期刊文献+

旋转调制式捷联惯导系统初始对准方案研究 被引量:2

Initial Alignment of Rotation-modulatioin Strapdown Inertial Navigation System
下载PDF
导出
摘要 初始对准技术是惯性导航的关键技术之一,其精度将直接影响导航精度。旋转调制式捷联惯导系统在一定的旋转方案下虽然可以将惯性组件的误差调制掉从而提高系统导航精度,但其初始对准的误差则不受调制,所以有必要对旋转调制式惯导系统的初始对准进行深入研究,确定适合旋转式捷联系统使用的对准技术和方案以进一步提高系统精度。文章对可应用于旋转调制式捷联惯导系统的三种对准方案做了研究分析并进行了仿真。结果显示,二位置对准方案可显著提高系统变量的可观测度,连续旋转方案对准精度最高,收敛速度最快,效果最好。 The initial alignment technology is one of the key technology of inertial navigation,and its precision will affect the navigation result.Based on certain scheme,the rotation-modulation strapdown system can modulate the errors of IMUs,therefore the precision of navigation system can be improved.But the errors of initial alignment of the system can not be modulated.So it is essential to study the initial alignment technology of rotation-modulation system and find a proper alignment scheme for such systems.In this paper,three schemes that can be used in rotaion-modulation systems are studied and analysed,at last the schemes are simulated.The results prove that the two-position scheme can improve the observability of system variables and the continous-rotaion scheme provides the best prcision,highest speed and best effects.
机构地区 海军工程大学
出处 《舰船电子工程》 2010年第8期63-65,共3页 Ship Electronic Engineering
关键词 旋转调制 二位置对准 奇异值分解 可观测度 rotation-modulatin two position alignment SVD observability
  • 相关文献

参考文献5

二级参考文献13

  • 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:32
  • 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.
  • 7万德钧 房建成.惯导系统初始对准[M].南京:东南大学出版社,1998.100-106.
  • 8Goshen-Meskin D,Bar-Itzhack I Y.Observability analysis of piece-wise constant systems-part Ⅰ:Theory[J].IEEE Transaction on Aerospace and Electronic Systems,1992,28(4).
  • 9Goshen-Meskin D,Bar-Itzhack I Y.Observability analysis of piece-wise constant systems-part Ⅱ:Application to inertial navigation in-flight alignment[J].IEEE Transaction on Aerospace and Electronic Systems,1992,28(4).
  • 10Jiang Y F,Lin Y P.Error estimation of INS ground alignment through observability analysis[J].IEEE Transaction on AES,1992 28(1):92-97.

共引文献80

同被引文献15

  • 1程建华,赵琳,宋君才,李刚,彭小兰.自动补偿技术在平台惯导系统状态切换中的应用研究[J].哈尔滨工程大学学报,2005,26(6):744-748. 被引量:5
  • 2H Jiang, W Q Yang. State Space Modeling of Random Drift Rate in High Precision Gyro [ J ]. IEEE Trans on AES, 32 ( 3 ) : 1138 - 1143.
  • 3D Goshen - Meskin, I Y Bar - Itzhack. Unified approach to iner- tial navigation system error modeling[ J]. AIAA: Journal of Guid- mace, Control, and Dynamics, 1992,15(3):648-653.
  • 4钱伟行.捷联惯导与组合导航系统高精度初始对准技术研究[D].南京航空航天大学,2009.
  • 5Xu Bo, Sun Feng. An Independent Damped Algorithm based on SINS for ShipC//International Conference on Computer Engineering and Technology, 2009 .. 88-92.
  • 6GAO Wei,ZHANG Yi, XU Bo,etc. Analysis of Damping Net- work Effect on SINS[C].//Proeeedings often 2009 IEEE International Conference on Mechatronics and Automation, Chang- chun, China: IEEE, 2009 : 2530-2536.
  • 7张德丰.Matlab小波分析与IT程应用[M].北京:国防工业出版社,2007:1617.
  • 8张小跃,张春熹,宋凝芳.基于组合导航技术的光纤捷联系统在线标定[J].航空学报,2008,29(6):1656-1659. 被引量:23
  • 9卫育新,白俊卿.车载SINS/DR组合导航系统的在线标定方法[J].中国惯性技术学报,2009,17(6):651-653. 被引量:20
  • 10吴平,雷虎民,邵雷,王飞.一种车载筒弹惯导装置不开箱标定方法[J].中国惯性技术学报,2010,18(1):28-32. 被引量:13

引证文献2

二级引证文献6

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