patent Office | 2018

    Free access