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Aerospace Shanghai
1006-1630
2011 Issue 3
Acoustic Emission Testing for Damage Evolutional of Composite Solid Propellant
LIU Cheng-wu;YANG Jian-hong;ZHANG Hui
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page:69-72
Integrated Relative Navigation Algorithm Based on IMU and CCD
ZHANG Li-jun;QIAN Shan;GUO Cai-fa;ZHANG Shi-feng
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page:8-16
Objective Multi-Factor Weight Allocation Method and Its Application
WU Jing;WU Xiao-yan;GAO Zhong-chang
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page:60-63
Research on Navigation Program of Reusable Booster Vehicle
MU Rong-jun;HAN Peng-xin;CUI Nai-gang
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page:1-7
xin xi dong tai
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page:7
Variable Step-Size Algorithm for Blind Source Separation Based on Fast Frobenius Diagonalization
SHEN Di;TONG Ning-ning;GUO Yi-duo
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page:42-45,72
Effect of Confining Pressure on NEPE Propellant\'s Intensity
WANG Guang;CHEN Gang
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page:55-59
Optimization Design of Composite Grid Stiffened Cylinder in Satellite Structure
CHEN Wei-ming
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page:50-54
Optimum Strategy of East-West Station-Keeping for Biased Momentum Satellite
CHEN Hong;ZHENG Jun;LI Yu-heng
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page:37-41,63
Research on Thermal Analysis for Some Remote Sensing Satellite
CHEN Jian-xin;LIU Wei-qiang
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page:46-49
Research of PXI-Based Real-Time Integrated Measurement System
CAO Hui;BI Jian-feng
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page:64-68
Pulsed Guidance Law for Exoatmospheric Interceptor
XIA Xi-wang;JING Wu-xing
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page:17-22,72
Automatic Orbit Design Approach Research of Manned Spacecraft
LIU Lu-hua;ZHENG Wei;TANG Guo-jian
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page:23-25,31
EM Scattering Analysis of Laser Plasma Antenna
XIA Xin-ren;XIE Hui;PENG Chuan;CHEN Chuang;YIN Cheng-you
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page:26-31
Spacecraft Attitude Tracking Control Based on Robust Adaptive Backstepping Approach
YAN Gen-ting;SONG Bin
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page:32-36,54