期刊文献+

基于逆坐标系的极区传递对准技术研究 被引量:5

Polar Transfer Alignment Research Based on Inverse Coordinate System
下载PDF
导出
摘要 针对舰船惯导在极区导航时,高纬度地区经度线快速收敛导致传统基于地理坐标系的传递对准模型和方程不适用的问题,文中提出了一种基于逆坐标系的传递对准方法。设计了基于逆坐标系的"速度+姿态"匹配传递对准的滤波模型,对舰船主子惯导之间的固定安装误差角进行估计,解决了在高纬度以及极区附近无法进行传递对准的问题。通过仿真验证了该算法的有效性。 A new transfer alignment algorithm was introduced for ship INS navigating in polar regions. Since rapid convergence of the Earth' s meridians, the transfer alignment model and equations based on the traditional geographic coordinate system were no longer appli- cable. To solve the problem, an inverse coordinate system was employed in this paper. A " velocity and attitude" matching Kalman filter was designed to estimate the fixed misalignment angle between MINS and SINS. The simulation results show that the algorithm is effective.
出处 《弹箭与制导学报》 CSCD 北大核心 2014年第4期179-182,186,共5页 Journal of Projectiles,Rockets,Missiles and Guidance
关键词 传递对准 极区导航 逆坐标系 卡尔曼滤波 transfer alignment polar navigation inverse navigation Kalman filter
  • 相关文献

参考文献8

二级参考文献51

  • 1孙昌跃,王司,邓正隆.舰载武器惯导系统对准综述[J].中国惯性技术学报,2005,13(3):81-88. 被引量:19
  • 2王有隆.北极地区飞行中的通信与导航特性[J].航空维修与工程,2006(1):46-48. 被引量:15
  • 3Chatfield A B.Fundamentals of high accuracy inertial navigation[M].USA:AIAA,1997:129-149.
  • 4Titterton D H,Weston J L.Strapdown inertial navigation technology[M].2nd Ed..UK:The Institution of Electrical Engineers,2004:25.
  • 5杨在金.航海仪器[M].大连海事大学出版社,19983.
  • 6Tarrant D, Roberts C, Jones D,et al. Rapid and robust transfer alignment[A]. IEEE Proceedings of Aerospace Control Systems[C], 1993: 758-762.
  • 7Klotz H A Jr, Derbak C B. GPS-aided navigation and unaided navigation on the joint direct attack munition[A]. IEEE Position Location and Navigation Symposium[C], 1998: 412-419.
  • 8Kain J E, Cloutier J R. Rapid transfer alignment for tactical weapon applications[R]. AIAA-89-3581.
  • 9Shortelle K J, Graham W R, Rabourn C. F-16 flight tests of a rapid transfer alignment procedure[A]. IEEE Position Location and Navigation Symposium[C], 1998:379-386.
  • 10Graham W R, Shortelle K J. Rapid alignment prototype (RAP) flight test demonstration[A]. System Dynamics International[R]. 1997, No. ISG-97-01: 30.

共引文献107

同被引文献28

引证文献5

二级引证文献7

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