Abstract We consider the aircraft system hardware and software to measure the angular deflections of control surfaces. The experimental studies of a photoelectric transducer for converting the control surface angular deflections into digital codes are performed. The mathematical models are obtained to describe a dependence of measuring errors on the coordinates of emitter arrangement. The optimal emitter arrangement is determined using the mathematical models and a pilot model of the aircraft system proposed has been developed.


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    Titel :

    Aircraft system for measuring the angular deflections of control surfaces


    Beteiligte:

    Erschienen in:

    Erscheinungsdatum :

    2013-10-01


    Format / Umfang :

    5 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




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    Koshevoi, N. D. / Kostenko, E. M. / Oganesyan, A. S. et al. | Online Contents | 2013


    Electro-optical System Measures Aircraft Deflections

    Fodale, B. / Hampton, H. R. / Seymour, H. R. et al. | NTRS | 1986


    Meshless Aeroelastic Simulations of Aircraft with Large Control Surface Deflections

    Lesoinne, M. / Kaila, V. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2005