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Journal of Chinese Inertial Technology
1005-6734
1993 Issue 1
The Study of GPS/SINS Integrated System Dynamic Performance
Pong Yunxiang;Wu Cheng Beijing Institute of Control Devices
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page:1-7
Accuracy Requirement of GPS-Kalman Augmented Inertial Navigation System for Fighter Aircraft
Zheng E Northwestern Polytechnical University
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page:8-14
Analysis of Coulomb Damping Isolation System in Inertial Instrument
Zhu Rong;Ye Manhua;Lu Kai Shanghai Hao--Tong University
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page:15-20
Techniques for Developing High Precision Ring Laser Gyro
Zhang Yanshen;Tang Quanan;Su Li Qinghua University
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page:21-25+7
Design and Application of the Active Magnetic Suspension
Jia Shiong;Zheng Kuiri Beijing Institute of Control Devices
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page:26-32+20
On the Measurement and Demarcation North-Seeking Accuracy of Land Navigation System
Chen Fengyu;Miao Lingjuan Beijing Institute of Technology
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page:33-36+14
A Non-Linear Model Suitable for Gyro Random Drift Forecast
Shi Zhaoyun;Wan Dejun Southeast University
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page:37-41
The Research and Application of the Rate-Gyro Self-Test Technology
Luo Linguang Beijing Qing Yun Instrument Factory
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page:42-48
Releasing Stress by Vibrating
Zheng Zhida Southeast University
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page:49-51
xue bao bian wei hui di er ci gong zuo hui yi zai tian jin zhao kai
ni yue fang ;
..............
page:51
On the Study of the Technology in Assembling and Debugging of Flexgyro
Liang Shilin;Zhou Baizhao;Ma Yongxiang National Defense University of Science and Technology
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page:52-60