超流体物质波干涉陀螺仪的噪声研究

doi:10.7527/S1000-6893.2013.0151

Abstract

Abstract:

Gyroscope accuracy is closely related to its noise. To develop a novel superfluid matter wave interference gyroscope with high accuracy, its noise should be studied systematically. First, according to the generating mechanism of gyroscope noise, its origins are analyzed. The noise types are classified as thermal, locking value fluctuation, temperature fluctuation, frequency fluctuation and detecting element noise. Then, based on the mathematic model of each noise, the gyroscope noise is analyzed by utilizing some common parameters. The results show that thermal noise is relevant to the gyroscope structure parameter and working parameter, but is irrelevant to detected angular velocity. Locking fluctuation noise is only relevant to structure parameter; the other noises are all related to structure parameter, working parameter and detected angular velocity. Detecting element, frequency and locking value fluctuation noises are the primary factors that contribute to gyroscope output noise. In the range of the changing value of angular velocity, the gyroscope output noise changes nonlinearly with arange from the order of -7 to -6 in 1 Hz bandwidth.

Key words: superfluid, gyroscopes, matter wave, interference, noise

CLC Number:

ZHAO Wei, ZHENG Rui, LIU Jianye, XIE Zheng. Research on the Noises of Superfluid Matter Wave Interference Gyroscope[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, doi: 10.7527/S1000-6893.2013.0151.

References

[1] Liu J Y, Zeng Q H, Zhao W, et al. Theory and application of navigation system. Xi'an: Northwestern Polytechnical University Press, 2010: 2-5. (in Chinese) 刘建业, 曾庆化, 赵伟, 等. 导航系统理论与应用. 西安: 西北工业大学出版社, 2010: 2-5.

[2] Qin Y Y. Current status and development trend of international inertial instrument. Aeronautical Manufacturing Technology, 2008(9): 68-69. (in Chinese) 秦永元. 国际惯性器件发展现状和趋势. 航空制造技术, 2008(9): 68-69.

[3] Wang W. Technology of interference fibre optic gyroscope. Beijing: China Astronautic Publishing House, 2010: 4-6. (in Chinese) 王巍. 干涉型光纤陀螺仪技术. 北京: 中国宇航出版社, 2010: 4-6.

[4] Gustavson T L, Landragin A, Kasevich M A. Rotation sensing with a dual atom interferometer Sagnac gyroscope. Classical and Quantum Gravity, 2000, 17(12): 2385-2398.

[5] Hoskinson E, Packard R E, Haard T M. Quantum whisling in superfluid helium-4. Nature, 2005, 443(7024): 376.

[6] Hoskinson E, Sato Y, Packard R E. Superfluid⁴He interferometer operating near 2K. Physical Review B, 2006, 74(10): 100509.1-100509.8.

[7] Sato Y. Fiske-amplified superfluid interferometry. Physical Review B, 2010, 81(17): 172502.1-172502.4.

[8] Narayana S, Sato Y. Superfluid quantum interference in multiple-turn reciprocal geometry. Physical Review Letters, 2011, 106(6): 255301.1-255301.4.

[9] Golovashkin A I, Zherikhina L N, Tskhovrebov A M, et al. Ordinary SQUID interferometers and superfluid helium matter wave interferometers: the role of quantum fluctuations. Journal of Experimental and Theoretical Physics, 2010, 111(2): 332-339.

[10] Golovashkin A I, Izmalov G N, Ozolin V V, et al. Scheme of laboratory measurements of gravimagnetic effects with SHeQUID equipped with a rotation flux transformer. Gravitation and Comology, 2010, 16(1): 78-84.

[11] Sato Y, Joshi A, Packard R E. Flux locking a superfluid interferomenter. Applied Physics Letters, 2007, 91(7): 074107.1-074107.3.

[12] Song B Z, Zhao W, Xie Z, et al. Research on modeling and simulation for new quantum whistling superfluid cryogenic gyroscope. Journal of Applied Sciences, 2009, 27(3): 321-325. (in Chinese) 宋宝璋, 赵伟, 谢征, 等. 新型低温哨音超流体陀螺模型. 应用科学学报, 2009, 27(3): 321-325.

[13] Xie Z, Liu J Y, Zhao W, et al. Analysis and simulation of measure range of double weak-links structured high sensitivity superfluid gyroscope. Journal of Chinese Inertial Technology, 2011, 19(1): 79-83. (in Chinese) 谢征, 刘建业, 赵伟, 等. 双弱连接结构的高精度超流体陀螺的量程分析. 中国惯性技术学报, 2011, 19(1): 79-83.

[14] Xie Z, Liu J Y, Zhao W, et al. The exploratory research of a novel gyroscope based on superfluid Josephson effect. 2010 IEEE/ION Position Location and Navigation Symposium (PLANS), 2010: 14-19.

[15] Feng M Y, Zhao W, Liu J Y, et al. Information extraction and range expanding technology of double weak-link structured superfluid gyroscope. Modern Electronic Technique, 2012, 35(2): 94-99. (in Chinese) 冯铭瑜, 赵伟, 刘建业, 等. 双弱连接超流体陀螺信息提取与量程扩展技术. 现代电子技术, 2012, 35(2): 94-99.

[16] Liu J Y, Xie Z, Feng M Y, et al. Current status and development of superfluid gyroscope. Acta Aeronautica et Astronautica Sinica, 2012, 33(1): 1-10. (in Chinese) 刘建业, 谢征, 冯铭瑜, 等. 超流体陀螺仪的发展概况与研究进展. 航空学报, 2012, 33(1): 1-10.

[17] Chui T, Holmes W, Penanen K. Fluctuations of the phase difference across an array of Josephson junctions in superfluid ⁴He near the Lambda transition. Physical Review Letters, 2003, 90(8): 085301.1-085301.4.

[18] Sato Y, Joshi A, Packard R E. Direct measurement of quantum phase gradients in superfluid ⁴He flow. Physical Review Letters, 2007, 98(19): 195302.1-195302.3.

[19] Welander P B, Hahn I. Miniature high-resolution thermometer for low-temperature applications. Review of Scientific Instruments, 2001, 72(9): 3600-3604.

[20] Sato Y, Parkard R E. Superfluid helium quantum interference devices: physics and applications. Reports on Progress in Physics, 2012, 75(1): 016401.1-016401.27.

[21] Hoskinson E, Sato Y, Penanen K, et al. A chemical potential "battery" for superfluid⁴He weak links. Proceedings of the 24th International Conference on Low Temperature Physics, 2005: 117-118.

[22] Sato Y. DC-SQUID based neodymium magnet displacement sensor for superfluid experiments. Review of Scientific Instruments, 2009, 80(5): 055102.1-055102.5.

Research on the Noises of Superfluid Matter Wave Interference Gyroscope

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