1000-1328
1999 Issue 3
di ba jie huan tai ping yang di qu guo ji kong jian hui yi long zhong zhao kai
zhong guo yu hang xue hui
zhong guo yu hang xue hui
..............page:12
STUDY OF TELESCIENCE SPACE COMMUNICATION LINK CONFIGURATION ACCORDING TO CCSDS PROTOCOL FOR ADVANCED ORBITING SYSTEMS
Zhang Wei;Wang Ying;Zhangeryang
Zhang Wei;Wang Ying;Zhangeryang
..............page:112-117
THE RESEARCH AND EXPECTATION OF SIX-DEGREE-OF-FREEDOM SIMULATION OF LARGE SCALE BALLISTIC VEHICLE
Deng Fanglin;Yan Bin;Wang Shicheng
Deng Fanglin;Yan Bin;Wang Shicheng
..............page:106-111
ADAPTIVE TWO-STEP FILTER WITH APPLICATIONS TO MISSILE GUIDANCE WITH PASSIVE MEASUREMENTS
Zhou Di;Mu Chundi;Hu Hengzhang
Zhou Di;Mu Chundi;Hu Hengzhang
..............page:101-105
A DESIGN METHOD OF ROBUST GUIDANCE CONTROLLER AGAINST RADOME EFFECT
Qi Baohua;Zhang Lin
Qi Baohua;Zhang Lin
..............page:53-60
STUDY ON INCREMENT MODOLING AND OPTIMAL CONTROL FOR LARGE SCALE SYSTEMS
Wang Qingchao;Yu Baocai
Wang Qingchao;Yu Baocai
..............page:43-52
ACCURATE MEASUREMENT OF A 3D MOVING OBJECT THROUGH CALIBRATION AND SUBPIXEL TECHNIQUES
Yu Qifeng;Sun Xiangyi;Zhang Dongsheng;Quan Tiehan;Lei Zhihui
Yu Qifeng;Sun Xiangyi;Zhang Dongsheng;Quan Tiehan;Lei Zhihui
..............page:38-42
POINT PATTERN RELAXATION MATCHING INVARIANT TO ROTATIONS AND SCALE CHANGES BY HOPFIELD NEURAL NETWORK
Sang Nong;Zhang Tianxu
Sang Nong;Zhang Tianxu
..............page:31-37
ANALYSE PARAMETERS OF HIGH RESOLUTION SPACEBORNE SAR
Huang Yan;Chen Jie;Li Chunsheng;Zhou Yinqing;Chen Yuanzao
Huang Yan;Chen Jie;Li Chunsheng;Zhou Yinqing;Chen Yuanzao
..............page:26-30
FBM-BASED FRACTAL SIMULATION OF TERRAIN
She Longhua;Shen Lincheng;Chang Wensen
She Longhua;Shen Lincheng;Chang Wensen
..............page:21-25
AUTONOMOUS ORBIT DETERMINATION WITH RADAR ALTITUDE SENSOR
Han Chao;Zhang Renwei
Han Chao;Zhang Renwei
..............page:13-20
A SOPHISTICATED DYNAMICAL MODEL OF TETHERED SATELLITE SYSTEMS
Zhu Renzhang;Lei Da;Lin Huabao
Zhu Renzhang;Lei Da;Lin Huabao
..............page:7-12
MODAL ANALYSIS FOR FRAME STRUCTURES VIA TRAVELING WAVE APPROACH
Zhu Guidong;Zhang Gangtie;Shao Chengxun
Zhu Guidong;Zhang Gangtie;Shao Chengxun
..............page:1-6
THE SCHEME OF COMBINING ADAPTATION WITH ROBUSTNESS CONTROL FOR SPACE MANIPULATOR SYSTEM WITH UNCERTAIN PARAMETERS
Chen Li;Liu Yanzhu
Chen Li;Liu Yanzhu
..............page:96-100
ON THE DYNAMICS,VIBRATION AND CONTROL OF SPACE MANIPULATOR
Gu Xiaoqin;Tan Zhaoyang
Gu Xiaoqin;Tan Zhaoyang
..............page:91-95
SEPARATING CONTROL METHOD OF SATELLITE GROUP
Guo Zhenyun;Ren Xuan
Guo Zhenyun;Ren Xuan
..............page:87-90
NECESSARY AND SUFFICIENT CONDITION OF GLOBAL COVERAGE FOR CONSTELLATION USING CIRCULAR ORBIT
Yuan Shigeng;Yang Weilian
Yuan Shigeng;Yang Weilian
..............page:82-86
ANALYSIS OF INFLUENCE OF VIBRATION TO BIT ERROR RATE FOR A SYSTEM OF SPACE OPTICAL COMMUNICATION
Ma Jing;Tan Liying;Jin Enpei;Geng Wanzhen;Huang Bo
Ma Jing;Tan Liying;Jin Enpei;Geng Wanzhen;Huang Bo
..............page:76-81
BILATERAL CONTROL OF MASTER-SLAVE TELEROBOT SYSTEM WITH FORCE TELEPRESENCE
Chen Weidong;Xi Yugeng;Cai Hegao
Chen Weidong;Xi Yugeng;Cai Hegao
..............page:69-75
ATTITUDE STABILITY OF SPACECRAFT WITH TWO FLEXIBLE SOLAR ARRAYS IN GRAVITATIONAL FIELD
Ge Xinsheng;Liu Yanzhu
Ge Xinsheng;Liu Yanzhu
..............page:61-68