طراحی، ساخت و تست تجربی ژیروسکوپ ارتعاشی استوانه‌ای

نوع مقاله : مقاله پژوهشی

نویسندگان

1 دانشکده مهندسی صنایع، دانشگاه علم و فناوری مازندران

2 دانشکده مهندسی هوافضا، دانشگاه تربیت مدرس

3 دانشکده الکترونیک، دانشگاه شاهد

4 دانشکده مهندسی مکانیک - دانشگاه علم و صنعت ایران

چکیده

ژیروسکوپ ارتعاشی مدور با رزوناتور استوانه­ای بر مبنای اثر کوریولیس طراحی و ساخته شده است. تحریک و دریافت پاسخ نوسانات به کمک پیزوالکتریک­ها انجام شده است. پس از راه­اندازی رزوناتور، جدایش فرکانسی اندازه­گیری شده و همچنین الگوی ارتعاشی رزوناتور با بهره­گیری از یک مکانیزم صوتی ثبت و به کمک آن شیفت فازی رزوناتور ثبت شده است. نتایج آزمون­ها نشان داد که طراحی رزوناتور با ضخامت پله­ای، سبب دستیابی به نسبت مناسبی برای دامنه پاسخ به تحریک شده است. همچنین جدایش فرکانسی رزوناتور تقریبا یک هرتزی بوده است. به علاوه استفاده از مکانیزم صوتی کارایی مناسبی را در ثبت موقعیت الگوی ارتعاشی نشان داد و اندازه­گیری شیفت فازی به کمک مکانیزم صوتی وجود شیفت فازی 4 درجه­ای را نشان داده است. تاثیر نرخ دوران رزوناتور بر جاماندگی موج ارتعاشی بررسی شد و ثبت تغییرات نرخ دوران در چرخش ساعتگرد و پادساعتگرد در ژیروسکوپ، تقریب خطی مناسبی را به همراه داشته است.

کلیدواژه‌ها

موضوعات


عنوان مقاله [English]

Design, Manufacturing and Testing of a Cylindrical Vibrating Gyroscope

نویسندگان [English]

  • Seyed Mahmoud Ghalehbandi 1
  • Saleh Fallah 2
  • Iman Halimi 3
  • Hamid Shafiee Alavije 4
1 Faculty of Industrial Engineering, University of Science and Technology of Mazandaran, Behshahr, Iran.
2 Faculty of Aerospace Engineering, Tarbiat Modares University, Tehran, Iran.
3 Faculty of Electronic Engineering, Shahed University, Tehran, Iran.
4 Faculty of Mechatronic Engineering, Iran University of Science and Technology, Tehran, Iran.
چکیده [English]

A resonating gyroscope with a cylindrical resonator is designed using finite element method with the aim of achieving the maximum oscillation amplitude. The gyroscope is manufactured with a resonator made of maraging steel and piezoelectric forcers and pick-offs. In order to investigate the effects of material and manufacturing method defects in the resonator frequency split and phase shift of the resonator are measured at the desired excitation frequency and mode shape. By measuring natural frequencies of two main axes in the desired mode shape, the frequency split of the resonator is measured and the factors affecting the accuracy of measurement have also been investigated experimentally. Also, the vibration pattern of the resonator has been recorded using an acoustic wave mechanism and the phase shift of the resonator has been measured. Measurement of frequency split showed that the resonator experiences a frequency split of about 1 Hz. In addition, the use of the acoustic wave mechanism showed a good efficiency in recording the position and shape of the vibration pattern. Measurement of the phase shift with the help of the acoustic mechanism has shown the presence of a 4-degrees phase shift. Finally, in order to prove the gyroscopic phenomenon, the effect of the resonator rotation rate on the vibration wave persistence was investigated and it has shown a suitable linear approximation.

کلیدواژه‌ها [English]

  • Gyroscope
  • resonator
  • phase shift
  • frequency split
  • coriolis effect
1. Mahmoudian, M., Filho, J., Melicio, R., Rodrigues, E., Ghanbari, M. and Gordo, P., 2023. Three-dimensional performance evaluation of hemispherical coriolis vibratory gyroscopes. Micromachines, 14(2), 254. https://doi.org/10.3390/mi14020254.
2. Remillieux, G. and Delhaye, F., 2014, Sagem coriolis vibrating gyros: A vision realized. In 2014 DGON Inertial Sensors and Systems (ISS), pp. 1-13. IEEE. https://doi.org/10.1109/InertialSensors.2014.7049409.
3. Jia, J., Ding, X., Qin, Z., Ruan, Z., Li, W., Liu, X. and Li, H., 2021. Overview and analysis of MEMS Coriolis vibratory ring gyroscope. Measurement, 182, 109704. https://doi.org/10.1016/j.measurement.2021.109704.
4. Amal, A. and Davidson, R.A., 2021, March. Design and development of control electronics for coriolis vibratory gyroscopes. In 2021 IEEE Aerospace Conference, 1-10. IEEE. https://doi.org/10.1109/AERO50100.2021.9438329.
5. Xiao, P., Qiu, Z., Pan, Y., Li, S., Qu, T., Tan, Z., Liu, J., Yang, K., Zhao, W., Luo, H. and Qin, S., 2020. Influence of electrostatic forces on the vibrational characteristics of resonators for coriolis vibratory gyroscopes. Sensors20(1), 295. https://doi.org/10.3390/s20010295.
6. Hou, B., Zhu, Y., He, C., Wang, W., Ding, Z., He, W., He, Y. and Che, L., 2024. A 3D-printed microhemispherical shell resonator with electrostatic tuning for a Coriolis vibratory gyroscope. Microsystems & Nanoengineering10(1), 32. https://doi.org/10.1038/s41378-024-00659-8.
7. Apostolyuk, V., 2016. Coriolis vibratory gyroscopes. InTheory and Design. Springer. https://doi.org/10.1007/978-3-319-22198-4.
8. Delahaye, L., Guérard, J. and Parrain, F., 2017, May. Coriolis Vibrating Gyroscope Modelling for parametric identification and optimal design. In Symposium on Design, Test, Integration and Packaging of MEMS/MOEMS (DTIP) 1-5. IEEE. https://doi.org/10.1109/DTIP.2017.7984461.
9. Sung, W.T., Sung, S., Lee, J.G. and Kang, T., 2007. Design and performance test of a MEMS vibratory gyroscope with a novel AGC force rebalance control. Journal of Micromechanics and Microengineering, 17(10), 1939. https://doi.org/10.1088/0960-1317/17/10/003.
10. Vatanparvar, D. and Shkel, A.M., 2020, October. Instabilities due to electrostatic tuning of frequency-split in coriolis vibratory gyroscopes. In2020 IEEE S (pp. 1-4). IEEE. https://doi.org/1109/SENSORS47125.2020.9278845.
11. Liu, J.Y., 2024, March. Auxiliary Gyroscope Approach for Balanced Performance via Gyro Self-Calibration. In 2024 IEEE International Symposium on Inertial Sensors and Systems (INERTIAL), 1-4. https://doi.org/10.1109/INERTIAL60399.2024.10502051.
12. Loper, E.J. and Lynch, D.D., 1983. Projected system performance based on recent HRG test results (low noise inertial rotation sensor). In Digital Avionics Systems Conference, 5 th, Seattle, WA, 18.
13. Lin, Z., Fu, M., Deng, Z., Liu, N. and Liu, H., 2015. Frequency split elimination method for a solid-state vibratory angular rate gyro with an imperfect axisymmetric-shell resonator. Sensors, 15(2), pp. 3204-3223. https://doi.org/10.3390/s150203204.
14. Ma, X. and Su, Z., 2015. Analysis and compensation of mass imperfection effects on 3-D sensitive structure of bell-shaped vibratory gyro. Sensors and Actuators A: Physical, 224, pp. 14-23. https://doi.org/10.1016/j.sna.2015.01.013.
15. Zeng, K., Hu, Y., Deng, G., Sun, X., Su, W., Lu, Y. and Duan, J.A., 2017. Investigation on eigenfrequency of a cylindrical shell resonator under resonator-top trimming methods. Sensors17(9), 2011. https://doi.org/10.3390/s17092011.
16.  Xi, X., Wu, Y., Wu, X., Tao, Y. and Wu, X., 2012. Investigation on standing wave vibration of the imperfect resonant shell for cylindrical gyro. Sensors and Actuators A: Physical, 179, pp.70-77. https://doi.org/10.1016/j.sna.2012.03.031.
17. Ma, X. and Su, Z., 2015. Analysis and compensation of mass imperfection effects on 3-D sensitive structure of bell-shaped vibratory gyro. Sensors and Actuators A: Physical224, pp.14-23. https://doi.org/10.1016/j.sna.2015.01.013.