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Academic literature on the topic 'Vibrating gyroscope'

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Published: 30 May 2022
Last updated: 31 May 2022

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Journal articles on the topic "Vibrating gyroscope"

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Zhang, Nuer, Yong Feng Ren, and Sheng Kun Li. "Research on Testing Method of Dynamic Characteristic for MEMS-Gyroscope." Advanced Materials Research 346 (September 2011): 515–20. http://dx.doi.org/10.4028/www.scientific.net/amr.346.515.

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Gave a test method of the dynamic characteristics about gyroscope. In the process of using Gyroscope, it will be affected by various external factors irresistibly in making the gyroscope working at certain vibration frequency. Designed the experiments of steel plate vibrating to examine the relationship between the sensitive angular rate of gyroscope and vibration frequency. Firstly, fixed the plate on the desk; then made the plate to vibrate, collected the data from the gyroscope which vibrating with steel plate. To analyze the data of collection, gained the dynamic characteristics of gyroscope. In addition, designed rotating floor calibration experiment, calibrated the relationship between input and output of gyroscope and verified the rationality of the steel plate vibrating experiment. The result prove that gain the dynamic characteristics of gyroscope by steel plate vibrating, not only the method is simple but the result also can achieve the good precision.
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Qin, Zhengcheng, Yang Gao, Jia Jia, Xukai Ding, Libin Huang, and Hongsheng Li. "The Effect of the Anisotropy of Single Crystal Silicon on the Frequency Split of Vibrating Ring Gyroscopes." Micromachines 10, no. 2 (February 14, 2019): 126. http://dx.doi.org/10.3390/mi10020126.

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This paper analyzes the effect of the anisotropy of single crystal silicon on the frequency split of the vibrating ring gyroscope, operated in the n = 2 wineglass mode. Firstly, the elastic properties including elastic matrices and orthotropic elasticity values of (100) and (111) silicon wafers were calculated using the direction cosines of transformed coordinate systems. The (111) wafer was found to be in-plane isotropic. Then, the frequency splits of the n = 2 mode ring gyroscopes of two wafers were simulated using the calculated elastic properties. The simulation results show that the frequency split of the (100) ring gyroscope is far larger than that of the (111) ring gyroscope. Finally, experimental verifications were carried out on the micro-gyroscopes fabricated using deep dry silicon on glass technology. The experimental results are sufficiently in agreement with those of the simulation. Although the single crystal silicon is anisotropic, all the results show that compared with the (100) ring gyroscope, the frequency split of the ring gyroscope fabricated using the (111) wafer is less affected by the crystal direction, which demonstrates that the (111) wafer is more suitable for use in silicon ring gyroscopes as it is possible to get a lower frequency split.
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Tanaka, K., Y. Mochida, M. Sugimoto, K. Moriya, T. Hasegawa, K. Atsuchi, and K. Ohwada. "A micromachined vibrating gyroscope." Sensors and Actuators A: Physical 50, no. 1-2 (August 1995): 111–15. http://dx.doi.org/10.1016/0924-4247(96)80093-8.

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Kim, Chang Boo, Chong Du Cho, and Hyeon Gyu Beom. "Dynamics of a Vibrating Micro Three-Axis Ring Gyroscope." Key Engineering Materials 306-308 (March 2006): 1241–46. http://dx.doi.org/10.4028/www.scientific.net/kem.306-308.1241.

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This paper presents electro-mechanical characteristics of a micro-machined vibrating silicon ring gyroscope which can measure angular velocity components about three orthogonal axes. The ring gyroscope has a ring connected to the gyroscope main body by support ligaments that are arranged with cyclic symmetry. The natural modes of its vibration can be distinguished into the in-plane motion and the out-of-motion that are coupled by the gyro-effect due to the rotation of the gyroscope main body. The motions of the ring are electro-statically driven, sensed and balanced by electrodes. The equations of motion are formulated with considering the electrostatic effects of electrodes. The measuring method of angular velocities of the gyroscope main body by force-torebalance is proposed. The dynamic characteristics of the ring gyroscope are discussed.
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Katz, Amnon, and Alton Highsmith. "The Optimal Size of a Resonant Vibrating Beam Gyroscope." Journal of Dynamic Systems, Measurement, and Control 123, no. 1 (August 14, 2000): 49–53. http://dx.doi.org/10.1115/1.1341201.

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The level of thermal noise in a resonant vibrating beam gyroscope is lower, the longer the beam. A limitation on the length of the beam arises from the consideration that the beam acts as a mechanical bandpass filter transmitting the signal being measured (the instantaneous rate of rotation) from the drive axis to the sense axis. A longer beam vibrates at a lower frequency and has a narrower resonance. The length that is acceptable depends on the bandwidth of the time variation of angular rate, which in turn, depends on the nature and mission of the vehicle that uses the gyroscope for inertial navigation. High rates of maneuvering indicate millimeter scale gyroscopes that are realized as micro-electro-mechanical devices. In the case of General Aviation, considerations of noise, as well as cost, favor a centimeter scale device.
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Liu, Yu, Yao Yu Duan, Shen Liu, and Yi Ou. "Research of Mechanical Sensibility on Vibrating-Beam Piezoelectricity Gyroscope." Applied Mechanics and Materials 184-185 (June 2012): 402–7. http://dx.doi.org/10.4028/www.scientific.net/amm.184-185.402.

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According to sensibility and output accuracy is effected by mechanical coupling of positive and negative piezoelectricity films, analysis change of vibration beam nodes which result from coupling of positive and negative piezoelectricity films. In this paper, a new mosaic method of mechanical coupling is proposed which based on structure of the vibration beam gyroscope; the numerical calculations which result from carrying out for 60mm alloyed vibration beam illustrate the sensitivity of the Vibrating-beam Piezoelectricity Gyroscope improved 6.64%. Simulation results demonstrate sensitivity is increased 6.57% and in line with the theoretical calculations.
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Inoue, Jun-ichi. "Piezoelectric Vibrating Gyroscope and Application." HYBRIDS 8, no. 4 (1992): 35–41. http://dx.doi.org/10.5104/jiep1985.8.4_35.

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Su,, Yan, Henggao Ding,, and Shou-Rong Wang,. "Silicon Micro-Machined Vibrating Gyroscope." Journal for Manufacturing Science and Production 4, no. 4 (June 2002): 197–202. http://dx.doi.org/10.1515/ijmsp.2002.4.4.197.

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Harris, A. J., G. Cooper, J. S. Burdess, J. Cruickshank, and D. Wood. "Vibrating silicon diaphragm micromechanical gyroscope." Electronics Letters 31, no. 18 (August 31, 1995): 1567–68. http://dx.doi.org/10.1049/el:19951070.

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Niu, Shao Hua, Shi Qiao Gao, Hai Peng Liu, and Lei Jin. "An ADRC Method for Vibrating MEMS Gyrosocope Drive." Advanced Materials Research 211-212 (February 2011): 264–69. http://dx.doi.org/10.4028/www.scientific.net/amr.211-212.264.

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The stability and accuracy of the drive mode are important for the performance of vibrating MEMS gyroscope. At present, the PI-like controller is always used in the control of the drive mode of vibrating MEMS gyroscope. The PI-like control has good effect on rejecting the literal disturbance, but it can’t reject the time-dependent disturbance well. The disturbance for the MEMS gyroscope is so uncertain that the stability and accuracy of the PI-like control for the gyro are comparatively low. In this paper, an ADRC method for vibrating MEMS gyroscope drive is introduced, and it is proved that this method can rapidly and stably control the MEMS gyro drive mode by simulation and comparing with the PI-like method.
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Dissertations / Theses on the topic "Vibrating gyroscope"

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Cruickshank, Jane Laura. "A vibrating silicon diaphragm micro gyroscope." Thesis, University of Newcastle Upon Tyne, 1999. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.285737.

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Avanesian, David. "HARDWARE IMPLEMENTATION OF ACTIVE DISTURBANCE REJECTION CONTROL FOR VIBRATING BEAM GYROSCOPE." Cleveland State University / OhioLINK, 2007. http://rave.ohiolink.edu/etdc/view?acc_num=csu1200587118.

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Gallacher, Barry J. "The design, fabrication and testing of a multi-axis vibrating ring gyroscope." Thesis, University of Newcastle Upon Tyne, 2002. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.413139.

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Tydor, Maximilián. "Univerzální senzorová testovací platforma." Master's thesis, Vysoké učení technické v Brně. Fakulta elektrotechniky a komunikačních technologií, 2015. http://www.nusl.cz/ntk/nusl-221234.

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This document deals with issues of testing semiconductor inertial sensors like gyroscopes and accelerometers, but also other sensors like magnetometers, inclinometers and others for aviation navigation purposes where strict requirements cover every system. The goal of this thesis is to create modular test platform for testing wide variety of sensors in different combinations under variable circumstances. The development covers mechanical design, electrical design – hardware and also control algorithm – software.
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Zaman, Mohammad Faisal. "Degree-per-hour mode-matched micromachined silicon vibratory gyroscopes." Diss., Atlanta, Ga. : Georgia Institute of Technology, 2008. http://hdl.handle.net/1853/28168.

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Thesis (M. S.)--Electrical and Computer Engineering, Georgia Institute of Technology, 2008.
Committee Chair: Dr. Farrokh Ayazi; Committee Member: Dr. Mark G. Allen; Committee Member: Dr. Oliver Brand; Committee Member: Dr. Paul A. Kohl; Committee Member: Dr. Thomas E. Michaels.
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Spelsberg-Korspeter, Gottfried [Verfasser]. "Self-excited vibrations in gyroscopic systems / Gottfried Spelsberg-Korspeter." Aachen : Shaker, 2007. http://d-nb.info/1164340719/34.

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White, Robert D. (Robert David) 1976. "Effects of impact and vibration on the performance of a micromachined tuning fork gyroscope." Thesis, Massachusetts Institute of Technology, 1999. http://hdl.handle.net/1721.1/16723.

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Thesis (S.B. and S.M.)--Massachusetts Institute of Technology, Dept. of Mechanical Engineering, 1999.
Includes bibliographical references (p. 188).
This electronic version was submitted by the student author. The certified thesis is available in the Institute Archives and Special Collections.
by Robert D. White.
S.B.and S.M.
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Gavrilovic, Nenad. "VIBRATION-BASED HEALTH MONITORING OF ROTATING SYSTEMS WITH GYROSCOPIC EFFECT." DigitalCommons@CalPoly, 2015. https://digitalcommons.calpoly.edu/theses/1358.

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This thesis focuses on the simulation of the gyroscopic effect using the software MSC Adams. A simple shaft-disk system was created and parameter of the sys-tem were changed in order to study the influence of the gyroscopic effect. It was shown that an increasing bearing stiffness reduces the precession motion. Fur-thermore, it was shown that the gyroscopic effect vanishes if the disk of system is placed symmetrically on the shaft, which reduces the system to a Jeffcott-Ro-tor. The second objective of this study was to analyze different defects in a simple fixed axis gear set. In particular, a cracked shaft, a cracked pinion and a chipped pinion as well as a healthy gear system were created and tested in Adams. The contact force between the two gears was monitored and the 2D and 3D frequency spectrum, as well as the Wavelet Transform, were plotted in order to compare the individual defects. It was shown that the Wavelet Transform is a powerful tool, capable of identifying a cracked gear with a non-constant speed. The last part of this study included fault detection with statistical methods as well as with the Sideband Energy Ratio (SER). The time domain signal of the individual faults were used to compare the mean, the standard deviation and the root mean square. Furthermore, the noise profile in the frequency spectrum was tracked with statistical methods using the mean and the standard deviation. It was demonstrated that it is possible to identify a cracked gear, as well as a chipped gear, with statistical methods. However, a cracked shaft could not be identified. The results also show that SER was only capable to identify major defects in a gear system such as a chipped tooth.
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Ling-Fang, Yao. "Design and analysis of a resonant gyroscope suitable for fabricaton using the LIGA process." Thesis, De Montfort University, 1997. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.391334.

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Петренко, Олексій Володимирович. "Удосконалення методів підвищення точності вібраційного гіроскопа з металевим циліндричним резонатором." Thesis, КПІ ім. Ігоря Сікорського, 2020. https://ela.kpi.ua/handle/123456789/36992.

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Робота виконана на кафедрі аерокосмічних систем управління Національного авіаційного університету Міністерства освіти і науки України та у Публічному акціонерному товаристві «Науково-виробниче об’єднання «Київський завод автоматики».
Дисертаційна робота присвячена науковому обґрунтуванню та розробці алгоритмів компенсації внутрішніх похибок та зовнішніх збурень у Коріолісовому вібраційному гіроскопі, а також удосконаленню його складових частин (резонатора, чутливого елементу). Автором розроблено методику та обладнання для робочого місця безелектродного вимірювання динамічних параметрів металевого резонатора після його виготовлення, розроблено конструкцію приладдя для приклеювання п’єзоелектродів до резонатора нової конструкції, методику та обладнання робочого місця для балансування мас. Розроблено та відпрацьовано на експериментальному зразку КВГ методики температурної корекції фаз сигналів квадратури та кутової швидкості, багатопараметричної корекції дрейфу нуля і масштабного коефіцієнту, що призводить до збільшення точності виміру кутової швидкості в умовах дії температурних градієнтів.
In the thesis the following new scientific results are obtained: 1. For the first time, a multi-parameter method of CVG scale factor correction is developed and implemented, which can be used during the CVG operation in the rate and in the differential modes. Ukraine patent have been obtained for this method. 2. Scientifically grounded analysis of a new design of a cylindrical resonator with holes on the walls of a cylinder having higher vibration resistance was first developed and carried out. 3. The multiparameter bias correction algorithm has been developed and implemented, which has advantages over the existing ones by accuracy. 4. For the first time experimental researches were carried out on a manufactured experimental sample of CVG with developed metal cylindrical resonator made of elenvar elloy, which showed high accuracy scale factor and bias drift correction under the action of temperature gradient, as well as high shockvibration resistance of the sample. The practical significance of thesis results are: − comparison of two designs of metallic cylindrical resonators with holes on the bottom and on the wall of the cylinder and by calculations and computer simulation the advantages of the second design over the first one in the part of shock resistance have been substantiated; − аn analysis of the different geometries of the holes has been made. Their influence on the resonant oscillation frequencies of a cylindrical resonator is revealed. Recommendations for the geometry of the resonator and its elements have been developed; − improved design of the base on which the newly designed resonator with holes on the wall of the cylinder is installed; − the choice of electrodes used for oscillation excitation and measurement of the signals is experimentally substantiated; − the technique and equipment for workplace electrodeless measurement of metallic resonator dynamic parameters after its manufacture have been developed; − the influence of frequency mismatch, wave angle and positioning errors of the electrodes on the CVG bias and scale coefficient have been evaluated; − a new accessory design has been developed to attach the electrodes to the new resonator design; − the technique and equipment of the workplace for balancing the mass of the resonator on the fourth harmonic of the unbalance to reduce its frequency mismatch have been developed. The technique was tested in the manufactured ample of CVG; − the technique of measuring the angles of non-orthogonality of the sensitive axis to its mounting surface has been developed and implemented in the experimental sample of CVG; − the use of CVG to improve the accuracy of armament stabilization was analyzed; − improved CVG standing wave control algorithm block diagram, which provides a fast start of the gyroscope when it is turned on at any temperature in the range of operating temperatures; − the techniques for temperature correction of quadrature and angular rate phases, multiparameter correction of CVG bias and scale factor have been developed and tested on experimental sample of CVG, which leads to an increase in the accuracy of measuring angular rate under temperature gradients; − the experimental results showed that the CVG with a metallic resonator is resistant to multiple shocks with amplitude 100 g and its bias is slightly dependent on the shock amplitude and does not exceed 5×10−3 deg/s. The bias sensitivity to vibration perturbations is 2.5×10−3 deg/s/g.
Диссертация посвящена научному обоснованию и разработке алгоритмов компенсации внутренних погрешностей и внешних возмущений в Кориолисового вибрационном гироскопе, а также совершенствованию его составных частей (резонатора, чувствительного элемента). Автором разработана методика и оборудование для рабочего места безэлектродного измерения динамических параметров металлического резонатора после его изготовления, разработана конструкция приспособления для приклеивания пьезоэлектродов к резонатору новой конструкции, методику и оборудование рабочего места для балансировки масс резонатора. Разработано и отработано на экспериментальном образце КВГ методики температурной коррекции фаз сигналов квадратуры и угловой скорости, многопараметрической коррекции дрейфа нуля и масштабного коэффициента, что приводит к увеличению точности измерения угловой скорости в условиях действия температурных градиентов.
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Books on the topic "Vibrating gyroscope"

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Kim, A. A. Boris Vladimirovich Bulgakov, 1900-1952. Moskva: "Nauka", 2000.

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Shubin, I. K. Dinamika dvukhrezhimnykh kursoukazateleĭ pri vibroudarnykh peregruzkakh. Leningrad: Izd-vo Leningradskogo universiteta, 1986.

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Ishida, Yukio, Christophe Pierre, ali ashrafizade, Anil Bajaj, Noel Perkins, and Gabriele D'Eleuterio. Stability of Gyroscopic Systems (Series on Stability, Vibration and Control of Structures , Vol 8). World Scientific Publishing Company, 1996.

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Shi, Jian-Feng. Embedded system software development for a single-gimbaled control moment gyroscope and the vibration damping of a clamped-free cantilevered beam. 2004.

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Book chapters on the topic "Vibrating gyroscope"

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Gopala Krishnamurthy, M., D. Dinakar, I. M. Chhabra, P. Kishore, N. V. N. Rao Pasalapudi, and K. C. Das. "Frequency Measurement of Resonator for Vibrating Gyroscope." In Engineering Vibration, Communication and Information Processing, 311–16. Singapore: Springer Singapore, 2018. http://dx.doi.org/10.1007/978-981-13-1642-5_28.

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Kim, Chang Boo, Chong Du Cho, and Hyeon Gyu Beom. "Dynamics of a Vibrating Micro Three-Axis Ring Gyroscope." In Fracture and Strength of Solids VI, 1241–46. Stafa: Trans Tech Publications Ltd., 2006. http://dx.doi.org/10.4028/0-87849-989-x.1241.

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Rapoport, Ilia, and Daniel Choukroun. "Investigation of a Symmetric Vibrating Gyroscope Characteristics Using a Simplified Dynamic Model." In Advances in Estimation, Navigation, and Spacecraft Control, 329–48. Berlin, Heidelberg: Springer Berlin Heidelberg, 2015. http://dx.doi.org/10.1007/978-3-662-44785-7_18.

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Qiu, A. P., Y. Su, S. R. Wang, and B. L. Zhou. "Effect of Residual Stresses on a Micromachined Z-Axis Vibrating Rate Gyroscope." In Key Engineering Materials, 101–6. Stafa: Trans Tech Publications Ltd., 2005. http://dx.doi.org/10.4028/0-87849-977-6.101.

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Lawrence, Anthony. "Vibrating Gyroscopes." In Modern Inertial Technology, 148–62. New York, NY: Springer US, 1993. http://dx.doi.org/10.1007/978-1-4684-0444-9_11.

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Lawrence, Anthony. "Vibrating Gyroscopes." In Mechanical Engineering Series, 152–68. New York, NY: Springer New York, 1998. http://dx.doi.org/10.1007/978-1-4612-1734-3_11.

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Billingsley, John. "Gyroscopes." In Essentials of Dynamics and Vibrations, 69–73. Cham: Springer International Publishing, 2017. http://dx.doi.org/10.1007/978-3-319-56517-0_7.

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Chang, Chia-Ou, and Chan-Shin Chou. "Vibration of Resonant Gyroscopes." In IUTAM Symposium on Vibration Control of Nonlinear Mechanisms and Structures, 131–40. Dordrecht: Springer Netherlands, 2005. http://dx.doi.org/10.1007/1-4020-4161-6_11.

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Matsushita, Osami, Masato Tanaka, Hiroshi Kanki, Masao Kobayashi, and Patrick Keogh. "Gyroscopic Effect on Rotor Vibrations." In Vibrations of Rotating Machinery, 153–80. Tokyo: Springer Japan, 2017. http://dx.doi.org/10.1007/978-4-431-55456-1_6.

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Lee, Chong-Won. "Gyroscopic Whirling of a Simple Rotor." In Vibration Analysis of Rotors, 57–98. Dordrecht: Springer Netherlands, 1993. http://dx.doi.org/10.1007/978-94-015-8173-8_2.

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Conference papers on the topic "Vibrating gyroscope"

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Ansari, Masoud, Ebrahim Esmailzadeh, and Nader Jalili. "On Coupled Flexural and Torsional Oscillations of a Vibrating Beam Gyroscopic System." In ASME 2009 Dynamic Systems and Control Conference. ASMEDC, 2009. http://dx.doi.org/10.1115/dscc2009-2630.

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Gyroscopes are commonly used to measure the angle of rotation and its rate of change in several critical systems like airplanes. Therefore, there is a never-ending desire for researchers to increase measurement precision of these devices. In order to achieve this goal, some new gyroscopes have been invented recently. Especially, advent of micro manufacturing has appeared some sophisticated to more pre´cised gyroscopic systems. The widely-used gyroscopes are vibrating beam gyroscopes; however they face a very important drawback, called cross-coupling error. In presence of the secondary base rotations, significant errors will be produced in measurement of the gyroscope output. In order to deal with this issue, this paper addresses a novel gyroscopic system, called rocking-mass gyroscope. It is consist of four beams attached to a rigid substrate, undergoing coupled flexural and torsional vibrations with a finite mass attached in the middle. This configuration is such that, it does not encounter the same problems as vibrating beam gyroscopes. This configuration makes the vibration analysis very complicated. Despite this fact, a thorough analysis is performed in this paper. Using Extended Hamilton’s principle, eight governing partial differential equations of motion along with their corresponding boundary conditions are derived. Further attempt is made to find the closed-form frequency equation of the system. Solving this equation needs high computational costs and gives the natural frequencies of the system. In spite of this fact, the system is analysed in the frequency domain using an exact method in full detail, for two cases of fixed and rotating base support. Furthermore, a detailed parameter sensitivity analysis is carried out to determine the effects of different parameters on the natural frequencies of the system. The contributions of this research are very important from two viewpoints. Firstly, determination of natural frequencies and resonance conditions are essential for design of the system, and design of appropriate control strategies. Secondly, frequency domain analysis forms the basis of time domain analysis, followed by exact mode superposition method.
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Bhadbhade, Vikrant, and Nader Jalili. "Coupled Flexural/Torsional Vibrations of a Piezoelectrically-Actuated Vibrating Beam Gyroscope." In ASME 2006 International Mechanical Engineering Congress and Exposition. ASMEDC, 2006. http://dx.doi.org/10.1115/imece2006-16049.

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In this paper, the coupled flexural-torsional vibrations of a cantilever beam with rigid mass attached to its end are studied. The beam base is subjected to a rotational motion, forming a vibrating beam gyroscope undergoing bending-twisting vibrations. The primary (flexural) vibrations are produced in the beam using a piezoelectric patch actuator. Due to the gyroscopic effect, secondary (torsional) vibrations are induced in the beam. First, a detailed mathematical modeling of the system is developed using extended Hamilton's Principle. Partial differential equations of the motion for both bending and torsion vibrations are derived, which are coupled through the gyroscopic terms. Expression for the frequency equation is presented, and the effect of the base rotation on the system natural frequencies is studied. Finally, the system governing equations are solved and simulated using assumed mode model to analyze the relationship between the base rotation and gyroscopic coupling. It is shown that the system natural frequencies are nearly independent of the magnitude of the base rotation for small rotation velocities. Furthermore, the natural frequencies depend on the magnitude as well as dimensions of the end mass. Also, it is shown that the gyroscopic effect increases with increase in base rotation rate and primary excitation amplitude.
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Putty, M. W., and K. Najafi. "A MICROMACHINED VIBRATING RING GYROSCOPE." In 1994 Solid-State, Actuators, and Microsystems Workshop. San Diego, CA USA: Transducer Research Foundation, Inc., 1994. http://dx.doi.org/10.31438/trf.hh1994.49.

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Putty, M. W., and K. Najafi. "A MICROMACHINED VIBRATING RING GYROSCOPE." In 1994 Solid-State, Actuators, and Microsystems Workshop. San Diego, CA USA: Transducer Research Foundation, Inc., 1994. http://dx.doi.org/10.31438/trf.hh1994.49.

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Qin, Z., X. Ding, J. Jia, and H. Li. "Vibration model of mode order optimized vibrating ring gyroscope." In 2021 DGON Inertial Sensors and Systems (ISS). IEEE, 2021. http://dx.doi.org/10.1109/iss52949.2021.9619807.

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Kirnos, Vasilii, Aleksander Vagachev, and Oleg Morozov. "Micro-machined Vibrating Ring Gyroscope Testing." In 2020 26th Conference of Open Innovations Association (FRUCT). IEEE, 2020. http://dx.doi.org/10.23919/fruct48808.2020.9087387.

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Zhang, Rong, Zhongyu Gao, and Zhiyong Chen. "Bulk micromachined vibrating wheel rate gyroscope." In International Symposium on Optoelectonics and Microelectronics, edited by Norman C. Tien and Qing-An Huang. SPIE, 2001. http://dx.doi.org/10.1117/12.444747.

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Wang, Qingyi, Weiping Chen, Liang Yin, Xiaowei Liu, and Zhiping Zhou. "Equivalent electrical model for quartz vibrating gyroscope." In 2012 International Conference on Optoelectronics and Microelectronics (ICOM). IEEE, 2012. http://dx.doi.org/10.1109/icoom.2012.6316325.

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Zhao, Q. C., X. S. Liu, L. T. Lin, Z. Y. Guo, J. Cui, X. Z. Chi, Z. C. Yang, and G. Z. Yan. "A doubly decoupled micromachined vibrating wheel gyroscope." In TRANSDUCERS 2009 - 2009 International Solid-State Sensors, Actuators and Microsystems Conference. IEEE, 2009. http://dx.doi.org/10.1109/sensor.2009.5285504.

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Khasawneh, Q., and C. Batur. "Design and control of a vibrating gyroscope." In Proceedings of the 2004 American Control Conference. IEEE, 2004. http://dx.doi.org/10.23919/acc.2004.1383841.

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