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  4. Vol 7, Issue 5, 2023

Research on Sliding Mode and Backstepping Control of Missile Pitch Channal System

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DOI: 10.23977/acss.2023.070501 | Downloads: 10 | Views: 346

Author(s)

Junwei Lei 1, Weiya Wang 1, Hong Wang 1, Lingling Wang 1

Affiliation(s)

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

Corresponding Author

Junwei Lei

ABSTRACT

A new type of proportional plus sliding mode inversion controller is constructed and applied to solve the attack angle tracking problem of missile pitch channel; At the same time, in order to solve the differential explosion problem of backstepping control, a method combining an integral type sliding surface with an accurate differentiator is proposed to solve the derivative of the desired pitch angular rate signal; At last, a kind of integral type Lyapunov function is constructed to prove the stability and boundness of the closed-loop signal of the whole system; Finally, a digital simulation experiment is done to verify the correctness of the method.

KEYWORDS

Tracking differentiator; stability; Backstepping method; Missile pitch channel; Automatic Control system

CITE THIS PAPER

Junwei Lei, Weiya Wang, Hong Wang, Lingling Wang. Research on Sliding Mode and Backstepping Control of Missile Pitch Channal System. Advances in Computer, Signals and Systems (2023) Vol. 7: 1-7. DOI: http://dx.doi.org/10.23977/acss.2023.070501.

REFERENCES

[1] Jason J G, Kathryn W J, et al. A simplified adaptive robust back-stepping approach using sliding modes and a z-swapping identifier[C]. Proceedings of the American Control Conference, Denver, 2003.
[2] 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, 2007.
[3] Lee T, Kim Y. Nonlinear adaptive flight control using back-stepping and neural networks controller [J]. Journal and Guidance, Control and Dynamics, 2001, 24(4): 675-682.
[4]. M.T. Yassen, Chaos control of chaotic dynamical systems using backstepping design, Chaos Soliton Fract. 27 (2006) 537-548.
[5] Seung-Hwan Kim, Yoon-Sik Kim, Chanho Song, Control engineering practice, 12(2004) pp. 149-154
[6] Hull R.A., & Z. Qu, 1995. Design and evaluation of robust nonlinear missile autopilot from a performance perspective. Proceedings of the ACC, 189–193
[7] Junwei Lei, Xinyu Wang, Yinhua Lei, Physics Letters A, Volume 373, Issue 14, 23 March 2009, Pages 1249-1256
[8] Junwei Lei, Xinyu Wang, Yinhua Lei, Communications in Nonlinear Science and Numerical Simulation, Volume 14, Issue 8, August 2009, Pages 3439-3448
[9] Xinyu Wang, Junwei Lei, Changpeng Pan, Applied Mathematics and Computation, 185 (2007) pp.989-1002

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