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Aerospace Shanghai
1006-1630
2005 Issue 2
nasa ji hua jian zao ji yu ji guang de wei xing gen zong wang luo
liu xin zuo
..............
page:64
mei ji hua shi yan xin xing xiao wei xing tui jin xi tong
xiao ze
..............
page:54
yi se lie yan zhi tu xiang shou ji she dan
zhang xiao zuo
..............
page:21
chui zhi fa she xing mi ka fang kong dao dan xi tong
zhang xiao zuo
..............
page:5
The Method of Hazard Assessment Applied on Rocket Propellant Operation
CONG Ji-xin;ZHANG Guang-you;CAO Ye;LI Zheng
..............
page:59-64
The Bistable Latch Valve Applied in Micro Satellite
WEI Qing;HAN Yun-xia
..............
page:55-58
Study of Robot Plane to Jam Modern Radar
XU Shao-yun;JIN Jia-wang;LI Xian-Mao
..............
page:51-54
The Application of the Latest FPGA Series in On-Board Embedded Computer
YANG Ya;WEI Xing-guo;GAO Jie;SHI Min-hua
..............
page:47-50
The Design and Realization of Imaging-Terminal Software for Meteorological Satellite
ZHANG Ru-yi
..............
page:43-46
The Application of Proton Exchange Membrane Fuel Cells in the Space Area
WANG Dong;ZHANG Wei;LIU Xiang
..............
page:39-42
Liquid Propellant Management for the HyperSoar Mobile Vehicle in the Atmospheric Layer
LIAO Shao-ying
..............
page:34-38
A Design of Portable Measurement System for Navy Missile Based on Virtual Instrument
LIAO Chao-wei;FENG Xiang-jun;LIAO Ying
..............
page:29-33
Application of Fuzzy Decision on Decision Assistant System for Naval Aircraft Antisubmarine
WU Hong-jun;QU Ye-pin
..............
page:26-28,58
Study on the Methods for a New Exterior Ballistic Measurement Based on Radio
ZHU Li-mei;ZHANG Xu-chun;DENG Hui
..............
page:22-25
Image Parallel-Manipulating System Technology
WEN Pei-gang;LIU Tao
..............
page:17-21
Determination of Relative Attitude between Satellites Using Least Square Estimator
LIN Xue;ZHANG Yu-lin;LIU Kun
..............
page:15-16,33
Research on Threat Evaluation Model of Air Attack Target
GAO Fang-jun
..............
page:11-14
Application of Fuzzy Control Technology in Attitude Control System for Launch Vehicle
ZHOU Ru-hao;TANG Guo-jin
..............
page:6-10
Conic Error Analysis of SINS in High Dynamic Environment
ZHANG Xu-chun;ZHOU Chun-jie
..............
page:1-5