This example evaluates the catastrophic failure case of total loss of the pitch axis of a fly‐by‐wire flight control system. It is a much simplified analysis, but serves to illustrate the principles and differences between the dependency diagram approach and the fault tree approach.


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    Title :

    Safety Analysis – Flight Control System


    Contributors:

    Published in:

    Publication date :

    2013-08-27


    Size :

    6 pages




    Type of media :

    Article/Chapter (Book)


    Type of material :

    Electronic Resource


    Language :

    English




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