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Aerospace Control
1006-3242
1991 Issue 3
THE CORRELATION ANALYSIS APPROACH IDENTIFYING THE FREQUANCY RESPONSES OF MATHEMATICAL MODELS IN DISCRETE TIME DOMAIN
Dong Weisan Beijing Aerospace Automatic Control Institute
..............
page:1-7
STATE TRANSFER MATRIX AND SYSTEM RESPONSE FUNCTION
Li Zhentao Beijing Aerospace Automatic Control Institute
..............
page:8-17
POSTBOOST CONTROL TECHNIQUE OF FOREIGN BALLISTIC MISSILE
Xu Jingfang Beijing Institute of control and electronic technology
..............
page:18-26
jie shao yi zhong xin xing hua xian ran se zi dong jian ce she bei
..............
page:26
A DESIGN METHOD OF CONTROL SYSTEMS POSSESSING INTEGRITY AND ITS APPLICATION IN FLEXIBLE SPACECRAFT
Ni MaoLin;Zheng Bing;Wu Hongxin Beijing Institute of Control Engineering
..............
page:27-35
nasa si jia hang tian fei ji de zui jin fei xing ji hua
zhang kang hua ;
..............
page:36
AN ON-GROUND REAL-TIME FAULT DIAGNOSIS EXPERT SYSTEM FOR THE SATELLITE ATTITUDE CONTROL SYSTEM (SCRDES)
Wang Nanhua;Ni Xingzhen;Li Dan;Tian He;Zhang Hanying Beijing Institute of Control Engineering
..............
page:37-44
A NEW DESIGN METHOD FOR ADAPTIVE ROBUST CONTROLLER BY USING THE GOLDEN SECTION
Xie Yongchun;Wu Hongxing Beijing Institute of Control Engineering
..............
page:45-56
DIGITAL CONTROL MODEL SIMULATION SOFTWARE DESIGN OF ATTITUDE CONTROL SYSTEM
Wu Changcai Beijing Aerospace Automatic control Institute
..............
page:57-66
REAL-TIME INTERFACE UNITS SPECIALIZED FOR MICRO VAX-Ⅲ COMPUTER
Yao Rongjiang Beijing Aerospace Automatic Control Institute
..............
page:67-75+66
THE TOPOLOGICAL DIAGRAM METHOD FOR THE DESIGN OF THE ANTINUCLEAR ELECTROMAGNETIC INPULSE OF COMPLEX ELECTRONIC SYSTEMS
Qiu Yang
..............
page:76-80+35-36
shou pi shou ti shi gps zhuang zhi jiao fu bu dui
sun mei ;
..............
page:81