期刊文献+

双质量硅微机械陀螺仪正交校正系统设计及测试 被引量:8

Design and test on quadrature error correction system of dual-mass silicon MEMS gyroscope
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摘要 为了减小正交误差对双质量硅微机械陀螺仪性能的影响,进一步提高陀螺精度和工程化成品率,对双质量结构正交耦合刚度校正法进行了研究。首先,针对双质量陀螺结构的特殊形式,分析了其左、右结构中正交耦合刚度不相等的原因,并结合相敏检测相位误差对正交耦合刚度值进行了计算,进一步量化了其对输出信号的影响;其次,结合正交校正梳齿结构介绍了耦合刚度校正法的工作原理,并基于左、右结构单独校正的方法设计了双质量结构正交校正控制系统;最后,对正交校正前后的双质量微机械陀螺仪进行了详细测试,结果证实了双质量单独校正比整体校正效果更好,各项参数均有较大提高,其中零偏稳定性从校正前的540(°)/h提高到了正交后的24.05(°)/h(1σ),证明了提出的两质量块单独校正方法的可行性和实用性。 The quadrature-coupling stiffness correction method for dual-mass silicon MEMS gyroscope is investigated to reduce the quadrature error's influence and improve the gyro's precision and the finished product rate. Firstly, the unequal reason of the left and right masses' s coupling stiffness is analyzed based on the dual-mass structure, and the quadrature stiffness value is calculated taking into account the phase sensitivity demodulation error which contributes great error and drift to the gyro output. Secondly, a quadrature error correction comb is introduced, and a two-mass quadrature error separate compensation system is proposed. Finally, experiments are conducted to test the gyro performance, which show that the separate correction method has better result compared with the integral correction method, and the parameters are significantly improved after quadrature error correction, in which the bias stability is increased to 24.05(°)/h(1σ) from 540(°)/h, verifying the feasibility and practicality of the proposed method.
出处 《中国惯性技术学报》 EI CSCD 北大核心 2015年第4期544-549,共6页 Journal of Chinese Inertial Technology
基金 总装预研基金项目(9140A09011313JW06119) 江苏省科技攻关项目(BE2014003-3) 国家杰出青年科学基金(51225504) 国防973(2012CB723404) 国家自然科学基金委员会 中国工程物理研究院联合基金资助(U1230114) 中北大学校基金
关键词 双质量硅微机械陀螺仪 正交误差 正交耦合刚度校正 两质量块单独校正 性能测试 dual-mess MEMS gyroscope quadrature error coupling stiffness correction two mass separate correction performance test
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参考文献11

  • 1曹慧亮,李宏生,王寿荣,杨波,黄丽斌.MEMS陀螺仪结构模型及系统仿真[J].中国惯性技术学报,2013,21(4):524-529. 被引量:18
  • 2Shkel A M. Precision navigation and timing enabled by microtechnology: Are we there yet?[C]//Proc SPIE Int Soc Opt Eng Micro- and Nanotech- nology Sensors, Systems, and Applications BI. 2011, vol.8031: 18.1-18.9.
  • 3Erdinc T, Said E A, Tayftm A. Quadra- ture-error compensation and corres- ponding effects on the performance of fully decoupled MEMS gyroscopes[J]. Journal of Micro-Electromechanical Sys- tems, 2012, 21(3): 656-667.
  • 4Chaumet B, et al. A new silicon tuning fork gyroscope for aerospace applica- tions[C]//Symposium Gyro Technology. 2009: 1.1- 1.13.
  • 5Lapadatu D, Blixhavn B, Holm R, et al. SAR500 - a high-precision high- stability butterfly gyroscope with north seeking capability[C]//IEEE/ION Posi- tion Location and Navigation Sympo- sium. 2010: 6-13.
  • 6Zaman M F, Sharma A, Hao zhili, et al. A mode-matched silicon-yaw tuning- fork gyroscope with subdegree-per- hour Allan deviation bias instability[J]. Journal of Microelectromechanical Sys- tems, 2008, 17(6): 1526-1536.
  • 7王晓雷,杨成,李宏生.硅微陀螺仪正交误差校正系统的分析与设计[J].中国惯性技术学报,2013,21(6):822-827. 被引量:5
  • 8Su Jian-bin, Xiao Dong-bang, Chen Zhi- hua, et al. Improvement of bias stability for a micromachined gyroscope based on dynamic electrical balancing of coupling stiffness[J]. J. Micro/Nanolith MEMS MOEMS, 2013, 12(3): 033008.
  • 9倪云舫,李宏生,杨波,黄丽斌,赵立业,王攀,刘嘉.硅微陀螺正交误差直流校正设计与分析[J].中国惯性技术学报,2014,12(1):104-108. 被引量:10
  • 10Cao Hui-liang, Li Hong-sheng. Investi- gation of a vacuum packaged MEMS gyroscope architecture's temperature robustness[J]. International Journal of Applied Electromagnetics and Mechanics, 2013(41): 495-506.

二级参考文献28

  • 1夏敦柱,周百令,王寿荣.实时小波滤波方法在硅微陀螺仪中的应用研究[J].中国惯性技术学报,2007,15(1):92-95. 被引量:9
  • 2杨军,高钟毓,张嵘,陈志勇,周斌.线振动硅微机械陀螺结构误差参数分离和辨识[J].中国惯性技术学报,2007,15(3):327-333. 被引量:12
  • 3Erdinc T, Said E A, Tayfun A. Quadrature-error compen- sation and corresponding effects on the performance of fully decoupled MEMS gyroscopes[J]. Journal of Micro- electromechanical Systems, 2012, 21(3): 656-667.
  • 4Sonmezoglu S, Alper S E, Akin T. An automatically mode-matched MEMS gyroscope with 50Hz band width [C]//IEEE 25th International Conference on Micro Electro Mechanical Systems(MEMS). Paris, France, 2012: 523- 526.
  • 5Cao Huiliang, Li Hongsheng. Investigation of a vacuum packaged MEMS gyroscope architecture's temperature robustness[J]. International Journal of Applied Electrom- agnetics and Mechanics, 2013 (41): 495-506.
  • 6Yang Bo, Wang Shourong, Li Hongsheng, et al. Mechanical-thermal noise in drive-mode of a silicon micro-gyroscope[J]. Sensors, 2009(9): 3357-3375.
  • 7Saukoski M, Aaltonen L, Halonen K A I. Zero-rate output and quadrature compensation in vibratory MEMS gyroscope [J]. IEEE Sensors Journal, 2007, 7(12): 1639-1652.
  • 8Cui J, Chi X Z, Ding H T, et al. Transiem response and stability of the AGC-PI closed-loop controlled MEMS vibratory gyroscopes[J]. Journal of Micromechanics and Microengineering, 2009, 19: 1-17.
  • 9Yang Bo, Zhou Bailing, Wang Shourong, et al. A quadrature error and offset error suppression circuitry for silicon micro-gyroscope[C]//Proceedings of the 3rd IEEE International Conference on Nano/Micro Engineered and Molecular Systems. Sanya, China, 2008: 422-426.
  • 10Shkel A M,Horowitz R,Seshia A A,et al.Dynamics and control of micromachined gyroscopes[C]//Proceedings of the American Control Conference.San Diego,USA,1999:2119-2124.

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