The Demonstration Advanced Avionics System, DAAS, is an integrated avionics system utilizing microprocessor technologies, data busing, and shared displays for demonstrating the potential of these technologies in improving the safety and utility of general aviation operations in the late 1980's and beyond. Major hardware elements of the DAAS include a functionally distributed microcomputer complex, an integrated data control center, an electronic horizontal situation indicator, and a radio adaptor unit. All processing and display resources are interconnected by an IEEE-488 bus in order to enhance the overall system effectiveness, reliability, modularity and maintainability. A detail description of the DAAS architecture, the DAAS hardware, and the DAAS functions is presented. The system is designed for installation and flight test in a NASA Cessna 402-B aircraft.


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    Title :

    Demonstration Advanced Avionics System (Daas) Function Description


    Contributors:
    A. J. Bailey (author) / D. G. Bailey (author) / R. J. Gaabo (author) / T. G. Lahn (author) / J. C. Larson (author)

    Publication date :

    1982


    Size :

    204 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English