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Flight Dynamics
1002-0853
2006 Issue 4
Study on the First Attack Probability of the Attacker on the Anti-Air Radar
ZHOU Jing-lun;MU Fu-ling;LUO Peng-cheng
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page:91-94
Flight Test of Stress Loads for an Air Propeller
QU Yu-chi;BAI Xiang-li;ZHANG Yong-feng
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page:88-90,94
Applying the Simulated Annealing Algorithm to Solve Airliner Aircraft Dispatching Problem
SUN Hong;ZHANG Xiang;XU Jie
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page:84-87
Research on Fighting Forms of an Anti-Satellite Satellite
ZHOU Ke-qiang;GAO Xiao-guang;BAI Yi
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page:80-83
The Research and Implementation of Flight Vehicle BLISS Distributed Platform
ZHOU hao;CHEN Wan-chun;YIN Xing-liang
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page:76-79
An Effective Algorithm of Terrain Avoidance/Terrain Following
NAN Ying;PENG Yun
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page:73-75
Aerodynamic Optimization Design and Experiment Study for a High-Lift Airfoil
ZHANG Ya-feng;SONG Bi-feng;LI Zhan-ke
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page:70-72
Research on Take-off Performance of the MA60 Aircraft at Plateau Airport
ZHANG Zhi-gang;WANG Bai-zheng;WANG He-ping
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page:65-69
Research on the Towed-Vehicle Flight Path Control Law in a Towed System
ZHANG Deng-cheng;TANG Shuo
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page:38-40,45
Research on Response Characteristic of Moving-Mass Control for the Low-Altitude Aircraft
XU Sheng-hong;GU Wen-jin
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page:34-37
Analysis of the Approach Power Compensator System with Constant Angle of Attack
ZHANG Yu-jie;YANG Yi-dong
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page:30-33
Design of Longitudinal Automatic Landing Control System Using the Block Diagonal Controller
ZHAO Guo-rong;LI Ji-xin;LIU Tao
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page:26-29
A Flight Control System Model of the Fighter Integrated Design Simulation System
LIU Yan;GAO Zheng-hong;SHANG Chong-yang
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page:22-25,29
Analysis on Ski-Jump Take-off Performance for a Fighter
BI Yu-quan;SUN Wen-sheng
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page:18-21
The Equivalent Moment Derivatives Model and Its Usage in Flight Simulation
SHANG Chong-yang;GAO Zheng-hong
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page:14-17
Verification of a SUAV's Longitudinal Dynamic Characters
JIN Yue;WANG Wei-jun;FANG Zhen-ping
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page:9-13
Routine Maneuver Performance Evaluation of a Fighter with Thrust Vector
HUA Yu-guang;XU Hao-jun;LIU Ling;GE Zhi-hao
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page:6-8,13
Research and Development on Joined Wing Aircraft and Sensorcraft
ZHENG Cheng-xing
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page:1-5
The Aircraft Take-off and Landing Performance Intelligent Computation Model and Its Applications
WEI Xun-kai;LI Hai-peng;WU Li-rong;HOU Sheng-li;LI Ying-hong
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page:61-64
Extra-atmospheric Trajectory Design of an Intercontinental Ballistic Missile
TANG Ming-liang;GU Liang-xian
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page:57-60
A Precise Initial Guidance Law for Orbit Interception
TANG Yi-hua;CHEN Shi-lu;XU Min;WAN Zi-ming
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page:53-56
On the Method of Determinating Explosion Height Based on Perturbation Theory
XIAN Yong
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page:50-52,56
Disturbed Modify Method of Fixed-Time Interception's Guidance in Orbit-Change Stage
ZHOU Xu-feng;TANG Shuo
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page:46-49
Research on the Extended Proportional Navigation Guidance Law Based on Lyapunov Stability
ZHAO Hong-chao;GU Wen-jin
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page:41-45