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)


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    Titel :

    Electromechanical Actuation Development Program (EADP). Power Control Development


    Beteiligte:
    S. Rowe (Autor:in) / D. Bailey (Autor:in) / R. Belanus (Autor:in)

    Erscheinungsdatum :

    1981


    Format / Umfang :

    146 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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