Extensive bent components as they are used e.g. at the fuselage assembly must be put together to a fuselage section with high precision without being exceeded given strength limits. In context of the project the material behaviour of the components of a fuselage section is analysed, modelled and simulated with Artificial Neural Networks (ANN). Other aim of the project is to create a concept for production accompanying analysis of component geometry of a fuselage section by ANN. Various outer influences can have an effect on the components of the fuselage section and can influence the assembly. They shall be compensated automatically by a Computational Intelligence (CI) control concept.


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    Title :

    Fuselage assembly with computational intelligence


    Contributors:
    Schneider, M. (author) / Tillmann, R. (author) / Lehmann, U. (author) / Krone, J. (author) / Langbein, P. (author) / Ament, C. (author) / Otto, P. (author) / Stark, U. (author)


    Publication date :

    2008


    Size :

    12 Seiten, 7 Bilder, 2 Tabellen, 10 Quellen



    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




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