期刊文献+

基于匀速率26位置法的iIMU-FSAS光纤陀螺仪标定 被引量:4

iIMU-FSAS FOG calibration based on uniform-rate 26-position method
下载PDF
导出
摘要 针对iIMU-FSAS光纤陀螺仪静态26位置法标定结果无法收敛的问题,提出了由外框轴提供稳定转速的匀速率26位置法标定方案,从理论上与静态26位置法进行了对比分析;采用该方法对i IMU-FSAS陀螺仪进行了多天的标定实验,结合静态26位置法有限次迭代的结果,对匀速率26位置法标定参数(零偏、标度因数和安装误差)的合理性和重复性等进行了分析。结果表明:与静态26位置法相比,匀速率26位置法的标定结果不仅能够收敛,且标定结果合理、性能稳定。 To solve the non-convergence problem of the static 26-position method in calibrating i IMU-FSAS fiber optic gyroscope, a uniform-rate 26-position method based on 12-parameter error model is proposed, in which the three-axis turntable is required to be able to provide stable angular rate along outer-axis to improve the gyro's input level. To test this new method, the experiments based on the i IMU-FSAS gyroscope are made for several days, and then the rationality and repeatability analysis are made through comparing the calibration results(bias, scale factor and installation error) between the static 26-position method using limited iterations and the proposed method. Experiment results show that, compared with the static 26-position method, the results by the new method is convergent, more reasonable and repeatable.
作者 刘万科 宋宇 朱锋 朱智勤 LIU Wan-ke SONG Yu ZHU Feng ZHU Zhi-qin(School of Geodesy and Geomatics, Wuhan University, Wuhan 430079, China Collaborative Innovation Center of Geospatial Technology, Wuhan University, Wuhan 430079, China Key Laboratory of Geospace Environment and Geodesy of Ministry of Education, Wuhan University, Wuhan 430079, China Wuhan Hi-Target Digital Cloud Technology Co. Ltd., Wuhan 430000, China)
出处 《中国惯性技术学报》 EI CSCD 北大核心 2017年第1期103-108,共6页 Journal of Chinese Inertial Technology
基金 国家重点研发计划项目(2016YFB0501803) 国家自然科学基金(91638203)
关键词 匀速率26位置法 静态26位置法 iIMU-FSAS光纤陀螺仪 标定参数 uniform rate 26-position method static 26-position method i IMU-FSAS FOG calibration parameter
  • 相关文献

参考文献4

二级参考文献25

  • 1刘西河,宋有山.任意初始位置平台误差模型自标定[J].中国惯性技术学报,1994,2(1):30-34. 被引量:5
  • 2Rogers R M.Applied mathematics in integrated navigation systems[C]//American Institute of Aeronautics and Astronautics,Inc.,2007. 被引量:1
  • 3Bekkeng J K.Calibration of a novel MEMS inertial reference unit[J].IEEE Transactions on Instrumentation and Measurement,2009,58(6):1967-1974. 被引量:1
  • 4Syed Z F,Aggarwal P,Goodall C,et al.A new multi-position calibration method for MEMS inertial navigation systems[J].Measurement Science and Technology,2007,18:1897-1907. 被引量:1
  • 5Yun Cho Seong,Gook Park Chan.A calibration technique for a redundant IMU containing low-grade inertial sensors[J].ETRI Journal,2005,27(4):418-425. 被引量:1
  • 6Seong-hoon P W,Farid G.A triaxial accelerometer calibration method using a mathematical model[J].IEEE Trans.on Instrumentation and Measurement,2010,59(8):2144-2152. 被引量:1
  • 7Zhang H L,Wu Y X,Wu W Q,et al.Improved multiposition calibration for inertial measurement units[J].Measurement Science and Technology,2010,21(1):151-158. 被引量:1
  • 8Cao Y,Cai H,Zhang S F,et al.A new continuous self-calibration scheme for a gimbaled inertial measurement unit[J].Meas.Sci.Technol.,2012,23(1):151-154. 被引量:1
  • 9Fong W T,Ong S K,Nee A Y C,et al.Methods for infield user calibration of an inertial measurement unit without external equipment[J].Meas.Sci.Technol.,2008,19(7):1-11. 被引量:1
  • 10Dan S.Optimal state estimation-Kalman,H∞and nonlinear approaches[M].John Wiley&Sons,2006:79-102. 被引量:1

共引文献57

同被引文献27

引证文献4

二级引证文献22

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部