Abstract In this paper, a research and development version of the computer-aided system of mass tensometry (SMT) for conduction of aircraft and rocket-space equipment vibration tests is considered. A technique of the system design and development that combines the advantages of the system and process approaches when using the modern element base around the high-performance integral microcircuits is a distinctive feature in this research and development problem solution. We describe the architecture and structure of the advanced computer-aided SMTs and present data on its basic components desigtn. Also determined are the list and functional parameters of ratio-measuring network modules as well as the scheme of their connection to the test object and the local computer network of the enterprise.


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    Titel :

    Research and development version of computer-aided system of aircraft and rocket-space equipment vibration tests


    Beteiligte:
    Komkov, V. A. (Autor:in) / Vasilevskii, V. V. (Autor:in) / Korolev, V. F. (Autor:in) / Mozgovoi, Yu. V. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    2012-04-01


    Format / Umfang :

    6 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




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