1000-1328
1999 Issue 2
..............page:118
ABSOLUTE VALUE MODAL STRAIN ENERGY METHOD FOR VISCOELASTIC DAMPING CONTROL OF TRUSS STRUCTURE
Lü Gang;Lu Feng;Zhang Jinghui
Lü Gang;Lu Feng;Zhang Jinghui
..............page:112-117
EXPERIMENTAL STUDY ON FLEXIBLE MULTIBODY DYNAMICS
Wang Jianming;Hong Jiazhen;Wang Shi;Zhou Xuejun
Wang Jianming;Hong Jiazhen;Wang Shi;Zhou Xuejun
..............page:107-111
ADVANCES IN SIMULATION STUDIES OF THE FLIGHT PERFORMANCE OF PARAFOIL SYSTEM FOR SPACECRAFT RECOVERY
Zhang Xiaojin;Qin Zizeng;Ma Hailiang;Ge Yujun
Zhang Xiaojin;Qin Zizeng;Ma Hailiang;Ge Yujun
..............page:104-106
TEMPERATURE TEST AND MODELING RESEARCH OF GYROSCOPE
Xu Lina;Deng Zhenglong;Zhang Guangying;Zhu Yijiang;Lü Xiren
Xu Lina;Deng Zhenglong;Zhang Guangying;Zhu Yijiang;Lü Xiren
..............page:99-103
DIGITAL SCENE IMAGE SYNTHESIS
Zhang Tianxu;Hu Bo
Zhang Tianxu;Hu Bo
..............page:93-98
THE THEORETICAL ANALYSIS AND EXPERIMENTAL RESEARCH ON THE PNEUMATIC SERVO SYSTEM WITH GENERALIZED PULSE CODE MODULATION
Wang Xuanyin;Yue Jiguang;Wang Xuyong;Liu Qinghe
Wang Xuanyin;Yue Jiguang;Wang Xuyong;Liu Qinghe
..............page:87-92
STUDY ON ATTITUDE DYNAMICS OF A LIQUID-FILLED SPACECRAFT WITH MANIPULATORS
Li Junfeng;Wang Zhaolin
Li Junfeng;Wang Zhaolin
..............page:81-86
A STUDY OF HF-GW RADAR SUPPRESSING LIGHTNING INTERFERENCE
Li Jianwei;Quan Taifan;Yu Changjun;Ma Zilong;Wang Hui
Li Jianwei;Quan Taifan;Yu Changjun;Ma Zilong;Wang Hui
..............page:75-80
STATISTICAL DIAGNOSIS METHOD FOR OUTLIERS FROM SPACECRAFT TRACKING DATA
Hu Shaolin;Sun Guoji
Hu Shaolin;Sun Guoji
..............page:68-74
THE SOFT FAULT DETECTING AND LSOLATING TO ENSURE THE ENTIRE ATTITUDE MEASURING OF A STRAPDOWN INERTIAL NAVIGATION SYSTEM
Qin Yongyuan;Niu Huifang
Qin Yongyuan;Niu Huifang
..............page:61-67
CRITERION AND ALGORITHM OF SATELLITES COVERAGE SITUATION
Yan Ye;Ren Xuan;Chen Lei
Yan Ye;Ren Xuan;Chen Lei
..............page:55-60
THE ESSENTIAL FEATURE OF STEADY DETONATION WAVE USING PROPULSION
Cui Dongming;Fan Baochun
Cui Dongming;Fan Baochun
..............page:48-54
STUDY ON SPACE MAST OF OCTAHEDRAL MODULE
Chen Wujun;Guan Fuling;Chen Xiangyang;Qiu Hongmei
Chen Wujun;Guan Fuling;Chen Xiangyang;Qiu Hongmei
..............page:41-47
ONE NONLINEAR OPTIMAL MISSILE GUIDANCE LAW
Cai Lijun;Zhou Fengqi
Cai Lijun;Zhou Fengqi
..............page:36-40
A DESIGN OF NONLINEAR CONTROL SYSTEM FOR LONG-DISTANCE AERODYNAMIC MISSILE
Gu Wenjin;Wang Shixing;Wei Feng
Gu Wenjin;Wang Shixing;Wei Feng
..............page:28-35
CONTINUOUS SLIDING MODE CONTROL BASED ON FUZZY LOGIC OF SPACECRAFT
Huang Xianlin;Wang Haibin;Zhou Jiansuo;Hu Hengzhang
Huang Xianlin;Wang Haibin;Zhou Jiansuo;Hu Hengzhang
..............page:22-27
SPACE BERTHING DYNAMIC AND CONTROL
Lin Laixing
Lin Laixing
..............page:14-21
FAULT-TOLERANT INTEGRATED NAVIGATION SYSTEM BASED ON NEURONS
Ma Xin;Yuan Xin
Ma Xin;Yuan Xin
..............page:7-13
THE ALL-COEFFICIENT ADAPTIVE CONTROL OF THE SLEW MANUVER OF A FLEXIBLE SPACECRAFT
Xie Yongchun;Mu Xiaogang;Wu Hongxin;Li Jisu
Xie Yongchun;Mu Xiaogang;Wu Hongxin;Li Jisu
..............page:1-6