Flight Dynamics 2010 Issue 6 Preliminary analysis on the sonic boom of supersonic aircraft

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Flight Dynamics
1002-0853
2010 Issue 6

Preliminary analysis on the sonic boom of supersonic aircraft
FENG Xiao-qiang;LI Zhan-ke;SONG Bi-feng

..............page:21-23,27

Research on coordinates based on the idea of "navigation dynamics"
XU Cheng;CHE Yan-wen;LI Yong-sheng;TANG Wei-feng

..............page:1-5

Close-carrier-area wind field modeling and carrier-landing simulation analysis
JIANG Kang-bo;LIU Chao;YUAN Dong

..............page:11-15

Design of UAV autonomous controller for formation in aerial refueling
GUO Jun;DONG Xin-min;LIAO Kai-jun;LI Hong-bo

..............page:36-40

Flight test on wet runway in type certification of transport category airplanes
XU Lei;QIU Tao

..............page:77-79,82

Identification of flight control system based on support vector machine
YIN De-yi;LI Zhong-jian

..............page:45-47,51

Coefficient diagram method based on PSO and its application in aerospace
LIU Zhong;ZHAO Yan-hui

..............page:64-67

Design of tracking controller of flight control system based on T-S model
LI Fei;XUE Jian-ping;WANG Xiao-dong;WANG Jian-gang

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

fei xing li xue kan zai lun wen qing kuang tong ji fen xi
zhang dong wei ; wang yu lin ; cui li feng

..............page:91-93

Research on scheme of SINS/celestial integrated navigation for ballistic missile
WEN Yong-zhi;WU Jie

..............page:87-90

Civil aircraft flight management simulation system design and realization
LI Yang;YANG Yong-sheng;JING Zhong-liang

..............page:72-76

Research on UAV\'s data link performance
FANG Wei;WANG Feng;DING Tuan-jie

..............page:68-71

Study of an approach to separate gyroscope drift error based on stellar navigation
GUO Qing-shu;XIAN Yong;LIU Qing

..............page:80-82

fei xing li xue zheng gao jian ze

..............page:封4

Design of robust loop-shaping autopilot for missile with swing nozzle thrust vector control
ZHANG Xiao-feng;ZHU Xiao-ping;YANG Jun

..............page:60-63

Design of aircraft pitching angle control system based on H∞ control
XU Yan-jun;LIN Zheng;SUN Yan;LI Ji-xin

..............page:24-27

Geomagnetic matching method based on probabilistic data association filter
LIU Yu-xia;ZHOU Jun;GE Zhi-lei

..............page:83-86

Research on robust control law design based on method of model reference inverse
CHEN Yong-liang;SHEN Hong-liang

..............page:28-31

State-space representation of lateral-directional unsteady aerodynamic model at high angle of attack
WANG Zheng-hua;SHI Zhi-wei

..............page:16-20

Numerical calculation and analysis on multiple jets interaction characteristics of missile
LIU Zhan-chen;XIE Zeng-hui;JING Xian-yong

..............page:56-59,63

APC/PIO evaluation methods for civil aircraft airworthiness certification
LIU Yan;GAO Zheng-hong;ZHAO Tao;LV Hai;LI Xiang-wei

..............page:6-10,15

Investigation on numerical simulation of missile\'s roll-damping moment coefficient based on steady N-S equation of FLUENT
ZHAN Chao;HE Xian-peng;WANG Zhan-jiang

..............page:52-55

Closed-loop ascent guidance of air-breathing aerospace vehicle
PAN Bin-feng;TANG Shuo

..............page:48-51

Design of a robust flight control law based on dynamic surface control and neural network
LIU Shu-guang;SUN Xiu-xia;DONG Weu-han;WANG Dong

..............page:41-44