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Aerospace Control
1006-3242
2012 Issue 2
zheng gao jian ze
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page:后插1
The Analysis and Simulation on File Delivery Time of Deferred NAK in CFDP Protocol
LIANG Yingchun
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page:80-83,88
The Study of Grey Analytic Hierarchy Process in the Survivability Application of Missile Weapon System
QIU Lingcun;HUI Yi
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page:17-21
The Study on Decision-making of the Maneuver in Satellite Orbits Based on Non-Keplerian
ZHANG Tuo;GAO Xiaoguang;FAN Hao
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page:51-56
The Multivariable Decoupling Control Based on H-Matrices and QFT for SRLV
ZHAO Zhifang;XIAO Lihong;NI Shaobo
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page:3-6
The Design and Research of Fault Injection on 1553B Bus
LIAN Meng;LI Xuefeng
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page:84-88
A Novel Method of Locating GEO Objects with Space-Based Optical Short Arcs Observation and the Geometric of Precision for Initial Orbit Determination
WANG Xueying;LI Jun;AN Wei
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page:46-50,56
A Filter Algorithm of Multi-Sensor Target Tracking Based on Out of Sequence Measurement
JIANG Chunlei
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page:63-68
The Simulink Simulation of the INS on the Near Space Hypersonic Vehicle
PENG Hui;XIONG Zhi;LIU Jianye;WANG Rong
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page:69-74
The Redundant Technology Based on Bridge-Control-Double-Networks for Reusable Launch Vehicle Control System
QI Guangping;SUN Peng;LI Guangjie
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page:89-95
The Simulation of Lifting Reentry Dynamic Properties Based on Orbiter Simulator
DONG Yanfei;TAN Zhaosheng;CHEN Xiaofei
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page:75-79
The Research on the Uncertainty of Pressure Center for Moving Mass Actuated Vehicle
WEI Pengxin;GAO Changsheng;JING Wuxing
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page:39-45
The Generation of Three-dimensional Constrained Entry Trajectories for Hypersonic Vehicle Based on the Gauss Pseudospectral Method
YAO Yinwei;LI Huabin
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page:33-38
A Method of Rectification for Star Map Distortion Based on Improved Genetic Algorithm
MU Yuqiang;WANG Danye;SUN Xiaosong;HUANG Xingli;CHEN Xinmin
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page:7-10,21
An Improved ECS Algorithm for SAR with Sub-Aperture Data
YANG Libo;LU Heping;GAO Lei
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page:22-27
Transfer Trajectory Design of Interplanetary Multiple Objects Encounter Based on the Gravity-Assisted Technology
HU Qinglong
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page:57-62
Attitude Control for Launchers Based on Robust State Observers
ZHOU Jun;SHUI Zunshi;GE Zhilei
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page:11-16,21
The Rapid Optimization of Entry Trajectory for Suborbital Launch Vehicle
WANG Wenhu
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page:28-32