TY - JOUR
T1 - Temperature Energy Influence Compensation for MEMS Vibration Gyroscope Based on RBF NN-GA-KF Method
AU - Cao, Huiliang
AU - Zhang, Yingjie
AU - Shen, Chong
AU - Liu, Yu
AU - Wang, Xinwang
AU - Tao, Kai
N1 - Publisher Copyright:
© 2018 Huiliang Cao et al.
PY - 2018
Y1 - 2018
N2 - This paper proposed three methods to compensate the temperature energy influence drift of the MEMS vibration gyroscope, including radial basis function neural network (RBF NN), RBF NN based on genetic algorithm (GA), and RBF NN based on GA with Kalman filter (KF). Three-axis MEMS vibration gyroscope (Gyro X, Gyro Y, and Gyro Z) output data are compensated and analyzed in this paper. The experimental results proved the correctness of these three methods, and MEMS vibration gyroscope temperature energy influence drift is compensated effectively. The results indicate that, after RBF NN-GA-KF method compensation, the bias instability of Gyros X, Y, and Z improves from 139°/h, 154°/h, and 178°/h to 2.9°/h, 3.9°/h, and 1.6°/h, respectively. And the angle random walk of Gyros X, Y, and Z was improved from 3.03°/h 1/2 , 4.55°/h 1/2 , and 5.89°/h 1/2 to 1.58°/h 1/2 , 2.58°/h 1/2 , and 0.71°/h 1/2 , respectively, and the drift trend and noise characteristic are optimized obviously.
AB - This paper proposed three methods to compensate the temperature energy influence drift of the MEMS vibration gyroscope, including radial basis function neural network (RBF NN), RBF NN based on genetic algorithm (GA), and RBF NN based on GA with Kalman filter (KF). Three-axis MEMS vibration gyroscope (Gyro X, Gyro Y, and Gyro Z) output data are compensated and analyzed in this paper. The experimental results proved the correctness of these three methods, and MEMS vibration gyroscope temperature energy influence drift is compensated effectively. The results indicate that, after RBF NN-GA-KF method compensation, the bias instability of Gyros X, Y, and Z improves from 139°/h, 154°/h, and 178°/h to 2.9°/h, 3.9°/h, and 1.6°/h, respectively. And the angle random walk of Gyros X, Y, and Z was improved from 3.03°/h 1/2 , 4.55°/h 1/2 , and 5.89°/h 1/2 to 1.58°/h 1/2 , 2.58°/h 1/2 , and 0.71°/h 1/2 , respectively, and the drift trend and noise characteristic are optimized obviously.
UR - http://www.scopus.com/inward/record.url?scp=85058947311&partnerID=8YFLogxK
U2 - 10.1155/2018/2830686
DO - 10.1155/2018/2830686
M3 - 文章
AN - SCOPUS:85058947311
SN - 1070-9622
VL - 2018
JO - Shock and Vibration
JF - Shock and Vibration
M1 - 2830686
ER -