Flight Dynamics 2010 Issue 3 Analysis of aircraft pilot coupling criteria

Analysis of aircraft pilot coupling criteria
liu hai tao ; liu zhen qin

..............page:85-88

Improved ADRC and its application in flight control augmentation
liu ji yu ; liu lin ; fan zhan qi

..............page:35-38

Research on lateral landing control law of carrier-based aircraft
zhang min ; chen bo ; zhang zong zuo

..............page:24-27

Constructing the maneuvering target estimation model with tracking-differentiator
peng jian liang ; sun xiu xia ; dong wen han ; li xiang qing

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

Design and simulation of model reference adaptive control for air-to-surface missile
shi zuo ; zhang xiao yi ; chen yong ; tang shuo

..............page:51-54

Survey of research for vehicle management systems
gao li ; wu wen hai ; qu zhi gang

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

Analysis on the estimation model of lift fan when designing VTOL
zheng zhi cheng ; zhou zhou

..............page:21-23

Optimal design for UAV\'s flight control system based on non-linear PID control
shang ying ; gao xiao guang ; fu xiao wei

..............page:47-50

Study of rendezvous angle of counter orbit satellite intercept based on ground TT&C station
li bang jie ; xian yong ; wang ming hai ; yang jun

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

Research on the integrated method of flight simulation system based on a flight simulator
zhang ling ; chen ning ; ji yun ; zhu jiang

..............page:39-42

Design of multi-missile formation hold controller
ma pei zuo ; zhang you an ; yu fei ; ji jun

..............page:69-73

Design of the guidance law based on the virtual target for ship-to-air missile beyond visual range
hu yun an ; zhao yong tao ; lin jia xin

..............page:55-58,63

Study of restraint of canard on non-linear pitchup of a strake-wing configuration
gong cui cui ; zhang bin qian ; li pei feng

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

Study of design method for FCS reconfiguration based-on H∞
zhang xiao jie ; wu wen hai ; zhou sheng ming

..............page:28-30,34

Active disturbance rejection control application to interceptor attitude control system
yang sheng jiang ; guo jian guo ; ge zhi lei ; zhou jun

..............page:78-81

Maximum cross range trajectory optimization based on quasi-equilibrium glide conditions
zhou hao ; chen wan chun

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

Design of helicopter all attitude controllers using H∞ loop shaping method
wang yong ; wang qing ; kang wei chang ; liang qing

..............page:43-46

Calculations of rain effects on aircraft performance
jue mou kai ; cao yi hua ; zhang rui min

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

Quantitative risk evaluation of flight testing subject based on operational characteristics of test pilot
liu dong liang ; liu lei ; xu hao jun ; li da wei

..............page:82-84,88

Longitudinal optimal trimming points research for three-surface CRW aircraft
li xing ; gao zheng hong ; liu yan

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

Modeling and simulation on propulsion system of minitype UAV
liu bin ; he jian ; zhang lin

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

Reconfiguration flight control to actuator\'s failure of helicopter
wang lin ; li guo yu ; zhao jian wei

..............page:31-34

Flight dynamic modeling and simulation for transport airdrop
yang miao sheng ; qu xiang ju

..............page:9-12

Control allocation for aircraft with multiple control effectors based on flight performance optimization
liu yan ; gao zheng hong

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

fei xing li xue zheng gao jian ze

..............page:封4