1002-0853
2000 Issue 4
A reconfigurable flight control system design by output feedback
TANG Xiao-jing;ZHANG Jun-chang;REN Zhang;ZHOU Zi-quan
TANG Xiao-jing;ZHANG Jun-chang;REN Zhang;ZHOU Zi-quan
..............page:85-88
Research on the control rule of air-surface missile
SU Hao-qin;WANG He-ping
SU Hao-qin;WANG He-ping
..............page:81-84
Study on the performance of the ejection sea
HU Guo-cai;XIANG Jin-wu
HU Guo-cai;XIANG Jin-wu
..............page:78-80,84
The research on the flying safety problem during ground attack target shooting
ZHANG Li-bin;SHI Shang-dong;LIU Jian-chao
ZHANG Li-bin;SHI Shang-dong;LIU Jian-chao
..............page:73-77
The influence of the trailing vortex on the flight safety of wing plane
AN Chong-jun;LIU Chang-wei
AN Chong-jun;LIU Chang-wei
..............page:69-72
H∞ control based on dropping-degree of the model and its application to airplane landing under wind disturbance
WANG Xin;SHI Zhong-ke
WANG Xin;SHI Zhong-ke
..............page:65-68
Robyst flight control system design based on QFT
LI Zhong-jian;AN Jin-wen
LI Zhong-jian;AN Jin-wen
..............page:37-40
The calculation of the modern fighter's directional-lateral mode characteristics
DONG Yan-fei;LI Jia-lin
DONG Yan-fei;LI Jia-lin
..............page:33-36,53
Research of attitude simulation using quaternion
ZHOU Jiang-hua;MIAO Yu-hong;LI Hong;SUN Guo-ji
ZHOU Jiang-hua;MIAO Yu-hong;LI Hong;SUN Guo-ji
..............page:28-32
Study of horizontal navigation and control for mini remotely piloted vehicles
YAN Xi-jun;GAO Jin-yuan;TU Ba-ning
YAN Xi-jun;GAO Jin-yuan;TU Ba-ning
..............page:24-27
The effects of rate limiting element on PIO
XU Yan-jun;JIAO Yun-tao
XU Yan-jun;JIAO Yun-tao
..............page:21-23,32
Introduction to operational effectiveness analysis for attacking aero-complex
AI Jian-liang;ZHANG Jun;WU Jing-bo
AI Jian-liang;ZHANG Jun;WU Jing-bo
..............page:17-20
The design and implementation of flight test management system
HUANG Ming-shi;LIU Yong-zhi;ZHENG Quan
HUANG Ming-shi;LIU Yong-zhi;ZHENG Quan
..............page:14-16
Research on the optimization of air refueling mission
SUN Jin-biao;SHI Ke-ru;WANG Ke-ge
SUN Jin-biao;SHI Ke-ru;WANG Ke-ge
..............page:10-13
The hardwire and their characters of the transport aircraft fly-by-light control system
LIU Yong;WU Mi-cui;WANG Zhong-ji
LIU Yong;WU Mi-cui;WANG Zhong-ji
..............page:6-9
Aeroservoelastic stability of missile
YANG Chao;WU Zhi-gang
YANG Chao;WU Zhi-gang
..............page:1-5
Application of mixed H2/H∞ robust control to aircraft
WANG Jin-hua;SHI Zhong-ke;CAO Li;DAI Guan-zhong
WANG Jin-hua;SHI Zhong-ke;CAO Li;DAI Guan-zhong
..............page:61-64,72
The application of system identification in the modeling of missile
CUI Li-ming;ZHOU Jun;ZHOU Feng-qi
CUI Li-ming;ZHOU Jun;ZHOU Feng-qi
..............page:58-60
To determine the shock and position error of an aircraft from supersonic speed to the stall area
ZHANG Pei-tian;WANG Qi;LI Shu-you
ZHANG Pei-tian;WANG Qi;LI Shu-you
..............page:54-57
Study on single-channel control for rotary missile
YI Yan;ZHOU Feng-qi;ZHOU Jun
YI Yan;ZHOU Feng-qi;ZHOU Jun
..............page:50-53
A gain variable proportional guidance law for stationary target
ZHU Zhan-xia;WANG Jian-pei
ZHU Zhan-xia;WANG Jian-pei
..............page:46-49
Optimal impulse orbit-transfer for making small satellite constellation
WANG Zhi-gang;LI Qing;CHEN Shi-lu;LI Ren-hou
WANG Zhi-gang;LI Qing;CHEN Shi-lu;LI Ren-hou
..............page:41-45