1002-0853
2002 Issue 4
Design of Nonlinear Adaptive Robust Control Systems for a Missile
hu yun an ; jin yu qiang ; zhang you an ; cui ping yuan
hu yun an ; jin yu qiang ; zhang you an ; cui ping yuan
..............page:65-68
Study on Nonlinear Three-Dimensional H∞ Robust Guidance Law
li xin guo ; chen hong ying
li xin guo ; chen hong ying
..............page:61-64
Study on Judgement of the Threat Level
wu qiang ; cao yi hua ; jin chang jiang
wu qiang ; cao yi hua ; jin chang jiang
..............page:56-60
Analysis to the Problem of Airplane's Cross-Wind Landing
zhang li bin ; su sheng xi
zhang li bin ; su sheng xi
..............page:51-55
Safe Operating Envelopes of Onboard Helicopter and Its Flight Test
zhao wei yi ; liu hang ; fu bai xian
zhao wei yi ; liu hang ; fu bai xian
..............page:48-50，60
..............page:44-47
Investigation on Wing Rock in a Low Speed Wind Tunnel for Fighter with Different Configurations
jiang yu biao ; sun hai sheng ; zhang jun ; li bao
jiang yu biao ; sun hai sheng ; zhang jun ; li bao
..............page:39-43
Design Researchon Advanced Aircraft Nonlinear H∞ Flight Control System
duan fu hai ; chen gang ; han chong zhao
duan fu hai ; chen gang ; han chong zhao
..............page:36-38,43
Hierarchical Variable Structure Reconfigurable Flight Control System
luo feng ; ding kai feng ; deng jian hua
luo feng ; ding kai feng ; deng jian hua
..............page:31-35
Reconfigurable Control System Design for the Aircraft Mounted Thrust Vector
su hao qin ; deng jian hua
su hao qin ; deng jian hua
..............page:27-30
Study of a Carrier Landing Mode with Neutral Stabilty Using Direct Lift Control
yu yong ; yang yi dong ; dai shi jun ; fan yan ming
yu yong ; yang yi dong ; dai shi jun ; fan yan ming
..............page:22-26
Attitude Estimation Using Modified Rodrigues Parameters
cheng yang ; yang di ; cui zuo tao
cheng yang ; yang di ; cui zuo tao
..............page:18-21，26
An Improved Method of Aerodynamic Calculation for the Fuselage of a Helicopter
chen gang ; duan fu hai ; he chang an
chen gang ; duan fu hai ; he chang an
..............page:14-17
Autorotation Flight Path Calculation of a Coaxial Helicopter
wang xiao yong ; deng yan min
wang xiao yong ; deng yan min
..............page:10-13
Research on Dynamics Integration Features for Unmanned Long-Endurance Flight Vehicles
zhou jie ; zhang shu guang
zhou jie ; zhang shu guang
..............page:6-9
Application and Development of Artificial Neural Networks in Flight Control Field
li feng ; wang yan yang ; jin chang jiang
li feng ; wang yan yang ; jin chang jiang
..............page:1-5