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《Journal of Harbin Institute of Technology》 2002-05
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Optimum technology for non-gyro micro inertial measuring unit

WANG Jin song, WANG Qi, SUN Sheng he (Dept. of Automated Test, Measurement and Control, Harbin Institute of Technology, Harbin 150001, China)  
An inertial navigational system with high anti g capability, low power consumption, small volume and low cost is needed on certain specific occasions. By using linear accelerometers unit at the different positions in space, a non-gyro micro inertial measuring unit is used to calculate the angular velocity and sense the axial acceleration of the carrier. A feasible inertial navigational system with medium accuracy can be designed in this way. The nine accelerometers were improved based on researched by foreign scholars and a novel calculation method was proposed to control the iterative error. The redundant information of sensors was used directly to calculate the absolute value of measured angular velocity and correct the solutions of differential equations thereby diminishing the accumulative errors for the solution of differential equations and reducing the shift of an inertial measurement unit.
【Fund】: 国防重点项目课题 (0 0 0 5NT0 0 67);; 航天科技创新基金资助项目 (2 0 0 1-0 9)
【CateGory Index】: V249.322
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【References】
Chinese Journal Full-text Database 10 Hits
1 CAO Yong-hong,ZHANG Hui,FAN Jin-biao,MA Tie-hua,ZU Jing(Key Laboratory of Instrumentation Science and Dynamic Measurement in Ministry of Education,North University of China,Taiyuan 030051,Shanxi,China);Research on Attitude Optimization Algorithm of Projectile at All Accelerometers' Installation Errors Based on GFIMU[J];Acta Armamentarii;2009-02
2 CAO Yong-hong, ZU Jing, LIN Zu-sen(Institute of Test Technology, North China Institute of Technology, Taiyuan 030051, China);Review of the Gyroscope Free Strap-Down Inertial Navigation System[J];Journal of Test and Measurement Technology;2004-03
3 Luo Yun-shun, Qi Wang, Ding Ming-li, Yin Xu Department of Automatic Test and Control, Harbin Institute of Technology, Harbin 150001, China;Design of an Inertial Measurement System Based on Accelerometers and Gyro-Free[J];Control Technology of Tactical Missile;2006-01
4 Shi Wen-ming, Yang Xiao-dong, Xu Bin Graduate Oragnization, Naval Submarine Academy, Qingdao 266071, China;Status and Future Development of Gyroscope-Free Strapdown Inertial Navigation System[J];Control Technology of Tactical Missile;2006-03
5 XU Wei-xing,QIN Li,YU Jing-na,ZHANG Hui-xin,ZHANG Wen-dong(The Key Laboratory of Instrumentation Science & Dynamic Measurement Ministry of Education,North University of China,Taiyuan,030051,China);Testing Research on Non-gyro Inertial Measurement Unit[J];Journal of Projectiles, Rockets, Missiles and Guidance;2006-01
6 LUO Yun-shun WANG Qi DING Ming-li (Harbin Institute of Technology.Harbin 150001,China);The Design and Experiment of A Gyro-free Inertial Measurement System[J];Journal of Projectiles,Rockets,Missiles and Guidance;2006-S9
7 Hao HongweiMa TiehuaFan Jinbiao(National Key Laboratory For Electronic Measurement Technology,North University of China,Taiyuan 030051);Design of non-gyro micro inertial measurement unit circuit[J];Electronic Measurement Technology;2009-01
8 CHEN Mu-qing,XU Jiang-ning,LIU Qiang(College of Electronic and Information Engineering,Naval Univ.of Engineering,Wuhan 430033,China);Design of algebra-based attitude angular velocity algorithm for GFSINS[J];Journal of Naval University of Engineering;2008-05
9 XIAO Wei-guang, DING Ming-li, WANG Qi (Department of Automatic Test and Control , Harbin Institute of Technology, Harbin 150001, China);Application of Total Least Square Algorithm in Static Decoupling of NGMIMU[J];中国航空学报(英文版);2004-04
10 Shi Wen-ming Wang Shuai;Gyroscope Free Strap-Down Inertial Navigation System[J];Chinese Journal of Ship Research;2006-02
【Co-references】
Chinese Journal Full-text Database 10 Hits
1 WANG Dai-hua,YUAN Gang,ZHAO Yan,HOU Xiang-hong (a.Key Lab.of Optoelectronic Technology and Systems of the Ministry of Education of China;b.Precision and Intelligence Lab.,Department of Optoelectronic Engineering,Chongqing University,Chongqing 400044,China);Study of Principle of a 6-DOF Accelerometer[J];Micronanoelectronic Technology;2007-Z1
2 Chi Xiaozhu  Wang Jinsong  Jin Hongzhang  Wang Daming  (College of Automation, Harbin Engineering University, Harbin, 150001 ) (49th Research Institute, China Electronics Technology Group Corporation );A STUDY ON THE DYNAMIC CHARACTERISTICS OF ACCELEROMETERS WORKING ON GYRO FREE MICRO INERTIAL MEASUREMENT UNITS[J];Acta Armamentarii;2004-03
3 WANG Xiao-na,WANG Shu-zong,ZHU Hua-bing(Department of Weaponry Engineering,Naval University of Engineering,Wuhan 430033,Hubei,China);Study on Models of Gyroscope-free Strap-down Inertial Navigation System[J];Acta Armamentarii;2006-02
4 Liu Qiang Yin Li (School of Mechanical Engineering and Automation, Beijing University of Aeronautics and Astronautics, Beijing 100083, China);Study on an improved recursive partial least-squares modeling approach and application[J];Journal of Beijing University of Aeronautics and Astronautics;2003-07
5 Liu Wei Xie Xuhui Li Shengyi (National University of Defense Technology, Changsha 410073, China);Attitude algorithm for strap-down inertial navigation system[J];Journal of Beijing University of Aeronautics and Astronautics;2005-01
6 Wang Danli Zhang Hongyue (Beijing University of Aeronautics and Astronautics,Dept. of Automatic Control);Methods for the Analysis of Observability and Their Application to INS Initial Alignment[J];JOURNAL OF BEIJING UNIVERSITY OF AERONAUTICS AND ASTRONAUTICS;1999-03
7 Wang Guanglong (Department of Engineering Safety, Beijing Institute of Technology, Beijing100081)Zu Jing\ \ Zhang Wendong\ \ Ma Tiehua (Department of Electronics Engineering, North China Institute of Technology, Taiyuan030051);Earth Magnetic Field Sensor and Its Application in Flight Body Attitude Measurement[J];JOURNAL OF BEIJING INSTITUTE OF TECHNOLOGY;1999-03
8 XIONG Yong hu, MA Bao hua, PENG Xing ping (School of Mechano Electronics Engineering, Beijing Institute of Technology, Beijing100081);Measurement of Angular and Linear Accelerations Using Linear Accelerometers[J];北京理工大学学报(英文版);2000-03
9 XIE Mei-ping , ZHAO Xi-ren(Dept.of Automatic Control,Harbin Engineering University,Harbin,150001,China);The Projection Pursuit Learning to the Extreme ShortPrediction of Big Ship Motion[J];JOURNAL OF SHIP MECHANICS;2000-04
10 TANG Furong, XUE Datong (Lanzhou Institute of Physics. Chinese Academy of Space Technology, Lanzhou 730000, P.R.China);Mechanics Principle and Damping Design of a Six-Axial Accelerometer[J];Journal of Transcluction Technology;2002-04
【Secondary References】
Chinese Journal Full-text Database 10 Hits
1 WANG Dai-hua,YUAN Gang,ZHAO Yan,HOU Xiang-hong (a.Key Lab.of Optoelectronic Technology and Systems of the Ministry of Education of China;b.Precision and Intelligence Lab.,Department of Optoelectronic Engineering,Chongqing University,Chongqing 400044,China);Study of Principle of a 6-DOF Accelerometer[J];Micronanoelectronic Technology;2007-Z1
2 WANG Wei,WAN Chao,HOU Hong-lu,ZHANG Xiong-xing (School of Optoelectronic Engineering,Xi'an Technological University,Xi'an 710032,China);Trajectory Axial Acceleration Measurement[J];Ordnance Industry Automation;2008-07
3 ZHANG Meng1,MA Tie-hua2,CAO Yong-hong1,ZU Jing(1.Key Lab for Instrumentation Science & Dynamic Measurement,North University of China,Ministry of Education,Taiyuan 030051,Shanxi,China;2.Department of Precision Instruments and Mechanology,Tsinghua University,Beijing 100084,China);A Navigation System for Spinning Projectile[J];Acta Armamentarii;2008-07
4 CAO Yong-hong,ZHANG Hui,FAN Jin-biao,MA Tie-hua,ZU Jing(Key Laboratory of Instrumentation Science and Dynamic Measurement in Ministry of Education,North University of China,Taiyuan 030051,Shanxi,China);Research on Attitude Optimization Algorithm of Projectile at All Accelerometers' Installation Errors Based on GFIMU[J];Acta Armamentarii;2009-02
5 Qin Jie Fang Jiancheng Sheng Wei(School of Instrument Science and Opto-electronics Engineering,Beijing University of Aeronautics and Astronautics,Beijing 100083,China);Novel inertial stellar compass based on gyroscope-free micro inertial measurement unit[J];Journal of Beijing University of Aeronautics and Astronautics;2007-11
6 QIAN Li,CHEN Wen-yuan Key Laboratory of Thin Film and Microfabrication Technology of Ministry of Education,Research Institute of Micron/Nanometer Science &Technology,Shanghai Jiao Tong University,Shanghai,200030,China;Study of Input System Based on MEMS Accelerometers[J];Chinese Journal of Sensors and Actuators;2009-05
7 WANG Xin1,SHI Xiao-feng1,LIN En-huai2 (1.School of Electronics and Information Engineering,Beihang University,Beijing 100083,China;2.Beijing Pulimen Technology CO.LTD.,Beijing 100041,China);Mathematic Modeling and Its Calibration Algorithm for Oil Well Inclometer[J];Well Logging Technology;2009-02
8 QIN Fangjun,XU Jiangning,FU Jun,ZHOU Hongjin(Electrical Engineering and Information Engineering College,Naval University of Engineering,Wuhan 430033,China);A Simplified Installation Error Calibration Method for Gyro-Free Inertial Navigation Systems[J];Journal of Test and Measurement Technology;2008-02
9 WU Junwei,LI Mianwei,WANG Xiaoxu,JIN Chunzhu (College Of Automation,Harbin Engineering University,Harbin 150001,China);An Identification Method for Installation Errors of GFSINS[J];Journal of Test and Measurement Technology;2008-05
10 MENG Song,ZHANG Zhijie,FAN Jinbiao,CAO Yonghong(Key Laboratory of Instrumentation Science & Dynamic Measurement (NUC),Ministry of Education,Taiyuan 030051,China);An BP ANN Forecast Model for Aerocraft Attitude[J];Journal of Projectiles,Rockets,Missiles and Guidance;2008-01
China Proceedings of conference Full-text Database 1 Hits
1 WANG Dai-hua YUAN Gang ZHAO Yan HOU Xiang-hong (a.Key Lab.of Optoelectronic Technology and Systems of the Ministry of Education of China;b.Precision anti Intelligence Lab.,Department of Optoelectronic Engineering,Chongqing University,Chongqing 400044,China);Study of Principle of a 6-DOF Accelerometer[A];[C];2007
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