期刊文献+

惯性/双星间断伪距约束定位 被引量:1

Discontinuous Pseudo Range Constrained Inertial/Double Satellites Integrated Positioning
下载PDF
导出
摘要 针对目前GNSS/INS组合导航算法在卫星信号失效后定位精度下降、系统易于发散的不足,提出了一种新的少可见星组合定位方法。在只有2颗可见星的情况下,利用多个时刻的两星位置信息、伪距信息以及惯性测量的相对运动信息,可以获得稳定、可信的定位结果,且不受惯导既有位置误差的影响,仿真验证了算法的正确性与有效性。 Considering the problems of the aecuracy deeline and the divergence of integrated filtering during outages of satellite signal in GNSS/INS integrated navigation, we proposed a new integrated navigation algorithm. With only two visible satellites, the algorithm can obtain stable and reliable positioning result by utilizing the position information and discontinuous pseudo ranges of the two satellites, and the relalive movemenl information at different moments. The positioning result is independent of the existing inertial navigation errors. The correctness and effectiveness of this algorithm are verified through simulations.
出处 《电光与控制》 北大核心 2016年第8期6-9,22,共5页 Electronics Optics & Control
基金 中国航天集团公司卫星应用研究院创新基金(2014-CXJJDH-06) 自然基金国际(地区)合作与交流项目(61320106010)
关键词 组合导航 双星 伪距约束 间断测量 integrated navigation double satellites pseudo range constraint discontinuous measurement
  • 相关文献

参考文献11

二级参考文献24

  • 1陈家斌,袁信.伪距解除相关法在GPS/SINS紧组合系统中的应用研究[J].航空学报,1995,16(6):707-710. 被引量:8
  • 2Yi Y D. Grejner-Brzezinska, Dorota A. Tightly-coupled GPS/INS integration using unscented Kalman filter and particle filter [C]//ION GNSS, 2006: 2182-2191. 被引量:1
  • 3Zhang Y F, Gao Y. Performance Analysis of a Tightly Coupled Kalman Filter for the Integration of Un-differenced GPS and Inertial Data [C]//ION National Technical Meeting, 2005: 270-275. 被引量:1
  • 4He X F, Hu X P, Wu M P, Qin H L. SINS/GPS Tightly Integrated Navigation Algorithm for Land Vehicle Applications [C]// Proceedings of the 26th Chinese Control Conference, 2007: 400-403. 被引量:1
  • 5James Bao-Yen Tsui. Fundamentals of Global Positioning System Receivers A Software Approach [M]. John Wiley & Sons, Inc, 2005. 被引量:1
  • 6Dong L. IF GPS Signal Simulator Development and Verification [D]. MS D Thesis, Calgary University, 2003. 被引量:1
  • 7Jan Wendel. Comparison of Extended and Sigma-Point Kalman Filters for Tightly Coupled GPSffNS Integration [R]. AIAA 2005-6055, 2005. 被引量:1
  • 8泰永元.卡尔曼滤波与组合导航原理[M].西安:西北工业大学出版社,1998.. 被引量:3
  • 9Evans,C.D.,Riggins,R.The design and analysis of integrated navigation systems using real INS and GPS data[C].Proceedings of the IEEE 1995 NEACON. 被引量:1
  • 10FRITZ J, RUSS D H. Integrated global positioning system and inertial navigation system integrity monitor performance [ D ]. Ohio, Athens : Ohio University, 2003:36-65. 被引量:1

共引文献66

同被引文献11

引证文献1

二级引证文献16

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