doi: 10.17586/2226-1494-2024-24-1-133-143


Providing operating modes for Coriolis vibration gyroscopes with low-Q resonators

V. V. Matveev, V. V. Likhosherst, A. V. Kalikanov, M. G. Pogorelov, M. D. Kirsanov, S. V. Telukhin


Read the full article  ';
Article in Russian

For citation:
Matveev V.V., Likhosherst V.V., Kalikanov A.V., Pogorelov M.G., Kirsanov M.D., Telukhin S.V. Providing operating modes for Coriolis vibration gyroscopes with low-Q resonators. Scientific and Technical Journal of Information Technologies, Mechanics and Optics, 2024, vol. 24, no. 1, pp. 133–143 (in Russian). doi: 10.17586/2226-1494-2024-24-1-133-143


Abstract
Coriolis vibration gyroscopes are a class of promising inertial primary information sensors that respond to the rotation of the resonator base through Coriolis inertial forces arising in the vibrating shell. Currently, two directions for the production of resonators for such gyroscopes have been developed: from quartz glass, a material with extremely low internal friction, and based on the processing of a metal alloy. When using the first direction, thanks to the high quality factor of quartz, it is possible to create navigation-class integrating gyroscopes. Existing samples of Coriolis vibration gyroscopes with metal resonators, as a rule, are angular velocity sensors. The problem of creating an integrating mode of a gyroscope with a metal resonator is associated with the low quality factor of metal alloys which usually does not exceed 35,000. With this value of quality factor, the duration of operation of the gyroscope in the angular deviation sensor mode will be several seconds. The paper presents methods for ensuring the functioning of Coriolis vibration gyroscopes, including the integrating gyroscope mode. A mathematical description of Coriolis vibration gyroscopes with a cylindrical cavity resonator is given based on the dynamic model of Dr. D. Lynch using the method of envelope amplitudes of oscillations. The mathematical model is supplemented with corrections that provide compensation for the dissipation of the resonator oscillations energy to implement the integrating mode of the gyroscope. The conditions for complete compensation of vibration energy dissipation are shown. A description of methods for exciting a standing wave in a resonator using periodic forcing and by creating self-oscillations is presented. It is shown that the duration of the transient excitation process is determined by the time constant of the resonator. The results of experimental studies of Coriolis vibration gyroscopes with a low-Q metal resonator are presented confirming the possibility of implementing an integrating mode of operation of the gyroscope. The initial excitation of the resonator oscillations is carried out by a self-oscillating circuit. According to the results of experimental studies, the quality factor of the metal resonator was increased by a factor of 17. The operating time of Coriolis vibrating gyroscopes has been equally increased. The possibility of constructing Coriolis vibration gyroscopes in the integrating gyroscope mode based on a low-Q metal resonator has been shown theoretically and experimentally. The solution to this problem was based on a circuitry method for increasing the quality factor. In principle, the quality factor of the resonator can be significantly increased compared to the figure achieved in the experiment. This will ensure a longer operating time of Coriolis vibration gyroscopes in the integrating mode.

Keywords: Coriolis vibration gyroscope, low-Q resonator, operating mode, excitation methods

Acknowledgements. The work was supported financially by the Ministry of Science and Higher Education of the Russian Federation within the framework of the state assignment on the topic FEWG-2022-0002.

References
  1. Vavilov V.D., Timoshenkov S.P., Timoshenkov A.S. Microsystem Sensors of Physical Quantities. Moscow, Technosphera Publ., 2018, 550 p. (in Russian)
  2. Peshekhonov V.G. The author of precision gyroscope. Gyroscopy and Navigation, 2020, vol. 11, no. 2, pp. 188–192. https://doi.org/10.1134/s2075108720020042
  3. Lunin B.S. Science and technology basis for the development of the hemispherical resonators for solid-state wave gyroscopes. Abstract of the dissertation for the degree of Doctor of Technical Sciences. Moscow, MSU, 2006, 32 p. (in Russian)
  4. Lunin B.S., Matveev V.A., Basarab M.A. Solid-State Wave Gyroscope. Moscow, Radiotehnika Publ., 2014, 176 p. (in Russian)
  5. Raspopov V.Ya., Egorov S.V. Design and verification of the finite element model of a wave solid-state gyroscope resonator. Izvestiya Tula State University. Technical sciences, 2021, no. 10, pp. 227–235. (in Russian)
  6. Raspopov V.Y., Likhosherst V.V. HRG with a metal resonator. Gyroscopy and Navigation, 2023, vol. 14, no. 1, pp. 14–26. https://doi.org/10.1134/S2075108723010066
  7. Raspopov V.Ia., Volchikhin I.A., Volchikhin A.I., Ladonkin A.V., Likhosherst V.V., Matveev V.V. Solid-State Wave Gyroscope with a Metal Resonator. Tula, Tula State University, 2018, 189 p. (in Russian)
  8. Chikovani V.V., Yatsenko Yu.A., Barabashov A.S., Kovalenko V.A., Tewksbury P. A set of high accuracy low cost metallic resonator CVG. Proc. of the 20th International Technical Meeting of the Satellite Division of The Institute of Navigation (ION GNSS 2007), 2007, pp. 1345–1350.
  9. Acar C., Shkel A. MEMS Vibratory Gyroscopes: Structural Approaches to Improve Robustness. Springer, 2009, 256 p. https://doi.org/10.1007/978-0-387-09536-3
  10. Matveev V.A., Lipatnikov V.I., Alekhin A.V. Design of the Solid State Wave Gyro. Moscow, Bauman Moscow State Technical University, 1998, 166 p. (in Russian)
  11. Klimov D.M., Zhuravlev V.F., Zhbanov Iu.K. Hemispherical Quartz Resonator (Solid-State Wave Gyroscope). Moscow, Kim L.A. Publ., 2017, 193 p. (in Russian)
  12. Lynch D.D. Coriolis vibratory gyroscope. IEEE Standard Specification Format Guide and Test Procedure for Coriolis Vibratory Gyros. IEEE std.1431 annex B. 2004, pp. 56–66.
  13. Sharma G.N., Sundararajan T., Gautam S.S. Thermoelastic damping based design, sensitivity study and demonstration of a functional hybrid gyroscope resonator for high quality factor. Gyroscopy and Navigation, 2021, vol. 12, no. 1, pp. 69–85. https://doi.org/10.1134/S2075108721010107
  14. Maslov A.A., Maslov D.A., Ninalalov I.G., Merkuryev I.V. Hemispherical resonator gyros (an overview of publications). Gyroscopy and Navigation, 2023, vol. 14, no. 1, pp. 1–13. https://doi.org/10.1134/S2075108723010054
  15. Lynch D.D. Vibratory gyro analysis by the method of averaging. Proc. of the 2nd St. Petersburg conference on gyroscopic technology and navigation. St. Petersburg, 1995, pp. 26–34.
  16. Severov L.A., Zolotarev S.K., Ovchinnikova N.A., Panferov A.I., Ponomarev V.K. Data characteristics of the micromechanical gyroscopes based on silicon technology microelectromechanical systems. Journal of Instrument Engineering, 2011, vol. 54, no. 8, pp. 12–22. (in Russian)
  17. Panovko Ia.G. Introduction to Mechanical Vibration Theory. Moscow, Nauka Publ., 1971, 239 p. (in Russian)
  18. Kucherkov S.G. Using the integrating properties of a vibrating micromechanical gyroscope with resonant tuning when constructing a compensation-type angular velocity sensor. Giroskopiya i Navigatsiya, 2002, no. 2, pp. 12–18. (in Russian)
  19. Chikovani V. Secondary wave control system of the Coriolis vibratory gyroscope resonator. Electronics and Control Systems, 2013, no. 3, pp. 58–61. https://doi.org/10.18372/1990-5548.35.5805
  20. Landau L., Lifshitz E. Course of Theoretical Physics. Vol. 1. Mechanics. Elsevier, 1988, 224 p.


Creative Commons License

This work is licensed under a Creative Commons Attribution-NonCommercial 4.0 International License
Copyright 2001-2024 ©
Scientific and Technical Journal
of Information Technologies, Mechanics and Optics.
All rights reserved.

Яндекс.Метрика