期刊文献+

GPS/INS超紧组合环路信息耦合模型及机理分析 被引量:3

Analysis on coupling model and mechanism of loop measurements in an ultra-tight GPS/INS integration
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摘要 在对不同GPS/INS超紧组合模型特点分析的基础上构建超紧组合中惯性与卫星环路信息耦合模型,提出了环路复制信号参量的外部控制方法,论证了超紧组合模型中环路信息与惯性导航结果的耦合机理.最后,进行了超紧组合耦合实验验证和分析,结果表明,超紧组合系统环路信号参量偏差与惯性状态误差间有着紧密的内在联系和深层次的耦合机理. An ultra-tightly coupled model and a method for controlling replica signals generation in the tracking loop are proposed based on the analysis of various ultra-tight GPS/INS integration model. Moreover, the intrinsic relationships between the loop measurements and INS navigation solutions in an ultra-tight GPS/INS Integration model are analyzed and demonstrated. Finally, the coupling experiments are carried out, and the experiment results indicate that there is an intrinsic relationship and a deep fusion mechanism between tracking loop measurements and INS navigation solutions in an ultra-tight GPS/INS integration model.
出处 《控制与决策》 EI CSCD 北大核心 2014年第4期611-616,共6页 Control and Decision
基金 国家自然科学基金项目(61273057 91016019) 航空科学基金项目(20100852010) 江苏高校优势学科建设工程项目 南航基本科研业务费专项科研项目
关键词 GPS INS超紧组合 组合导航 跟踪环路 耦合机理 ultra-tightGPS/INSintegration integrated navigation tracking loop coupling mechanism
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参考文献11

  • 1Soloviev A, Dickman T J. Deeply integrated GPS for indoor navigation[C]. Indoor Positioning and Indoor Navigation(IPIN). Zurich, 2010: 1-9.
  • 2Schmidt G T, Phillips R E. INS/GPS integration architectures[R]. Boston: NATO RTO Lecture Series RTO- EN-SET-116, 2011.
  • 3Landis D, Thorvaldsen T, Fink B, et al. A deep integration estimator for urban ground navigation[C]. Proc of IEEE/ION PLANS. San Diego, 2006: 927-932.
  • 4Buck T M, Wilmot J, Cook M J, et al. MEMS based, deeply integrated, INS/GPS, guidance, navigation and control flight management unit[C]. Proc of IEEE/ION PLANS. San Diego, 2006: 772-794.
  • 5Lashley M, Bevly D M, Hung J Y. Performance analysis of vector tracking algorithms for weak GPS signals in high dynamics[J]. IEEE J of Selected Topics in Signal Processing, 2009, 3(4): 661-673.
  • 6Debo Sun. Ultra-tight GPS/reduced IMU for land vehicle navigation[D]. Calgary: Department of Geomatics Engineering, Dissertation in University of Calgary, 2010.
  • 7Luke Edwards W, Benjamin J Clark, David M Bevly. Implementation details of a deeply integrated GPS/INS software receiver[C]. Proc of IEEE/ION PLANS. Indian Wells, 2010: 1137-1146.
  • 8Dyrud L, Woessner B, Jovancevic A, et al. Ultra-tightly coupled GPS/INS receiver for TSPI applications[C]. Proc of ION GNSS. Fort Worth, 2007: 2563-2572.
  • 9Paul D Groves, Petovello M G, Lachapelle G. What are the differences between the coherent and non- coherent versions of deep integration of combined inertial navigation and GNSS systems[J]. Inside GNSS, 2008, 1(3): 26-28.
  • 10Miao Jianfeng,Chen Wu,Sun Yongrong,Liu Jianye.Low C/N_0 Carrier Tracking Loop Based on Optimal Estimation Algorithm in GPS Software Receivers[J].Chinese Journal of Aeronautics,2010,23(1):109-116. 被引量:18

二级参考文献12

  • 1LIAO Bingyu YUAN Hong LIN Baojun.Smoother and Bayesian filter based semi-codeless tracking of dual-frequency GPS signals[J].Science in China(Series F),2006,49(4):533-544. 被引量:5
  • 2Giremus A, Tourneret J Y, Calmettes V. A particle filtering approach for joint detection/estimation of multipath effects on GPS measurements[J]. Signal Processing, 2007, 55(4): 1275-1285.
  • 3Miller I, Campbell M. Particle filtering for map-aided localization in sparse GPS environments[C]. IEEE Int Conf on Robotics and Automation. Pasadena, 2008:1834-1841.
  • 4Aggarwal P, Syed Z, E1-Sheimy N. Hybrid extended particle filter(HEPF) for integrated civilian navigation system[C]. IEEE/ION Position, Location and Navigation Symposium. Monterey, 2008: 984-992.
  • 5Schon T, Gustafsson F, Nordlund P J. Marginalized particle filters for mixed linear/nonlinear state-space models[J]. IEEE Trans on Signal Processing, 2005, 53(7): 2279-2289.
  • 6Kotecha J H, Djuri6 P M. Gaussian particle filtering[J]. IEEE Trans on Signal Processing, 2003, 5t(10): 2592- 2601.
  • 7Wu Y X, Hu D W, Wu M P, et al. Quasi-Gaussianparticle filtering[C]. Int Conf on Computational Science. Glasgow, 2006: 689-696.
  • 8Yang D K, Zhou X L. U-GPF information fusion algorithm for GPS/DR integrated positioning systemiC]. Int Conf on Machine Learning and Cybernetics. Hong Kong, 2007: 1424-1427.
  • 9Kotecha J H, Djurik P M. Gaussian sum particle filtering[J]. IEEE Trans on Signal Processing, 2003, 51(10): 2603- 2613.
  • 10Schon T, Gustafsson F, Nordlund P J. Marginalized particle filters for mixed linear/nonlinear state-space models[J]. IEEE Trans on Signal Processing, 2005,53(7): 2279-2289.

共引文献29

同被引文献82

  • 1YANG Yuanxi1 & WEN Yuanlan2 1. Xi’an Research Institute of Surveying and Mapping, Xi抋’an 710054, China,2. College of Aerospace and Material Engineering, National University of Defense Technology, Changsha 410073, China.Synthetically adaptive robust filtering for satellite orbit determination[J].Science China Earth Sciences,2004,47(7):585-592. 被引量:23
  • 2杨元喜,任夏,许艳.自适应抗差滤波理论及应用的主要进展[J].导航定位学报,2013,1(1):9-15. 被引量:86
  • 3陈家斌,袁信.惯性速度辅助下GPS/捷联惯导组合系统性能研究[J].南京航空航天大学学报,1994,26(6):730-736. 被引量:4
  • 4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
  • 5Alban S. Performance analysis and architectures for INS-aided GPS track~.ng loops[C]//Proc, of the National Technical Meet- ing of the Institute of Navigation, 2003.. 22 - 24.
  • 6Copps E M, Geier G J, Fidler W C, et al. Optimal processing of GPS signals[J]. Journal of the Institute of Navigation, 1980, 27 (3):171-182.
  • 7Horslund J M, Hooker J R. Increase jamming immunity by opti- mizing processing gain for GPS/INS systems[P]. United States Patent 5983160,1999.
  • 8Gustafson D, Dowdle J, Flueckiger K. A deeply integrated adaptive GPS-based navigator with extended range code tracking[C]//Proc. of the IEEE Plans, 2000 : 118 - 124.
  • 9Lewis D. Ultra-tightly coupled GPS/INS tracking performance[C]// Proc. of the AIAA ' s 3rd Annual Aviation Technology , Integra- tion, and Operations Forum, 2003 : 1 - 7.
  • 10Timothy M, Buck A, High G. MEMS based, deeply integrated, INS/GPS, guidance, navigation and control flight management unit[C]//Proc, of the IEEE / ION on Position, Location, and Navigation Symposium, 2006 .. 772 - 794.

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