Flight Dynamics 2009 Issue 3 Status and Future of Control Allocation for Aerospace Vehicle

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Flight Dynamics
1002-0853
2009 Issue 3

Status and Future of Control Allocation for Aerospace Vehicle
MA Jian-jun;LI Wen-qiang;LI Peng;ZHENG Zhi-qiang

..............page:1-5,10

Flow Mechanism of the Influence of Forward-Swept Angle on the Longitudinal Characteristics of Aerodynamic Configuration with Forward-Swept Wing
MI Kang;WANG Xu;LIU Wen-fa

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

On Partial Optimization Design for a C-wing Configuration
ZHU Wei-dong;ZHANG Bin-qian

..............page:11-14

Research on the Guidance Precision Distribution Method Based on the Variance Analysis
SHANG Lei-yun;TANG Shuo

..............page:93-96

Method of Controlling West-East Orbit Longitude Drift Rate with a Given Longitude
ZHAO Yong-gang;DENG Fu-qi;LI Heng-nian

..............page:90-92,96

Influence and Compensation of High-Orbit Satellite Imaging Based on Orbit Motion
CHEN Yin-chao;WANG Zhi-gang;CHEN Shi-lu

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

Reduced-Thrust Takeoff Technique Applied to Passenger Airplanes
LIU Xiao-ming;ZHAO Ting-yu;WEN Xiao-hang;CHAO Hai-tao;JIANG Ling-ping

..............page:83-85

Calculation of Transonic Unsteady Flow Using Dynamic Unstructured Grids
WANG Jun-li;ZHOU Zhou

..............page:78-82

Forecast Modeling of Flight Accident Rate for Aircraft Based on LS-SVM Method
HU Liang-mou;XU Hao-jun;MENG Jie;DONG Xin-min

..............page:74-77

Research on Flight Test Technology of the Instant Agility Scale
MENG Jian-wen;WANG Qi;ZHOU Chang-yue

..............page:71-73,77

Nonlinear Dynamic-Inversion Reentry Flight Control of Suborbital Reusable Launch Vehicle
TAN Zheng;LI Xin-guo

..............page:66-70

Dynamics Analysis for an Internal Air Launch Vehicle Launched from a Cargo Aircraft with Gravity Extraction
LI Yi;TANG Shuo;XU Zhi

..............page:62-65

Analysis of Sliding Mode Stability in Variable Structure Guidance Under Restrained Overload
GUO Jian-guo;ZHOU Jun

..............page:58-61

Design of Missile's Flight Control System Based on PSO Algorithm
LI Dong;LI Yu-tong;TIAN Bao-jie;ZHOU Xiao-guang

..............page:54-57,61

Flight States Estimate of the Missile Active Phase Based on Moving-Based Gravity Gradiometer
WANG Ji-ping;WANG Ming-hai;LIU Xin-xue;YAN Jian-zheng

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

Research on Super-Sonic Missile Guidance Plan Based on the Terminal Angular Constraint
ZHANG Ru-chuan;GU Wen-jin;ZHAO Hong-chao

..............page:45-49

Indirect Method for the Hypersonic Vehicle Maximum-Glide Problem
LI Jia-feng;ZHOU Hao;CHEN Wan-chun

..............page:41-44,49

Research on Robust Terminal Guidance Law for Blend-Control Missiles
XIE Zeng-hui;LIU Zhan-chen;LI Wei

..............page:36-40

Integrated Guidance and Control for the Pitch Plane of a Guided Bomb with SINS/GPS
LIANG Zhuo;XUE Xiao-zhong;WANG Hang;MA Wei

..............page:32-35,40

Dynamic Surface Backstepping Control for Supermaneuverable Flight
SONG Hong-fei;SUN Xiu-xia;DONG Wen-han;LIN Yan

..............page:28-31

Design of Optimal Arresting Force in Aircraft Arresting System
WU Juan;SUN Juan-ping;DU Juan

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

Small Unmanned Aerial Vehicle Aerodynamic Design of Low Reynolds Number
BAI Feng;BAI Junq-iang;CHEN Ke-jia

..............page:19-22,27

Study of Initial Launching States for Ship-Based UAV
ZHANG Shi-hui;ZHU Xiao-ping;ZHOU Zhou;YAO Jian-guo

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