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Journal of Chinese Inertial Technology
1005-6734
1993 Issue 2
Analysis of Attitude Errors and Determination of Models on Strapdown "Mathematical Platform"
Wu Wei Beijing Institute of Control Devices
..............page:1-5+27
Realization of INS/GPS Integrated Navigation System
Mao Long Xian Flight Automatic Control Research Institute
..............page:6-10
A Kind of Algorithm for Optimal Decoupled Distributed Kalman Filters
Wang Shuhua;Yang Daqing Nanjing Aeronautical Institute
..............page:11-21
Study on the Model and Emulation of the Dynamic Gyroscope Drill Survey Instrument
JinIi;Du ZhuIiang;He Shusen Beijing Automatic Control Institute
..............page:22-27
Application of Kalman Filter to Inertial Survey Systems
Gu Qital;Zhou Liqiang;Liu Xuebin Tsinghua University
..............page:28-33
The Ground Simulating Drill System of Inertial Navigation
Zhang Zongling;Zai Youxin;Zhu Jiahai;Tong Zhige Xian Air Force College of Engineering
..............page:34-38
The Selection of Parameters about Accelerometers
Yu Zhihui Centre of Instrument and Measurement.;Shenyang Xinle Precision Machinery Co.
..............page:39-49
Theoretical Researches on Frictional Coefficients of High-Speed Radial Ball Bearings and Angular-Contact Ball Bearings in Missile Gyroscopes
Xu Dawei;Gu Peizhi Shanghai Machinery Technology Institute Shanghai Jiao Tong Universty
..............page:50-56
PRBS——A Pulse Response Test System of Inertial System Based on Correlative Identification
Hu Changhua;Xu Hualong;Miao Dong Xian Second Artillery Engineering Institute
..............page:62-65