Flight Dynamics 2010 Issue 4 Investigation of Gurney flap on improving dynamic stall aerodynamic characteristics of an airfoil

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Flight Dynamics
1002-0853
2010 Issue 4

Investigation of Gurney flap on improving dynamic stall aerodynamic characteristics of an airfoil
wang yuan yuan ; zhang bin qian

..............page:5-8

Study of two engines multi kinetic vehicle guidance law
wang lei ; cai yuan wen

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

The reconfigurable flight control design of adaptive sliding mode control based on simple adaptive control
qi xiao hui ; yang zhi jun ; wu xiao zuo

..............page:37-41

Mission planning for multiple UCAVs under the information netting
meng bo bo ; gao xiao guang

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

Flight test method for validating the aerodynamic model of post-stall maneuvering
yang sheng min ; liu chao ; liu ya hui

..............page:77-81

Study on optimum cruise trim of hypersonic wing-body configuration
zhong fan jun ; wang zheng ping

..............page:29-31,36

Robust adptive inversion automatic landing flight control based on neural network
chen long sheng ; wang chang kun

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

Robust control law design for aeroelastic vehicle based on model-following method
hu meng hui ; shen hong liang

..............page:21-24

Configuration design and experiment study of an adaptive wing for UAV
li wen ; song bi feng ; zhang zuo

..............page:17-20

New sliding mode variable structure control and its application to the flight control
hu jian bo ; wang jian hao

..............page:46-49

Identification and prediction of aerodynamic data in flight simulation based on SVR
xue yuan ; xu hao jun ; chai shi jie ; liu dong liang

..............page:9-13

Control augmentation system design for a large jet with relaxed static stability
li le yao ; li zuo ; wang xin min

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

Longitudinal control system design for UAV without vertical gyroscope
yang fang wei ; huang yi min ; sun chun zhen

..............page:50-53,58

Constraints modeling and simulation of the internally carried air-launched vehicle
zheng xiao long ; tang shuo

..............page:64-67,72

Flight program design for small launch vehicle in atmosphere flight stage
yang xi xiang ; jiang zhen yu ; zhang wei hua

..............page:68-72

Cooperative control system for multi-missiles high-dynamic autonomous formation
mu xiao min ; wu sen tang

..............page:59-63

Spin flight simulation tests for a certain fly-by-wire aircraft
yang jian guo ; zhang pei tian ; wang qi

..............page:85-88,92

Implied function analysis for maximum-range flight with fixed fuel consumption
chen zuo li ; dong xin min

..............page:89-92

fei xing li xue zheng gao jian ze

..............page:封4

Design of aerocraft landing-glide controller based on direct feedback linearization method
li xue song ; li ying zuo ; xu hao jun ; guo chuang

..............page:42-45

Controller design based on nonlinear missile dynamic inverse error compensate
yang zhi feng ; lei hu min ; li qing liang ; xu xin zhong ; xu jian zuo

..............page:54-58

PIO susceptibility evaluation approach based on sequential quadratic programming
zhao zhi zhong ; liu yan ; gao zheng hong

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

Flight test analysis on helicopter rotor vortex ring
zhang xi ; sun jie

..............page:82-84

High precision numerical simulation method for static aeroelastic analysis of wing
liu fu long ; zhan hao

..............page:14-16