The work described in this paper has been supported under NASA contract NAS1-18099, Integrated Airframe/Propulsion Control System Architecture (IAPSA II). This contract addresses methodology, analysis, and detailed design of integrated control system architectures suitable for high-performance aircraft of the 1990's. 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. This paper addresses the methodology and supporting tools.


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    Title :

    Methods for evaluating integrated airframe/propulsion control system architectures


    Additional title:

    Methoden fuer die Auswertung integrierter Architekturen von Flugzeugzelle/Antriebssteuerungssystemen


    Contributors:
    Cohen, G.C. (author) / Lee, C.W. (author) / Palumbo, D.L. (author)


    Publication date :

    1987


    Size :

    7 Seiten, 6 Bilder, 6 Quellen


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English





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