Flight Dynamics 2007 Issue 4 LQG/LTR Multivariable Controller Design for a Gust Load Alleviation System

LQG/LTR Multivariable Controller Design for a Gust Load Alleviation System
ZHANG Jun-hong;LI Zhen-shui;ZHAN Meng-quan;GAO Ya-kui

..............page:33-36

Research of Handling Characteristics of Aircraft in Low Dynamic Pressure Situation
WANG Xin-hua;YANG Yi-dong;ZHU Hua

..............page:29-32,36

Parachute Landing Recovery Motion Analysis for Unmanned Aerial Vehicle
LI Guang-chao;MA Xiao-ping

..............page:25-28

The Controller Design of UAV Formation Flight
ZHU Zhan-xia;ZHENG Li-li

..............page:22-24

Scaled Helicopter Modeling for Flight Control System Design
SONG Yan-guo;WANG Huan-jin

..............page:17-21

Structure Self-Adapting ANN Method in Modeling of Unsteady Aerodynamics
GONG Zheng;SHEN Hong-liang

..............page:13-16

Control System Design and Emulation for Vectored Thrust Aircraft
WANG Mei-xian;LI Ming;ZHANG Zi-jun

..............page:8-12

Research on Longitudinal Aerodynamic Parameter Optimize of a Joined-Wing Configuration Aircraft
WU Guang-hui;WANG Miao-xiang;ZHANG Jian

..............page:5-7,12

Simulation Research of Flight Test Techniques for Battle Effectiveness Evaluation of IFFPC System
LIU Xuan-min;TIAN Fu-li;YANG Jan-guo

..............page:1-4

fei xing li xue zheng gao jian ze

..............page:封底

Dynamic and Static Weapon-Target Assignments of Air Defense
JIANG Huan;CHEN Wan-chun

..............page:90-93

Positioning and Orientation Error Propagation Models for Submarine-Launched Ballistic Missile
ZHENG Wei;TANG Guo-jian

..............page:86-89

Study on Design of the Structure Self-Stabilization for Satellite Constellation
XIANG Jun-hua;FAN Li;ZHANG Yu-lin

..............page:81-85

Design and Capability Analysis of an Aircraft with Inflatable Wing
LV Qiang;YE Zheng-yin;LI Dong

..............page:77-80,85

Modeling and Simulation of the Tanker's Wake Field
CHEN Bo;DONG Xin-min;XU Yue-jian;CHEN Ya-li

..............page:73-76

A Study on Stealth Technology in UAV Inlet Design
YU Xin-hua;ZHAO Ming-yu

..............page:69-72

Application of μ-Analysis in Clearance of Stability Margin of Flight Control System
JI Duo-hong;LIU Lin;TANG Qiang

..............page:64-68

A Fast-Reconstruction Algorithm for Aircraft Ascending Trajectory
WAN Song;FANG Qun;ZHU Zhan-xia

..............page:61-63,68

On an Online Data Computation Method Based on Air Launch Point
XIAN Yong;WANG Ming-hai;CHENG Yan-meng

..............page:58-60

An Analytic Solution of the Ballistic Missile's Reentry Trajectory
QIAN Shan;ZHENG Wei;ZHANG Shi-feng;CAI Hong

..............page:54-57

Error Analysis of Guidance Based on Virtual Target Point
WANG Ji-ping;WANG Ming-hai

..............page:50-53

Study on Iteration of the Ballistic Missile's Standard Trajectory
MA Dan-shan;WANG Ming-hai;CHE Ming-bo

..............page:48-49,53

Design of Thrust Vector Control System for a Ballistic Missile
ZHAO Hong-chao;WANG Ting;GU Wen-jin;ZHANG Ru-chuan

..............page:44-47

Research of Missile Flight Route for Radar Exposure Minimization
MA Pei-bei;ZHANG You-an;FAN Zuo-e;JI Jun

..............page:40-43

Interception Guidance Design for Interceptor with Terminal Aspect Angle Constraint
XING Li-dan;CHEN Wan-chun;YIN Xing-liang

..............page:37-39