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Aerospace Control
1006-3242
1992 Issue 3
Re-entry Guidance with Variable structure for Maneuverable Vehicle
Zhan HongBeijing Institute of Control and Electronic Technology
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page:1-7
Optical Measurement Algorithm of Position & Attitude for Spacecraft
Huang Yuming Zhou Shian Wang Lixin Fan Ruying Wu HongxinBeijing Institute of Control Engineering
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page:8-15
The Design of attitude control system for large maneuvering aircrafts
Yao Yu Wang ZicaiHarbin Institute of Technology
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page:16-25+7
Using fast fourier transform to identify the frequency responses of digital networks
Dong WeisanBeijing aerospace automatic control institude
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page:26-32
Multisensor Information Fusion for Space Robots
Huang Yuming Li GentianBeijing Institute of Control Engineering
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page:33-37
The Application of the Multiprocessor Parallel Simulation Technologies in the Missile Guidence Accuracy Analysis
Lu Hongbin
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page:38-46
Real time control calculation of differential algebrdic problems
FeijingGaoBeijing computer application and simulation technigue Institute
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page:47-56
Effects of Turn Table Errors on the Hardware In-the-Loop Simulations of Spinning Missiles
Meng daikui Jiang Lan fang Li YongxinBeijing Institute of Electronic System Engineering
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page:57-61
The Hardware-in-the-loop Simnlation Experiments of the Solid Rocket Attitude Control Systems by YH-F
1
Chen YuexlanBeijing Aerospace Automatic Control Institute
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page:62-67
Raising relay quality by the monitoring method
Ji LonggenBeijing Aerospace Automatic Control Institute
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page:68-72
ji dian qi chao xing cheng de shi bo qi jian cha fa
lv zhi gong ;
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page:73+37
hui yi jian xun
xu geng bao ;
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page:74-75