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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
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page:1-5+27
Realization of INS/GPS Integrated Navigation System
Mao Long Xian Flight Automatic Control Research Institute
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page:6-10
A Kind of Algorithm for Optimal Decoupled Distributed Kalman Filters
Wang Shuhua;Yang Daqing Nanjing Aeronautical Institute
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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
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page:22-27
Application of Kalman Filter to Inertial Survey Systems
Gu Qital;Zhou Liqiang;Liu Xuebin Tsinghua University
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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
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page:34-38
The Selection of Parameters about Accelerometers
Yu Zhihui Centre of Instrument and Measurement.;Shenyang Xinle Precision Machinery Co.
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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
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page:50-56
Study for Frequency Domain Transfer Relation Between General Precision of Large Centrifuge and It’s Main Axis Motor Ripple Moment
He Zeng;Sun Tao;Yuan Zhejun Harbin Institute of Technology
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page:57-61
PRBS——A Pulse Response Test System of Inertial System Based on Correlative Identification
Hu Changhua;Xu Hualong;Miao Dong Xian Second Artillery Engineering Institute
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page:62-65
A method and Theoretical Basis to Check and Accept Assembly Language Program of Real-time Algorithm of Strapdown Inertial Navigation
Zhu Xinhua Southeast University
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page:66-72
xi an guan xing ji shu xue hui di san jie xue shu jiao liu hui zai yin chuan shi ju xing
li wen zuo ;
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page:72