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Journal of Chinese Inertial Technology
1005-6734
2008 Issue 1
zhong guo guan xing ji shu xue bao zheng gao jian ze
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page:封3
Inertial sensors automatic test system based on virtual instrument
CHENG Long;CAI Yuan-wen;YAO Jing-bo;REN Jiang-tao
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page:122-126
Bomber electro-optic countermeasure simulation system research and design
XING Chao;LI Yan-jun;ZHANG Ke;YU Rui-xing
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page:119-121,126
Risk management of inertial system development cycle based on 5S operation methods
ZHANG Zi-jian
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page:113-118
Risk analysis and improved algorithm of chi-square statistical test
LI Jin-liang;ZHANG Zong-lin;XU Yong-jun
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page:108-112
Three-phase and two-phase PM brushless motor controlled by back EMF
LIU Ju-sheng;PAN Long-fei;ZHAO Hui;LIU Chun-he
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page:104-107,118
Engineering realization of calibrating FOG's scale factor in segments
ZHANG Zhi-xin;XIA Jin-qiao;CAI Chun-long
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page:99-103
Systematic calibration method for laser gyro SINS
YANG Xiao-xia;HUANG Yi
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page:1-7
Parameter identification method based on frequency domain of flexure hinged pendulum accelerometer
MIN Yue-jun;XUE Xu
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page:94-98,103
Model identification method based on SVM for FOG
WANG Yu;WU Jun
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page:90-93
Compensation for bias in capacitive micro accelerometer
LIU Min-jie;DONG Jing-xin
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page:86-89
Integrated navigation system filter algorithms based on evolutionary artificial neural networks
XU Xiao-su;LIU Jian-juan
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page:82-85,89
Design of GPS/SINS pseudo-range(pseudo-range rate) integrated navigation system based on UKF
BAO Qi-lian;ZHOU Yuan-yuan
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page:78-81
Observable degree analysis of Beidou double-star/SINS integrated navigation system based on pseudo-range
LI Jian-wen;ZHANG Zong-lin
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page:73-77
SINS/GPS/CNS integrated navigation method based on microminiaturized sensors
CUI Nai-gang;HAN Peng-xin;MU Rong-jun
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page:68-72
Design of distributed system for embedded navigation computer system based on dual DSPs
ZHANG Guo-long;XU Xiao-su;FU Wen-shu
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page:64-67
Model of combined observations of Galileo and GPS carrier phase
YI Bing-xin;HUANG Yong-bo;LIN Gang-chui
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page:58-63
Novel suppression method for narrow-band interference in GPS receiver
ZHANG Lan;XIAO Chang-chun;HAN zhi-xue;WANG Bing
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page:54-57
Parameter analysis method for optimizing rotation vector
ZHU Yan-hua;LIU Jian-ye;ZENG Qing-hua;ZHAO Wei
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page:49-53
All-attitude accelerometer north finder based on arithmetic of correlation filtering algorithm
LI Xu-dong;MENG Fan-wei;LIN Yu-rong
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page:44-48
Design for an accurate strapdown attitude algorithm
YU Yang;ZHANG Hong-yue
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page:39-43
Generalized results based on duality between SINS coning and sculling algorithms
QINYong-yuan;SHI Xiao-wen
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page:34-38
Design and simulation on SINS self-alignment for carrier born aircraft
QIN Yong-yuan;ZHU Xin-ying;ZHAO Chang-shan;BAI Liang
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page:28-33
Magnetic deviation compensation using recursive least square for AHRS
GUO Peng-fei;HUA Chun-hong;REN Zhang;DING Xin-chun
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page:24-27
Optimization coning algorithms to the fixed frequency motion
PAN Xian-fei;WU Mei-ping;WU Wen-qi;HU Xiao-ping
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page:20-23
Design of CAN to FOG strapdown attitude heading reference system
SONG Ning-fang;REN Lei;LIN Heng;ZHU Lu-feng
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page:16-19
Research platform for strapdown navigation algorithm based on LabVIEW Model
WANG Jun-pu;WANG Zhe;TIAN Wei-feng
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page:12-15
Transfer alignment simulation system of guided bomb based on 1553B bus
WU Pan-long;DU Guo-ping;JIANG Fu-xian
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page:8-11