The integrated application of reliability, failure effects and system simulator methods in establishing the airworthiness of a flight critical digital flight control system (DFCS) is demonstrated. The emphasis was on the mutual reinforcement of the methods in demonstrating the system safety.


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    Title :

    Integrated assurance assessment of a reconfigurable digital flight control system


    Contributors:
    Ness, W. G. (author) / Davis, R. M. (author) / Benson, J. W. (author) / Smith, M. K. (author) / Eldredge, D. (author)

    Publication date :

    1983-04-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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