Education, Science, Technology, Innovation and Life
Open Access
Sign In

Research on Sliding Mode Observer Control for Missile Pitch System

Download as PDF

DOI: 10.23977/acss.2023.070415 | Downloads: 10 | Views: 285


Junwei Lei 1, Hong Wang 1, Jing Yu 1, Lingling Wang 1


1 College of Coast Defence, Aval Aviation University, Yantai, 264001, China

Corresponding Author

Junwei Lei


A new type of three sliding mode surface disturbance observer was design for the pitch channel control system of missile attack angle tracking. The error and disturbance of attack angle loop is approximate by the sliding mode type observer; and also the pitch speed signal loop was also designed by sliding mode observer with an integral sliding mode surface. And based on backstepping method, the pitch speed error loop was designed by sliding mode control method, and the whole system is stable according to Lyapunov stability theory with three sliding mode controller s and two sliding mdoe observers. At last, Numerical experiment was done to test the stability of the whole system with designed controller.


System Disturbance; Nonlinear Observer; Backstepping Design Method; Missile Pitch Channel Control System


Junwei Lei, Hong Wang, Jing Yu, Lingling Wang. Research on Sliding Mode Observer Control for Missile Pitch System. Advances in Computer, Signals and Systems (2023) Vol. 7: 103-109. DOI:


[1] Feigenbaum M J.Quantitative universality for a class of nonlinear transformations [J], J.Stat. Phys. 1978, 19:25-52.
[2] Pecora L M and Carroll T L.Synchronization in chaotic systems[J],Phys.Rev. Lett.1990, 64:821-824.
[3] GE S S, Wang C, Lee T H. Adaptive backstepping control of a class of chaotic systems[J]. Int J Bifurcation and chaos. 2000, 10 (5): 1140-1156.
[4] GE S S, Wang C, Adaptive control of uncertain chus’s circuits[J]. IEEE Trans Circuits System. 2000, 47(9): 1397-1402.
[5] Alexander L, Fradkov, Markov A Yu. Adaptive synchronization of chaotic systems based on speed gradient method and passification [J]. IEEE Trans Circuits System 1997, 44(10):905-912.
[6] Dong X. Chen L. Adaptive control of the uncertain Duffing oscillator[J], Int J Bifurcation and chaos. 1997, 7(7):1651-1658.
[7] Tao Yang, Chun-Mei Yang and Lin-Bao Yang, A Detailed Study of Adaptive Contorl of Chaotic Systems with Unknown Parameters[J] . Dynamics and Control. 1998, (8):255-267.
[8] M.T. Yassen, Chaos control of chaotic dynamical systems using backstepping design, Chaos Soliton Fract. 27 (2006) 537–548.
[9] Seung-Hwan Kim, Yoon-Sik Kim, Chanho Song, Control engineering practice, 12(2004) pp. 149-154
[10] Hull, R.A., & Z. Qu, 1995. Design and evaluation of robust nonlinear missile autopilot from a performance perspective. Proceedings of the ACC, 189–193
[11] Junwei Lei, Xinyu Wang, Yinhua Lei, Physics Letters A, Volume 373, Issue 14, 23 March 2009, Pages 1249-1256
[12] Junwei Lei, Xinyu Wang, Yinhua Lei, Communications in Nonlinear Science and Numerical Simulation, Volume 14, Issue 8, August 2009, Pages 3439-3448
[13] Xinyu Wang, Junwei Lei, Changpeng Pan. Applied Mathematics and Computation, 185 (2007)pp. 989-1002

Downloads: 9239
Visits: 226826

Sponsors, Associates, and Links

All published work is licensed under a Creative Commons Attribution 4.0 International License.

Copyright © 2016 - 2031 Clausius Scientific Press Inc. All Rights Reserved.