Sliding mode control for a miniature helicopter

Jian Fu, Wen Hua Chen, Qing Xian Wu

Research output: Chapter in book / Conference proceedingConference article published in proceeding or bookAcademic researchpeer-review

9 Citations (Scopus)

Abstract

A controller based on UAS-SM, sliding mode and open-loop control methodologies is developed for autonomous operation of the Trex-250 helicopter. This controller is composed of a nested sequence of rotor dynamic, angular rate, Euler angle, velocity and position loops. By the controller, coupling of lateral channel and longitudinal channel is greatly reduced. Meanwhile, the feasibility of UAS-SM for implementation is also evaluated in this paper. A practical experiment for Trex-250 is given for the benefits of combined controller.

Original languageEnglish
Title of host publicationProceedings of 2011 17th International Conference on Automation and Computing, ICAC 2011
Pages98-103
Number of pages6
Publication statusPublished - 2011
Event2011 17th International Conference on Automation and Computing, ICAC 2011 - Huddersfield, United Kingdom
Duration: 10 Sept 201110 Sept 2011

Publication series

NameProceedings of 2011 17th International Conference on Automation and Computing, ICAC 2011

Conference

Conference2011 17th International Conference on Automation and Computing, ICAC 2011
Country/TerritoryUnited Kingdom
CityHuddersfield
Period10/09/1110/09/11

Keywords

  • open-loop control
  • practical experiment
  • sliding mode
  • Trex-250
  • UAS-SM

ASJC Scopus subject areas

  • Computational Theory and Mathematics

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