The design of an advanced digital avionics system (basic avionics module) for general aviation aircraft operated with a single pilot under IFR conditions is described. The microprocessor based system provided all avionic functions, including flight management, navigation, and lateral flight control. The mode selection was interactive with the pilot. The system used a navigation map data base to provide operation in the current and planned air traffic control environment. The system design included software design listings for some of the required modules. The distributed microcomputer uses the IEEE 488 bus for interconnecting the microcomputer and sensors.


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    Title :

    Basic Avionics Module Design for General Aviation Aircraft


    Contributors:
    R. K. Smyth (author) / D. E. Smyth (author)

    Publication date :

    1978


    Size :

    155 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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    Smyth, R. K. / Smyth, D. E. | NTRS | 1978



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