The stages in the development and integration of the TIGER basic avionic system are described. The most important integration tools for avionic integration purposes are described. These include an integrating rig for the installation and operation of the avionic equipment, patch panels which allow an access to all avionic signals, and a test system for complex measurements and tests. Besides the test system, various laboratory test equipment for direct signal stimulation for measurements are used. The tasks of the real time test system used for integration of the TIGER avionic system are described. These include the validation and monitoring of interface data flow, and simulation of environment/equipment data. The test system performance is considered. It is concluded that the test means for the TIGER basic avionic system offer the required flexibility for the integration of the various national versions of this helicopter at the same test rig. The use of an off the shelf test system avoids any development risks of a 'selfmade' solution.


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    Titel :

    Test and Integration Concept for Complex Helicopter Avionic Systems


    Beteiligte:
    H. Goelzenleuchter (Autor:in) / L. Dietl (Autor:in)

    Erscheinungsdatum :

    1991


    Format / Umfang :

    8 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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    HALKO, C. / JADICO, T. | AIAA | 1981



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    Rid, S. / Deutsche Forschungsanstalt fur Luft und Raumfahrt | British Library Conference Proceedings | 1995


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    Goelzenleuchter, H. / Erismann, P. / Associazione Italiana di Aeronautica ed Astronautica et al. | British Library Conference Proceedings | 1993


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    JANEX, ALBERT | AIAA | 1988