Providing operating modes for Coriolis vibration gyroscopes with low-Q resonators
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 d...
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| Format: | Article |
| Language: | English |
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Saint Petersburg National Research University of Information Technologies, Mechanics and Optics (ITMO University)
2024-02-01
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| Series: | Naučno-tehničeskij Vestnik Informacionnyh Tehnologij, Mehaniki i Optiki |
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| Online Access: | https://ntv.ifmo.ru/file/article/22601.pdf |
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| author | Valery V. Matveev Vladimir V. Likhosherst Alexey V. Kalikanov Maxim G. Pogorelov Maxim D. Kirsanov Sergey V. Telukhin |
| author_facet | Valery V. Matveev Vladimir V. Likhosherst Alexey V. Kalikanov Maxim G. Pogorelov Maxim D. Kirsanov Sergey V. Telukhin |
| author_sort | Valery V. Matveev |
| collection | DOAJ |
| description | 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. |
| first_indexed | 2024-03-08T03:00:18Z |
| format | Article |
| id | doaj.art-a6a336853af44c6a9e85cb6481d1dae7 |
| institution | Directory Open Access Journal |
| issn | 2226-1494 2500-0373 |
| language | English |
| last_indexed | 2024-03-08T03:00:18Z |
| publishDate | 2024-02-01 |
| publisher | Saint Petersburg National Research University of Information Technologies, Mechanics and Optics (ITMO University) |
| record_format | Article |
| series | Naučno-tehničeskij Vestnik Informacionnyh Tehnologij, Mehaniki i Optiki |
| spelling | doaj.art-a6a336853af44c6a9e85cb6481d1dae72024-02-13T11:21:24ZengSaint Petersburg National Research University of Information Technologies, Mechanics and Optics (ITMO University)Naučno-tehničeskij Vestnik Informacionnyh Tehnologij, Mehaniki i Optiki2226-14942500-03732024-02-0124113314310.17586/2226-1494-2024-24-1-133-143Providing operating modes for Coriolis vibration gyroscopes with low-Q resonatorsValery V. Matveev0https://orcid.org/0000-0001-8997-0297Vladimir V. Likhosherst1https://orcid.org/0009-0009-4315-5997Alexey V. Kalikanov2https://orcid.org/0000-0002-1590-4278Maxim G. Pogorelov3https://orcid.org/0009-0005-9731-3066Maxim D. Kirsanov4https://orcid.org/0009-0002-2872-9322Sergey V. Telukhin5https://orcid.org/0009-0001-2649-8420D.Sc., Associate Professor, Leading Researcher, Head of Department, Tula State University, Tula, 300012, Russian Federation, sc 56382006100PhD, Senior Researcher, Associate Professor, Tula State University, Tula, 300012, Russian Federation, sc 57190385346Junior Researcher, Assistant, Tula State University, Tula, 300012, Russian Federation, sc 5755680050PhD, Head of Laboratory, Associate Professor, Tula State University, Tula, 300012, Russian Federation, sc 55983327300Junior Researcher, Associate Professor, Tula State University, Tula, 300012, Russian Federation, sc 79539670944PhD, Associate Professor, Tula State University, Tula, 300012, Russian Federation, sc 56770129600Coriolis 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.https://ntv.ifmo.ru/file/article/22601.pdfcoriolis vibration gyroscopelow-q resonatoroperating modeexcitation methods |
| spellingShingle | Valery V. Matveev Vladimir V. Likhosherst Alexey V. Kalikanov Maxim G. Pogorelov Maxim D. Kirsanov Sergey V. Telukhin Providing operating modes for Coriolis vibration gyroscopes with low-Q resonators Naučno-tehničeskij Vestnik Informacionnyh Tehnologij, Mehaniki i Optiki coriolis vibration gyroscope low-q resonator operating mode excitation methods |
| title | Providing operating modes for Coriolis vibration gyroscopes with low-Q resonators |
| title_full | Providing operating modes for Coriolis vibration gyroscopes with low-Q resonators |
| title_fullStr | Providing operating modes for Coriolis vibration gyroscopes with low-Q resonators |
| title_full_unstemmed | Providing operating modes for Coriolis vibration gyroscopes with low-Q resonators |
| title_short | Providing operating modes for Coriolis vibration gyroscopes with low-Q resonators |
| title_sort | providing operating modes for coriolis vibration gyroscopes with low q resonators |
| topic | coriolis vibration gyroscope low-q resonator operating mode excitation methods |
| url | https://ntv.ifmo.ru/file/article/22601.pdf |
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