1000-1328
1998 Issue 3
SEVERAL ISSUES ON FAILURE MONITORING CONTROL FOR LIQUID PROPELLANT ROCKET ENGINE OF LAUNCH VEHICLE
Tan songlin;Zhangbaokun
Tan songlin;Zhangbaokun
..............page:110
DYNAMICS AND PARAMETERS IDENTIFICATION OF JOINTS IN SPACECRAFT
Wu Zhigang;Wang Benli;Ma Xingrui
Wu Zhigang;Wang Benli;Ma Xingrui
..............page:103-109
APPLICATION OF DECOMPILATION TO AEROSPACE INDUSTRY
Zhao Lei;Wu Yan;Wang Kaizhu
Zhao Lei;Wu Yan;Wang Kaizhu
..............page:97-102
STUDY ON THE STABILITY OF NONLINEAR VIBRATIONS OF A DEPLOYING FLEXIBLE APPENDAGE OF A SPACECRAFT
Li Junfeng;Wang Zhaolin
Li Junfeng;Wang Zhaolin
..............page:93-96
CONTROL AND COMPENSATION FOR NONLINEAR SERVO SYSTEMS BASED ON NEURAL NETWORKS
Xu Lixin;Wang Changhong;Zhuang Xianyi
Xu Lixin;Wang Changhong;Zhuang Xianyi
..............page:83-92
OPTIMAL SWITCH STATE SETTING OF VARY-MODEL CONTROLLER IN THE TURNTABLE'S SERVO SYSTEM
Li Qiuming;Feng Rupeng;Yu Lei;Liu Shengcai
Li Qiuming;Feng Rupeng;Yu Lei;Liu Shengcai
..............page:79-82
STUDY OF EDGE MATCHING APPROACH TO AIRCRAFT NAVIGATION
Ding Mingyue;Wu Yan;Peng Jiaxiong
Ding Mingyue;Wu Yan;Peng Jiaxiong
..............page:72-78
NUMERICAL INVESTIGATION OF THREE-DIMENSIONAL SEPARATED FLOWS ABOUT A HEMISPHERE-CYLINDER
Chen Liang;Yan Chao;Ding Xiaomei
Chen Liang;Yan Chao;Ding Xiaomei
..............page:68-71
ACOUSTIC EMISSION TECHNIQUE OF WATER-PRESSURE-TEST IN FILAMENT-WOUND CASE
Duan Dengping;Luo Haian;Liu Zhengxing
Duan Dengping;Luo Haian;Liu Zhengxing
..............page:62-67
EFFECT OF PREDEFORMATION AND AGING TREATMENT IN AN ELECTRIC FIELD ON MICOSTRUCTURE AND MECHANICAL PROPERTIES OF 1420 Al-Li ALLOY
Li Renshun;Wang Xiufang;Luo Jian
Li Renshun;Wang Xiufang;Luo Jian
..............page:57-61
THE THERMAL CONDUCTANCE ACROSS RUBY BALL BEARINGS AT LOW TEMPERATURE
Tian Huaizhang;Chen Wenyong;Li Xinzhong;Wu Yezheng
Tian Huaizhang;Chen Wenyong;Li Xinzhong;Wu Yezheng
..............page:52-56
TWO PHASE COLD FLOW SIMULATION OF WITH AND WITHOUT BAFFLES IN LIQUID ROCKET ENGINE
Zhao Wentao;Nie Wansheng;Zhuang Fengchen
Zhao Wentao;Nie Wansheng;Zhuang Fengchen
..............page:46-51
A NEW INSPECTING TECHNIQUE AND APPLICATION FOR NONLINEARITY IN VIBRATION TEST
Tan Zhiyong;Yu Haichang;Qiu Jibao
Tan Zhiyong;Yu Haichang;Qiu Jibao
..............page:41-45
THE RESEARCH OF FDF ROBUST DECISION METHOD
He Yingzi;Zhang bing;Wu Hongxin
He Yingzi;Zhang bing;Wu Hongxin
..............page:33-40
THE INERTIAL CONTROLLING METHOD TO HEIGHT OF BALLISTIC REENTRY VEHICLE
Yang Huiyao;Wang Shicheng;Deng Fanglin
Yang Huiyao;Wang Shicheng;Deng Fanglin
..............page:29-32
AIRPLANE TARGET RECOGNITION BASED ON ENERGY SPECTRUM IN THE POLARIZATION DOMAIN
Xiao Shunping;Wang Xuesong;Guo Guirong;Zhuang Zhaowen
Xiao Shunping;Wang Xuesong;Guo Guirong;Zhuang Zhaowen
..............page:23-28
CONTROL SCHEMES FOR TERMINAL SPACECRAFT RENDEZVOUS
Yu Shaohua;Yang Linna
Yu Shaohua;Yang Linna
..............page:16-22
ADAPTIVE PASSIVE FAULT-TOLERANT CONTROL BASED ON SYSTEM CHARACTERISTIC EXTRACT AND ITS APPLICATION
Xie Yongchun;He Yingzi;Wu Hongxin
Xie Yongchun;He Yingzi;Wu Hongxin
..............page:10-15
NUMERICAL SIMULATION ON VACUUM PLUME AND NUMERICAL ANALYZING STUDY ON VACUUM PLUME CONTAMINATION
Cai Guobiao;Wang Huiyu;Zhuang Fenggan
Cai Guobiao;Wang Huiyu;Zhuang Fenggan
..............page:1-9