An integrated avionics system design was carried out to the level which indicates subsystem function, and the methods of overall system integration. Sufficient detail was included to allow identification of possible system component technologies, and to perform reliability, modularity, maintainability, cost, and risk analysis upon the system design. Retrofit to older aircraft, availability of this system to the single engine two place aircraft, was considered.


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    Title :

    Preliminary Candidate Advanced Avionics System for General Aviation


    Contributors:

    Publication date :

    1977


    Size :

    248 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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