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Aerospace Control
1006-3242
1991 Issue 2
OPTIMAL RENDEZVOUS BETWEEN TWO SPACECRAFTS USING TWO IMPULSES
Pan Keyan Beijing Institute of Control Engineering
..............page:14-23
EFFECT ON DYNAMICS AND CONTROL OF RENDEZVOUS AND DOCKING DUE TO LIQUID SLOSHING INTERNAL TO SPACECRAFT
Wang Zhaolin;Li LeiDepartment of Engineering Mechnaics;Qinhua University
..............page:24-32
THE STABILITY ANALYSIS AND MATHEMATICAL SIMULATION FOR ATTITUDE MOTION OF SPINING VEHICLE
Gao YulinBeijing Aerospace Automatic Control Institute
..............page:33-39
THE LEVEL OF CONTROLLABILITY AND OBSERVABILITY FOR FLEXIBLE SPACECRAFT
Hu Hengzhang Ge ShengminHarbin Institute of Technology
..............page:40-48
DIGITAL SCENE MATCHING ARE CORRELATOR (DSMAS)IS USED IN THE TOMAHAWK CRUISE MISSILE
Wang XizhenBeijing Aerospace Automatic Control Institute
..............page:49-56+39
YH REAL-TIME SIMULATION SYSTEM
Xu Gengbao;Wang LinBeijing Aerospace Automatic Control Institute
..............page:57-65+23
STUDY OF RELIABILITY ANALYSIS METHOD FOR THE COMPLEX VEHICLE CONTROL SYSTEMS
Yang ShuangjingBeijing Aerospace Automatic Control Institute
..............page:66-73
MATERIAL AND ELEMENTS OF FOUR FREQUENCIES LASER GYRO
Yang ShulinBeijing Aerospace Automatic Control Institute
..............page:74-79
cm-01 xing zhi neng ji yin fang da yi
zhou zhang hua ;
..............page:80
itc xi lie zhi neng wen du kong zhi yi
zhou zhang hua ;
..............page:80