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激光陀螺旋转惯导系统IMU的磁屏蔽设计及优化分析 被引量:3

Magnetic shielding design and optimization for IMU of rotation RLG INS
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摘要 为了提高激光陀螺旋转惯导系统的环境适应性,需要对惯性测量单元(IMU)进行磁屏蔽设计。对IMU的磁屏蔽效率进行了理论计算和有限元仿真,对磁屏蔽材料的厚度、接缝宽度及接缝处贴片的大小等参数进行了仿真分析。利用赫姆霍兹线圈对IMU进行了磁敏感性测试,实验结果表明:设计的IMU磁屏蔽结构的屏蔽效率在23~30 dB范围内,磁场引起的三个激光陀螺漂移小于0.002°/h/mT,满足高精度单轴旋转惯导系统的实用要求。该方法对旋转惯导系统的结构设计及磁屏蔽设计具有一定的参考意义。 In order to improve the adaptability of ring laser gyroscope(RLG) single-axis rotation inertial navigation system(INS) in magnetic environment,the magnetic shielding design of its inertial measurement unit(IMU) is conducted.The magnetic shielding efficiency of the IMU is calculated theoretically and simulated by finite element method.The thickness of material,width of joint and length of chock are emulated by ANSYS.By testing the IMU in Helmholtz coil,it is found that the shielding efficiency of structure is in the range of 23 to 30 dB and the RLG drift induced by magnetic field is less than 0.002 °/h/mT,which can satisfy the requirements of high precision RLG single-axis rotation INS.This method can provide some references for structure design and magnetic shielding design of the rotation INS.
出处 《中国惯性技术学报》 EI CSCD 北大核心 2012年第3期283-286,共4页 Journal of Chinese Inertial Technology
关键词 激光陀螺 磁屏蔽 有限元分析 ring laser gyroscope magnetic shielding finite element analysis
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参考文献8

  • 1Tucker T, Levison E. The AN/WSN-7B marine gyrocompass/navigator [C]//ION NTM 2000. Anaheim, CA, 26-28 January, 2000: 348-357.
  • 2Yuan Baolun, Liao Dan, Han of an optical gyro INS Measurement Science and 25102-25110. Songlai. Error compensation by multi-axis rotation[J]. Technology, 2012, 23(2):.
  • 3Joint S. Master positioning, navigation, and timing plan [R]. Washington, D.C. 20318-06002003 CJCS.31 March 2003.
  • 4王国臣.空间环路四频激光陀螺及其组成的双轴旋转惯导系统关键技术研究[D].长沙:国防科学技术大学,2010.
  • 5于旭东,王宇,张鹏飞,汤建勋,龙兴武.单轴旋转对惯导系统误差特性的影响[J].中国惯性技术学报,2008,16(6):643-648. 被引量:54
  • 6汪之国,龙兴武,王飞,袁杰.四频差动激光陀螺的磁敏感性与最佳工作点[J].光学学报,2009,29(11):3202-3206. 被引量:13
  • 7Cai H F, Zhang H, Zheng Y K. Soft magnetic devices applied for low zero excursion (0.01~/h) four-mode ring laser gyro[J]. IEEE Transactions on Magnetics, 2007, 43 (6): 2686-2688.
  • 8Richard B S, Plantz V C, Brushm D R. Shielding theory and practice[J]. IEEE Transactions on Electromagnetic, 1988, 30(8): 187-201.

二级参考文献17

  • 1金世龙,李晓红,黄云,龙兴武,周宁平.激光陀螺新型槽片[J].光学学报,2006,26(2):259-263. 被引量:7
  • 2金世龙,龙兴武,王飞,赵洪常,卢广锋,张文.激光陀螺克服高、低温冲击的技术研究[J].光学学报,2006,26(3):409-414. 被引量:19
  • 3金世龙,龙兴武,李晓红,袁杰,赵洪常.激光陀螺新型光路程长控制镜的研制[J].光学学报,2006,26(4):562-566. 被引量:16
  • 4高玉凯,林玉荣,邓正隆.改善激光陀螺输出特性的随机噪声注入方法[J].中国激光,2007,34(4):481-484. 被引量:13
  • 5Tucker T, Levison E. The AN/WSN-7B marine gyrocompass/navigator[C]//ION NTM 2000, 26-28 Anaheim, CA2000: 348-357.
  • 6Jang Q L, Chan Q P, Heung W P. Multiposition alignment of strapdown inertial navigation system[J]. IEEE Transactions on Aerospace and Electronic Systems, 1993: 1323-1328.
  • 7Dohyoung C, Jang G L, Chan G P. Strapdown INS error model for multi-position alignment[J]. IEEE Transactions on Aerospace and Electronic Systems, 1996, 32(4): 1362-1366.
  • 8Levison E, ter Horst J, Willcocks M. The next generation marine inertial navigator is here now[J]. IEEE Position Location and Navigation Symposium, 1994: 121-127.
  • 9M. Fernandez, B. Ebner, N. Dahlen. Zero-lock^TM laser gyro [C]. Guidance and control 1989: Proceedings of the Annual Rocky Mountain Guidance and Control Conference, Keystone, CO, 1989:235-241.
  • 10C. H. Volk, S. C. Gillespie, J. G. Mark et al.. Multioscillator ring laser gyroscopes and their applications[A]. D. Loukianov, R. Rodloff, H. Sorg et al.. optical gyros and their application [C]. RTO AGARDograph 339, 1999:4.1-4.26.

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