The architecture, requirements, and system elements of an ultrareliable, advanced flight control system are described. The basic criteria are functional reliability of 10 to the minus 10 power/hour of flight and only 6 month scheduled maintenance. A distributed system architecture is described, including a multiplexed communication system, reliable bus controller, the use of skewed sensor arrays, and actuator interfaces. Test bed and flight evaluation program are proposed.


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    Title :

    Advanced Flight Control System Study


    Contributors:
    J. C. Mcgough (author) / K. Moses (author) / J. F. Klafin (author)

    Publication date :

    1982


    Size :

    374 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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