doi: 10.17586/2226-1494-2019-19-3-531-537


3D-MODELING OF QUARTZ GLASS SENSORY ELEMENTS OF HEMISPHERICAL RESONATOR GYRO AND PENDULUM ACCELEROMETER

D. S. Gnusarev, V. V. Skorobogatov, E. A. Deputatova


Read the full article  ';
For citation:
Gnusarev D.S., Skorobogatov V.V., Deputatova E.A. 3D-modeling of quartz glass sensory elements of hemispherical resonator gyro and pendulum accelerometer. Scientific and Technical Journal of Information Technologies, Mechanics and Optics, 2019, vol. 19, no. 3, pp. 531–537 (in Russian). doi: 10.17586/2226-1494-2019-19-3-531-537


Abstract
Subject of Research. The paper considers physical processes occurring in sensory elements of angular rate and apparent acceleration measuring devices, such as hemispherical resonator gyro and pendulum accelerometer. Inertial masses of the studied sensory elements are made of KU-1 quartz glass. Method. Actual engineering drawings of the sensory elements are converted into a specialized 3D environment to simulate the performance of devices under different input effects, that is impossible with real devices. Moreover, traditional mathematical modeling approach, that involves such software packages as Matlab, does not provide a complete picture. Main Results. Visual information on the nature of motion of inertial masses was obtained using the results of 3D modeling, making it possible to improve and correct the known mathematical models of devices for subsequent Matlab analysis with closed control loop, since the studied gyro and accelerometer are compensation type devices with positive and negative feedback, respectively. Resonant frequencies of the considered devices were calculated as well. Practical Relevance. Considering the accelerometer, the obtained information on resonant frequencies made it possible to calculate band pass filters in order to suppress reactions to disturbances at these frequencies in the device pass band, and for the hemispherical resonator gyro it provides the possibility to define more precisely the resonator working frequency of oscillations.

Keywords: Subject of Research. The paper considers physical processes occurring in sensory elements of angular rate and apparent acceleration measuring devices, such as hemispherical resonator gyro and pendulum accelerometer. Inertial masses of the studied sensory elements are made of KU-1 quartz glass. Method. Actual engineering drawings of the sensory elements are converted into a specialized 3D environment to simulate the performance of devices under different input effects, that is impossible with real devices. Moreover, traditional mathematical modeling approach, that involves such software packages as Matlab, does not provide a complete picture. Main Results. Visual information on the nature of motion of inertial masses was obtained using the results of 3D modeling, making it possible to improve and correct the known mathematical models of devices for subsequent Matlab analysis with closed control loop, since the studied gyro and accelerometer are compensation type devices with positive and negative feedback, respectively. Resonant frequencies of the considered devices were calculated as well. Practical Relevance. Considering the accelerometer, the obtained information on resonant frequencies made it possible to calculate band pass filters in order to suppress reactions to disturbances at these frequencies in the device pass band, and for the hemispherical resonator gyro it provides the possibility to define more precisely the resonator working frequency of oscillations.

References
1. Matveev V.V., Raspopov V.Ya. Basics of Constructing Strapdown Inertial Navigation Systems. St. Petersburg, OAO Kontsern TsNII Elektropribor Publ., 2009, 280 p. (in Russian)
2. Branets V.N., Shmyglevskii I.P. Introduction to the Theory of Strapdown Inertial Navigation Systems. Moscow, Nauka Publ., 1992, 280 p. (in Russian)
3. Branets V.N. Lectures on the Theory of Strapdown Inertial Navigation Systems. Moscow, MFTI Publ., 2009, 302 p. (in Russian)
4. Kalikhman D.M., Deputatova E.A., Skorobogatov V.V., Gnusarev D.S. Prospects for the SINS development on modern types of gyroscopes and accelerometers in space technology. Proc. 7th Int. Conf. on Problems of Control, Information Processing and Transmission. Saratov, Russia, 2019, pp. 26–51.
5. Mel’nikov V.E. Quartz Glass based Electromechanical Converters. Moscow, Mashinostroenie Publ., 1984, 160 p. (in Russian)
6. Kalikhman L.Ya., Kalikhman D.M., Nakhov S.F. et al. Thermal Invariant Meter of Linear Acceleration. Patent RU2528119, 2017.
7. Skorobogatov V.V., Kalikhman L.Ya., Kalikhman D.M., Nakhov S.F., Grebennikov V.I. Method for Providing Scale Coefficient Linearity of Pendulum Wide-Range Accelerometer of Compensatory Type. Patent RU2627970, 2017.
8. Grebennikov V.I., Kalikhman L.Ya., Kalikhman D.M., Nakhov S.F., Skorobogatov V.V., Samitov R.M., Kozhevnikov V.E., Pozdnyakov V.M. Method for Providing Linearity of Pendulous Accelerometer Scale Coefficient of Compensatory Type. Patent RU2626071, 2017.
9. Grebennikov V.I., Kalikhman L.Ya., Kalikhman D.M., Nakhov S.F., Skorobogatov V.V., Smirnov E.S. Method for Providing Vibration Resistance of Pendulum Accelerometer of Linear Accelerations with Digital Feedback and Vibration Pendulum Accelerometer. Patent RU2615221, 2017.
10. Skorobogatov V.V. Basics of development of heat-free thermo- invariant angular velocity meaters and seemingly accelerated for control systems of rocket-space objects. Dis. PhD Eng. Sci. Saratov, Russia, 2018.
11. Deputatova E.A., Grebennikov V.I., Kalikhman D.M., Skorobogatov V.V., Chibirev A.S. Mathematical model of a sensitive element of quartz pendulum accelerometer. Proc. 5th Int. Conf. on Problems of Control, Information Processing and Transmission. Saratov, Russia, 2017, pp. 54–61. (in Russian)
12. Deputatova E.A., Gnusarev D.S., Kalikhman D.M. Analysis of noise components in quartz pendulum accelerometer with digital feedback amplifier. Scientific and Technical Journal of Information Technologies, Mechanics and Optics, 2018, vol. 18, no. 6, pp. 1091–1098 (in Russian). doi: 10.17586/2226-1494- 2018-18-6-1091-1098
13. Negri C., Labarre E., Lignon C., Brunstein E., Salaün E. A new generation of IRS with innovative architecture based on HRG for satellite launch vehicles. Gyroscopy and Navigation, 2016, vol. 7, no. 3, pp. 223–230. doi: 10.1134/S2075108716030135
14. Zhuravlev V.F., Klimov D.M. A Wave Solid-State Gyroscope. Moscow, Nauka Publ., 1985, 126 p. (in Russian)
15. Jeanroy A., Bouvet A., Remillieux G. HRG and marine applications. Gyroscopy and Navigation, 2014, vol. 5, no. 2, pp. 67–74. doi: 10.1134/s2075108714020047
16. Schmidt G.T. INS/GPS technology trends, advances in navigation sensors and integration technology. RTO Lecture, 2004, no. 232, p. 11.
17. Barbour N.M. Inertial navigation sensors, advances in navigation sensors and integration technology. RTO Lecture, 2004, no. 232, p. 7.
18. Delhaye F., Girault J.P. HRG technological breakthrough for advanced space launcher inertial reference system. Proc. 25th St. Petersburg Int. Conf. on Integrated Navigation Systems. St. Petersburg, 2018, pp. 267–271.
19. Raspopov V.Ya. Micromechanical Devices. Moscow, Mashinostroenie Publ., 2007, 400 p. (in Russian)
20. Luk’yanov D.P., Raspopov V.Ya., Filatov Yu.V. Applied Theory of Gyros. St. Petersburg, OAO Kontsern TsNII Elektropribor Publ., 2015, 316 p. (in Russian)
 


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