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:

    CEAS Aeronautical Journal ; 2 , 1 ; 289-294


    Erscheinungsdatum :

    2011-08-20


    Format / Umfang :

    6 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




    Optimization of avionic system architectures

    Schulz, Mario / Zerbe, Volker / Yang, Kai et al. | Online Contents | 2011


    Modular avionic architectures

    Trujillo, E. | Tema Archiv | 1989



    Rapid Prototyping of Complex Avionic System Architectures

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