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Flight Dynamics
1002-0853
2006 Issue 1
Research on the Altitude Control Device of a Mini-UAV Engine's Diaphragm Carburetor
LI Yu-zhen;MA Zhen;WANG Xing-hai;BAI Jing-yuan;GAO Pi-zhou
..............
page:93-96
Information Fusion Technique and Its Application in Integrated Navigation
LI Zheng-qiang;WANG Hong-li;YANG Yi-qiang;LIU Chun-zhuo;CHEN Qi
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page:89-92
Study on a Kind of Local Path Replanning Algorithm for UAVs
XIAO Qin-kun;GAO Xiao-guang
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page:85-88
Application of Auto-Disturbance-Rejection-Controller to a Missile
CHEN Xin-long;YANG Di;GENG Bin-bin
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page:81-84
Helicopter Flight Control System Simulation Research
DAI Ning;SI Yun-ling;LEI Ya-ping
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page:77-80,84
Application of the Polynomial Fit Algorithm in the Aircraft Flight Test
ZHANG Chun-wei;WU Su;ZHOU You-ming;LU Xiao-dong
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page:73-76
Application of a Robust Flutter Margin Method
QU Fu-cun;SHI Zhong-ke
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page:70-72
Flight Dynamics Problems in Design of Control Augmentation Systems for Aircraft
LIU Zhen-qin;ZHOU Xiao-qiao
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page:66-69
Research of the Trajectory Simulation Equations Based on the Earth's Core Frame of Axes
LEI Gang;XIAN Yong;WANG Ming-hai
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page:63-65
Near Fuel-Optimal Nonlinear Control for Satellite Formation Keeping
WU Bao-lin;CAO Xi-bin
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page:59-62
Separation Dynamics Process of Piggyback Satellite from Launch Vehicle
FU Bi-hong;DU Guang-hua
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page:55-58
Study of Terminal Guidance Laws for Space Intercept
MA Hui;FANG Qun;YUAN Jian-ping
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page:52-54,58
Parachute Downward Motion Analysis for an Air Launch Rocket
XU Zhi;TANG Shuo
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page:48-51
Optimum Design of Climb Trajectory for a Cruise Missile
HOU Hong-lu;LIU Chang-an;ZHOU De-yun;HE Hong-li
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page:45-47,51
Research on the Error Correction Algorithm of Ballistic Missile CNS/INS Integrated Navigation
LI Bang-jie;WANG Ming-hai
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page:41-44
Six-Degree-of-Freedom System Simulation for the Joint Direct Attack Munition
LI Zhuo-peng;LI Xin-guo
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page:37-40
Research on the Stability in the Overload Control of Missile Based on a Kind of Integral-Type Sliding Surface
GU Wen-jin;LEI Jun-wei;FENG Guo-hu
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page:33-36,40
Approximitive Solution of the Ballistic Missile's Reentry Trajectory
LI Fang-qing;ZHANG Yi;WANG Fang
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page:30-32
Missile's Optimal Glide Trajectory Design and Its Existed Problems
SUN Ming-wei;PENG Nan-nan;YANG Ming
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page:26-29
The Design and Examination of Flight Robust Controller
MAO Shi-bin;SHI Zhong-ke
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page:22-25
A Solution for Aircraft Control Allocation
CAO Zong-tao;MA Rui-ping;ZHANG Ming-lian
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page:17-21
Control Allocation for High Performance Aircraft with Multi-Control Effectors
ZHAN Zheng-yong;LIU Lin
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page:13-16,21
Conceptual Study on Flight Control Laws for a Trans-Aerosphere Vehicle in Climbing Phase
ZHOU Yu-xiao;ZHANG Zi-yan;MING Xiao
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page:9-12
The Influence and Compensation of Deck Motion in Carrier Landing Approach
SHI Ming;QU Xiang-ju;WANG Meng-hui
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page:5-8
Rapid Prototyping of Flight Control System
WANG Xiao-dong;TANG Shuo;ZHOU Xu-feng
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page:1-4