Advanced flight control actuation systems require that the actuator be capable of interfacing with centralised digital computing systems.The actuation specialist must consider the electro hydraulic system as a whole, including the closed loop servo electronics, from the command distribution databus to the final output member.This paper discusses the overall approach of a primary flight control specialist company, with the lateral implications of direct drive and multi redundant valve configurations, higher system pressures and direct rotary actuation.


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    Title :

    Advanced Flight Control Actuation Systems and Their Interface with Digital Commands


    Additional title:

    Sae Technical Papers


    Contributors:
    Mattos, F. (author) / Anthony, M. J. (author)

    Conference:

    A-6 Symposium Program Advanced Actuation, Controls, and Integration for Aerospace Vehicles ; 1985



    Publication date :

    1985-10-01




    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




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