Data bus systems as defined in MIL-STD-1553B are widely used in aerospace instrumentation systems for digital data transmissions between units on the bus. Although the bus is protected against a short circuit which may occur in the remote unit electronics or transformer, it has no protection against a cable termination failure. Open or short failure along main bus cable results in failure of the entire bus system. A data bus interface technique is described which is insensitive to cable termination failure. The key to this technique is a directional coupling transformer which is only slightly more complicated than standard interface transformers. Design equations for the directional coupling transformer and experimental results of new data bus systems are presented.


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    Title :

    New data bus interface technique


    Additional title:

    Neue Datenbus-Interface-Technik


    Contributors:
    Lee, K.H. (author) / Maschhoff, R.H. (author)

    Published in:

    Publication date :

    1985


    Size :

    6 Seiten, 4 Quellen



    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




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