Study of Airship Attitude Tracking System

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WANG Xiao-liang, SHAN Xue-xiong. Study of Airship Attitude Tracking System[J]. Applied Mathematics and Mechanics, 2006, 27(7): 805-811.

Citation:

WANG Xiao-liang, SHAN Xue-xiong. Study of Airship Attitude Tracking System[J]. Applied Mathematics and Mechanics, 2006, 27(7): 805-811.

Citation:

WANG Xiao-liang, SHAN Xue-xiong. Study of Airship Attitude Tracking System[J]. Applied Mathematics and Mechanics, 2006, 27(7): 805-811.

Department of Engineering Mechanics, Shanghai Jiaotong University, Shanghai 200030, P. R. China

[1]	OUYANG Jin,QU Wei-dong,XI YU-geng.Stratospheric verifying airship modeling and analysis[J].Journal of Shanghai Jiaotong University,2003,37(6):956—960.
[2]	Segio B,Varella Gomes,Josue Jr G Romos.Airship dynamic modeling for autonomous operation[A].In:Proceedings of the 1998 IEEE International Conference on Robotics and Automation[C].Leuven:IEEE,1998,3462—3467.
[3]	Isidori, Alberto.Nonlinear Control Systems[M].2nd.New York:Springer Press,1989.
[4]	XIA Xiao-hua,GAO Wei-bing.Nonlinear Control Systems and Decoupling[M].Beijing: Science Press, 1997.
[5]	Huijberts H J C,Moog C H,Pothin R.Input-output decoupling of nonlinear systems by static measurement feedback[J].Systems and Control Letters,2000,39(2):109—114. doi: 10.1016/S0167-6911(99)00095-X
[6]	李琳琳,杨国军,赵长安.卫星姿态跟踪系统的鲁棒控制器设计[J].航空学报,2001,14(2):94—99.
[7]	Sun Y.Global exponential stabilization for a class of uncertain nonlinear systems with control constraint[J].IEEE Trans on AC,1998,43(5):674—677. doi: 10.1109/9.668833
[8]	Behtash S. Robust output tracking for non-linear systems[J].International Journal of Control,1990,51(6):1381—1407. doi: 10.1080/00207179008934141