Aerospace computer implementations are entering a new era, characterized by two fundamental trends: significant interst in commercially-based products, designs, and technology, requirements for non-proprietary 'standard' systems that are interoperable and scalable. The primary drivers that appear to motivate these trends, in both military and space systems, are: cost - a result of severely limited budget resources, schedules - need the systems sooner, rapid technology turnover, fear of obsolescence, etc. Designs that satifsy these trends are deemed to be 'open', and will exhibit an 'open system architecture'. Typical features for open and non-open (or 'closed') computer systems will be examined and compared in this paper, and advantages and disadvantages of each approach discussed. Representative examples will be shown for each system approach along with a trade of salient parameters.


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    Title :

    Open architecture considerations for aerospace computer systems


    Additional title:

    Offene Architektur-Betrachtungen für Aerospace Computer Systeme


    Contributors:


    Publication date :

    1992


    Size :

    6 Seiten, 5 Bilder, 1 Tabelle, 7 Quellen




    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




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