A novel Kalman filter for combining outputs of MEMS gyroscope array

► Fusing outputs of the MEMS gyroscopes array to improve accuracy is presented. ► Theoretical mathematical model for the accuracy improvement is described. ► A combined Kalman filter is designed and analyzed by an analytic solution. ► A linear equation is developed for choosing a variance for modeli...

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Veröffentlicht in:Measurement : journal of the International Measurement Confederation 2012-05, Vol.45 (4), p.745-754
Hauptverfasser: Xue, Liang, Jiang, Cheng-Yu, Chang, Hong-Long, Yang, Yong, Qin, Wei, Yuan, Wei-Zheng
Format: Artikel
Sprache:eng
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Zusammenfassung:► Fusing outputs of the MEMS gyroscopes array to improve accuracy is presented. ► Theoretical mathematical model for the accuracy improvement is described. ► A combined Kalman filter is designed and analyzed by an analytic solution. ► A linear equation is developed for choosing a variance for modeling rate signal. ► ARW and bias drift are reduced from 6.2°√h to 1.6°√h and 62°/h to 17.2°/h by KF. In this paper, a Kalman filter for combining outputs of a gyroscope array is presented to improve the accuracy of microelectromechanical system (MEMS) gyroscope. A theoretical mathematical model for the accuracy improvement is described. Especially, a discrete-time filter is designed by solving the covariance differential equation with an analytic solution. Performances of presented filter are analyzed by the simulations. Finally, a developed system consisting of six-gyroscope array is implemented to test the performance of the Kalman filter. The experimental results showed a noise density of 0.03°/s/√Hz for the combined rate signal compared to the 0.11°/s/√Hz for the individual gyroscope in the array. The analysis of results measured from Allan variance demonstrated a bias instability of 17.2°/h and angular random walk of 1.6°/√h, whereas the corresponding values for the individual gyroscope is 62°/h and 6.2°/√h, respectively. It proved that the presented approach is effective to improve the MEMS gyroscope accuracy.
ISSN:0263-2241
1873-412X
DOI:10.1016/j.measurement.2011.12.016