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《Engineering of Surveying and Mapping》 2005-03
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Analyses and comparisons of some strategies for nonlinear Kalman filter in GPS navigation

YANG Yuan-xi1, ZHANG Shuang-cheng2, GAO Wei-guang3 (1. Xi'an Institute of Geodesy and Geomatics, Xi'an 710054, China0 2. School of Geology Engineering and Geomatics, chang'an University, Xi'an 710054, China; 3. School of Geodesy and Geomatics, Info-science and Technology Uni., Zhengzhou 450052, China)  
Standard Kalman filter is usually adopted to deal with GPS dynamic data in navigation. Since the high order termsin linear modeling and influence of the initial value on the linear modeling isomit-ted, the reliability of the estimated statesin navigation isnot satisfied with precise kinematic GPS user. In order to choose reasonable strategies to deal with nonlinear models in filter, the extend Kalman filter, Bancroft algorithm and refined measure equationsby using surveying information are analyzed and com-pared in this paper. The estimation formulae and calculation strategy aswell asan example are given.
【Fund】: 国家自然科学基金项目(40474001和40274002)
【CateGory Index】: P228.4
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【Citations】
Chinese Journal Full-text Database 3 Hits
1 YANG Yuan xi 1, HE Hai bo 2, XU Tian he 2 (1. Xi'an Research Institute of Surveying and Mapping, Xi'an 710054,China; 2. Institute of Surveying and Mapping, Information Engineering University of PLA, Zhengzhou 450052, China);Adaptive Robust Filtering for Kinematic GPS Positioning[J];Acta Geodaetica Et Cartographic Sinica;2001-04
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【Co-citations】
Chinese Journal Full-text Database 10 Hits
1 GONG Zhen-chun, SONG Zhi-huan, Li ping (Department of Control Science and Engineering, Zhejiang University, Hangzhou, 310027, China);Coordinate Transform and Its Application in GPS Navigation of SUAV[J];Ordnance Industry Automation;2005-04
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4 Ma Jun(School of Astronautics,Beijing University of Aeronautics and Astronautics,Beijing 100083,China)Jiao Wenhai(Satellite Navigation Positioning Laboratory,Xi'an Institute of Surveying and Mapping,Xi'an 710054,China)Xiao Yelun(School of Astronautics,Beijing University of Aeronautics and Astronautics,Beijing 100083,China);Error analysis of prediction orbit determined by GLONASS ephemeris[J];Journal of Beijing University of Aeronautics and Astronautics;2005-10
5 Wang Rui Yan Peng(School of Instrument Science and Opto-electronics Engineering,Beijing University of Aeronautics and Astronautics,Beijing 100083,China)Liu Hongying(School of Science,Beijing University of Aeronautics and Astronautics,Beijing 100083,China)Zhang Guangjun(School of Instrument Science and Opto-electronics Engineering,Beijing University of Aeronautics and Astronautics,Beijing 100083,China);Visual 3D motion estimation of UAV and landing target based on extended Kalman filter[J];Journal of Beijing University of Aeronautics and Astronautics;2006-11
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7 Chen Diansheng Shao Zhihao(School of Mechanical Engineering and Automation,Beijing University of Aeronautics and Astronautics,Beijing 100191,China)Lei Xusheng(School of Instrument Science and Opto-electronics Engineering,Beijing University of Aeronautics and Astronautics,Beijing 100191,China)Wang Tianmiao(School of Mechanical Engineering and Automation,Beijing University of Aeronautics and Astronautics,Beijing 100191,China);Multiscale fyzzy-adaptive Kalman filtering methods for MEMS gyros random drift[J];Journal of Beijing University of Aeronautics and Astronautics;2009-02
8 WEI Gaosheng,ZHANG Xinxin,YU Fan,CHEN KuiMechanical Engineering School,University of Science and Technology Beijing,Beijing,100083,China;Thermal diffusivity measurements on xonotlite insulation materials by the laser-flash method[J];Journal of University of Science and Technology Beijing;2006-08
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5 Geng Jian-zhong Yao Hai-lin (AVIC Ⅰ The First Aircraft Institute,Xi'an,Shanxi,710089);Aircraft Flight State Estimation Based on Unscented Kalman Filter[A];[C];2008
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7 Ma Xing LI Jie LIU Jun Qu Yun Hong Huihui National Key Laboratory for Electronic Measurement Technology,Taiyuan 030051,China Key Laboratory of Instrumentation Science & Dynamic Measurement(North University of China),Ministry of Education Taiyuan,030051,;Application and Implementation of Kalman Filter in MEMS Gyroscope’s Random Drift Error Compensation[A];[C];2007
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【Co-references】
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【Secondary References】
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1 WU Jiangfei1 HUANG Cheng2 (1 Institute of Surveying and Mapping,Information Engineering University,66 Middle Longhai Road,Zhengzhou 450052,China) (2 Shanghai Astronomical Observatory,Chinese Academy of Sciences,80 Nandan Road,Shanghai 200030,China);Nonlinear Adaptively Robust Filter for Orbit Determination[J];Geomatics and Information Science of Wuhan University;2008-02
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