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Aerospace Shanghai
1006-1630
2009 Issue 1
An Improved Method of Solving Initial Value and Model of Initial Orbit Determination by Space-Based Angle Measurement
LIU Lei;XI Xiao-ning;RONG Peng-zhi
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page:1-5,23
The Method of Parameter Estimation Based on Nonlinear Constraint Condition and Application on Orbit Determination
LIU Jing;PAN Xiao-gang
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page:6-9,19
Piecewise Linear Recursive Convolution for Magnetized Plasma Using FDTD
XIA Xin-ren;HUANG Ye;YIN Cheng-you
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page:10-14
Sliding Mode Observer Design of Nonlinear Uncertain System
LIU Yun-feng;LIU Hua-feng
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page:15-19
Study on Driving Laws of Sun Synchronous Orbit Satellite's Solar Arrays
ZHAI Kun;YANG Di;CHEN Xin-long;ZHAO Yong-De
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page:20-23
Study on Transfer Alignment Technology for Space-BasedWeapon System under Attitude Maneuver
HU Zheng-dong;QIAN Shan;CAI Hong
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page:24-27
Absolute Position Determination for Geosynchronous Satellite Using X-Ray Pulsars
ZHENG Guang-lou;LIU Jian-ye;QIAO Li;HE Liang;XIONG Zhi
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page:28-30,60
DOA Estimation of Coherent Signals Based on UCA with Improved MUSIC Algorithm
ZHU Li;ZHANG Guo-quan;WANG Guang-ming
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page:31-33,52
Analysis and Design for Pixel Electromagnetic Crystal
FU Shu-hong;TONG Chuang-ming;LI Xi-min
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page:34-37
Core-Cluster Combination-Based Shared Tree Algorithm for LEO Satellite IP Networks
TIAN Xiao-fang;CHENG Lian-zhen
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page:38-42
Design of a Cone-Perch Docking Mechanism for Micro-Satellites Station
XU Ying;SHAO Xiao-wei;CHEN Ji-an;DUAN Deng-ping
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page:43-47,56
Design and Analysis of MR Bumper about Lunar Damper Soft Landing
ZHANG Ying;NIE Hong;CHENG Jin-bao
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page:48-52
Simulation Analysis of Separation for Some Satellite Fairing
XU Yong-cheng;GOU Yong-jie;WANG Shi-gang
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page:53-56
Investigation of Coordinated Control of Lunar Rover Locomotion
LIU Xiao-feng;DING Tong-cai
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page:57-60
Software and Hardware Co-Design Technology in On-Board Embedded Computer
YANG Ya;SHI Min-hua;YANG Rong;ZHOU Hua
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page:61-64