Hostname: page-component-8448b6f56d-t5pn6 Total loading time: 0 Render date: 2024-04-19T06:20:53.152Z Has data issue: false hasContentIssue false
  • English
  • Français

MISSILE CONTROL DESIGN BASED ON THE LINEAR MULTIPLE SLIDING MODE RECURSIVE METHOD

Part of: Controllability, observability, and system structure

Published online by Cambridge University Press:  01 April 2008

Y. J. SHI  and
G. F. MA
Y. J. SHI*
Affiliation:
University of Electronic Science and Technology of China, Chengdu, P R China (email: Yingjing.Shi@gmail.com)
G. F. MA
Affiliation:
School of Astronautics, Harbin Institute of Technology, Harbin, P R China
*
✉For correspondence; e-mail: Yingjing.Shi@gmail.com
Rights & Permissions [Opens in a new window]

Abstract

Core share and HTML view are not available for this content. However, as you have access to this content, a full PDF is available via the ‘Save PDF’ action button.

To ensure that the elevator of a cruise missile is operating within the design specification in high-attitude flight, we present a design method for the construction of a sliding mode recursive variable structure controller. In this design method, a target sliding mode surface is first designed without considering the engineering specification of the elevator. Secondly, by using this specification, the critical state is solved. Then, the transitional sliding mode surfaces are designed recursively by using the critical state of the previous sliding mode surface so that the state will move smoothly from one transitional sliding mode surface to the next until the target sliding mode surface. This design method is based on linear sliding mode variable structure theory. Thus, the controller obtained is simple in structure and practical. Furthermore, the elevator will operate within the engineering specification. The simulation results show the effectiveness of the proposed method.

Keywords

cruise missilevariable structure controlsliding mode controlmultiple sliding mode recursive method

MSC classification

Secondary: 93B12: Variable structure systems
Type
Research Article
Information
The ANZIAM Journal , Volume 49 , Issue 4 , April 2008 , pp. 573 - 587
Copyright
Copyright © Australian Mathematical Society 2008

References

[1]Hu, Y. A. and Chen, Y., “Design and application of double-sliding modes variable structure control systems”, in Proc. Fifth Int. Symp. on Instrumentation and Control Technology (Proceedings of the SPIE, Beijing, China, 2003) 635–638.CrossRefGoogle Scholar
[2]Liao, X. H., Sun, Z. and Song, Y. D., “Chattering-free variable structure control with application to flight vehicles”, in Proc. 38th Southeastern Symp. on System Theory (Tennessee Technological University, Cookeville, TN, 2006) 406–410.Google Scholar
[3]Mehrabian, A. R. and Roshanian, J., “Skid-to-turn missile autopilot design using scheduled eigenstructure assignment technique”, Proc. Inst. Mech. Eng. G, J. Aerospace Eng. 220 (2006) 225–239.CrossRefGoogle Scholar
[4]Pan, Y., Furuta, K., Suzuki, S. and Hatakeyama, S., “Design of variable structure controller-from sliding mode to sliding sector”, in Proc. IEEE Conf. on Decision and Control (IEEE Computer Society, Sydney, Australia, 2000) 1685–1690.Google Scholar
[5]Salamci, M. U., Ozgoren, M. K. and Banks, S. P., “Sliding mode control with optimal sliding surfaces for missile autopilot design”, J. Guid. Control Dyn. 23 (2000) 719–727.CrossRefGoogle Scholar
[6]Shima, T., Idan, M. and Golan, O. M., “Sliding-mode control for integrated missile autopilot guidance”, J. Guid. Control Dyn. 29 (2006) 250–260.CrossRefGoogle Scholar
[7]Shi, Y. J., Ma, G. F. and Ma, H. Z., “Study of the compound control of cruise missile based on variable structure control method”, J. Ballistics, in press, 2008.Google Scholar
[8]Shtessel, Y. B., Shkolnikov, I. A. and Levant, A., “Smooth second-order sliding modes: missile guidance application”, Automatica 43 (2007) 1470–1476.Google Scholar
[9]Shyu, K. K. and Lin, C. Y., “Adaptive sliding mode control for variable structure systems with constraint control input”, Dynam. Control 6 (1996) 49–61.CrossRefGoogle Scholar
[10]Wei, J. H. and Guan, C., “Derivation and integral sliding mode variable structure control of hydraulic velocity tracking system”, Chin. J. Mech. Eng. 18 (2005) 224–227.CrossRefGoogle Scholar
[11]Zhao, Y. S., Zhang, Y. Q., Yang, J. and Chen, L. P., “Enhanced fuzzy sliding mode controller for robotic manipulators”, Int. J. Robot. Autom. 22 (2007) 170–183.Google Scholar
[12]Zhou, D., Mu, C. D. and Xu, W. L., “Adaptive sliding-mode guidance of a homing missile”, J. Guid. Control Dyn. 22 (1999) 589–594.Google Scholar