航空学报 > 2011, Vol. 32 Issue (11): 2106-2116   doi: CNKI:11-1929/V.20110627.1733.004

高精度光纤IMU的磁屏蔽方法及实验研究

李金涛, 房建成   

  1. 北京航空航天大学 "新型惯性仪表与导航系统技术"国防重点学科实验室, 北京 100191
  • 收稿日期:2011-04-11 修回日期:2011-05-03 出版日期:2011-11-25 发布日期:2011-11-24
  • 通讯作者: 房建成 E-mail:fangjiancheng@buaa.edu.cn
  • 作者简介:李金涛(1980- ) 男,博士研究生。主要研究方向:光纤陀螺误差建模补偿技术,惯性/卫星组合导航技术。 Tel: 010-82337331 E-mail: lijintao@aspe.buaa.edu.cn 房建成(1965- ) 男,教授,博士生导师,北京航空航天大学仪器科学与光电工程学院院长。主要研究方向:惯性导航、组合导航及航天器姿态控制技术等。 Tel: 010-82339487 E-mail: fangjiancheng@buaa.edu.cn
  • 基金资助:

    国家 "973"计划(2009CB724001, 2009CB724002);国家"863"计划(2008AA121302)

Magnetic Shielding Method and Experiment Study of Inertial Measurement Unit Based on High Precision Fiber-optic Gyroscope

LI Jintao, FANG Jiancheng   

  1. Fundamental Science on Novel Inertial Instrument & Navigation System Technology Laboratory, Beihang University, Beijing 100191, China
  • Received:2011-04-11 Revised:2011-05-03 Online:2011-11-25 Published:2011-11-24

摘要: 惯性测量单元(IMU)是位置姿态系统(POS)的核心部分,IMU的精度很大程度上决定着POS精度。由于高精度光纤陀螺(FOG)的光纤线圈对磁场敏感,基于高精度FOG的IMU精度会受磁场影响而降低。本文研究了FOG磁敏感性机理,通过实验得出高精度光纤IMU对磁场敏感的结论。采用电磁场有限元分析软件Ansoft Maxwell研究了磁屏蔽体采用不同材料、不同厚度时的磁屏蔽效能(SE),并进行了IMU磁屏蔽结构设计。通过亥姆霍兹线圈测试得到的磁屏蔽体实际屏蔽效能最高为48.20 dB,与有限元分析结果基本一致。转台环境测试表明:屏蔽体使FOG漂移减小到9%以上;亥姆霍兹线圈测试表明:通过磁屏蔽使FOG零偏磁敏感度衰减2~21 dB,漂移磁敏感度衰减9~23 dB,对提高光纤IMU测试和应用精度以及机载环境适应性有重要意义。

关键词: 惯性测量单元, 光纤陀螺, 频谱分析, 功率谱密度, 有限元方法, 磁屏蔽

Abstract: The inertial measurement unit (IMU) is the core of a position and orientation system (POS), whose accuracy has a crucial impact on POS accuracy. But the IMU accuracy based on high precision fiber-optic gyroscope (FOG) is degraded because of the sensitivity of the FOG fiber coil to the magnetic field. This paper studied the magnetic sensitivity mechanism of the FOG, and through experimental study reached the conclusion that the IMU based on a high precision FOG is also sensitive to the magnetic field. An IMU shielding is designed, and its shielding effectiveness (SE) is analyzed by electromagnetic field finite element analysis software Ansoft Maxwell for different materials with different thicknesses. The best SE of 48.20 dB is achieved with a Helmholtz coil test, which is consistent with the results of the finite element analysis. The turn table test shows that a reduction of over 9% of the FOG drift is achieved with the enclosure. The Helmholtz coil test with magnetic shielding demonstrates that the bias and drift magnetic sensitivity of the FOG are decreased by 2-21 dB and 9-23 dB respectively. The shielding is valuable for improving the IMU test and application precision and its adaptability to airborne environment.

Key words: inertial measurement unit, fiber-optic gyroscope, frequency spectrum analysis, power spectral density, finite element method, magnetic shielding

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