Remote control guidance law design using variable structure control

Xiu Yun Meng*, Qi Wang

*Corresponding author for this work

Research output: Contribution to journalArticlepeer-review

Abstract

A method of sliding mode variable structure control for the missile body being a time varying system is presented. A remote control guidance law is designed. The method has strong robustness to target's maneuver. To reduce the chattering phenomena, quasi-sliding mode variable structure control method is used. Simulation results show that the proposed method has small miss distance for any kind of maneuvering targets and requires small control energy.

Original languageEnglish
Pages (from-to)81-84
Number of pages4
JournalJournal of Beijing Institute of Technology (English Edition)
Volume15
Issue number1
Publication statusPublished - Mar 2006

Keywords

  • Reaching mode
  • Remote control guidance law
  • Sliding mode
  • Variable structure control

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