A triplex digital fly by wire flight control system was developed and installed in an F-8C aircraft to provide fail operative, full authority control. Hardware and software redundancy management techniques were designed to detect and identify failures in the system. Control functions typical of those projected for future actively controlled vehicles were implemented.


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    Title :

    Ground and flight test experience with a triple redundant digital fly by wire control system


    Contributors:


    Publication date :

    1981-02-01


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English




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