Abstract The complexity of modern systems requires a holistic approach to modeling and simulation during the design phases. This often includes an integrated model of the overall system (architecture, function, and environment) as well as a link-up of computer-aided design tools, because there are many occasions in which there are aspects of the system that cannot be described in one tool. The paper introduces a converter program that bridges the gap between a CAD tool and a system design tool. Non-functional information that is relevant for the simulation is extracted from the three-dimensional CAD model and automatically inserted into the behavioral model of the system design tool. The latter is used for performance evaluation and indirect design optimization.


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    Titel :

    Optimization of avionic system architectures


    Beteiligte:
    Schulz, Mario (Autor:in) / Zerbe, Volker (Autor:in) / Yang, Kai (Autor:in) / Zimmermann, Armin (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    2011




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch



    Klassifikation :

    BKL:    50.03 Methoden und Techniken der Ingenieurwissenschaften / 50.03 Methoden und Techniken der Ingenieurwissenschaften, Methoden und Techniken der Ingenieurwissenschaften / 55.50 Luftfahrzeugtechnik / 55.50 Luftfahrzeugtechnik, Luftfahrzeugtechnik
    DDC:    629.105



    Optimization of avionic system architectures

    Schulz, Mario / Zerbe, Volker / Yang, Kai et al. | Springer Verlag | 2011


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    Trujillo, E. | Tema Archiv | 1989



    Avionic Architectures for Space Exploration Missions

    Tramutola, A. / Martelli, A. / Caramia, M. et al. | British Library Conference Proceedings | 2011


    Rapid Prototyping of Complex Avionic System Architectures

    L. Berardi / N. Giorgi / W. Mellano et al. | NTIS | 1987