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《Journal of Chinese Inertial Technology》 2011-02
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Improved algorithm for high dynamic strapdown inertial navigation system

ZHAO Xin,WANG Shi-cheng,YANG Dong-Fang,GAO Yun-guang,LUO Da-cheng (1.The Second Artillery Engineering College,Xi'an 710025,China; 2.Department of Computer Science and Technology,Tsinghua University,Beijing 100084,China)  
To accurately compensate the large coning error aroused by high dynamic circumstance,an improved three-sample multi-loop equivalent rotation vector iterative algorithm is presented.Firstly,the paper analyses the influence to SINS brought by high dynamic circumstance,and expatiates the basic theory of strapdown solution.Then several main attitude solution algorithms are compared and contrasted.To solve the problem that common algorithms can not compensate the coning error perfectly,this paper,based on the multi-sample dual-loop equivalent rotation vector iterative algorithm,considers the algorithm performance from heightening precision and reducing calculation,and studies an improved three-sample multi-loop equivalent rotation vector iterative algorithm.Finally,the performance of the proposed algorithm is analyzed.The low-dynamic testing experiment and high dynamic simulation experiment results show that the attitude accuracy of the improved algorithm is similar to that of Peano Baker quaternion numbers in low dynamic conditions,but is higher than the attitude accuracy of Peano Baker quaternion numbers by 3 orders of magnitude in high dynamic conditions.
【Key Words】: SINS attitude solution equivalent rotation vector high dynamic circumstance
【Fund】: 国家863课题资助项目(2009AA7050411);; 国家自然科学基金(60572061)
【CateGory Index】: V249.322
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【Citations】
Chinese Journal Full-text Database 4 Hits
1 ZHANG Rong-hui1,2,JIA Hong-guang1,CHEN Tao1,ZHANG Yue1(1.Changchun Institute of Optics,Fine Mechanics and Physics,Chinese Academy of Sciences,Changchun 130033,China;2.Graduate University of Chinese Academy of Sciences,Beijing 100039,China);Attitude solution for strapdown inertial navigation system based on quaternion algorithm[J];Optics and Precision Engineering;2008-10
2 SUN Xun1,DU Xiao-jing2,MA Chun-yan3,CHENG Bao-dong4 (1.The 4th department,Command and Engineering Institute of Chemical Defence,Beijing 102205,China;2.School of Mechatronics Engineering,Beijing Institute of Technology,Beijing 100081,China;3.The 33rd Institute,3rd Academe,Spaceflight Science and Engineering Group,Beijing 100074,China;4.School of Software,Beijing Institute of Technology,Beijing 100081,China);Attitude Solving and Three Dimensional Visual Simulation of High Dynamic Aircraft[J];Journal of System Simulation;2007-14
3 ZHU Yan-hua, LIU Jian-ye, ZENG Qing-hua, ZHAO Wei (Navigation Research Center, College of Automation, NUAA, Nanjing 210016, China);Parameter analysis method for optimizing rotation vector[J];Journal of Chinese Inertial Technology;2008-01
4 YANG Sheng,FANG Jian-cheng(School of Instrument Science and Opto-electronics Engineering,Beijing University of Aeronautics and Astronautics,Beijing 100191,China);A Single-Sample Rotation Vector Attitude Algorithm[J];Journal of Astronautics;2010-03
【Co-citations】
Chinese Journal Full-text Database 10 Hits
1 JI Yong1,2,LI Ming1,2,JIA Hong-guang1,CHEN Juan1,WANG Yi-fan1,CHEN Chang-qing1 (1.Changchun Institute of Optics,Fine Mechanics and Physics,Chinese Academy of Sciences,Changchun 130033,China;2.Graduate Universty of Chinese Academy of Sciences,Beijing 100039,China);Flight parameter computing platform under wind field environment[J];Optics and Precision Engineering;2009-08
2 WEI Qiang,WANG Xiao-hao,ZHOU Zhao-ying,XIONG Shen-su(State Key Laboratory of Precision Measurement Technology and Instruments,Tsinghua University,Beijing 100084,China);Guidance and implement of micro system based on GPS[J];Optics and Precision Engineering;2009-07
3 L Shao-lin,XIE Ling,CHEN Jia-bin (Automation School,Beijing Institute of Technology,Beijing 100081,China);Prefiltering for initial alignment of ring laser gyroscope SINS on rocking base[J];Optics and Precision Engineering;2009-10
4 DENG Yong1,HUANG Jing-pin2(1.Department of Mathematics of Kashi Teachers college,Kashi 844006,China;2.College of Computer and Information Science,Guangxi University for Nationalities,Nanning 530006,China);Numerical methods on a kind of linear matrix equation systems over quaternion field[J];Pure and Applied Mathematics;2010-05
5 HU Chun-bo,ZENG Qing-hua,QIAN Wei-xing (Navigation Research Center of Nanjing University of Aeronautics & Astronautics,Nanjing 210016,China);Semi-Physical Simulation of Transfer Alignment and Navigation Integration[J];Journal of Naval Aeronautical and Astronautical University;2009-06
6 ZHANG Rong-hui1,WANG Hai-wei2,JIA Hong-guang3,CHEN Tao3,ZHANG Yue3(1.College of Engineering,Zhejiang Normal University,Jinhua 321004,China;2.College of Transportation,Jilin University,Changchun 130022,China;3.Changchun Institute of Optics,Fine Mechanics and Physics,Chinese Academy of Sciences,Changchun 130033,China);Disturbance compensate control algorithm for strapdown inertial navigation system in initial alignment[J];Journal of Jilin University(Engineering and Technology Edition);2010-03
7 GAO Ning-jun1,ZHANG Zhi-yong1,GAO Chao1,CHEN Chun-peng2 (1.Unit 91336 of PLA,Qinhuangdao 066326,China;2.Unit 91404 of PLA,Qinhuangdao 066000,China);Research of Distributed Hardware-in-the-loop Simulation System Based on Guided Weapons[J];Command Control & Simulation;2010-06
8 YAN Gong-min1, YAN Wei-sheng1,2, XU De-min1,2 (1. College of Marine, Northwestern Polytechnical University, Xi’an 710072, China; 2. National Key Laboratory for Underwater Information Process & Control, Xi’an 710072, China);Limitations of error estimation for classic coning compensation algorithm[J];Journal of Chinese Inertial Technology;2008-04
9 QI Ze-hua1,DU Xiao-jing1,LIAO Yan-ping1,YU Shi-kui2 (1.School of Astronautics Science and Technology,Beijing Institute of Technology,Beijing 100081,China;2.The 4th Department,Command and Engineering Institute of Chemical Defence,Beijing 102205,China);Research of Multiple Rocket Simulation Training System Based on Vega Prime[J];Journal of System Simulation;2010-02
10 WANG Jun-pu,JIN Zhi-hua (Department of Instrumentation Engineering,Shanghai Jiao Tong University,Shanghai 200240,China);Applicability of parameter analysis method for optimizing rotation vector attitude algorithms[J];Journal of Chinese Inertial Technology;2010-01
China Proceedings of conference Full-text Database 1 Hits
1 Jiang Nan~1 Zhu Yueting~2 (1 Kunming Shipborne Equipment Research and Test Center,Kunming 650051,China;2 Dalian University of Technology,Dalian 116001);Visualization of Strap-down Inertial Measuring Data Processing Based on SIMULINK[A];[C];2010
【Secondary Citations】
Chinese Journal Full-text Database 10 Hits
1 Wei Xiaohong Zhang Chunxi Zhu Kuibao(School of Instrument Science and Opto-electronics Engineering,Beijing University of Aeronautics and Astronautics,Beijing 100083,China);High accuracy coning compensate algorithm by angular velocity[J];Journal of Beijing University of Aeronautics and Astronautics;2005-12
2 Yu Yang Zhang Hongyue(School of Automation Science and Electrical Engineering,Beijing University of Aeronautics and Astronautics,Beijing 100191,China);Three descriptions of coning motion and its influence[J];Journal of Beijing University of Aeronautics and Astronautics;2008-08
3 Lin Xueyuan 1,2 Liu Jianye 1 Zhao Wei 1 ( 1Center of Navigation, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China) ( 2Electronic Department, Naval Aeronautics Engineering Academy, Yantai 264001, China);Improved rotation vector attitude algorithm[J];Journal of Southeast University (Natural Science Edition);2003-02
4 WANG Jia-qi, JIN Guang, YAN Chang-xiang(Changchun Institute of Optics, Fine Mechanics and Physics, Chinese Academy of Sciences, Changchun 130033);Orientation error analysis of airborne opto-electric tracking and measuring device[J];Optics and Precision Engineering;2005-02
5 LI Xiao-guang~(1,2),WANG Zhao-nan~3,WANG Zhi~2,JIN Guang~2,ZHANG Li-ping~2,DING Yuan~4(1.Jilin Teacher's Institute of Engineering and Technology,Changchun 130052,China;2.Changchun Institute of Optics,Fine Mechanics and Physics,Chinese Academy of Sciences,Changchun 130033,China;3.College of Electronic Science and Engineering,Jilin University,Changchun 130025,China;4.Mechanical Engineering Department,Changchun University,Changchun 130032,China);Research on location compute method of object[J];Optics and Precision Engineering;2006-06
6 YANG Jin-xian,YUAN Gan-nan (College of Automation,Harbin Engineering University,Harbin 150001,China);Design and experiment for INS based on MIMU/GPS[J];Optics and Precision Engineering;2008-02
7 JIANG Ming1,2,HE Xiao-yuan2 (1.College of Civil Engineering,University of Science and Technology of Suzhou,Suzhou 215011,China;2.College of Civil Engineering,Southeast University,Nanjing 210096,China);Optical testing of dynamic characteristic of vibrating wheel micromechanical gyroscope[J];Optics and Precision Engineering;2008-02
8 LIAN Jun-xiang,HU De-wen,HU Xiao-ping,WU Wen-qi(Department of Automatic Control,College of Mechatronics and Automation,NationalUniversity of Denfense Technology,Changsha 410073,China);Research on Coning Error and Quantization Error of SINS Attitude Algorithm[J];Acta Aeronautica Et Astronautica Sinica;2006-01
9 Zhou Jianghua\+\{1,2\} Wang Feng\+1 Sun Guoji\+1 1.Institute of Systems Engineering, Xi'an Jiaotong University, Xi'an 710049 2.603\+#, The Second Artillery Engineering College, Xi'an 710025;General Formulas of Rotation Vector Based Attitude Algorithm of SDINS[J];Aerospace Control;2002-02
10 Chen Lei, Wang Haili, Ren Xuan (Department of Automatic Control,National University of Defense Technology,Changsha 410073);Object-oriented Realization of Real-time Three-dimensional Scene Visualization[J];COMPUTER ENGINEERING AND APPLICATIONS;2000-09
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