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ROBUST, NONLINEAR CONTROL DESIGN FOR A POSTSTALL MANEUVER AIRCRAFT
FAN Zi-qiang;FANG Zhen-ping
2002, (3): 193-196.
PDF [ 162 K ]( 758 ) HTML
NUMERICAL SIMULATION OF A DUAL-SWEPT/DUAL-RAMP INLET UNDER GROUND RUNNING
TAN Hui-jun;GUO Rong-wei;LIU Xi-peng
2002, (3): 197-201.
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INITIATION AND PROPAGATION OF FATIGUE CRACK IN EDGE REGION OF HOLE IN A SHEET WITH CENTRAL HOLE
GONG Ming;ZHAO Jian-hua;DONG Ben-han;WANG Xian-feng;LI Cheng-zhi
2002, (3): 202-205.
PDF [ 432 K ]( 1109 ) HTML
DESIGN OF FMECA SOFTWARE BASED ON RSMTL-CAD FRAMEWORK
SU Tie-jun;SUN Lin-ling;ZHAO Ting-di
2002, (3): 206-210.
PDF [ 319 K ]( 720 ) HTML
OPTIMUM DESIGN AND ELECTRICAL SIMULATION OF COMB-GIMBAL MICROMACHINED GYROSCOPE
CHE Lu-feng;XIONG Bin;WANG Yue-lin
2002, (3): 211-214.
PDF [ 174 K ]( 482 ) HTML
THREE-DIMENSIONAL FATIGUE FRACTURE IN COMPLEX ENVIRONMENTS
GUO Wan-lin
2002, (3): 215-220.
PDF [ 239 K ]( 684 ) HTML
STUDY ON LASER SINTERING OF Ni-BASED ALLOY POWDERS
ZHANG Jian-feng;SHEN Yi-fu;ZHAO Jian-feng;HUANG Yin-hui;YU Cheng-ye
2002, (3): 221-225.
PDF [ 199 K ]( 664 ) HTML
TOOTH CONTACT ANALYSIS OF SPIRAL BEVEL GEARS BASED ON THE DESIGN OF TRANSMISSION ERROR
FANG Zong-de;LIU-Tao;DENG Xiao-zhong
2002, (3): 226-230.
PDF [ 343 K ]( 2217 ) HTML
ANALYSIS AND PREDICTION OF PILOT-INDUCED OSCILLATION WITH ACTUATOR RATE LIMITING OF A FLY-BY-WIRE FIGHTER AND A METHOD FOR ALLEVIATING PIO
WU Wei;FANG Zhen-ping
2002, (3): 231-233.
PDF [ 256 K ]( 750 ) HTML
NEW METHOD FOR JUDGING CARTESIAN GRID VERTICES INSIDE OR OUTSIDE ARBITRARILY GEOMETRIC BODIES
LI Zhi-hong;TAO Zhi;CAI Wei-hua
2002, (3): 234-236.
PDF [ 117 K ]( 884 ) HTML
ANALYSIS ON THE VIBRATION CHARACTERISTICS OF CRACKED ROTOR WITH NONLINEAR OIL FILM BEARING
WAN Fang-yi;XU Qing-yu;HUA-Jun
2002, (3): 237-240.
PDF [ 159 K ]( 585 ) HTML
ANALYSIS OF ISOTROPY FOR THE SIX-AXIS FORCE/TORQUE SENSOR BASED ON STEWART PLATFORM
ZHAO Ke-ding;YANG Hao-quan;WU Sheng-lin;YUAN Li-peng
2002, (3): 241-244.
PDF [ 149 K ]( 924 ) HTML
MULTIDISCIPLINARY DESIGN OPTIMIZATION BASED ON DISTRIBUTED COEVOLUTION-ALGORITHM AND APPLICATION IN MISSILE DESIGN
CHEN Qi-feng;DAI Jin-hai;LI Xiao-bin
2002, (3): 245-248.
PDF [ 157 K ]( 661 ) HTML
A PROBABILITY MODEL FOR THE CORROSION DAMAGE OF AIRCRAFT STRUCTURE IN SERVICE ENVIRONMENT
CHEN Yue-Liang;LU Guo-zhi;
2002, (3): 249-251.
PDF [ 196 K ]( 744 ) HTML
RELIABILITY ANALYSIS OF MULTI-DEGREE-OF-FREEDOM NONLINEAR VIBRATION SYSTEMS WITH INDEPENDENCE FAILURE MODES
ZHANG Yi-min;WEN Bang-chun
2002, (3): 252-254.
PDF [ 250 K ]( 1129 ) HTML
RESEARCH ABOUT LIFE-DECIDING TECHNOLOGY ON HELICOPTERS
JIN Ping;CHEN Yue-liang;DUAN Cheng-mei
2002, (3): 255-258.
PDF [ 160 K ]( 748 ) HTML
CHAOS PREDICTION FOR MAGNETIC LEVITATION CONTROL SYSTEMS
YAO Hong;GUO Lei;LI Xu-ren
2002, (3): 259-261.
PDF [ 130 K ]( 569 ) HTML
ROBUST GUIDANCE LAW DESIGN FOR HOMING MISSILES USING NEURAL NETWORKS
ZHOU Rui;ZHANG Peng
2002, (3): 262-264.
PDF [ 126 K ]( 590 ) HTML
RESEARCH ON COMPLETE GPS/INS INTEGRATION USING H_∞ FILTER
ZHAO Wei;YUAN Xin;LIN Xue-yuan
2002, (3): 265-267.
PDF [ 140 K ]( 851 ) HTML
CHATTERING ATTENUATION MULTI-MODEL SWITCHING CONTROL FOR BTT MISSILE
MU Xiang-yu;ZHOU Di;DUAN Guang-ren
2002, (3): 268-271.
PDF [ 199 K ]( 878 ) HTML
OTF AMBIGUITY RESOLUTION IN GPS BASED ATTITUDE DETERMINATION
ZHENG Qing-hui;ZHANG Yu-lin
2002, (3): 272-275.
PDF [ 139 K ]( 886 ) HTML
INFLUENCE OF HIGH TEMPERATURE TREATMENT ON MICROSTRUCTURE AND MECHANICAL PROPERTIES OF 2D-C/C COMPOSITES PREPARED BY LIQUID-VAPORIZED PROCESSING
SUN Wan-chang;LI He-jun;ZHANG Xiu-lian
2002, (3): 276-278.
PDF [ 352 K ]( 725 ) HTML
CLASSING PARAMETER'S STUDY OF LUBRICATING OIL METAL DEBRIS
CHEN Guo;ZUO Hong-fu
2002, (3): 279-281.
PDF [ 124 K ]( 641 ) HTML
CRACK ARREST IN ALUMINUM ALLOY PLATE BY PART CROSSOVER USING ELECTROMAGNETIC HEAT EFFECTS
FU Yu-ming;BAI Xiang-zhong;ZHENG Li-juan;TIAN Zhen-guo
2002, (3): 282-284.
PDF [ 227 K ]( 531 ) HTML
SURFACES MATCHING ALGORITHM BASED ON GENETIC ALGORITHM AND LEAST SQUARE CRITERION
WU Dian-liang;HUANG Hai-liang;DING Yu-cheng;ZHAO Wan-hua
2002, (3): 285-288.
PDF [ 316 K ]( 1300 ) HTML
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