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Tytuł artykułu

Modelling of Influence of Hypersonic Conditions on Gyroscopic Inertial Navigation Sensor Suspension

Treść / Zawartość
Identyfikatory
Warianty tytułu
Języki publikacji
EN
Abstrakty
EN
The upcoming hypersonic technologies pose a difficult task for air navigation systems. The article presents a designed model of elastic interaction of penetrating acoustic radiation with flat isotropic suspension elements of an inertial navigation sensor in the operational conditions of hypersonic flight. It has been shown that the acoustic transparency effect in the form of a spatial-frequency resonance becomes possible with simultaneous manifestation of the wave coincidence condition in the acoustic field and equality of the natural oscillation frequency of a finite-size plate and a forced oscillation frequency of an infinite plate. The effect can lead to additional measurement errors of the navigation system. Using the model, the worst and best case suspension oscillation frequencies can be determined, which will help during the design of a navigation system.
Rocznik
Strony
357--368
Opis fizyczny
Bibliogr. 24 poz., rys., tab., wykr., wzory
Twórcy
  • Warsaw University of Technology, Faculty of Mechatronics, Św. A. Boboli 8, 02-525 Warsaw, Poland
autor
  • National Technical University of Ukraine, Kyiv Polytechnic Institute, 37 Peremogy, Kyiv, Ukraine
autor
  • National Technical University of Ukraine, Kyiv Polytechnic Institute, 37 Peremogy, Kyiv, Ukraine
autor
  • Industrial Research Institute for Automation and Measurements PIAP, Al. Jerozolimskie 202, 02-486 Warsaw, Poland
Bibliografia
  • [1] Beshenkov, S.N. (1974). Study of acoustic properties of sandwich constructions. Acoustic Magazine, 20 (2), 276-281.
  • [2] Madeira, J.F.A., Araújo, A.L., Mota Soares, C.M., Mota Soares, C.A., Ferreira, A.J.M. (2015). Multiobjective design of viscoelastic laminated composite sandwich panels. Composites Part B: Engineering, 77(1), 391-401.
  • [3] Wang, T., Li, S., Nutt, S.R. (2009). Optimal design of acoustical sandwich panels with a genetic algorithm. Applied Acoustics, 70(3), 416-425.
  • [4] Chronopoulos, D., Collet, M., Ichchou, M., Antoniadis, I. (2015).Wave based design optimisation of composite structures operating in dynamic environments. COMPDYN 2015 − 5th ECCOMAS Thematic Conference on Computational Methods in Structural Dynamics and Earthquake Engineering, 4390-4408.
  • [5] Bogolepov, I.I. (1986). Industrial soundproofing. Monograph. L. Sudostroenie, 386.
  • [6] Brekhovskih, I.M. (1973). Waves in layered structures. Monograph. M. Nauka, 344.
  • [7] Valeev, K.G. (1970). Definition of stress state of flat panels in the acoustic field of the exhaust stream. Adventure of Mechanic, VI(4), 30-43.
  • [8] Goloskokov, E.G. (1980). Elastic and acoustic problems of sandwich construction dynamics. Monograph. Kharkiv. Vyshcha shkola, 189.
  • [9] Kanibolotskiy, M.A. (1980). Optimal design of layered structures. Monograph. Novosibirsk. Nauka. Sib. Department, 176.
  • [10] Xu, F., Wang, W., Shao, X., Liu, X., Liang, Y. (2015). Optimization of surface acoustic wave-based rate sensors. Sensors, 15(10,12), 25761-25773.
  • [11] Hamdaoui, M., Robin, G., Jrad, M., Daya, E.M. (2014). Optimal design of frequency dependent threelayered rectangular composite beams for low mass and high damping. Composite Structures, 120, 174-182.
  • [12] Karachun, V., Mel’nick, V., Korobiichuk, I., Nowicki, M., Szewczyk, R., Kobzar, S. (2016). The Additional Error of Inertial Sensor Induced by Hypersonic Flight Condition. Sensors, 16(3).
  • [13] Karachun, V.V. (2012). Influence of Diffraction Effects on the Inertial Sensorg of a Gyroscopically Stabilized Platform: Three-Dimansional Problem. International Applied Mechanics, 48(4), 458-464.
  • [14] Karachun, V.V. (2014). Ware coincidence and errors of floating gyroscope at the resonance Level. News of Science and Education, Technical Science, Mathematics. Science and Education Ltd, 31(21), 56-62.
  • [15] Karachun, V.V. (1989). Vibration of a plate under an acoustic load. Engineering, Technology Science, PA, 20(37), 391-394.
  • [16] Mostafapour, A., Ghareaghaji, M., Davoodi, S., Ebrahimpour, A. (2016). Theoretical analysis of plate vibration due to acoustic signals. Applied Acoustics, 103, 82-89.
  • [17] Geng, Q., Li, Y. (2012). Analysis of dynamic and acoustic radiation characters for a flat plate under thermal environments. International Journal of Applied Mechanics, 4(3).
  • [18] Alzahabi, B., Almic, E. (2011). Sound radiation of cylindrical shells. International Journal of Multiphysics, 5(2), 173-185.
  • [19] Korobiichuk, I. (2016). Mathematical model of precision sensor for an automatic weapons stabilizer system. Measurement, 89, 151-158.
  • [20] Lee, S.W., Rhim, J.W., Park, S.W., Yang, S.S. (2007). A novel micro rate sensor using a surface-acousticwave (SAW) delay-line oscillator. Proc. of IEEE Sensors, 1156-1159.
  • [21] Korobiichuk, I., Nowicki, M., Szewczyk, R. (2015). Design of the novel double-ring dynamical gravimeter. Journal of Automation, Mobile Robotics and Intelligent Systems, 9(3), 47-52.
  • [22] Mehta, A., Jose, K.A., Varadan, V.K. (2002). Numerical simulation of a surface acoustic wave (SAW) gyroscope using HP EEsof. Proc. of SPIE. The International Society for Optical Engineering. 4700, 169-177.
  • [23] Korobiichuk, I., Koval, A., Nowicki, M., Szewczyk, R. (2016). Investigation of the Effect of Gravity Anomalies on the Precession Motion of Single Gyroscope Gravimeter. Solid State Phenomena, 251, 139-145.
  • [24] Creagh, M.A., Beasley, P., Dimitrijevic, I., Brown, M., Tirtey, S. (2012). A Kalman-filter based Inertial navigation system processor for the SCRAMSPACE 1 hypersonic flight experiment. 18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference 2012, Tours, France.
Uwagi
PL
Opracowanie ze środków MNiSW w ramach umowy 812/P-DUN/2016 na działalność upowszechniającą naukę (zadania 2017).
Typ dokumentu
Bibliografia
Identyfikator YADDA
bwmeta1.element.baztech-a6615873-00da-4617-b61e-840fe12f084d
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