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Aerospace Control
1006-3242
1992 Issue 1
The interconversion of attitude deviations of aerospacecraft during large attitude flight
Gao yu-lin Beijing Aerospace Automatic Control Institude
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page:1-10
Spacecraft Modular Attitude Control System(MACS)
Chen Zugui Beijing Institute of Control Engineering
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page:11-18
VARIABLE STRUCTURE MODEL-FOLLOWING CONTROL OF SWITCHING ATTITUDE SYSTEM OF SPACECRAFT
Dai Xuefong Department of Astronautics Engineering Harbin Shipbuilding Engineering Institute
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page:19-24
OPTIMAL MULTIPLE-IMPULSE RENDEZVOUS
Chen Ying Harbin Institute of Technology Wang Xudong Beijing Institute of Control Engineering
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page:25-32
DYNAMICS AND SAFE MODE OF RENDEZVOUS BETWEEN TWO SPACECRAFTS IN SPNCE
Lin Laixing Beijing Institute of Control Engineenng
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page:33-42
HYBRID SIMULATE LANGUAGE EICSL
Xu Gengbao Beijing Aerospace Automatic Control Institute
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page:43-54
A directly optimizing algorithm for minimizing the resources of series system
Yang shuangjin Beijing Aerospace Automatic Control Institute
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page:55-61
Vibrating Response of Equipment Carried in vehicle
Huan longcai Beijing Aerospace Automatic Control Institute
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page:62-69
di er ke xie zhen qi tuo luo yi xin xing guan xing xi tong de guan jian
wang xi zuo ;
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page:70-71