Methodology, analysis, and detailed design of integrated control system architectures suitable for high-performance aircraft of the 1990s are presented. A methodology, with supporting analytical tools, has been developed to provide system designers with the capability to specify candidate architectures and accurately predict their reliability and performance in the early stages of design development. The authors address the methodology and supporting tools.


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    Title :

    Methods for Evaluating Integrated Airframe/Propulsion Control System Architectures


    Contributors:

    Conference:

    IEEE National Aerospace and Electronics Conference (NAECON 87) ; 1987 ; Dayton, OH, US



    Publication date :

    1987-05-18


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English




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