1002-0853
2014 Issue 1
Study on longitudinal flight dynamic characteristics of high altitude flexibility solar UAV
feng yang fan ;, xiao wei ;, zhou zhou ;
feng yang fan ;, xiao wei ;, zhou zhou ;
..............page:1-4
Optimal trim for helicopter based on GA and LM hybrid algorithm
ni xian ping ;, tan jian feng ;, wang hao wen ;, wu chao ;
ni xian ping ;, tan jian feng ;, wang hao wen ;, wu chao ;
..............page:5-9,19
Numerical simulations of Reynolds number effect on flow characteristics at high-lift devices
li zhong wu ;, liang yi hua ;
li zhong wu ;, liang yi hua ;
..............page:10-14
Vertical gust alleviation control law designed based on IWOABC algorithm
qiu yue heng ;, zhang wei guo ;, zhao peng xuan ;, zhu jiang le ;
qiu yue heng ;, zhang wei guo ;, zhao peng xuan ;, zhu jiang le ;
..............page:15-19
Guidance and control of autonomous aerial refueling rendezvous
wang xin hua ;, yuan suo zhong ;, zheng feng ying ;
wang xin hua ;, yuan suo zhong ;, zheng feng ying ;
..............page:20-24
Research on multiple mode conversion technology of carrier-based aircraft landing
cai li qing ;, jiang ju ;, pan zuo zuo ;, wang xin hua ;
cai li qing ;, jiang ju ;, pan zuo zuo ;, wang xin hua ;
..............page:25-28,37
Robust dynamic surface control for underactuated VTOL aircraft
liu jin zuo ;, yuan rui xia ;
liu jin zuo ;, yuan rui xia ;
..............page:29-33
Research on entry trajectory optimization of lifting reentry vehicle
li wei ;, luo qiao ;, wang zhi gang ;
li wei ;, luo qiao ;, wang zhi gang ;
..............page:34-37
Design of optimal guidance law with higher-order dynamic lags
chen huan ;, liu zuo long ;, wei jian li ;, yu yun feng ;
chen huan ;, liu zuo long ;, wei jian li ;, yu yun feng ;
..............page:38-42,47
Precision analysis of missile guidance system based on SLAM
an jin ;, peng shao xiong ;, wang hai tao ;, zou qiang ;
an jin ;, peng shao xiong ;, wang hai tao ;, zou qiang ;
..............page:43-47
Near-optimal midcourse guidance law for hypersonic missile
chen wan chun ;, qiao qing qing ;
chen wan chun ;, qiao qing qing ;
..............page:48-52
Nonlinear control system design for hypersonic vehicle
guo jian guo ;, lei bo juan ;, wang guo qing ;, zhou jun ;
guo jian guo ;, lei bo juan ;, wang guo qing ;, zhou jun ;
..............page:53-56,61
Study on integrated guidance and control of reusable launch vehicles
li xin guo ;, wang qian ;
li xin guo ;, wang qian ;
..............page:57-61
Design of predictive controller used in hypersonic vehicle cruise phase
guo jian guo ;, wang guo qing ;, zhang tian yi ;, zhou jun ;
guo jian guo ;, wang guo qing ;, zhang tian yi ;, zhou jun ;
..............page:62-64,69
Coverage area of orbit-interception with single-impulse action
li ya xiong ;, liu xin xue ;, shu jian sheng ;, wu jian ;, zuo jian zuo ;
li ya xiong ;, liu xin xue ;, shu jian sheng ;, wu jian ;, zuo jian zuo ;
..............page:65-69
Research on intelligent maneuver penetration of missile based on differential game theory
shi jin zuo ;, tian hai peng ;, wang jian ;, xian yong ;
shi jin zuo ;, tian hai peng ;, wang jian ;, xian yong ;
..............page:70-73,83
Prediction and evaluation method for PIO based on modified differential evolution
chen yun xiang ;, ji xiao ning ;, li lin ;, li qian ;
chen yun xiang ;, ji xiao ning ;, li lin ;, li qian ;
..............page:74-77,83
Analysis of the effect of altitude on RNP approach safety
zhang guang ming ;
zhang guang ming ;
..............page:78-83
Modeling and simulation of atmospheric turbulence
wang hua dong ;
wang hua dong ;
..............page:84-87,92
Research of requirements and queuing network model of aviation security for carrier-based aircraft
li xin fei ;, lv kai dong ;, zhu qi dan ;
li xin fei ;, lv kai dong ;, zhu qi dan ;
..............page:88-92
Real-time calibration method of magnetometer
bao wei min ;, tang guo jian ;, yang yu bin ;
bao wei min ;, tang guo jian ;, yang yu bin ;
..............page:93-96
..............page:封4