Back-stepping sliding mode control for missile systems based on an extended state observer

IET Control Theory and Applications - Tập 5 Số 1 - Trang 93-102 - 2011
Yuanqing Xia1, Zheng Zhu1, Mengyin Fu1
1Dept. of Autom. Control, Beijing Inst. of Technol., Beijing, China

Tóm tắt

Từ khóa


Tài liệu tham khảo

10.2514/2.4792

10.1109/TCST.2007.916352

10.2514/2.4588

10.1109/87.556026

10.1016/0005-1098(88)90092-1

10.2514/2.4029

10.1109/TAES.2007.357136

10.2514/1.13030

Huang, 2001, Proc. 40th IEEE Conf. on Decision and Control, 1, 223, 10.1109/CDC.2001.980102

10.2514/1.25834

10.1109/41.184820

10.1109/41.370376

10.1080/00207720701409363

10.1109/TAC.2003.812815

10.1016/0005-1098(94)00154-B

10.1109/41.704892

10.1016/j.automatica.2005.07.001

10.1109/TAC.2006.890391

10.1016/S0005-1098(98)80019-8

10.1016/j.camwa.2007.11.021

10.1109/TIE.2008.2011621

10.1109/TIE.2007.909047

10.1016/j.ijmachtools.2007.07.002

10.1080/002077299292641

10.1109/TIE.2005.847583

10.1049/iet-cta:20050138

10.1109/TRO.2004.829458

10.1016/j.isatra.2008.06.004

Qian, X.F., Lin, R.X., and Zhao, Y.N.: ‘Missile flight dynamics’, (Beijing Institute of Technology, Beijing 2000)

‘Quaternions applied to missile systems’, Technical, A232250, 1977

‘Quaternion utilization in a missile model’, Technical, AD/A084263, 1980

Khalil, H.K.: ‘Nonlinear systems’, (Prentice-Hall, Englewood Cliffs, NJ 2002)

Han, J.Q.: ‘Active disturbance rejection control technique – the technique for estimating and compensating the uncertainties’, (National Defense Industry Press, Beijing 2008)

Gao, 2003, Proc. American Control Conf., 6, 4989