1000-6893
1998 Issue 6
..............page:755
..............page:690
DESIGN AND SIMULATION OF A NEW KIND OF COMBINATIVE INTELLIGENCE FLIGHT CONTROL SYSTEM AND INTEGRATED FIRE/FLIGHT CONTROL SYSTEM OF ADVANCED ARMED HELICOPTER
Jiang Changsheng;Guo Shujun;Wang Pihong;Yang Keming;Sun Longhe
Jiang Changsheng;Guo Shujun;Wang Pihong;Yang Keming;Sun Longhe
..............page:719-725
EFFECT OF PROOF TESTING ON FATIGUE STRENGTH OF CERAMICS
L Baotong;Wang Hong
L Baotong;Wang Hong
..............page:715-718
NUMERICAL ANLYSES OF STRESS WAVE PROPAGATION IN A VARIABLE SECTION BAR
Cao Zengqiang;She Gongfan;Zhou ingqing
Cao Zengqiang;She Gongfan;Zhou ingqing
..............page:710-714
SOLUTION OF QPNS EQUATIONS TO SIMULATE AERODYNAMIC FORCES AND HEATING FOR ROTATION BODIES AT HIGH SPEED USING FINITE ELEMENT METHOD
Zhang Guofu;Hua Xiqing
Zhang Guofu;Hua Xiqing
..............page:706-709
DEVELOPMENT OF A METHOD AND APPLICATION FOR IMPROVING THE PILOT MODELING ACCURACY
Xu Zhongxiang;Qu Xiangju
Xu Zhongxiang;Qu Xiangju
..............page:700-705
THEORETICAL AND EXPERIMENTAL STUDY ON CONTACT CHARACTERISTICS OF SPIRAL BEVEL GEARS FOR AEROENGINES WITH ELASTIC SUPPORTS
Wang Sanmin;Dong Haijun;Li Jiqing
Wang Sanmin;Dong Haijun;Li Jiqing
..............page:696-699
STUDY AND APPLICATION OF CNC SYSTEM FAULT DIAGNOSIS BASED ARTIFICIAL NEURAL NETWORKS AND EXPERT SYSTEM
Wang Runxiao;Qin Xiansheng;Luo Qi;Zhou Hui;Yang Li
Wang Runxiao;Qin Xiansheng;Luo Qi;Zhou Hui;Yang Li
..............page:691-695
MACHINING FEATURE RECOGNITION BASED ON SHAPE FEATURE-BASED MODEL
He Xiaozhao;Shen Mei;Jiang Xieming;Zhang Tiechang
He Xiaozhao;Shen Mei;Jiang Xieming;Zhang Tiechang
..............page:685-690
APPLICATION OF ARTIFICIAL NEURAL NETWORKS IN INTELLIGENT CAD OF AIRCRAFT PRELIMINARY CONFIGURATION DESIGN
Liu Zhenkai;Gui Zhonghua;Cai Qing
Liu Zhenkai;Gui Zhonghua;Cai Qing
..............page:678-684
METHODS OF STRUCTURE FAULT DETECTION AND RECONFIGURATION OF SELF-REPAIRING CONTROL LAW FOR A FIGHTER
Hu Shousong;Guo Wei;Zhang Defa
Hu Shousong;Guo Wei;Zhang Defa
..............page:674-677
NEW PRINCIPLE OF FIBER GYROSCOPE IN NON-SAGNAC EFFECT-VIEWED PHYSICAL METHODOLOGY
Zhang Jiahua;Li Yingzi
Zhang Jiahua;Li Yingzi
..............page:668-673
FAULT-TOLERANT DECENTRALIZED FILTERING METHOD
Qiu Hongzhuan;Zhang Hongyue
Qiu Hongzhuan;Zhang Hongyue
..............page:662-667
STABILITY MARGIN ANALYSIS OF THE MULTILOOP FLIGHT CONTROL SYSTEMS
Wu Bin;Cheng Peng
Wu Bin;Cheng Peng
..............page:657-661
STUDY ON NONLINEAR CONTINUOUS DAMAGE CUMULATIVE MODEL FOR UNIAXIAL FATIGUE
Shang Deguang;Yao Weixing
Shang Deguang;Yao Weixing
..............page:647-656
AIRFOIL SHAPE OPTIMIZATION FOR HIGH AERODYNAMIC EFFICIENCY/LOW OBSERVABILITY
Zhu Ziqiang;Zubair Islam;Zhu Yikun;Li Haiming
Zhu Ziqiang;Zubair Islam;Zhu Yikun;Li Haiming
..............page:641-646
..............page:705
..............page:673
TWO-DIMENSIONAL P-AND-DOWN ETHOD
Fu uimin;Yin ang
Fu uimin;Yin ang
..............page:748
ESTABLISHING HE NOWLEDGE ASE F ARAMETERS OR SHAPING UBE ND AR RODUCTS N HE EURAL-NETWORK
Qi Lehua;Hou Junjie;Yang Fang;Li Hejun
Qi Lehua;Hou Junjie;Yang Fang;Li Hejun
..............page:744-747
FATIGUE CHARACTERIZATION OF COMPOSITE HONEYCOMB CORE SANDWICH PANELS AFTER LOW VELOCITY IMPACT
Cheng Xiaoquan;Kou Changhe;Li Zhengneng
Cheng Xiaoquan;Kou Changhe;Li Zhengneng
..............page:740-743
BAYESIAN APPROACH TO HIGH RESOLUTION DIRECTION-OF-ARRIVAL ESTIMATION
Chen Jianfeng;Liu Chunming;Huang Jianguo
Chen Jianfeng;Liu Chunming;Huang Jianguo
..............page:736-739
EFFECTIVE METHOD FOR 3-D AIRCRAFT TARGET AUTOMATIC RECOGNITION
Liao Wenjian;Cheng Yu
Liao Wenjian;Cheng Yu
..............page:730-735
MULTISENSOR INFORMATION FUSION FOR TARGET IDENTIFICATION USING A RADAR SENSOR AND AN INFRARED SENSOR
Hao Chongyang;Tang Wenbin
Hao Chongyang;Tang Wenbin
..............page:726-729