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:

    Entwicklung fluidischer Flugregelungs- und Stellsysteme fuer Hochleistungsflugzeuge


    Contributors:
    Hair, K.A. (author)

    Published in:

    SAE-Papers ; Oct ; 1-9


    Publication date :

    1987


    Size :

    9 Seiten, 9 Bilder, 8 Quellen


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English





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