Design of Missile Longitudinal Control System Based on Backstepping Control

Article Preview

Abstract:

Missile control system is not block strict feedback system which is suitable to use backstepping method. So in this paper, a backstepping control method is proposed to design a missile longitudinal autopilot and is proved to be asymptotically stable by Lyapunov stability theory. The simulation results show that the designed system can still track commands quickly and accurately and is robust with aerodynamic perturbation and control input saturation.

You might also be interested in these eBooks

Info:

Periodical:

Pages:

1401-1406

Citation:

Online since:

January 2014

Export:

Price:

Permissions CCC:

Permissions PLS:

Сopyright:

© 2014 Trans Tech Publications Ltd. All Rights Reserved

Share:

Citation:

* - Corresponding Author

[1] Krstic M, Kanellakopoulos I, Kokotovic P. Nonlinear and Adaptive Control Design [M]. New York: Willy Interscience Publication John Wiley & Sons, (1995).

Google Scholar

[2] Heon S N, Seung-Hwan K, Chanbo S. A Robust Nonlinear Control Approach to Missile Autopilot Design [J]. SICE, 2001: 310-314.

DOI: 10.1109/sice.2001.977852

Google Scholar

[3] Zheng Minjie, Xu Shijie. Spacecraftattitude control system design via back-stepping method [J]. FlightDynamics, 2005, 23(4): 63-66.

Google Scholar

[4] DONG Changhong, ZHOU Guojie, XU Shijie. Application of Backstepping Control Method in Missile Nonlinear Control System Design [J]. Aerospace Control, 2010(2): 3-6.

Google Scholar

[5] Hu Yunan, Jin Yuqiang, Zha Xu. Robust adaptive controller design for block BTT missile model [J]. Journal of Astronautics, 2004, 25(2): 225-229.

Google Scholar

[6] Zhou Y, Wu Y, Hu Y. Robust backstepping sliding mode control of a class of uncertain MIMO nonlinear systems [C]. 2007 IEEE International Conference on Control and Automation, Guangzhou, China. May 30 to June 1, 2007: 1917-(1921).

DOI: 10.1109/icca.2007.4376695

Google Scholar

[7] Zheng Jianhua, Yang Di. The application of Robust Control Theory on Bank-to-Turn Missile [M]. Beijing: National Defense Industry Press, (2001).

Google Scholar

[8] Yu Jianqiao, Wen Zhonghui, Mei Yuesong, Long Teng. Overall Design of Tactical Missile [M]. Beijing: Beijing University of Aeronautics and Astronautics Press, (2010).

Google Scholar

[9] Hu Yunan, Chen Ye. Design of Missile Overload Baekstepping Control Systems [C]. 2003 Academic Conference on System Simulation Technology and its Application, Shanghai, China, 1 July, 2003: 558-562.

Google Scholar

[10] Zhu Kai, Qi Naiming. Adaptive backstepping sliding mode control for BTT missiles with control input constraints [J]. Systems Engineering and Electronics, 2011, 33(5): 1094-1097.

DOI: 10.1109/icma.2009.5244807

Google Scholar