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Добірка наукової літератури з теми "Dynamically tuned gyroscope"

Автор: Grafiati
Опубліковано: 30 травня 2022
Оновлено: 31 травня 2022

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Статті в журналах з теми "Dynamically tuned gyroscope"

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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Дисертації з теми "Dynamically tuned gyroscope"

1

Maitland, J. K. "Investigation of the behaviour of a dynamically tuned gyroscope with a view of controller design." Thesis, University of Hertfordshire, 1986. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.384082.

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The strapdown dynamically tuned gyroscope (DTG) is a candidate for use as the angular motion sensor in s'trapdown inertial navigation systems and autopilots. However, the dynamic performance of the strapdown DTG is one of the limiting factors restricting usage of the instrument in these systems. This research project considers control strategies to enhance the strapdown DTG performance. The DTG equations of motion are derived, with damping terms, and angular speed components introduced about the spin axis. The DTG equations of motion are solved numerically using a 4th order Runge-Kutta method, and taking advantage of rotating reference frames to eliminate time varying elements in the system matrix. This approach reduces the number of computations per time step and improves numerical stability. The tuning conditions for a multigimbal DTG are derived. A modal analysis is carried out on the DTG system matrix for different tuning conditions. This work provides the basis for the reduction of the DTG equations of motion to a free rotor gyroscope form. A parameter estimation procedure is designed which reflects the sensitivity of the DTG dynamic characteristics to certain parameters. A comprehensive experimental programme is carried out to validate the DTG mathematical model and estimate the numerical value of critical DTG parameters. A control strategy which processes the torquer and demodulator signals of the strapdown DTG is formulated. This strategy, used on the strapdown DTG, improves the diagonal dominance of the system transfer function matrix. Throughout the bandwidth the amplitude of the nutation response is at least 20 dB down on the amplitude of the precession response, compared with only 6 dB down on an uncompensated strapdown DTG. The compensator-strap down DTG system bandwidth is extended, compared to the strapdown DTG. The increase in bandwidth and improvement in system diagonal dominance depends on the precise form of the compensator and the manner of implementation; analogue, digital or hybrid. The compensator is feed-forward and can therefore be integrated into a system without altering the strapdown loops. The flexibility of the strategy enables the system designer to balance conflicting requirements of performance allied with minimal, cost, hardware and processing increases. An analogue and hybrid version of the compensator has been added to a strapdown DTG with subsequent test results in close agreement with theoretical studies. The control strategy has potential applications wherever strapdown DTG's are used.
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2

Cain, Jeffrey S. "Investigation of the crossed flexure pivot and the dynamics of the momentum management system spacecraft control component and the dynamically tuned gyroscope." Thesis, National Library of Canada = Bibliothèque nationale du Canada, 1999. http://www.collectionscanada.ca/obj/s4/f2/dsk1/tape8/PQDD_0003/NQ42788.pdf.

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3

Cain, Jeffrey S. (Jeffrey Stuart) Carleton University Dissertation Engineering Mechanical and Aerospace. "Investigation of the crossed flexure pivot and the dynamics of the momentum management system, spacecraft control component and the dynamically tuned gyroscope." Ottawa, 1999.

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4

Wilson, Sarah Louise. "The vibrational response of dynamically-tuned gyroscopes using a new analytical model." Thesis, University of Cambridge, 1993. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.307104.

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5

Балабанова, Татьяна Васильевна. "Динамика и погрешности двухрамочного динамически настраиваемого гироскопа с одноколечной схемой сборки при ускорениях основания". Doctoral thesis, 2011. https://ela.kpi.ua/handle/123456789/753.

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Книги з теми "Dynamically tuned gyroscope"

1

United States. National Aeronautics and Space Administration., ed. Reliability testing of the MOD III-T two axis dynamically tuned gyroscope: Final technical report. Wilmington, Mass: The Division, 1996.

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Частини книг з теми "Dynamically tuned gyroscope"

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Lawrence, Anthony. "The Dynamically Tuned Gyroscope." In Modern Inertial Technology, 127–47. New York, NY: Springer US, 1993. http://dx.doi.org/10.1007/978-1-4684-0444-9_10.

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2

Lawrence, Anthony. "The Dynamically Tuned Gyroscope." In Mechanical Engineering Series, 131–51. New York, NY: Springer New York, 1998. http://dx.doi.org/10.1007/978-1-4612-1734-3_10.

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3

Pan, Yuxiong, Qingdong Li, and Zhang Ren. "Research on Prognostics of Dynamically Tuned Gyroscope Storage Life." In Lecture Notes in Electrical Engineering, 325–32. Berlin, Heidelberg: Springer Berlin Heidelberg, 2013. http://dx.doi.org/10.1007/978-3-642-38460-8_36.

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4

Fan, Chunling, Feng Gao, and Zhihua Jin. "Bayesian Neural Networks for Life Modeling and Prediction of Dynamically Tuned Gyroscopes." In Lecture Notes in Computer Science, 749–54. Berlin, Heidelberg: Springer Berlin Heidelberg, 2004. http://dx.doi.org/10.1007/978-3-540-28648-6_120.

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Тези доповідей конференцій з теми "Dynamically tuned gyroscope"

1

Lee, Byeungleul, Yong-Soo Oh, Kyu-Yeon Park, Byeoungju Ha, Younil Ko, Jeong-gon Kim, Seokjin Kang, Sangon Choi, and Ci M. Song. "Dynamically tuned vibratory micromechanical gyroscope accelerometer." In Far East and Pacific Rim Symposium on Smart Materials, Structures, and MEMS, edited by Alex Hariz, Vijay K. Varadan, and Olaf Reinhold. SPIE, 1997. http://dx.doi.org/10.1117/12.293580.

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2

Podchezertsev, V. P., and D. D. Nguyen. "Compensation mode synthesis of dynamically tuned gyroscope." In XLIV ACADEMIC SPACE CONFERENCE: dedicated to the memory of academician S.P. Korolev and other outstanding Russian scientists – Pioneers of space exploration. AIP Publishing, 2021. http://dx.doi.org/10.1063/5.0036028.

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3

Zhang, Lianchao, Dapeng Fan, Xinliang Pang, and Shixun Fan. "Bond Graph Modeling and Simulation of Dynamically Tuned Gyroscope." In 2007 International Conference on Mechatronics and Automation. IEEE, 2007. http://dx.doi.org/10.1109/icma.2007.4303662.

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4

Lianchao, Zhang, Fan Dapeng, and Fan Shixun. "Modeling and Error Analysis of Dynamically Tuned Gyroscope Based on Bond Graph." In 2010 International Conference on Digital Manufacturing and Automation (ICDMA). IEEE, 2010. http://dx.doi.org/10.1109/icdma.2010.204.

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5

Xia, Dunzhu, Cheng Yu, Shourong Wang, Hongsheng Li, and Lun Kong. "Structure design and simulation of micro dynamically tuned gyroscope with three equilibrium rings." In 2013 8th IEEE International Conference on Nano/Micro Engineered and Molecular Systems (NEMS). IEEE, 2013. http://dx.doi.org/10.1109/nems.2013.6559883.

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6

Chen, Weiyi, Qi Xie, and Yun Luo. "Application of Wavelet Transform in the Signal Processing of the Dynamically Tuned Gyroscope." In 2010 International Conference on Computational and Information Sciences (ICCIS). IEEE, 2010. http://dx.doi.org/10.1109/iccis.2010.60.

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7

May, David. "Modeling the dynamically tuned gyroscope in support of high-bandwidth capture loop design." In AeroSense '99, edited by Michael K. Masten and Larry A. Stockum. SPIE, 1999. http://dx.doi.org/10.1117/12.352852.

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8

Lee, Seok-Ku, and Chong-Won Lee. "Unidirectional Excitation Technique for Complex Modal Testing of Asymmetric Rotor Systems: Application to DTG." In ASME 1997 Design Engineering Technical Conferences. American Society of Mechanical Engineers, 1997. http://dx.doi.org/10.1115/detc97/vib-4045.

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Abstract Unidirectional excitation technique is presented for the complex modal testing of asymmetric rotor systems. The theoretical development, which is made strictly in the stationary coordinate system, enables the unidirectional excitation to effectively estimate the directional frequency response functions. It far lessens the testing efforts a numerical example of the dynamically tuned gyroscope (DTG) is treated to demonstrate the practicality of the complex modal testing.
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9

Hegazy, Salem Abd El-Hakem, AbdelMageed Mahmoud, Ahmed M. Kamel, Ibrahim Ismail Arafa, and Yehia Z. Elhalwagy. "Calibration and Compensation of Scale Factor Non-linearity and Non-Orthogonality Errors for Dynamically Tuned Gyroscope (DTG)." In 2020 12th International Conference on Electrical Engineering (ICEENG). IEEE, 2020. http://dx.doi.org/10.1109/iceeng45378.2020.9171734.

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10

Sadeghi-Emamgholi, Amin, Askar Azizi, and Hamid Nourisola. "Modeling and design of appropriate compensation for DTG (Dynamically Tuned Gyroscope) and improving sensor response using a Kalman filter." In 2016 4th International Conference on Robotics and Mechatronics (ICROM). IEEE, 2016. http://dx.doi.org/10.1109/icrom.2016.7886847.

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