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Aerospace Control
1006-3242
2011 Issue 6
The Design for Terminal Guidance Law of Decoupling Three-dimensional Optimal Variable Structure
SI Xuehui;LI Xiaobing;ZHANG Yan
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page:54-59
Relative Navigation for Space-based Platform with Extended Kalman Filter
YANG Xu;CHEN Binglong
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page:34-38,59
The Method of Quaternion Applied to Description of Man-made Satellite Orbit
FAN Kuiwu
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page:14-16,21
Finite-Time Control for Electromagnetic Formations of Fractionated Spacecraft Based on Terminal Sliding Mode Technique
HU Min;ZENG Guoqiang
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page:22-27,33
The Research and Application of a New Strong Tracking Filter Method Based on H∞
ZHAO Bin
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page:60-63,83
Research on the Attitude Control of Launch Vehicle Upper Stage
YANG Hua;CHEN Zongji;QIN Xudong
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page:84-87
The Warhead Attitude Robust Controller Design Based on Double-loop Sliding Mode
DONG Jie;HE Youzhi
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page:64-67,83
An Image Processing Platform Design Based on FPGA
LI Changsen;MA Biao;LI Ting
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page:68-71
A Method for Precision Evaluation Integrating Prior Information Under Extreme Small Sample
ZHANG Zongmei;SONG Weijun;LI Shuangxi;GAO Xiaoying
..............
page:49-53
Overview of Fault Diagnosability Evaluation and Design
LIU Wenjing;LIU Chengrui;WANG Nanhua
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page:72-78,87
Research of Certain Aircraft Ground Power Fault Diagnosis Based on D-S Evidence Theory
WU Yubin;ZHANG Hexin;LV Yongjia
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page:79-83
Research on a Rolling Guidance Law of Asymmetric Reentry Vehicle
LI Zixing;L1 Gaofeng
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page:44-48,53
The Research on the Pointing Strategy of Space-based Visible Space Surveillance
DIAO Huafei;LI Zhi
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page:39-43
zheng gao jian ze
..............
page:91
A Prediction Method of GLONASS Satellites Orbits and Visibilities Based on the Almanac
CUI Yingying;LV Lingou;BAO Liang;LIANG Shengjie;WANG Lei
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page:17-21
The Analysis of Dark Matter Principle for the Formation of Inertial Physics Mechanism and Inertial Force Physics Mechanism(part2)
BAI Linwu;WANG Yongping
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page:88-91
Optimal Trajectory Designing and Tracking Control for Space Autonomous Rendezvous
ZHANG Song;HOU Mingshan;SHEN Yuheng
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page:28-33
The Kinematics Analysis of Lunar Rovers Based on Vector Method
LIU Jianjun;CHEN Jianxin
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page:8-13
The Switching Sequence Design of Switched System
LIU Xinglong
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page:3-7,13