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Chinese Space Science and Technology
1000-758X
2011 Issue 5
Relative Guidance Accuracy Analysis for Non-cooperative Space Target by Range-only Measurement of Satellite Formation
Su Jianmin;Dong Yunfeng
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page:48-56
Optimal Analysis of the Reliability for Torsion Spring Based on Multi-failure Modes
Wang Mei;Chen Guoding;Xiao Yong
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page:57-63
Selection of the Beacon Pulsars in Pulsars Navigation
Chu Yonghui;Wang Dayi;Huang Xiangyu
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page:64-69
Review on Integral Stiffened Shell Structure Technology of Large Space Station
Yu Dengyun;Lai Songbai;Chen Tongxiang
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page:31-40
Adaptive Controller for Spacecraft Attitude Maneuver Based on Extended State Observer
Yuan Guoping;Shi Xiaoping;Li Long
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page:9-17
Optimal Control of Spacecraft Fly-around Releasing Using Continuous Thrust Based on Gauss Pseudospectral Method
Duan Chuanhui;Dong Yunfeng
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page:18-24
Shape Optimization Design and Simulation of Near Space Airship
Yang Yanchu;Wang Sheng;Gu Yidong;Li Yingtang;Miao Jinggang
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page:76-83
xin xi dong tai
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page:封2,8,17
Vision-aided Attitude Determination for Air-bearing Simulator of Rendezvous and Docking
Wei Xiqing;Song Shenmin
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page:41-47,56
Analytical Solution of Two-Point Boundary Value Problem for Spacecraft Relative Motion
Yuan Yunxia;Yue Xiaokui;Lou Yunfeng
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page:25-30
Constructing China\'s Ocean Satellite System to Enhance the Capability of Ocean Environment and Disaster Monitoring
Yang Baohua
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page:1-8
Soft Landing Imoact Simulation of Lunar Lander
Lin Qing;Nie Hong;Chen Jinbao;Wan Junlin;Li Lichun
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page:70-75,83