1002-0853
2014 Issue 2
Development and prospect of variable swept wing
dong yan fei ;, chen yuan zuo ;, peng jin jing ;
dong yan fei ;, chen yuan zuo ;, peng jin jing ;
..............page:97-100
..............page:封4
Research on calculating the effect of winglets on aircraft safety spacing of wake vortex
wei zhi qiang ;, liu fei ;, liu zuo ;
wei zhi qiang ;, liu fei ;, liu zuo ;
..............page:101-104
Effects of deck motion on carrier-based aircraft's catapult launching performance
cai li qing ;, jiang ju ;, wang xin hua ;, pan zuo zuo ;
cai li qing ;, jiang ju ;, wang xin hua ;, pan zuo zuo ;
..............page:105-109
Research for NA/AOA limiter law design
wang zuo ;, wang bo ;, li de shang ;
wang zuo ;, wang bo ;, li de shang ;
..............page:110-113
Constant wind effects on free flight of unmanned aerial vehicle
gao jiu zhou ;, duan zhen ;, jia hong guang ;
gao jiu zhou ;, duan zhen ;, jia hong guang ;
..............page:114-117
Analysis of roll step-input response of a cyclogyro
du fan ;, hu yu ;
du fan ;, hu yu ;
..............page:118-121
Modeling and trimming of tiltrotor aircraft
wang qi ;, wu wen hai ;, qu zhi gang ;, he jian ;
wang qi ;, wu wen hai ;, qu zhi gang ;, he jian ;
..............page:122-125
Calculation of helicopter tail rotor vortex ring boundary
sun wen sheng ;, ma hong ru ;
sun wen sheng ;, ma hong ru ;
..............page:126-128
Analysis of helicopter main hub drag with CFD
li dong feng ;, li li zhou ;, xiao feng le ;, li cai xia ;
li dong feng ;, li li zhou ;, xiao feng le ;, li cai xia ;
..............page:129-131,144
Design and research for conceptual parameters of solar-powered non-stop airplanes
cao qing ;, zhou zhou ;, chang min ;
cao qing ;, zhou zhou ;, chang min ;
..............page:132-136
Design of sliding mode attitude control system for stratospheric airship
wang ling ;, guo jian guo ;, zhou jun ;, wang guo qing ;
wang ling ;, guo jian guo ;, zhou jun ;, wang guo qing ;
..............page:137-139
Research on variable structure guidance law for large-airspace spiral maneuver of missile
gao xiao dong ;, zhao hong chao ;, song gui bao ;
gao xiao dong ;, zhao hong chao ;, song gui bao ;
..............page:140-144
θ-D approach-based 3-dimensional terminal guidance law with impact angle constraint
wang hong xue ;, li xin guo ;, wang chen zuo ;
wang hong xue ;, li xin guo ;, wang chen zuo ;
..............page:145-148,159
Optimization of multi-objective reentry trajectory for hypersonic gliding vehicle
ren yang ;, cao lin ping ;, guo hai feng ;, ding da li ;
ren yang ;, cao lin ping ;, guo hai feng ;, ding da li ;
..............page:149-154
Transitional orbit optimization research of space-based interceptor
gao hao ;, zhang ke ;, wang pei ;
gao hao ;, zhang ke ;, wang pei ;
..............page:155-159
Curve-fitted modeling method for hypersonic vehicle
cui jian feng ;, zhang ke ;, lv mei bai ;
cui jian feng ;, zhang ke ;, lv mei bai ;
..............page:160-164,169
Attitude pointing tracking control for fractionated spacecraft
li zhao ming ;, gao yong ming ;, niu ya feng ;, huang yong ;, li lei ;
li zhao ming ;, gao yong ming ;, niu ya feng ;, huang yong ;, li lei ;
..............page:165-169
Research of optimal on-off control for satellite formation flying
chen xiang ;, liao he ;, tong qing wei ;, song tao ;
chen xiang ;, liao he ;, tong qing wei ;, song tao ;
..............page:170-173
Predicting method of the elevator rate saturating induced longitudinal PIO's tendency
liu zuo ;, wang hai wei ;, jia xiao peng ;
liu zuo ;, wang hai wei ;, jia xiao peng ;
..............page:174-178
Identification of CRW UAV's dynamic model in cruising mode
wang ban ;, zhan hao ;, huang jing ;
wang ban ;, zhan hao ;, huang jing ;
..............page:179-182,188
An approach of UAV's aerodynamic parameter identification
li han bing ;, wu da wei ;
li han bing ;, wu da wei ;
..............page:183-188
..............page:189-192