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基于均匀设计的MEMS陀螺温度标定试验设计

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作者:高爽, 张晓娇, 李慧鹏, 蔡晓雯, 李胜臣, 王文杰, 张维睿

作者单位:北京航空航天大学惯性技术重点试验室, 北京 100191


关键词:MEMS陀螺;均匀设计法;温度;标定误差补偿


摘要:

针对传统的温度试验方案存在试验量大、耗费时间长的问题,提出基于均匀设计法的三轴微电子机械系统(micro-electromechanical systems,MEMS)陀螺温度标定误差补偿试验方案。设计基于均匀设计的四因素(测试温度点、温变速率、MEMS陀螺转速及转动方向)试验方案。首先,构造试验所需的均匀设计表;其次,根据LP-偏差确定MEMS陀螺温度标定误差补偿实验的最佳试验方案;最后,搭建出MEMS陀螺温度标定的实验装置进行测试。试验结果表明:与将每一个因素的不同水平组合的全面设计方案相比,该试验方案不仅节省12.5%的试验时间,还进一步减少MEMS陀螺温度标定误差试验量,缩短研究周期,节约试验成本。


The temperature calibration of MEMS gyro experiment design based on uniform design

GAO Shuang, ZHANG Xiaojiao, LI Huipeng, CAI Xiaowen, LI Shengchen, WANG Wenjie, ZHANG Weirui

Key Laboratory on Inertial Science and Technology, Beihang University, Beijing 100191, China

Abstract: In order to improve time-consuming traditional temperature test programs requiring substantial amount of testing, a temperature calibration error compensation method of three-axis MEMS gyro based on uniform design method was proposed. One temperature calibration compensation testing program based on four factors was designed. The four factors include testing temperature point, temperature changing rate, MEMS gyro speed and direction of rotation. Firstly, the uniform design table was established. Secondly, the best test method of MEMS gyro temperature calibration error compensation was determined according to LP-deviation test program. Finally, the MEMS gyro temperature calibration experimental device was built. The test results show that the designed method which compared different levels of each factor saved 12.5% testing timecompared with the traditional design. This test program contributes to reduce the amount of experiments, shorten the research cycle and save experimental cost.

Keywords: MEMS gyro;uniform design method;temperature;calibration error compensation

2016, 42(12): 8-11  收稿日期: 2016-03-10;收到修改稿日期: 2016-04-29

基金项目: 

作者简介: 高爽(1977-),女,陕西咸阳市人,讲师,博士,研究方向为惯性导航。

参考文献

[1] 毛奔,张晓宇. 微惯性系统及应用[M]. 哈尔滨:哈尔滨工程大学出版社,2013:35-48.
[2] JACQUES G, ABOELMAGD N, MICHAEL J, et al. Low-cost three-dimensional navigation solution for RISS-GPS integrated using mixture particle filter[J]. IEEE Transactions on Vehicular technology,2010,59(2):599-615.
[3] GU D Q, NASER E. Heading accuracy improvement of MEMS IMU-DGPS integrated navigation system for land vehicle[C]//IEEE. New York:IEEE,2008:1292-1296.
[4] RADE S, STEVICA G. The integration of strap-down INS and GPS based on adaptive error damping[J]. Robotics and Autonomous Systems,2010,58(1):1117-1129.
[5] GAIFFE T, COTTREAU Y, FAUSSOT N, et al. Highly compact fiber optic gyrocompass for applications at depths up to 3000 meters[C]//International Symposium on Underwater Technology,2000:155-160.
[6] LEE J, PARK C, PARK H. Multi-position alignment of strap-down inertial navigation system[J]. IEEE Transaction on Aerospace and Electronic System,1993,29(4):1323-1328.
[7] FAUSSOT N. Standard specification format guide and test procedure for single axis interfero-metric fiber optic gyros[C]//IEEE Std. New York:IEEE,2012:952-1997.
[8] 段志梅.基于混沌理论的光纤陀螺仪温度非线性建模[J].激光杂志,2016,37(1):59-62.
[9] 孙亮,余震虹,陈浩,等. 闭环光纤陀螺零偏与标度因数的综合补偿[J]. 仪表技术与传感器,2014(6):1-3.
[10] 谢愈,郑伟,汤国建. 基于均匀设计的神经网络建模在惯导工具误差模型弹载验证试验方案优化中的应用[C]//均匀试验设计学术交流会论文集,2007:189-194.
[11] 张国秋,王文璇. 均匀试验设计方法应用综述[J]. 数理统计与管理,2013,32(1):89-99.
[12] 于昌龙,张红线,吴衍记,等. 基于均匀设计的光纤陀螺温度建模试验方案研究[J]. 红外与激光工程,2009,38(2):330-334.
[13] 孙英杰. 光纤陀螺温度漂移误差建模及补偿技术研究[D].哈尔滨:哈尔滨工业大学,2010.
[14] 方开泰,马长兴. 正交与均匀试验设计[M]. 北京:科学出版社,2001:96-103.
[15] 方开泰. 均匀设计与均匀设计表[M]. 北京:科学出版社,1994:35-41.
[16] 艾纯明,吴爱祥. 基于均匀设计实验的膏体配比优化[J].科技导报,2016,34(2):210-214.
[17] AGGARWAL P, SYED Z, NIU X, et al. A standard testing and calibration procedure for low cost MEMS inertial sensors and units[J]. The Journal of Navaigation,2008(61):323-336.
[18] BLIN S, HK K. Reduced thermal sensitivity of a fiber-optic gyroscope using an air-core photonic-bandgap fiber[J].Lightwave Technology Journal,2007,25(3):861-865.
[19] 于洵,申双琴,徐岩,等.一种基于陀螺的炮塔转角动态高精度测量方法[J]. 国外电子测量技术,2012,31(12):36-39.
[20] 周红进,钟云海,易成涛. MEMS惯性导航传感器[J]. 舰船科学技术,2014,36(1):115-121.
[21] 彭孝东,陈瑜,李继宇,等. MEMS三轴数字陀螺仪标定方法研究[J]. 传感器与微系统,2013,32(6):63-65.
[22] DZHASHITOV V, PANKRATOV V. The determined chaos in disturbed by temperature dynamic systems with gyros[C]//IEEE on Physics & Control. Washington DC:IEEE,2003:638-643.
[23] 袁建国,袁艳涛,刘飞龙. MEMS陀螺仪的一种新颖高精度标定算法研究[J]. 重庆邮电大学学报,2014,26(5):666-669.
[24] DZHASHITOV V, PANKRATOV V. Using the method of elementary balances for analysis and synthesis of thermal control system for FOG SINS based on peltiermodules[J]. Gyroscopy & Navigation,2014,5(4):245-256.
[25] 王励扬,翟昆朋,何文涛,等. 低成本MEMS陀螺实时滤波方法[J]. 电子技术应用,2015,41(1):50-52.