Skip to main navigation Skip to search Skip to main content

Backstepping sliding mode control for BTT missiles based on second-order sliding mode

  • Kai Zhu*
  • , Nai Ming Qi
  • , Chang Mao Qin
  • *Corresponding author for this work
  • School of Astronautics, Harbin Institute of Technology

Research output: Contribution to journalArticlepeer-review

Abstract

Based on backstepping design and second-order sliding mode control, a new backstepping sliding mode controller is designed for back-to-turn (BTT) missiles nonlinear dynamics with unmatched uncertainties. Sliding mode control is used in each step of the backstepping design to compensate for uncertainty, and nonsingular second-order sliding mode control is used in the last step of the backstepping design. In this way, the chattering problem which does harm to rudders can be avoided, meanwhile, the accumulated error is reduced.computation explosion is reduced by introducing an exact robust differentiator, and the tracking error of the system is proved ultimately bounded. Simulation result shows that the tracking errors converge to an arbitrary small neighborhood of the origin by adjusting the design parameters of the controller.

Original languageEnglish
Pages (from-to)829-832
Number of pages4
JournalXi Tong Gong Cheng Yu Dian Zi Ji Shu/Systems Engineering and Electronics
Volume32
Issue number4
StatePublished - Apr 2010
Externally publishedYes

Keywords

  • Backstepping control
  • Bank-to-turn(BTT) missile
  • Nonsingular
  • Second-order sliding mode control
  • Terminal sliding mode

Fingerprint

Dive into the research topics of 'Backstepping sliding mode control for BTT missiles based on second-order sliding mode'. Together they form a unique fingerprint.

Cite this