Investigation into Optoelectronic Aviation Angle Meter by the Design-of-Experiments Method
A.S. Oganesyan, M.V. Thehovsky, N.D. Koshevoy, and V.A. Gordienko
National Aerospace University “Kharkkiv Aviation Institute”,
Kharkiv 61085, Ukraine
Abstract
This paper considers both an aviation angle meter to measure the aircraft control surface angles and the operation of angle meter electronic bloc. A description is given of the process of synthesizing mathematical models of this particular device using the design-of-experiments method.
KEY WORDS: angle meter, infrared light-emitting diode (LED), design of experiments, full factorial experiment, orthogonal central composition full factorial experiment
References
- Koshevoy, N.D. and Oganesyan, A.S., (2007), A universal photoelectric sensor of aircraft control surface angular displacement, Sbornik nauchnykh trudov KNU, Kiev: 34-37 (in Russian).
- Oganesyan, A.S., Koshevoy, N.D., and Tsehovsky, M.V., (2009), Circuitry designing of an optical device for measuring a turning angle of the aircraft control surface, Svetotekhnika and Elektroenergetika. 10(3):75-78 (in Russian).
- Adler, Yu.P., Markova, E.V., and Granovsky, Yu.V., (1976), The design of experiments in searching optimal conditions, Nauka, Moscow: 279 p. (in Russian).
- Akhnazarova, S.L. and Kafarov, V.V., (1985), Methods of optimizing an experiment in chemical technology, Vyshsaya Shkola, Moscow: 327 p. (in Russian).
|
|