1006-3242
1990 Issue 2
THE DESIGN AND FLYING TEST FOR ATTITUDE CONTROL SYSTEM OF LM-4A LAUNCH VEHICLE
Chen Baichu Shentu XinLin Shanghai Instrument Factory
Chen Baichu Shentu XinLin Shanghai Instrument Factory
..............page:1-7
A SIMPIE BASE-POINT COMPUTATION METHOD FOR MEASURING INERTIAL VELOCITY AND POSITION OF ROCKET
Li Zhentao Beijing Aerospace Automatic Control Institute
Li Zhentao Beijing Aerospace Automatic Control Institute
..............page:8-14
A SUMMARY ABOUT A BANK-to-TURN CONTROL TECHNOLOGY
Wu Xingfen Shanghai Electromechanic System Engineering Research Institude Ministry of Aerospace Industry
Wu Xingfen Shanghai Electromechanic System Engineering Research Institude Ministry of Aerospace Industry
..............page:15-26
MULTIVARIABLE FREQUENCY DOMAIN DESIGN METHOD OF AUTOMATIC DOCKING CONTROL SYSTEM BETWEEN TWO SPACECRAFTS
Li Yuanchun Wu Yaohua Yang Di Harbin Institute of Technology
Li Yuanchun Wu Yaohua Yang Di Harbin Institute of Technology
..............page:27-35
DYNAMICAL MODELS OF THE FLEXIBLE SPACE MECHANICAL ARMS
Liu Dun Yang Daming Harbin Institute of Technology
Liu Dun Yang Daming Harbin Institute of Technology
..............page:36-43
DYNAMICS AND CONTROL OF SOFT-DOCKING CONCEPT BETWEEN TWO SPACECRAFTS
Hong Jiazhen Shi Pengfei Shanghai Jiao Tong University
Hong Jiazhen Shi Pengfei Shanghai Jiao Tong University
..............page:44-52
THE ASTRONAUT’S FUZZY CONTROL MODEL AND PROSPECT FOR ITS APPLICATION
Long Shengzhao Institute of space medico-Engineering Beijing;CHINA
Long Shengzhao Institute of space medico-Engineering Beijing;CHINA
..............page:53-59
HARDWARE IN THE LOOP SIMULATION METHOD USED TO SIMULATE AN ATTITUDE CONTROL SYSTEM OF A BINDING TYPE LAUNCH VEHICLE
Xu Gengbao Beijing Aerospace Automatic Control Institute
Xu Gengbao Beijing Aerospace Automatic Control Institute
..............page:60-68
THE FINE STRUCTURE OF PASS/FAIL TEST RESULT VECTORS AND THE IMPROVED UMVE ORDERING METHOD
Liao Jiongsheng Beijing Institute of Control Engineering
Liao Jiongsheng Beijing Institute of Control Engineering
..............page:69-80