Flight Dynamics 2011 Issue 4 fei xing li xue zheng gao jian ze

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Flight Dynamics
1002-0853
2011 Issue 4

fei xing li xue zheng gao jian ze

..............page:后插1

Gust alleviation control system design of large civil aircraft based on multiple control surfaces
YUAN Gang;LI Ai-jun;WANG Chang-qing;XU Xiao-ye

..............page:65-67

Model and simulation of cooperative multi-task assignment for multi-UAV system
LONG Guo-qing;ZHU Xiao-ping;ZHOU Zhou

..............page:68-71,76

Aerodynamic optimization design for the three-dimensional wing
JIA Jie;WANG Tao

..............page:45-48

Identify of aircraft dynamic derivatives based on CFD technology and analysis of reduce frequency
SUN Tao;GAO Zheng-hong;HUANG Jiang-tao

..............page:15-18

Investigation on pitch control technique for an airfoil with ground effect
SHEN Dong;CHEN Ying-chun;ZHANG Bin-qian

..............page:37-40,44

Summary of guidance law based on cooperative attack of multi-missile method
WANG Jian-qing;LI Fan;ZHAO Jian-hui;WAN Cong-mei

..............page:6-10

Study of hypersonic airfoil pitch oscillation unsteady aerodynamic force
LIU Luo-cheng;XU Min;YAO Wei-gang;CAI Tian-xing

..............page:28-31,36

State transition matrix of high speed relative motion equations in space short range
ZHOU Ying;YAN Ye;TAN Li-fen;TANG Guo-jin

..............page:84-87

Research on aircraft adaptive control reference model establishment method
LIU Shao-hua;DUAN Zheng-yu

..............page:56-59,64

Research on kinematics model of relative motion between spacecrafts
TIAN Yuan;HE Xing-suo;LI Xue-hua

..............page:92-96

Wind-tunnel investigation of aerodynamic force for airfoil using Gurney flap
HAO Li-shu;QIAO Zhi-de;SONG Wen-ping;ZHOU Hong

..............page:53-55

Flight simulation and control effectiveness analysis for aircraft post-stall maneuvers
YANG Sheng-min;LIU Chao;LIU Ya-hui

..............page:23-27

Survey of aircraft trajectory optimization methods
CHEN Gong;FU Yu;GUO Ji-feng

..............page:1-5

Airfoil design for tailless configurations using DISC algorithm
LI Pei-feng;ZHANG Bin-qian;CHEN Ying-chun;SHEN Dong

..............page:49-52

One method of missile motion modeling based on the execute coordinate system
ZHANG Da-yuan;ZHAO Yu-qin;LEI Hu-min;ZHANG Xu

..............page:88-91,96

Rapid calculation of entry footprint of suborbital launch vehicles
XIE Yong-feng;TANG Shuo

..............page:72-76

Research on stability of aircraft-pilot closed loop system based on matching of equivalent system
LI Da-wei;XU Hao-jun;HU Xin-jiang;LIU Dong-liang

..............page:19-22

Numerical research of rolling characteristics on canard missiles by fin trailing edge sweepback angle
JING Dai-yong;LI Jian

..............page:77-79

Study on aircraft lateral-directional character with different winglets
ZHANG Jian-jun;YANG Shi-pu;SI Jiang-tao

..............page:41-44

Design and software realization of the predictive control synthesis strategy
ZHANG Zhi-sheng;CHEN Huai-min;WU Cheng-fu;MA Song-hui

..............page:60-64

Dynamic stability of aircraft with rigid and flexible motion coupling
CAO Qi-kai;ZENG Hui-hua;BAI Nan

..............page:11-14,18

Design for nonlinear robust guidance law with structured uncertainties
TIAN Hong-liang;LIANG Xiao-geng;JIA Xiao-hong;WANG Peng-ju

..............page:80-83

Effects of ice accretion on aircraft dynamic response
ZHOU Li;XU Hao-jun;MIN Gui-long;LIN Min

..............page:32-36