A Novel Filtering Method for the Random Drift of MEMS Gyroscope

Article Preview

Abstract:

In engineering application, the nonlinearity effect of the environment noise is inconsistent with the successive starting state of MEMS gyroscope which will induce the random drifts. It manifests as the weak nonlinearity, non stability and slow time varying which cannot be compensated by the conventional method. In order to overcome the problems of the great random drift error model established based on the time series for MEMS gyroscope and the non Gaussian noise, the method of Iteration Unscented Kalman Particle Filter (IUKPF) is proposed in this paper. This method is based on the Particle Filter combing the Unscented Transformation (UT) with Iteration Kalman Filter (IKF), and it solved the instability of the precision for the conventional filtering methods and the degradation for the weight of the particle filter. The filtering result shows that the method of IUKPF can effectively restrain the random drift error under nonlinear and non Gaussian noise. The standard deviation for the output noise of MEMS gyroscope has decreased 81.9% by IUKPF which verifies the efficiency and superiority of this method.

You might also be interested in these eBooks

Info:

Periodical:

Pages:

73-79

Citation:

Online since:

February 2014

Export:

Price:

Permissions CCC:

Permissions PLS:

Сopyright:

© 2014 Trans Tech Publications Ltd. All Rights Reserved

Share:

Citation:

* - Corresponding Author

[1] Masako Tanaka. An industrial and applied review of new MEMS devices features [J]. Microelectronic Engineering, Vol. 84, No. 5 (2007), pp: 1341-1344.

DOI: 10.1016/j.mee.2007.01.232

Google Scholar

[3] Song Jilei, Wu Xunzhong and Guo Ling. Research on Modeling and Filter of Micro Electro Mechanical System Gyroscope Random Drift [J]. MISSILES AND SPACE VEHICLES, 2012, Vol. 320, No. 4 (2012), pp: 35-38.

Google Scholar

[4] Soken H E, Hajiyev C. Adaptive unscented Kalman filter with multiple fading factors for pico satellite attitude estimation[C]. Recent Advances in Space Technologies, 4th International Conference on IEEE, 2009, pp: 541-546.

DOI: 10.1109/rast.2009.5158254

Google Scholar

[5] Piro C, Accardo D. A Vertical Gyro Model Based on Particle Filters [J]. Aerospace Conference, 2007 IEEE, 2007, pp: 1-12.

DOI: 10.1109/aero.2007.353048

Google Scholar

[6] Closasy P, Fernadndez-Prades C and Ferndndez-Rubio. A Particle Filtering Tracking Algorithm for GNSS Synchronization Using Laplace's Method [C]. IEEE International Conference on Acoustics, Speech and Signal Processing, 2008, pp: 3409-3412.

DOI: 10.1109/icassp.2008.4518383

Google Scholar

[7] ZHOU F, MENG X. In-flight alignment research for airborne INS/GPS based on adaptive unscented Kalman filter algorithm [J]. Systems Engineering and Electronics, 2010, Vol. 32, No. 2, pp: 367-371.

Google Scholar

[8] Wang F, Lin Y. Improving Particle Filter with A New Sampling Strategy [C]. Computer Science & Education, 2009. ICCSE09. 4th International Conference on. IEEE, 2009, pp: 408-412.

DOI: 10.1109/iccse.2009.5228418

Google Scholar

[9] Liu Y, Wang B and He W. Fundamental principles and applications of particle filters [C]. Intelligent Control and Automation, 2006. Wcica2006. The 6th World Congress on. IEEE, 2006, 2, pp: 5327-5331.

DOI: 10.1109/wcica.2006.1714087

Google Scholar

[10] Zhang G, Zhao Z. Overview of particle filter and its applications in integrated navigation system [J]. Journal of Chinese Inertial Technology. 2006, Vol. 14, No. 6, pp: 91-94.

Google Scholar

[11] Li L, Ji H and Luo J. Iterated extended kalman particle filtering [J]. Journal of Xidian University (Natural Science), 2007, Vol. 14, No. 2, pp: 233-238.

Google Scholar

[12] Zhao H, Wang Z. MEMS Sensors Based Attitude Measurement System Using UKF [J]. Chinese Journal of Sensors and Actuators, 2011, Vol. 24, No. 5, pp: 642-646.

Google Scholar