期刊文献+

光纤惯导系统连续旋转对准技术研究 被引量:5

Initial Alignment of Rotation-modulation Strapdown Inertial Navigation System
在线阅读 下载PDF
导出
摘要 初始对准是惯性导航的关键技术之一,对准结果会直接影响系统的导航精度。针对光纤陀螺惯导系统,缩短对准时间、提高系统对准精度等技术难点,开展了高精度光纤惯导系统连续旋转对准技术研究,深入分析了常值陀螺漂移、随时间变化的陀螺漂移、陀螺标度因数常值误差、陀螺标度因数不对称误差、陀螺安装误差、陀螺随机游走等误差项对系统对准精度的影响,对比了现有旋转方案的优点与不足,提出了一种改进的单轴二位置旋转方案。试验结果表明,在采用该旋转方案的情况下,对准时间8min方位角对准精度可达到30″(1σ),具有重要的工程应用价值。 The initial alignment technology is one of the key technology of inertial navigation, and its precision will affect the navigation result. Studying of the initial alignment of rotation-modulation strapdown inertial navigation system in order to shorten the alignment time and improve alignment accuracy. Analyzing the errors of IMUs that impact the precision of navi- gation system, include the constant drift of gyro, the drift over time of gyro, the constant error of scale factor of gyro, the asymmetric error of scale factor of gyro, gyro misalignment, the random error of gyro and so on. Compare the advantages and disadvantages of the existing rotation scheme, proposed an improved single-axis rotation scheme second position. The result of experiment show that the heading error is less than 30" after 8min initial alignment experiments in the scheme, the scheme has great merits in engineering applications.
出处 《导航定位与授时》 2016年第2期1-6,共6页 Navigation Positioning and Timing
关键词 惯导系统 旋转调制 误差分析 旋转方案 Navigation system Rotation modulation Error analysis Rotating scheme
  • 相关文献

参考文献6

  • 1Li An, Chang Guobin, Qin Fangjun, et al. Improvedprecision of strapdown inertial navigation system brought by dual-axis con- tinuous rotation of inertial measurement unit [ C ]//2010 2"a In- ternational Asia Conference on Informatics in Control, Automation and Robotics. 2010: 284-287.
  • 2高钟毓.惯性导航技术[M].北京:清华大学出版社,2012:224-253.
  • 3Banerjee K, Dam B, Majumdar K, et al. An improveddither- stripping scheme for strapdown ring laser gyroscopes [ J ]. IEEE Transaction on Aerospace and Electronic Systems, 2004, 7 (2) : 54-59.
  • 4翁海娜,陆全聪,黄昆,张宇飞,杨功流.旋转式光学陀螺捷联惯导系统的旋转方案设计[J].中国惯性技术学报,2009,17(1):8-14. 被引量:69
  • 5Yuan Baolun, Liao Dan, Han Songlai. Error compensation of an optical gyro multi-axis rotation [ J ]. Measurement Science and Technology, 2012, 23 (2): 297-301.
  • 6可伟,乔海岩,孟凡强.船用激光陀螺惯导单轴旋转系统[J].舰船科学技术,2012,34(12):67-71. 被引量:3

二级参考文献9

  • 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:70
  • 2颜苗,翁海娜,谢英.系统参数标定以及惯性元件安装误差测量与补偿技术研究[J].中国惯性技术学报,2006,14(1):27-29. 被引量:30
  • 3王其,徐晓苏.旋转IMU在光纤捷联航姿系统中的应用[J].中国惯性技术学报,2007,15(3):265-268. 被引量:33
  • 4Lahham J I, Wigent D J, Coleman A L. Tuned support structure for structure-borne noise reduction of inertial navigator with dithered ring laser gyros(RLG)[C]//Proceedings of the IEEE Position Location and Navigation Symposium, 2000:419-428.
  • 5Levinson E, ter Horst J, Willcocks M. The Next Generation Marine Inertial Navigator is Here Now[C]//Proceedings of the IEEE Position Location and Navigation Symposium, 1994:121-127.
  • 6Titterton D H, Weston J L. Strapdown Inertial Navigation Technology[M]. Second Edition. Lexington, Massachusetts, USA. Copublished by the American Institute of Aeronautics and Astronautics and the Institution of Electrical Engineers, 2004: 342-344.
  • 7LEVINSON E,GIOVANNI C S. Laser gyro potential for long endurance marine navigation [ C ]. IEEE Position Location and Navigation Symposium. 1980 : 115 - 129.
  • 8HIBBARD R, WYLIE B, LEVISON E. Sperry marine MK- 49,the world best ring laser gyro ships inertial navigation system [ C ]. JSDE Proceedings, Orlando, FL, November, 1996.
  • 9许国帧.惯性技术手册[M].北京:宇航出版社,1995.

共引文献70

同被引文献31

引证文献5

二级引证文献21

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