Flight Dynamics 2010 Issue 1 Modeling and simulation research on error origin of fresnel lens optical landing system

Modeling and simulation research on error origin of fresnel lens optical landing system
huang zuo ; hong guan xin

..............page:92-96

Simulaiton modeling of air-to-air missile based on UML
li bo ; gao xiao guang

..............page:61-64

Sliding mode controller design based on SMOD
gu wen jin ; fan zuo e ; bi lan jin ; wang xiao jie

..............page:53-56

Equilibrium computation of helicopters used by hybrid genetic algorithm
dai ji yang ; wu guo hui ; zhu guo min

..............page:24-28

Dynamics analysis of the constrained and centroid biased on-orbit satellite separation
jiang chao ; wang zhao kui ; fan li ; zhang yu lin

..............page:76-79

Numerical study on longitudinal static stability of a canard WIG craft
li yu long ; yang zuo ; yang zhi gang

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

Research on the new generation RLV reentry trajectory fuzzy control
zhang bin ; xu min ; chen shi zuo

..............page:69-71,75

Study of control law and modelling on unmanned air vehicle launching process
cai yun peng ; zuo jian guo ; wang liang

..............page:80-83

fei xing li xue zheng gao jian ze

..............page:封4

Research on sliding mode guidance method for air-to-ground missile
yin yong zuo ; yang ming ; wu peng

..............page:44-46,52

Method for clearance of nonlinear flight control laws research
lv quan xi ; zhan zheng yong

..............page:20-23,28

Key technologies of solar powered unmanned air vehicle
gao guang lin ; li zhan ke ; song bi feng ; ding xiang

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

3-D path planning for UAV in radar threat condition
hao zhen ; zhang jian ; zhu fan ; cai man yi

..............page:47-52

Research for the flight path planning based on adaptive genetic algorithm
liu chao ; ou jie ; cao zuo

..............page:36-39

Quantified effects of rain on aircraft longitudinal flying qualities
huang cheng tao ; wang li xin

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

Impact-angle-control guidance law of missile in 3-space
zhang gong ; li fan ; wan cong mei ; zhang wen peng

..............page:65-68

An optimal guidance law considering second order missile-body characteristics with terminal angle constraint
wang jing ; guo jian guo ; zhou jun ; zou min huai ; chen yong

..............page:72-75

Evaluating effectiveness for formation beyond visual range air combat based on multi-step adjudication method
ma dong li ; zheng jiang an ; zhao juan juan

..............page:88-91

Modeling and experiment of tilt-rotor aircraft in hover mode
zou can dong ; wang wei jun ; qu xiang ju

..............page:84-87

Research on flying qualities criteria of the unmanned aerial vehicle
tao yu jin ; wang jian pei

..............page:13-15,19

Gain scheduling method of aircraft control law in the large flight envelope
li guang wen ; jia qiu ling ; zhang wei guo ; liu xiao xiong

..............page:29-31,35

Design of the on-off control laws of kinetic kill vehicle\'s attitude and orbit control thrustors
duan jun hong ; gao xiao guang

..............page:57-60

Flapping control mechanism for insect-like flapping micro aerial vehicles
xia feng ; zhang jian bo ; zhang peng peng

..............page:16-19

New method for lateral directional axis control of aircraft based on total energy control
ke ji ; wang wei ; li ai jun ; wang chang qing

..............page:32-35

Research on topology-fixed distributed control of multi-UAV flocking
shen dong ; wei rui xuan ; huang zuo ; song min ; hu ming lang

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