期刊文献+

双轴旋转式SINS自主标定技术 被引量:6

Self-calibration for dual-axis rotary SINS
下载PDF
导出
摘要 在双轴旋转式SINS中,惯性元件常值漂移误差对系统的影响可以得到调制,但安装误差和标度因数误差对系统的影响无法得到调制,同时这些误差会与旋转角速率耦合,引起速度锯齿波等误差从而降低了系统的各项性能指标。为了减少这种影响,分析了光学陀螺双轴旋转式SINS误差传播特性,利用奇异值分解法对系统的可观测程度进行了分析,经分析,与转动轴相关的安装误差和标度因数误差的可观测度较好,据此设计了系统的自主标定方案及滤波算法,进行了数字仿真和半实物仿真验证试验。试验结果表明,利用设计的自主标定方案,在1 h内能估计出转轴上两个陀螺的标度因数误差及与转轴相关的四个安装误差,估计精度能达到95%以上。导航试验验证表明,利用自主标定的参数,相对于传统标定方法,使系统定位精度提高了20%。 In strapdown inertial navigation system, the dual-rotary modulation can completely eliminate the inertial elements constant errors of the three axes to improve the system accuracy. But the error caused by the misalignment angles and the scale factor error cannot be eliminated through dual-rotary modulation. These errors could also cause sawtooth wave velocity errors due to coupling with rotation rates. In this paper, the self-calibration of dual-axis is studied to eliminate these errors. The error models of the dual-axis rotary SINS are established, and the calibration scheme was designed based on the sixteen sequence index. Then, the PWCS observation and Kalman filter were used to analyze the observability and estimate the error factors. The results of simulation and experiments show that the designed methods are effective, and the estimation value can get 95% of the set value, the position error is reduced by 20%.
出处 《中国惯性技术学报》 EI CSCD 北大核心 2012年第2期146-151,共6页 Journal of Chinese Inertial Technology
基金 武器装备重点预研基金项目(014A0903108001)
关键词 自主标定技术 双轴旋转调制 捷联惯性导航系统 PWCS可观测分析 卡尔曼滤波技术 self-calibration dual-axis rotary modulation SINS PWCS observability analysis Kalman filter
  • 相关文献

参考文献6

二级参考文献12

共引文献130

同被引文献41

  • 1袁保伦,饶谷音.光学陀螺旋转惯导系统原理探讨[J].国防科技大学学报,2006,28(6):76-80. 被引量:68
  • 2黄凤荣,高峰,付中泽,蒋茂荣,孙伟强.基于小波滤波的激光陀螺SINS晃动基座初始对准[J].中国惯性技术学报,2014,12(2):157-160. 被引量:8
  • 3Levinson E,Majure R. Accurary enhancement techniques applied to the marine ring laser inertial navigator(MARLIN)[J].Journal of the Institute of Navigation,1987,(01):64-86.
  • 4Yuan Ballun,Liao Dan,Han Songlai. Error compensation of an optial gyro INS by multi-axis rotation[J].Measure-ment Science and Technology,2012,(02):025102.1-025102.9.
  • 5Xie Bo,Qin Yongyuan,Wan Yanhui. A high-accuracy calibration method of optical gyro SINS[A].Harbin,2010.507-510.
  • 6Zhang Hongliang,Wu Yuanxin,Wu menqi. Improved multi-position calibration for inertial measure-ment unit[J].Measurement Science and Technology,2010,(01):015107.1-01510711.
  • 7Savage P G. Strapdown analytics[A].Minnesota:Strapdown Associates,Ins,2007.
  • 8Kenneth R. Britting. Inertial navigation systems analysis[M].Artech House Publishers,2010.
  • 9Bekkeng J K. Calibration of a novel MEMS inertial reference unit[J].IEEE Transactions on Instrumentation and Measurement,2009,(06):1967-1974.
  • 10Bekkeng J K. Calibration of a novel MEMS inertial refer-ence [J], IEEE Transactions on Instrumentation andMeasurement, 2009,58(6) : 1967 — 1974.

引证文献6

二级引证文献25

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