A dissimilar FCS based on fluidic technology, integrated with a redundant electronic FCS, promises to increase the mission reliability and survivability of high performance aircraft by providing protection from common mode and potential EMI/EMP induced failures. Current emphasis is on developing critical hydrofluidic servoactuation systems and components which will meet demanding requirements for performance, size, weight, reliability and power consumption.


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    Title :

    Development of Fluidic Flight Control and Actuation Systems for High Performance Aircraft


    Additional title:

    Sae Technical Papers


    Contributors:

    Conference:

    Aerospace Technology Conference and Exposition ; 1987



    Publication date :

    1987-10-01




    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English





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