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MEMS陀螺误差辨识与补偿 被引量:18

Error identification and compensation of MEMS gyroscope
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摘要 由于制造工艺等原因,MEMS陀螺的随机漂移非常大,严重影响了系统的性能。通过自制的基于MEMS的捷联惯导系统的相关实验,对MEMS陀螺的确定性误差和随机误差分别进行了辨识和补偿。完成确定性误差补偿,对MEMS陀螺随机误差进行了时间序列分析,并建立了AR模型,根据所选模型参数建立了随机误差的系统方程,采用经典卡尔曼滤波进行随机误差补偿。实验结果说明:无论是静态下还是动态下,补偿后信号的方差都大大下降,说明了滤波效果较为明显,具有一定的工程应用价值。 MEMS gyro' s random drift is very large, because of the manufacturing process and other reasons, which seriously affect on system performance. Through experiments of MEMS strapdown inertial navigation system, deterministic and stochastic error was identified and compensated. After deterministic error was compensated, the stochastic error was analyzed based on time series and AR model was set up. System equation of stochastic error was established based on the selected model and the error was compensated by Kalman Filter. Test results show that variance of MEMS gyroscope stochastic error reduced greatly after filter, which illustrates the filtering effect is obvious,and has a certain value of engineering application.
出处 《传感器与微系统》 CSCD 北大核心 2010年第3期39-41,共3页 Transducer and Microsystem Technologies
关键词 MEMS陀螺 时间序列分析 AR模型 卡尔曼滤波 MEMS gyroscope time series analysis AR model Kalman filter
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  • 1杨叔子 吴雅 等.时间序列分析的工程应用[M].武汉:华中理工大学出版社,1996..
  • 2胡广书 编著.数字信号处理[M].清华大学出版社,1998..
  • 3Winkler S, Buschmann M, Kordes T, et al. MEMS-based IMU development, calibration and testing for autonomous MAV navigation[A]. ION 59th Annual Meeting/CIGTF 22nd Guidance Test Symposium[C]. Jun. 23-25, 2003, Albuquerque, New Mexico, USA.
  • 4J.Beser, S.Alexander, R.Crane, et al. TRUNAVTM: A Low-cost Guidance/Navigation Unit Integrating A SAASM-BASED GPS and MEMS IMU in A Deeply Coupled Mechanization[C], ION GPS 2002, Sep.24-27,2002, Portland, Oregon, USA.
  • 5C. Hide, T. Moore, M. Smith. Adaptive Kalman filtering for low cost INS/GPS[A]. ION GPS 2002[C]. Sep. 24-27, 2002,Portland, Oregon, USA.
  • 6Rios J A, White E. Fusion filter algorithm enhancements for a MEMS GPS/IMU[C]. ION NTM 2002, Jan.28-30,2002, San Diego, California, USA
  • 7W Chen, C Hu, Y Sun. Attitude determination with A low cost GPS/IMU unit[A]. ION 58th Annual Meeting/CIGTF 21st Guidance Test Symposium[C]. Jun. 24-26, 2002, Albuquerque, New Mexico, USA.
  • 8Gregory T A Kovacs.微传感器与微执行器全书[M].张文栋,译.北京:科学出版社,2003.
  • 9Bernstein J. An overview of MEMS inertial sensing technology [J]. Sensors, 2003, (2).
  • 10R.E. Hopkins, J.T. Borestein, et al. The silicon oscillating accelerometer: A MEMS inertial instrument for strategic missile guidance[A]. AIAA. Reprinted, with permission from the missile Sciences Conference held in Monterey[C]. Nov. 7-9, 2000,California, USA.

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