Flight Dynamics 2012 Issue 1 Integral sliding mode fault tolerant control for over-actuated vehicle

Home | Survey | Payment| Talks & Presentations | Job Opportunities

Journals A B C D E F G H I J K L M N O P Q R S T U V W X Y Z

Flight Dynamics
1002-0853
2012 Issue 1

Integral sliding mode fault tolerant control for over-actuated vehicle
BAO E-er-dun;WANG Xiao-ping;DONG Xin-min;CHEN Yong

..............page:38-42,47

Airworthiness validation and accreditation for SCADE-based flight control software
ZHANG Ya-ni;LI Yan;LI Xiao-xun

..............page:34-37

The application technique of a flight control for the drop model test of a fly-by-wire aircraft
LIU Shang-min;ZHAO Lei

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

Study on the positioning and posture measurement for the capture of tethered satellite system
HU Zhen-jian;XIAN Yong;FENG Jie;LEI Gang

..............page:71-73,78

Research on lateral-directional flying qualities of multi-propeller solar powered UAV
WANG Rui;ZHU Xiao-ping;ZHOU Zhou

..............page:5-8

Experimental investigation in typical parachute opening process
XU Hong;CAO Yi-hua

..............page:74-78

Investigation of an aerodynamic characteristic evaluation method for the deformable wing
SUN Dian-jie;GU Liang-xian;GONG Chun-lin

..............page:13-16

Application of experiment design method in performance simulation validation for flight vehicle
YAN Xiao-dong;HAN Bing

..............page:79-82

Research of on-line orbit optimization based on direct collocation method
WANG Zhi-gang;CHEN Xiang

..............page:53-56

Decentralized optimal control for UAV formation forming
ZHANG Li-peng;WEI Rui-xuan;LIU-Yue;Guo Li-pu

..............page:25-28,33

Cooperative guidance law for active protection based on adaptive sliding-mode control
HUA Wen-hua;CHEN Xing-lin;SONG Chao

..............page:66-70

Soft-fault study on carrier landing guidance system
WU Wen-hai;LV Xue-tao;QU Zhi-gang;WANG Jun-yan

..............page:1-4

mou yun shu ji quan ji gou xing lei nuo shu xiao ying zu li xiu zheng yan jiu
zhang hui ; li jie ; gong zhi bin

..............page:20-22

Modeling and analyzing the afterbody external nozzle of a flexible hypersonic flight vehicle
ZHU Qiang-jun;TANG Shuo;TAN Yi-ming

..............page:48-52

Analysis and evaluation of air-combat effectiveness based on simulation
JIN Lei;ZHANG Shu-guang;SUN Jin-biao

..............page:87-91,96

Scheme selection of aircraft top-layer design based on multi-criteria decision-making approach
ZHAO Suo-zhu;LI Jun

..............page:29-33

fei ji zhuo lu guo cheng zhong ti gao qi dong xing neng de yi zhong xin fang fa
zuo meng xi ; ye zheng yin ; ye kun ; yang qing

..............page:17-19

Modeling and simulating on kinematic trajectory of ground-to-air missile controled by three-point method
ZHANG Da-yuan;ZHAO Yu-qin;LEI Hu-min;WU Yi-ming

..............page:57-60,65

Research on conceptual layout design and flight test for a multimode aircraft
CAO Fei;ZHAN Hao

..............page:9-12

fei xing li xue zheng gao jian ze

..............page:封4

Multi-UAVs cooperative path planning based on A* fixed length search algorithm
XIAO Zi-bing;YUAN Dong-li;QU Yao-hong

..............page:92-96

Decoupling controller design for bank-to-turn hypersonic vehicle based on sliding mode variable structure
XIONG Ke;XIA Zhi-xun;GUO Zhen-yun

..............page:61-65

Reserch on the surrogate of model aerodynamic performance of cone derived waverider
WANG Shuo;LI Ping;CHEN Wan-chun

..............page:43-47