Wave tasks of inertial navigation systems

1Karachun, VV, 2Kayuk, Ya.F, 1Mel'nik, VN
1National Technical University of Ukraine «Kyiv Polytechnic Institute», Kyiv, Ukraine
2S.P. Timoshenko Institute of Mechanics of the National Academy of Sciences of Ukraine, Kyiv, Ukraine
Kosm. nauka tehnol. 2007, 13 ;(6):039-045
Section: Space Navigation and Communications
Publication Language: Ukrainian
We present our results of the analysis of elastic interaction of suspend gyroscope with penetrating acoustic radiation and influence of sound waves on sensitive elements of system of correction.
Keywords: correction system, gyroscope, sound waves
1. Gladky V. F. Dynamics of Flying Vehicle Structure, 496 p. (Nauka, Moscow, 1969) [in Russian].
2. Foks Vil'jams D. E. The noise of high-speed missiles. In: Crandall S. H.( Ed.) Random Vibration, 45 —49 (Mir, Moscow, 1967) [in Russian].

3. Koshljakov V. N., Karachun V. V., Mel'nik V. N., et al. The some aspects of flaigt safety in conditions penetrate acoustic radiation. In: Aviation in the XXI-st Century: World Congress, Kyiv, 14—16 September, 2003, 2.37—2.40 (National Aviation University, Kyiv, 2003).