1005-6734
2015 Issue 3
Initial alignment of CNS/INS integrated navigation system based on recursive least square method
ZHOU Ling-feng;ZHAO Xiao-ming;ZHAO Shuai;YAO Qi;YANG Lin;College of Automation;Harbin Engineering University;Tianjin Navigation Instrument Research Institute;
ZHOU Ling-feng;ZHAO Xiao-ming;ZHAO Shuai;YAO Qi;YANG Lin;College of Automation;Harbin Engineering University;Tianjin Navigation Instrument Research Institute;
..............page:281-286
Fast alignment of space-stable systems based on position and velocity observations
HE Qian-en;WU Qiu-ping;Department of Precision Instruments;Tsinghua University;
HE Qian-en;WU Qiu-ping;Department of Precision Instruments;Tsinghua University;
..............page:287-292
Multi-position alignment with arbitrary rotation axis for SINS
TAN Cai-ming;ZHU Xin-hua;WANG Yu;SU Yan;School of Mechanical Engineering;Nanjing University of Science and Technology;
TAN Cai-ming;ZHU Xin-hua;WANG Yu;SU Yan;School of Mechanical Engineering;Nanjing University of Science and Technology;
..............page:293-297
Linear optimized self-alignment for SINS using Rodrigues parameters
MEI Chun-bo;QIN Yong-yuan;YANG Peng-xiang;School of Automation;Northwestern Polytechnical University;No.203 Research Institute of China Ordnance Industries;
MEI Chun-bo;QIN Yong-yuan;YANG Peng-xiang;School of Automation;Northwestern Polytechnical University;No.203 Research Institute of China Ordnance Industries;
..............page:298-302
Navigation scheme design and modeling of a novel gyro-free SINS
LI Cheng-gang;XIE Zhi-hong;YOU Jing-jing;XIA Yu-hui;WEI Xue-dong;College of Mechanical and Electronic;Nanjing University of Aeronautics and Astronautics;College of Mechanical and Electronic Engineering;Nanjing Forestry University;Aviation Key Laboratory of Science and Technology on Inertia;Flight Automatic Control Research Institute;
LI Cheng-gang;XIE Zhi-hong;YOU Jing-jing;XIA Yu-hui;WEI Xue-dong;College of Mechanical and Electronic;Nanjing University of Aeronautics and Astronautics;College of Mechanical and Electronic Engineering;Nanjing Forestry University;Aviation Key Laboratory of Science and Technology on Inertia;Flight Automatic Control Research Institute;
..............page:303-310
Transfer alignment approach to near space vehicles based on star sensors
CHENG Xiang-hong;HAN Xu;CHEN Hong-mei;DAI Chen-xi;Key Laboratory of Micro-inertial Instrument and Advanced Navigation Technology of Ministry of Education;School of Instrument Science & Engineering;Southeast University;
CHENG Xiang-hong;HAN Xu;CHEN Hong-mei;DAI Chen-xi;Key Laboratory of Micro-inertial Instrument and Advanced Navigation Technology of Ministry of Education;School of Instrument Science & Engineering;Southeast University;
..............page:311-314
Pedometer method based on adaptive peak detection algorithm
CHEN Guo-liang;LI Fei;ZHANG Yan-zhe;School of Environment Science and Spatial Informatics;China University of Mining and Technology;
CHEN Guo-liang;LI Fei;ZHANG Yan-zhe;School of Environment Science and Spatial Informatics;China University of Mining and Technology;
..............page:315-321
Application of neural network by genetic algorithm optimization in SINS/GPS
XU Xiao-su;ZHOU Feng;ZHANG Tao;LI Yao;TIAN Zei-xin;Key Laboratory of Micro-inertial Instrument and Advanced Navigation Technology;Ministry of Education;School of Instrument Science & Engineering;Southeast University;
XU Xiao-su;ZHOU Feng;ZHANG Tao;LI Yao;TIAN Zei-xin;Key Laboratory of Micro-inertial Instrument and Advanced Navigation Technology;Ministry of Education;School of Instrument Science & Engineering;Southeast University;
..............page:322-327
Closed-loop endo-atmospheric guidance of launch vehicle based on hybrid optimization approach
CUI Nai-gang;HUANG Pan-xing;WEI Chang-zhu;FU Yu;CHENG Chao;Department of Astronautics;Harbin Institute of Technology;Beijing Institute of Astronautical Systems Engineering;
CUI Nai-gang;HUANG Pan-xing;WEI Chang-zhu;FU Yu;CHENG Chao;Department of Astronautics;Harbin Institute of Technology;Beijing Institute of Astronautical Systems Engineering;
..............page:328-333
Method of jointly determining ship attitude by dual star sensors
PAN Liang;ZHOU Hai-yuan;ZHANG Tong-shuang;ZHAO Li-jian;Joint Lab of Flight Vehicle Ocean-Based Measurement and Control;China Satellite Maritime Tracking& Controlling Department;
PAN Liang;ZHOU Hai-yuan;ZHANG Tong-shuang;ZHAO Li-jian;Joint Lab of Flight Vehicle Ocean-Based Measurement and Control;China Satellite Maritime Tracking& Controlling Department;
..............page:334-338
Adaptive sliding mode guidance law with input constraints and autopilot lag
SONG Jun-hong;SONG Shen-min;Center for Control Theory and Guidance Technology;Harbin Institute of Technology;
SONG Jun-hong;SONG Shen-min;Center for Control Theory and Guidance Technology;Harbin Institute of Technology;
..............page:339-344
Optimized method of building underwater terrain navigation database based on triangular irregular network
WANG Li-hui;GAO Xian-zhi;LIANG Bing-bing;YU Le;ZHU Xue-fen;Key Laboratory of micro-inertial instrument and advanced navigation technology;Ministry of education;School of instrument science and engineering;Southeast University;Science and Technology on Space Physics Laboratory;
WANG Li-hui;GAO Xian-zhi;LIANG Bing-bing;YU Le;ZHU Xue-fen;Key Laboratory of micro-inertial instrument and advanced navigation technology;Ministry of education;School of instrument science and engineering;Southeast University;Science and Technology on Space Physics Laboratory;
..............page:345-349
Attitude and position calculations for SINS/GPS aided by space resection of aeronautic single-image under small inclination angles
XIA Lin-lin;YU Jin-xin;CHU Yan;ZHU Bi-hui;School of Automation Engineering;Northeast Dianli University;College of Computer Science and Technology;Harbin Engineering University;
XIA Lin-lin;YU Jin-xin;CHU Yan;ZHU Bi-hui;School of Automation Engineering;Northeast Dianli University;College of Computer Science and Technology;Harbin Engineering University;
..............page:350-355
Rapid trajectory optimization for cooperative penetration of missile formation based on two-stage RRT-GMP strategy
HUANG Rong;CUI Nai-gang;WEI Chang-zhu;WANG Jin-bo;HUANG Pan-xing;School of Astronautics;Harbin Institute of Technology;China Academy of Launch Vehicle Technology;China Aerospace Science and Technology Corporation;
HUANG Rong;CUI Nai-gang;WEI Chang-zhu;WANG Jin-bo;HUANG Pan-xing;School of Astronautics;Harbin Institute of Technology;China Academy of Launch Vehicle Technology;China Aerospace Science and Technology Corporation;
..............page:356-362
Method on underwater assisted navigation system using two-dimensional terrain feature matching based on Hu moments
XU Xiao-su;YUE Zeng-yang;ZHANG Tao;TANG Jun-jun;Key Laboratory of Micro-inertial Instrument and Advanced Navigation Technology;Ministry of Education;Southeast University;School of Instrument Science & Engineering;Southeast University;
XU Xiao-su;YUE Zeng-yang;ZHANG Tao;TANG Jun-jun;Key Laboratory of Micro-inertial Instrument and Advanced Navigation Technology;Ministry of Education;Southeast University;School of Instrument Science & Engineering;Southeast University;
..............page:363-368
Seabed terrain-aided SINS location based on constrained particle swarm optimization method
ZHOU Ling;CHENG Xiang-hong;School of Instrument Science & Engineering;Key Laboratory of Micro-inertial Instrument and Advanced Navigation Technology;Ministry of Education;Southeast University;Department of Physics and Electronic Engineering;Yuncheng University;
ZHOU Ling;CHENG Xiang-hong;School of Instrument Science & Engineering;Key Laboratory of Micro-inertial Instrument and Advanced Navigation Technology;Ministry of Education;Southeast University;Department of Physics and Electronic Engineering;Yuncheng University;
..............page:369-372+384
MEMS gyroscope structure with low mechanical-thermal noise and weak mechanical coupling
CHEN Zhi-yong;ZHANG Rong;ZHOU Bin;Department of Precision Instruments;Tsinghua University;
CHEN Zhi-yong;ZHANG Rong;ZHOU Bin;Department of Precision Instruments;Tsinghua University;
..............page:373-378
Control methods for drive mode of MEMS vibratory gyroscope with spring hardening nonlinearity
DING Xu-kai;LI Hong-sheng;NI Yun-fang;SHAO An-cheng;Key Laboratory of Micro-Inertial Instrument and Advanced Navigation Technology of Ministry of Education;School of Instrument Science and Engineering;Southeast University;
DING Xu-kai;LI Hong-sheng;NI Yun-fang;SHAO An-cheng;Key Laboratory of Micro-Inertial Instrument and Advanced Navigation Technology of Ministry of Education;School of Instrument Science and Engineering;Southeast University;
..............page:379-384
Algorithm of improving scale factor stability for micromechanical gyro driven by rotating carrier
ZHANG Zeng-ping;ZHANG Fu-xue;ZHANG Wei;School of Computer & Information Management;Inner Mongolia University of Finance and Economics;Sensing Technique Research Center;Beijing Information Science and Technology University;
ZHANG Zeng-ping;ZHANG Fu-xue;ZHANG Wei;School of Computer & Information Management;Inner Mongolia University of Finance and Economics;Sensing Technique Research Center;Beijing Information Science and Technology University;
..............page:385-389
Analysis on fiber alignment dislocation characteristics of photo-detector component
DING Dong-fa;LIU Guo-jun;LIU Jian-chun;GAO Feng;YANG Chang-wang;ZHENG Da-kun;Changchun University of Science and Technology;Beijing Aerospace Control Instrument Research Institute;
DING Dong-fa;LIU Guo-jun;LIU Jian-chun;GAO Feng;YANG Chang-wang;ZHENG Da-kun;Changchun University of Science and Technology;Beijing Aerospace Control Instrument Research Institute;
..............page:390-393+398
Design and implementation of high-precision data acquisition and parameter compensation system for silicon resonant accelerometer
WANG Yan;ZHANG Ling;XING Chao-yang;ZENG Qing-lin;Beijing Aerospace Control Device Institute;
WANG Yan;ZHANG Ling;XING Chao-yang;ZENG Qing-lin;Beijing Aerospace Control Device Institute;
..............page:394-398
Influence of air pressure variation on FOG bias stability and its improvement
LV Xiao-qin;HUANG Xin-yan;GAO Feng;WANG Xue-feng;Beijing Aerospace Times Optical-electronic Co. Ltd;
LV Xiao-qin;HUANG Xin-yan;GAO Feng;WANG Xue-feng;Beijing Aerospace Times Optical-electronic Co. Ltd;
..............page:399-401+408
Dynamic model identification and computation of servo system for simulation turntable
LI Hui;CHEN Qian-rong;ZHU Zhen;GAN Lin;Luoyang Electronic Equipment Test Center of China;
LI Hui;CHEN Qian-rong;ZHU Zhen;GAN Lin;Luoyang Electronic Equipment Test Center of China;
..............page:402-408
Doppler interpolation method based on extrapolation and CIC filter
CHENG Chao;MU Rong-jun;CAI Ling;QIAO Li-wei;WEI Jia-qing;Harbin Institute of Technology;Tianjin Navigation Instrument Research Institute;
CHENG Chao;MU Rong-jun;CAI Ling;QIAO Li-wei;WEI Jia-qing;Harbin Institute of Technology;Tianjin Navigation Instrument Research Institute;
..............page:409-414
Diagnosis and classification of ball bearing faults in gyro motors by stator current signature analysis
DONG Lei;ZHOU Hao;PAN Long-fei;CHEN Wei;JIN Chen;LI Nan;LI Wei-min;School of Mechanical Engineering;Hebei University of Technology;Tianjin Navigation Instruments Research Institute;
DONG Lei;ZHOU Hao;PAN Long-fei;CHEN Wei;JIN Chen;LI Nan;LI Wei-min;School of Mechanical Engineering;Hebei University of Technology;Tianjin Navigation Instruments Research Institute;
..............page:415-420
..............page:421