1002-0853
2013 Issue 6
..............page:封4
Research on waypoint flight simulation based on pilot control characteristics
hou shi fang ;, pei bin bin ;, su chen ;, xu hao jun ;, zhang jiu xing ;
hou shi fang ;, pei bin bin ;, su chen ;, xu hao jun ;, zhang jiu xing ;
..............page:481-485
Numerical simulation and analysis on aerodynamics of fiat plate airfoil in ground effect
chen shi shi ;, xiong fen fen ;
chen shi shi ;, xiong fen fen ;
..............page:486-490
Numerical simulation of hypersonic flow fields around sphere-cone-shaped dome
li xin ;, wang ya hui ;, xu li ;, xu dong ;
li xin ;, wang ya hui ;, xu li ;, xu dong ;
..............page:491-495
Research on the RSCSSO based on self-adaptive approximation model and its application
hu yu ;, liu ming hang ;
hu yu ;, liu ming hang ;
..............page:496-500
Analysis of converse spin characteristics about a certain aircraft based on flight parameters
li song ;, liu xiu juan ;, ming lei ;, wang shu qiang ;, wu gao long ;
li song ;, liu xiu juan ;, ming lei ;, wang shu qiang ;, wu gao long ;
..............page:501-503,507
Control law design and simulation based on LQR for super-low-altitude airdrop
gao ya kui ;, hei wen jing ;, xue yuan ;
gao ya kui ;, hei wen jing ;, xue yuan ;
..............page:504-507
A method of quadratic programming control allocation based on BFGS algorithm
li guang wen ;, zhang ning ;, zhang wei guo ;
li guang wen ;, zhang ning ;, zhang wei guo ;
..............page:508-511
Design and simulation of control law for large transport aircraft with heavy cargo continuous airdropping
wang pei ;, zhang xi tao ;
wang pei ;, zhang xi tao ;
..............page:512-515
Feedback linearization controller design for quadrotor UAV with multiple specifications
ke yi jie ;, wang sheng ;, zhou jiang hua ;
ke yi jie ;, wang sheng ;, zhou jiang hua ;
..............page:516-520
Double-loop hybrid iterative quasi-sliding mode control strategy for autolanding of UAV
gao yang jun ;, liu xi ;, liu yu kun ;, sun xiu xia ;
gao yang jun ;, liu xi ;, liu yu kun ;, sun xiu xia ;
..............page:521-525
Research on small unmanned helicopter modeling and robustness control
wang qi ;, wu wen hai ;, xu li ;
wang qi ;, wu wen hai ;, xu li ;
..............page:526-529,534
Helicopter model-following control based on fatigue damage feedback
fang xing ;, liu jing ;, wu ai guo ;
fang xing ;, liu jing ;, wu ai guo ;
..............page:530-534
LPV gain-scheduling control of tactical missile with morphing wings
duan chao yang ;, liao zhi zhong ;, zhang gong ping ;
duan chao yang ;, liao zhi zhong ;, zhang gong ping ;
..............page:535-539
Research on firing criterion and firing logic of trajectory control engine for an intercept missile
ge zhi lei ;, lei zuo jie ;, zhou jun ;
ge zhi lei ;, lei zuo jie ;, zhou jun ;
..............page:540-544
Influences of aerodynamic shapes on reentry footprint of space vehicle
hu hai long ;, nan ying ;
hu hai long ;, nan ying ;
..............page:545-548,552
Reasearch on fighter forced landing technologies
cui yi hua ;, han yi xin ;, wang qi ;
cui yi hua ;, han yi xin ;, wang qi ;
..............page:549-552
Application of HQRM on airworthiness certification
zhang tong ;
zhang tong ;
..............page:553-557
Research on flight control technology of the high-aspect-ratio flying wing model aircraft
liu chao jun ;, liu shang min ;, sun jian ;
liu chao jun ;, liu shang min ;, sun jian ;
..............page:558-560,565
A maintaining control method for maneuvering-net space robot
huang pan feng ;, ma jun ;, meng zhong jie ;
huang pan feng ;, ma jun ;, meng zhong jie ;
..............page:561-565
Parallel runway arrival aircraft-sequencing optimization
gu qiu li ;, wang li li ;
gu qiu li ;, wang li li ;
..............page:566-569
Matching relation between the payload of loitering monition and the loading space of long rang rocket missile
li yong ze ;, lu yong gang ;, sun chuan jie ;
li yong ze ;, lu yong gang ;, sun chuan jie ;
..............page:570-573