Errors of two-stage gyro in semi-natural conditions of hypersonic flight
Heading:
| 1Shybetskiy, VYu. 1National Technical University of Ukraine “Kyiv Polytechnic Institute”, Kyiv, Ukraine |
| Kosm. nauka tehnol. 2014, 20 ;(2):52-54 |
| https://doi.org/10.15407/knit2014.02.052 |
| Publication Language: Ukrainian |
Abstract: We present our results of semi-natural bench tests of uniform angular velocity sensor in the ultrasound beam which occurs in the operation of a hypersonic aircraft. It is proved that there are additional areas of caustic in wave pattern space. |
| Keywords: angular velocity gyro sensor, hypersonic aircraft |
References:
1. Karachun V., Mel’nick V., Shibetskii V. Gyro errors conditioned by developing pitching motion of fuselage during flight operations. Eastern-European Journal of Enterprise Technologies. N 5/7 (65), 45—47 (2013) [in Russian].
2. Shibeckij V. Ju. nfluence of the Gaussian curvature of the suspension of floating gyroscope on the elastic compliance in the acoustic field. Young Scientist, N 12, 116—120 (2012) [in Russian].
3. Shibeckij V. Ju., Karachun V. V. Float in the gyro suspension at the flight operations. Izv. GUAP.Aerokosmicheskoe priborostroenie. Issue 4, 41—44 (2013) [in Russian].
4. Karachun V. V., Mel'nick V. N. Influence of diffraction effects of the inertial sensors of a gyroscopically stabilized platform: three-dimensional problem. Int. Appl. Mech. 48(4), 458—464 (2012).
https://doi.org/10.1007/s10778-012-0533-y