Electromechanical actuation of primary flight control surfaces has been demonstrated by the development of an integrated rotary hingeline dual-redundant actuation unit. Improved system bandwidth was demonstrated after employing improved sensors and electronic controls. (Author)


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Electromechanical Actuation Development Program (EADP). Power Control Development


    Contributors:
    S. Rowe (author) / D. Bailey (author) / R. Belanus (author)

    Publication date :

    1981


    Size :

    146 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




    Electromechanical Actuation Development

    R. A. Lewis / J. Gray / N. E. Wood | NTIS | 1980


    Electromechanical flight control actuation

    Bird, D.K. | Tema Archive | 1977


    Electromechanical Flight Control Actuation

    Bird, Daniel K. | SAE Technical Papers | 1977


    The Development of Electromechanical Actuation for Aircraft Systems

    White, J.A.P. | Emerald Group Publishing | 1987


    Electromechanical Flight Control Actuation Update

    BIRD, DANIEL K. | SAE Technical Papers | 1978