Journal of Chinese Inertial Technology 2012 Issue 5 Measurement method of projectile's roll angle based on MEMS accelerometers

Measurement method of projectile's roll angle based on MEMS accelerometers
LIU Zhao-hua;WANG Yong;MAO Yu-liang;SONG Chun-lei

..............page:505-509

Approach of Kalman filtering estimation of guided projectile attitude
NIU Chun-feng;LIU Shi-ping;WANG Zhong-yuan

..............page:510-514

Approach for robust spherical simplex UKF in SINS initial alignment
CHENG Xiang-hong;WANG Yu;YANG Wen-bo

..............page:540-543

Parameter calibration based on attitude errors of space-stable INS
HU Pei-da;GAO Zhong-yu;WU Qiu-ping;CHEN Jing-chun

..............page:521-524

Time-delay's effect on velocity matching transfer alignment
LIU Hong-guang;CHEN Zhi-gang;CHEN Gang

..............page:544-551

Fractal characteristic and interpolation method for SIMU error coefficients
WANG Li-xin;WANG Jian-hua;LI Cheng

..............page:515-520

New rapid two-position alignment method of SINS
ZHOU Shao-lei;WU Xiu-zhen;XU Hai-gang;LIU Chong

..............page:525-529

Transfer alignment of carrier-born aircraft under large azimuth misalignment angle
WEI Xue-tong;GAO Lei

..............page:552-556

Test platform for SINS algorithm based on flight simulation
LI Jun-wei;CHENG Yong-mei;CHEN Ke-zhe;CHEN Si-jing;SONG Chun-hua

..............page:530-535

Three-dimensional magnetic compass error compensation algorithm based on ellipsoid surface fitting
ZHU Jian-liang;WANG Xing-quan;WU Pan-long;BO Yu-ming;ZHANG Jie

..............page:562-566

Self-alignment method based on H∞ filter for SINS of carrier plane on the sea
WANG Yong-jun;XU Jing-shuo;YUAN Tao

..............page:536-539

Personal navigation method based on foot-mounted MEMS inertial/magnetic measurement unit
QIAN Wei-xing;ZHU Xin-hua;SU Yan

..............page:567-572

Simulation of Galileo E1/E5/E6 digital IF signal
ZHU Xue-fen;CHEN Xi-yuan;CHEN Jian-feng

..............page:557-561

Model noise Kalman filter algorithm for electro-optical tracking
WANG Qiu-ping;LI Feng;MA Chun-lin

..............page:573-576,582

Thermal drift prognosis and compensation model of MEMS accelerometer
XU Zhe;LIU Yun-feng;DONG Jing-xin

..............page:601-604,610

Application of a new developed adaptive federated Kalman filter in tactical missile integrated navigation system
LIU Ying;TIAN Wei-feng;ZHAO Jian-kang;BAO Qi-lian;ZHU Shi-qing

..............page:577-582

Three-dimensional transient thermal modeling of FOG fiber coil
WANG Wei;XIANG Zheng;XING Hui

..............page:605-610

Integrated navigation based on X-ray pulsars and asteroids during interplanetary cruise
YANG Cheng-wei;ZHENG Jian-hua

..............page:583-586,592

Analysis of shock-response signal of non-driven structure silicon micro-machined gyro
YAN Qingwen-wen;ZHANG Fu-xue;LIU Yu;ZHAO Hui;ZHANG Zhen-ping

..............page:611-616

Effect of octupole-winding on temperature performance of fiber optic gyroscope
WANG Yue-ze;CHEN Xiao-dong;ZHANG GUI-cai;LIU Bo-han;CHEN Gui-hong

..............page:617-620

Fast resolution for three-frequency carrier ambiguity of long-range network RTK based on optimal combination
DENG Jian;PAN Shu-guo;WANG Sheng-li

..............page:587-592

Modeling and analysis of fiber optic gyroscope random drifts
BAI Jun-qing;ZHANG Ke;WEI Yu-xin

..............page:621-624

Calibration of gyro error model coefficients on precision centrifuge with counter-rotating platform
WANG Shi-ming;REN Shun-qing;WANG Chang-hong

..............page:625-630

Inductive magnetic field with deep ocean waves
ZHANG Yang;KANG Chong;LV Jin-ku

..............page:593-595

zhong guo guan xing ji shu xue bao zheng gao jian ze

..............page:封3

SINS/CNS nonlinear tightly integrated method based on additive quaternion
XIONG Jian;WEI Lin-sheng;GUO Hang;QU Qiang

..............page:596-600