期刊文献+

陆地车辆GNSS/MEMS惯性组合导航机体系约束算法研究 被引量:3

Body Frame Constraint for a GNSS/MEMS INS Integrated System in Land Vehicle Navigation
下载PDF
导出
摘要 针对陆地车辆导航应用,基于速度特性建立了机体系约束用以提高卫星导航系统(GNSS)/微硅机械(MEMS)惯性组合导航系统的性能.该约束将与车体运动方向相垂直的平面上的线速度近似为0,从而增加了组合系统的扩展卡尔曼滤波时间上连续的两维虚拟观测量,卫星信号失效时可保持滤波器的量测更新,当无外部观测量且车辆处于动态情况下,滤波可持续估计与反馈.车载实验表明,组合系统在卫星信号失效30s时,采用该算法可以将系统的定位精度提高约75%,姿态精度及速度精度也有相应的提高. For global navigation satellite system(GNSS) and micro-electro mechanical system (MEMS) inertial navigation system (INS) integrated system in land vehicle application, a particular constraint based on features of a vehicle's motion is setup on its body frame to improve the system performance. Body frame constraint limits the velocities along the plane perpendicular to the vehicle's moving direction to approximate zero, which accordingly introduces couple of additionally virtual measurements into the extended Kalman filter (EKF) that is typically applied for two systems fusion. Thanks to those virtual measurements, the EKF is able to keep its measurement updates even over GNSS signal outage period. The filter continuously produces error estimations and feedbacks during the absence of external observables from GNSS, whatever the vehicle's dynamics is. The field test indicates that the system accuracy of positioning can be improved by 75% over 30 s GNSS outages and the accuracy of attitude and velocity is improved as well.
出处 《北京理工大学学报》 EI CAS CSCD 北大核心 2013年第5期510-515,共6页 Transactions of Beijing Institute of Technology
基金 国家自然科学基金资助项目(61173076)
关键词 MEMS惯性导航系统 卫星导航 组合导航 机体系约束 扩展卡尔曼滤波 MEMS intertial navigation system(INS) global navigation satellite system (GNSS) integrated navigation body frame constraint extended Kalman filter (EKF)
  • 相关文献

参考文献10

  • 1Veth M, Raquet J. Fusion of low-cost imaging and inertial sensors for navigation[C] // Proceedings of the 19th International Technical Meeting of the Satellite Division of the Institute of Navigation. Fort Worth, USA: ION, 2006:1093-1103.
  • 2Hopkins R, Miola J, Sawyer W. The silicon oscillating accelerometer: a high-performance MEMS accelero- meter for precision navigation and strategic guidance ap- plieation[R]. The Charles Stark Draper Laboratory, 2005:970- 979.
  • 3李荣冰,刘建业,曾庆化,华冰.基于MEMS技术的微型惯性导航系统的发展现状[J].中国惯性技术学报,2004,12(6):88-94. 被引量:91
  • 4康岳林,高杨,高立.基于MEMS的GPS/SINS组合导航技术发展现状[J].船电技术,2011,31(5):26-29. 被引量:3
  • 5秦永元,张洪钺,汪淑华.卡尔曼滤波与组合导航原理[M].西安:西北工业大学出版社,2010:33-48.
  • 6付相松,高社生,张学渊.基于MEMS技术的车载组合导航系统研究[J].计算机测量与控制,2009,17(2):338-341. 被引量:7
  • 7马建仓,陈静.MEMS SINS-GPS组合导航系统设计[J].传感技术学报,2009,22(10):1437-1441. 被引量:12
  • 8Johannes M, Poison N. Particle filtering[M]. Berlin:Handbook of Financial Time Series, 2009.
  • 9Grewal M S, Andrews A P. Kalman filtering theory and practice[M]. Hoboken: John Wiley Sons, Inc,2001.
  • 10Shin Eun-Hwan, Naser E1-Sheimy. Accuracy improvement of low cost INS/GPS for land applications [C] /// Proceedings of the 2002 National Technical Meeting of the Institute of Navigation. San Diego, USA: ION,2002:146 - 157.

二级参考文献39

共引文献116

同被引文献17

引证文献3

二级引证文献17

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