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Aerospace Shanghai
1006-1630
2009 Issue 3
Equivalent Modeling for Axisymmetric Tank of Spacecraft with Accelerate
ZHANG Shu-yu;GUO Wen-yan;LI Cai-feng;XIA Yong-jiang;LIU Fu-cheng
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page:1-7
The Application of M Methods to Orbit Determination
LONG Han;PAN Xiao-gang;ZHOU Hai-yin;JIAO Yuan-yuan
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page:8-11,17
The Scheme of Space Anti-Satellite Operation Based on Space Rendezvous
ZHOU Wen-ya;LIU Heng;LI Shun-li;CHEN Hong-bo
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page:12-17
The WKB Method of Random Incident Electromagnetic Wave to Nonuniform Plasma
XIA Xin-ren;YIN Cheng-you;JIN Xian-long;WANG Shou-jie
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page:18-20,34
The Design Features and Research Processing of YH-1 Mars Probe
CHEN Chang-ya;FANG Bao-dong;CAO Zhi-yu;JIANG Shi-chen;HOU Jian-wen
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page:21-25,61
Analytical Solution of Temperature Field of Solid Rocket Motor Laminated Structure with High-Temperature Thermal Shock
LEI Yong-jun;WU Fei
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page:26-29,61
Numerical Simulation of Blunted Cone-Flare in Hypersonic Flow
LU Jian-wei;WANG Qiang
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page:30-34
Shape Reconstruction Based on Far Field Pattern
ZHONG Wei-jun;TONG Chuang-ming;ZHAO Yu-lei;HUANG Guo-rong
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page:35-37
On Orbit Servicing for Spacecraft
ZHAO Yang;ZHANG Da-wei;TIAN Hao;GUAN Ying-zi
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page:38-41
Various Matching Manners of Transfer Alignment for Weapon System on Space Platform
NI Xin-guo;HU Zheng-dong;ZHANG Shi-feng;YANG Hua-bo
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page:42-46
Analysis of Station-Keeping Strategies for Collocation of Geostationary Satellites Based on Eccentricity and Inclination Perpendicular Separation
SHI Shan-bin;DONG Guang-liang;LUO Qiang
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page:47-55
Digitized Design on Nonlinear Control System of Some Ship-Air Missile
YAO Qin
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page:56-61
A Method of Quick Location of GPS Receiver by Initial Setting
WANG Dan-dan;CHEN Xiao-jun;HOU Xiong;LIU Wei
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page:62-64