Effects of transient electrical signals evaluated in laboratory tests. Method of evaluating nominally fault-tolerant, aircraft-type digital-computer-based control system devised. Provides for evaluation of susceptibility of system to upset and evaluation of integrity of control when system subjected to transient electrical signals like those induced by electromagnetic (EM) source, in this case lightning. Beyond aerospace applications, fault-tolerant control systems becoming more wide-spread in industry; such as in automobiles. Method supports practical, systematic tests for evaluation of designs of fault-tolerant control systems.


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    Title :

    Testing For EM Upsets In Aircraft Control Computers


    Contributors:

    Published in:

    Publication date :

    1994-02-01



    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English





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