期刊文献+

基于EKPF的GPS导航模型研究 被引量:2

STUDY ON GPS NAVIGATION MODEL BASED ON EKPF
下载PDF
导出
摘要 通过模拟GPS卫星系统的运行以及接收机的运动轨迹,采用11状态PVA(Position-Velocity-Acceleration)导航模型进行导航定位分析,并分别采用扩展卡尔曼粒子滤波和扩展卡尔曼滤波计算导航解,结果表明两种滤波均能得出较好导航解,并且前者削弱了多路径效应的影响,进一步提高了导航定位精度,尤其在高程方向精度提高更为明显。 In order to assess the system performance, the GPS constellation and the moving trajectory of receiver are simulated, a 11-dimensional state Position-Velocity-Acceleration (PVA) navigation model is used for analysis. The EKF and EKPF model are separately adopted to obtain the navigation solution, the simulated results show that both the two models are satisfactory, while the navigation performance of the proposed EKPF algorithm is superior to EKF, especially in vertical direction, and impact of multipath effect has been reduced.
出处 《大地测量与地球动力学》 CSCD 北大核心 2013年第2期139-142,共4页 Journal of Geodesy and Geodynamics
基金 江苏高校优势学科建设工程资助项目(PAPD) 国土资源部公益性行业科研专项(201011015-2)
关键词 GPS导航 导航模型 粒子滤波 扩展卡尔曼滤波 扩展卡尔曼粒子滤波 GPS navigation navigation model particle filter(PF) extended Kalman filter(EKF) extended Kal- man particle filter
  • 相关文献

参考文献10

二级参考文献36

  • 1李乡儒,吴福朝,胡占义.均值漂移算法的收敛性[J].软件学报,2005,16(3):365-374. 被引量:88
  • 2王新洲.GPS基线向量网粗差定位试验[J].武汉测绘科技大学学报,1995,20(2):157-162. 被引量:12
  • 3高为广,杨元喜,崔先强,张双成.IMU/GPS组合导航系统自适应Kalman滤波算法[J].武汉大学学报(信息科学版),2006,31(5):466-469. 被引量:40
  • 4聂建亮,张卉.基于自适应Kalman滤波的BP神经网络在导航中的应用[J].大地测量与地球动力学,2007,27(3):56-59. 被引量:4
  • 5Gordon N J, Salmond D J and Smith A F M. Novel approach to nonlinear/non-Gaussian Bayesian state estimation [ J ]. IEE Proceedings-f, 1993,140 (2) : 107 - 113.
  • 6De Freitas M J F G, et al. Sequential Monte Carlo methods to train neural network models [ J ]. Neural Computation, 2000,12:955 - 993.
  • 7Fagin S L. Recursive linear regression theory, optimal filter theory and error analysis of optimal system [ J ]. IEEE Int. Convert, Record, 1964,12:216 - 240.
  • 8Sorenson H W and Sacks J E. Recursive fading memory filtering[J]. Inform, SCI,1971,3:101 - 119.
  • 9Rudolph van der Merwe. Sigma-point Kalman filters for probabilistic inference in dynamic state - space models [ D]. Oregon Health & Science University,2004.
  • 10Doucet A, Gordon N J and Krishanmurthy V. Particle filters for state estimation of jump Markov linear systems [ J ]. IEEE Trans on Signal Processing, 2001,49 (3) :613 -624.

共引文献52

同被引文献20

  • 1聂士忠.Vondrak数据平滑方法及其在微机上的实现[J].石油大学学报(自然科学版),1994,18(4):111-114. 被引量:13
  • 2李德仁,袁修孝.误差处理与可靠性理论[M].武汉:武汉大学出版社,2012.
  • 3de Marina H G,Pereda F J,Giron-Sierra J M,et al.UAV attitude estimation using unscented Kalman filter and TRIAD[J].IEEE Transactions on Industrial Electronics,2012,59(11):4465-4474.
  • 4Brown R G,Hwang P Y C.Introduction to random signals and applied Kalman filtering[M].New York:John Wiley & Sons,1992.
  • 5Jwo D J,Yang C F,Chuang C H,et al.A novel design for the ultra-tightly coupled GPS/INS navigation system[J].Journal of Navigation,2012,65(4):717-747.
  • 6Li Y,Efatmaneshnik M,Dempster A G.Attitude determination by integration of MEMS inertial sensors and GPS for autonomous agriculture applications[J].GPS Solutions,2012,16(1):41-52.
  • 7Wang W,Liu Z,Xie R.Quadratic extended Kalman filter approach for GPS/INS integration[J].Aerospace Science and Technology,2006,10(8):709-713.
  • 8Julier S J,Uhlmann J K,Durrant-Whyte H F.A new approach for filtering nonlinear systems[C]// Proceedings of the 1995 American Control Conference.Seattle,1995:1628-1632.
  • 9Gordon N J,Salmond D J,Smith A F M.Novel approach to nonlinear/non-Gaussian Bayesian state estimation[J].Radar and Signal Processing,1993,140(2):107-113.
  • 10Rigatos G G.Nonlinear Kalman filters and particle filters for integrated navigation of unmanned aerial vehicles[J].Robotics and Autonomous Systems,2012,60(7):978-995.

引证文献2

二级引证文献4

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