Experimental measuring system for control of aircraft hull surfaces
https://doi.org/10.17586/0021-3454-2023-66-5-430-436
Abstract
A measuring system for monitoring aircraft hull surfaces is studied experimentally. Results of experimental research into the measurement range, the output signal amplitude, as well as the measurement error are presented. A comparative analysis of the results of experimental measurements and independent measurements performed with a certified instrument is carried out. The dependences of the averaged amplitude of the output signal on the distance of the output signal from the optical pupil to the surface under investigation during the controlled object movement, as well as on the light beam diameter at the object surface, are obtained.
About the Authors
E. Е. Maiorov
St. Petersburg State University of Aerospace Instrumentation
Russian Federation
Russian Federation
Evgeny E. Maiorov - PhD, Associate Professor; St. Petersburg State University of Aerospace Instrumentation, Department of Applied Mathematics.
St. Petersburg
G. A. Kostin
St. Petersburg State University of Civil Aviation
Russian Federation
Russian Federation
Gennady A. Kostin - Dr. Sci., Associate Professor; St. Petersburg State University of Civil Aviation, Department of Applied Mathematics and Computer Science; Vice-Rector for Science and Digitalization.
St. Petersburg
T. A. Chernyak
St. Petersburg State University of Civil Aviation
Russian Federation
Russian Federation
Tatiana A. Chernyak - PhD, Associate Professor; St. Petersburg State University of Civil Aviation, Department of Higher Mathematics; Head of the Department.
St. Petersburg
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Review
For citations:
Maiorov E.Е., Kostin G.A., Chernyak T.A. Experimental measuring system for control of aircraft hull surfaces. Journal of Instrument Engineering. 2023;66(5):430-436. (In Russ.) https://doi.org/10.17586/0021-3454-2023-66-5-430-436
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