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Journal articles on the topic 'Dynamically tuned gyroscope'

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Author: Grafiati

Published: 30 May 2022

Last updated: 31 May 2022

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1

Podchezertsev, V. P., and D. Z. Nguyen. "Issues of Synthesis and Practical Evaluation of the Compensation Mode Error of a Two-Component Gyroscope." Proceedings of Higher Educational Institutions. Маchine Building, no. 9 (738) (September 2021): 108–16. http://dx.doi.org/10.18698/0536-1044-2021-9-108-116.

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The paper introduces the results of studying the characteristics of various dynamically tuned gyroscopes operating in the mode of a variable rate sensor. Within the study, we determined the dependence of the dynamic error of the rate sensor on the amplitude and frequency of angular oscillations of the gyroscope body. We analyzed the methodological and hardware support for evaluating the dynamic error of a dynamically tuned gyroscope — the rate sensor in order to reduce its influence on the operational characteristics of the device. To experimentally research and practically evaluate the dynamic error of the dynamically tuned gyroscope — the rate sensor, we proposed a design of the rotary vibration test bench, developed requirements for it, and calculated its elastic-mass characteristics.

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2

ZHAO Jian-yuan, 赵建远, 李醒飞 LI Xing-fei, and 田凌子 TIAN Ling-zi. "Subspace identification for dynamically tuned gyroscope." Optics and Precision Engineering 23, no. 2 (2015): 423–29. http://dx.doi.org/10.3788/ope.20152302.0423.

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3

Cain, Jeffrey S., Douglas A. Staley, Glenn R. Heppler, and John McPhee. "Stability Analysis of a Dynamically Tuned Gyroscope." Journal of Guidance, Control, and Dynamics 29, no. 4 (July 2006): 965–69. http://dx.doi.org/10.2514/1.17232.

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4

Qin, Zhong Bao, Guang Bin Liu, Jian Feng Guo, and Xiao Long Hu. "Modal Analysis of Dynamically Tuned Gyroscope Based on ANSYS11.0." Applied Mechanics and Materials 152-154 (January 2012): 1183–86. http://dx.doi.org/10.4028/www.scientific.net/amm.152-154.1183.

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This paper proposed a method to analyses and obtain the vibration identities of DTG(Dynamically Tuned Gyroscope) within the vibration-overloading environment based on ANSYS11.0. Finite element model of DTG was constructed by ANSYS11.0. The Natural Frequencies and vibration modals of DTG in the cases of both being stationary and rotating were studied respectively through the method of modal analysis. The influence of each-rank vibration model of DTG on its output was investigated. The result of this paper provides a stable basis for improving the design of DTG and enhancing the functions of it.

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5

Bafghi, Mohammadhossein Barzegari, Abolfazl Vahedi, and Javad Soleimani. "Optimized Design of PM Torquer for Dynamically Tuned Gyroscope." IEEE Transactions on Industry Applications 48, no. 6 (November 2012): 2268–76. http://dx.doi.org/10.1109/tia.2012.2226923.

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6

Xia, Dunzhu, Cheng Yu, and Lun Kong. "A Micro Dynamically Tuned Gyroscope with Adjustable Static Capacitance." Sensors 13, no. 2 (February 6, 2013): 2176–95. http://dx.doi.org/10.3390/s130202176.

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7

Sharova, M. A., and S. S. Diadin. "Allan variance in dynamically tuned inertial-unit gyro error analysis." Journal of «Almaz – Antey» Air and Space Defence Corporation, no. 3 (September 30, 2019): 69–77. http://dx.doi.org/10.38013/2542-0542-2019-3-69-77.

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The purpose of the study was to consider an algorithm for obtaining the measurement information from a dynamically tuned gyroscope in the mode of an angular velocity sensor and output signal noise component estimate, the algorithm being based on the Allan variance method. The results obtained were evaluated

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8

Xu, Guoping, Weifeng Tian, and Zhihua Jin. "An AGO–SVM drift modelling method for a dynamically tuned gyroscope." Measurement Science and Technology 17, no. 1 (December 15, 2005): 161–67. http://dx.doi.org/10.1088/0957-0233/17/1/026.

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9

Kang, Taesam, Jang Gyu Lee, and Chan Gook Park. "Performance improvement of a dynamically tuned gyroscope using an input compensator." Journal of Guidance, Control, and Dynamics 15, no. 2 (March 1992): 404–9. http://dx.doi.org/10.2514/3.20850.

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10

Malyutin, D. M. "THE STABILIZATION SYSTEM ON PAYLOAD BUILT ON A DYNAMICALLY TUNED GYROSCOPE." Devices and Methods of Measurements 7, no. 1 (June 6, 2016): 32–40. http://dx.doi.org/10.21122/2220-9506-2016-7-1-32-40.

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11

Woo Song, Jin, Jang Gyu Lee, and Taesam Kang. "Digital rebalance loop design for a dynamically tuned gyroscope using H2 methodology." Control Engineering Practice 10, no. 10 (October 2002): 1127–40. http://dx.doi.org/10.1016/s0967-0661(02)00079-5.

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12

Poletkin, Kirill V., Alexsandr I. Chernomorsky, and Christopher Shearwood. "Proposal for a Micromachined Dynamically Tuned Gyroscope, Based on a Contactless Suspension." IEEE Sensors Journal 12, no. 6 (June 2012): 2164–71. http://dx.doi.org/10.1109/jsen.2011.2178020.

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13

Xia, Dunzhu, Peizhen Ni, and Lun Kong. "A Digitized Decoupled Dual-axis Micro Dynamically Tuned Gyroscope with Three Equilibrium Rings." Journal of Electrical Engineering and Technology 12, no. 1 (January 2, 2017): 385–95. http://dx.doi.org/10.5370/jeet.2017.12.1.385.

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14

Fu, Li, Xi Yang, and Ling Ling Wang. "A novel calibration procedure for dynamically tuned gyroscope designed by D-optimal approach." Measurement 46, no. 9 (November 2013): 3173–80. http://dx.doi.org/10.1016/j.measurement.2013.05.026.

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15

Lee, S.-K., and C.-W. Lee. "Errors of the dynamically tuned strapdown gyroscope to constant and harmonic rate inputs." Proceedings of the Institution of Mechanical Engineers, Part C: Journal of Mechanical Engineering Science 211, no. 8 (August 1, 1997): 627–37. http://dx.doi.org/10.1243/0954406981522005.

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The drift errors for constant and harmonic rotational rate inputs are derived for the dynamically tuned strapdown gyroscope with a single gimbal and orthogonally placed double gimbals. To account for the recent design tendencies of higher rate input, higher acceleration capability and smaller size, the analytic expressions for the drift errors, which include the influences of gimbal moments of inertia, asymmetries of flexure stiffnesses and rotor moments of inertia, and higher order terms related to misalignments, are presented. The drift errors are classified according to the sources and the characteristics of each error are investigated. The compensation and design to develop a more accurate sensor by reducing the drift errors are also discussed.

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16

M, Arif Sanjid, Raghunandan Prasad S, Andhra Thejam A, and Shalini G. "A novel method to measure the decay frequency of a dynamically tuned gyroscope flexure." Measurement Science and Technology 14, no. 12 (October 6, 2003): 2081–88. http://dx.doi.org/10.1088/0957-0233/14/12/006.

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17

Qian, Li, Guoping Xu, Weifeng Tian, and Junpu Wang. "A novel hybrid EMD-based drift denoising method for a dynamically tuned gyroscope (DTG)." Measurement 42, no. 6 (July 2009): 927–32. http://dx.doi.org/10.1016/j.measurement.2009.01.017.

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18

Xu, Guoping, Weifeng Tian, and Li Qian. "EMD- and SVM-based temperature drift modeling and compensation for a dynamically tuned gyroscope (DTG)." Mechanical Systems and Signal Processing 21, no. 8 (November 2007): 3182–88. http://dx.doi.org/10.1016/j.ymssp.2007.05.006.

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19

Xu, Guoping, Weifeng Tian, Zhihua Jin, and Li Qian. "Temperature drift modelling and compensation for a dynamically tuned gyroscope by combining WT and SVM method." Measurement Science and Technology 18, no. 5 (March 20, 2007): 1425–32. http://dx.doi.org/10.1088/0957-0233/18/5/030.

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20

Fan, Chunling, Zhihua Jin, and Weifeng Tian. "A novel hybrid grey-based strategy for improving the model precision of a dynamically tuned gyroscope." Measurement Science and Technology 14, no. 6 (April 24, 2003): 759–65. http://dx.doi.org/10.1088/0957-0233/14/6/308.

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21

Li, Jian Rong, Cheng Wu Shen, and Shao Jin Liu. "Research on High Precision Temperature Control System of Strap-Down North-Seeking." Applied Mechanics and Materials 740 (March 2015): 269–73. http://dx.doi.org/10.4028/www.scientific.net/amm.740.269.

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In order to make the dynamically tuned gyroscope of Strap-down North-seeking working on the best temperature environment, reduce errors caused by temperature changes, a high-precision temperature control system is built up on the base of control theory and engineering. This system is a two-stage temperature control system. In order to realize high precision temperature control at a predetermined temperature range, temperature measurement circuit is analyzed and calculated on a two-stage temperature control had different measurement circuit match. Experimental results show that the accuracy of can achieve ± 0.1 °Cwhen the environment temperature within the range of-40 °C ~ + 60 °C. It can meet the temperature requirements of Strap-down North-seeking system.

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22

Belyanin, Lev, and Doan Ket Vu. "Nutation damping of dynamically tuned gyroscopes." MATEC Web of Conferences 102 (2017): 01008. http://dx.doi.org/10.1051/matecconf/201710201008.

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23

Kablov, E. N., O. G. Ospennikova, V. P. Piskorskiy, R. A. Valeyev, I. I. Rezchikova, and A. V. Buzenkov. "Ring magnets with radial texture for dynamically tuned gyroscopes." «Aviation Materials and Technologies», s5 (2014): 89–94. http://dx.doi.org/10.18577/2071-9140-2014-0-s5-89-94.

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24

FU, Li, Yongquan ZHU, Lingling WANG, and Xinling WANG. "A D-optimal Multi-position Calibration Method for Dynamically Tuned Gyroscopes." Chinese Journal of Aeronautics 24, no. 2 (April 2011): 210–18. http://dx.doi.org/10.1016/s1000-9361(11)60025-3.

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25

Nikolov, Svetoslav, and Nataliya Nedkova. "Gyrostat Model Regular And Chaotic Behavior." Journal of Theoretical and Applied Mechanics 45, no. 4 (December 1, 2015): 15–30. http://dx.doi.org/10.1515/jtam-2015-0021.

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AbstractDuring recent years, the interest in the phenomena of chaos in gyroscopic systems has been increasing. It is well-known, that depending on the speed of rotation, a gyroscopic system may lose or gain stability. Despite the overwhelming number of studies reporting the occurrence of various chaotic structures, little is known yet about the construction details and the generality of the underlying bifurcation scenarios that give rise to such chaotic (complex) behaviour.In this paper, we report a detailed investigation of the abundance of regular and chaotic behaviour for rigid body (gyrostat) motion. The model contains 6 parameters that may be tuned to produce rich dynamical scenarios. The results confirm that homoclinic and heteroclinic structures with two fixed points from saddle-focus type occur and the emergence of Shilnikov chaos takes place. Finally, we find new results concerning the system’s evolution and bifurcation scenarios for its routes to chaos.

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26

"Choice of configuration and parameters of the vibration protection system for gyroscopic angular velocity meters." Automation. Modern Techologies, 2021. http://dx.doi.org/10.36652/0869-4931-2021-75-4-187-192.

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The rationale for the choice of a technical solution to the issue of vibration protection of gyroscopic angular velocity meters, built on the basis of dynamically tuned gyroscopes (DTG) is presented. The proposed vibration protection system consists of shock absorbers with high elasticity and dynamic vibration dampers (DVD) with nonlinear elastic and damping characteristics. The main factors that determine the peculiarities of choosing a vibration protection system for precision gyroscopic devices are indicated. Keywords dynamically tuned gyroscope (DTG); dynamic vibration damper (DVD); vibration protection system; gyroscopic angular velocity meter

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27

Sushchenko, O. A., and Y. V. Beliavtsev. "MATHEMATICAL MODEL OF DYNAMICALLY TUNED GYROSCOPE." Electronics and Control Systems 1, no. 51 (July 5, 2017). http://dx.doi.org/10.18372/1990-5548.51.11705.

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28

Nikandrov, Vladimir. "Mathematical model of a dynamically tuned gyroscope." Science and Education of the Bauman MSTU 13, no. 04 (April 3, 2013). http://dx.doi.org/10.7463/0413.0550951.

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29

Цинь, Цзыхао, and В. П. Подчезерцев. "Influence of Design Features and Gas Filling Parameters on Dynamically Tuned Gyroscope Characteristics." Herald of the Bauman Moscow State Technical University. Series Instrument Engineering, no. 93 (April 2017). http://dx.doi.org/10.18698/0236-3933-2017-2-4-20.

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30

Синюань, Т., and В. П. Подчезерцев. "Algorithms of dynamically tuned gyroscope certification under conditions of real-world orientation relative to the geographic coordinate system." Engineering Journal: Science and Innovation, no. 71 (September 2017). http://dx.doi.org/10.18698/2308-6033-2017-10-1691.

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31

Дубинин, А. В., and К. В. Смолян. "Dependence of Load Carrying Capacity of Gas-Dynamic Support of Dynamically Tuned Gyroscope upon Gaps in Gas-Dynamic Support." Engineering Journal: Science and Innovation, no. 3 (November 2012). http://dx.doi.org/10.18698/2308-6033-2012-3-117.

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32

Zhou, Xin, Chun Zhao, Dingbang Xiao, Jiangkun Sun, Guillermo Sobreviela, Dustin D. Gerrard, Yunhan Chen, et al. "Dynamic modulation of modal coupling in microelectromechanical gyroscopic ring resonators." Nature Communications 10, no. 1 (October 31, 2019). http://dx.doi.org/10.1038/s41467-019-12796-0.

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Abstract Understanding and controlling modal coupling in micro/nanomechanical devices is integral to the design of high-accuracy timing references and inertial sensors. However, insight into specific physical mechanisms underlying modal coupling, and the ability to tune such interactions is limited. Here, we demonstrate that tuneable mode coupling can be achieved in capacitive microelectromechanical devices with dynamic electrostatic fields enabling strong coupling between otherwise uncoupled modes. A vacuum-sealed microelectromechanical silicon ring resonator is employed in this work, with relevance to the gyroscopic lateral modes of vibration. It is shown that a parametric pumping scheme can be implemented through capacitive electrodes surrounding the device that allows for the mode coupling strength to be dynamically tuned, as well as allowing greater flexibility in the control of the coupling stiffness. Electrostatic pump based sideband coupling is demonstrated, and compared to conventional strain-mediated sideband operations. Electrostatic coupling is shown to be very efficient, enabling strong, tunable dynamical coupling.

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33

Lingling, Liu, Ma Ruonan, and Omid Koochakianfard. "Size-dependent vibrational behavior of embedded spinning tubes under gravitational load in hygro-thermo-magnetic fields." Proceedings of the Institution of Mechanical Engineers, Part C: Journal of Mechanical Engineering Science, January 27, 2022, 095440622110687. http://dx.doi.org/10.1177/09544062211068730.

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In the present investigation, with the aim of performance improvement of size-dependent bi-gyroscopic structures, the vibrational behavior of spinning small-scale tunes conveying fluid embedded in various foundations subjected to distributed tangential load and hygro-thermo-magnetic environments by including gravitational effect is investigated. The modified couple stress theory is used to study the microscale tube, and the modified nonlocal theory is utilized to model the nanoscale tubes. A parametric investigation is also conducted to highlight the impacts of various key factors such as gravity, flow profile modification factor, fluid velocity, spinning speed, substrate coefficients, boundary conditions, size-dependent parameters, and environmental attacks on divergence and flutter thresholds of the structure. The dynamical equations are solved using Laplace transformation as well as Galerkin discretization techniques, and forward and backward frequencies are identified accordingly. Meanwhile, the instability borders of the system are obtained analytically. Campbell and stability diagrams, and the time history of the system, are acquired. The results revealed that contrary to influences of gravity, magnetization, and size-dependent parameters, the compressive tangential load and humidity have decreasing effects on the vibrational frequencies and make the system prone to experience static and dynamical instabilities. Moreover, it is determined that applying the viscous foundation eliminates the re-stabilization zone in the system stability evolution, and after the occurrence of the divergence phenomenon, the system immediately undergoes the flutter instability.

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