Design approach for Malfunction Detection System (MDS) to be used on board manned spacecraft; design is directed toward orbiting laboratory type vehicles, in which man will be subjected to hostile environments for extended periods of time; prime purpose of MDS will be to monitor and evaluate critical signals and display out-of-tolerance conditions; mathematical model approach to monitoring-system design; feasibility of using some value less than specified tolerance as signal "test" limit; various design decisions and trade-offs involved in choosing monitoring subsystem configuration are discussed, and conclusion is that approach is feasible and could be expanded to include other capabilities.


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    Title :

    Malfunction detection system for advanced spacecraft


    Additional title:

    IEEE -- Trans Aerospace Electronic Systems


    Contributors:


    Publication date :

    1966


    Size :

    9 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :





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