Compensation method for temperature error of fiber optical gyroscope based on relevance vector machine

被引:16
作者
Wang, Guochen [1 ]
Wang, Qiuying [2 ]
Zhao, Bo [3 ]
Wang, Zhenpeng [1 ]
机构
[1] Harbin Engn Univ, Coll Automat, Harbin 150001, Peoples R China
[2] Harbin Engn Univ, Coll Informat & Commun, Harbin 150001, Peoples R China
[3] Harbin Inst Technol, Anshan Ind Technol Res Inst, Anshan 114051, Peoples R China
基金
中国国家自然科学基金;
关键词
Gyroscopes - Error compensation;
D O I
10.1364/AO.55.001061
中图分类号
O43 [光学];
学科分类号
070207 ; 0803 ;
摘要
Aiming to improve the bias stability of the fiber optical gyroscope (FOG) in an ambient temperature-change environment, a temperature-compensation method based on the relevance vector machine (RVM) under Bayesian framework is proposed and applied. Compared with other temperature models such as quadratic polynomial regression, neural network, and the support vector machine, the proposed RVM method possesses higher accuracy to explain the temperature dependence of the FOG gyro bias. Experimental results indicate that, with the proposed RVM method, the bias stability of an FOG can be apparently reduced in the whole temperature ranging from -40 degrees C to 60 degrees C. Therefore, the proposed method can effectively improve the adaptability of the FOG in a changing temperature environment. (C) 2016 Optical Society of America
引用
收藏
页码:1061 / 1066
页数:6
相关论文
共 17 条
[1]  
[Anonymous], 2000, ACM C UNCERTAINTY AR
[2]  
[白俊卿 Bai Junqing], 2013, [压电与声光, Piezoelectrics and Acoustooptics], V35, P201
[3]   Application of relevance vector machine and logistic regression for machine degradation assessment [J].
Caesarendra, Wahyu ;
Widodo, Achmad ;
Yang, Bo-Suk .
MECHANICAL SYSTEMS AND SIGNAL PROCESSING, 2010, 24 (04) :1161-1171
[4]  
[程骏超 Cheng Junchao], 2013, [仪器仪表学报, Chinese Journal of Scientific Instrument], V34, P721
[5]  
Cheng Yuming, 1997, Journal of Shanghai Jiaotong University, V31, P123
[6]  
[冯丽爽 FENG Lishuang], 2006, [宇航学报, Journal of Chinese Society of Astronautics], V27, P939
[7]  
Hai W., 2007, J BEIJING U AERONAUT, V33, P549
[8]  
Han Bing, 2009, Journal of Chinese Inertial Technology, V17, P218
[9]  
Jin Jing, 2007, Acta Aeronautica et Astronautica Sinica, V28, P1449
[10]  
Liu GF, 2001, J CHINA INERTIAL TEC, V9, P48