A new approach to the organization of a reliable aerospace computer system is described in this paper. The organization is based on the use of a multithreading design in which a multiplicity of paths are available, any of which can perform the minimum data processing functions. The combination of all of the multithreading paths comprises a total data processing system which is capable of handling more than the minimum task for which the highest reliability is required. This approach utilizes active redundancy to provide a higher capability for more extensive data processing tasks during that period in which no failures have occurred. Optimum utilization of system weight is achieved through use of a minimum of inactive redundant hardware.


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    Title :

    Multithreading Design of a Reliable Aerospace Computer


    Contributors:


    Publication date :

    1966-11-01


    Size :

    1746160 byte




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English



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