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Attitude tracking control of a 3-DOF helicopter with input and output constraints

Research output: Chapter in Book/Report/Conference proceedingConference contributionpeer-review

Abstract

A novel attitude tracking controller is proposed for the 3-DOF helicopter under input and output constraints. A barrier Lyapunov function is employed to address input constraint, and an auxiliary design system for output constraint. Combining the backstepping technique, a nonlinear disturbance observer is explored to tackle the unknown nonlinear functions. We proved that the presented method can control the system output errors converge to a neighbourhood of zero for any sufficient smooth and bounded time-varying trajectory, and simultaneously the input and output states remains in the prescribed set uniformly. Simulation results demonstrate the effectiveness of the proposed controller for the 3-DOF helicopter.

Original languageEnglish
Title of host publicationProceedings of the 35th Chinese Control Conference, CCC 2016
EditorsJie Chen, Qianchuan Zhao, Jie Chen
PublisherIEEE Computer Society
Pages10608-10612
Number of pages5
ISBN (Electronic)9789881563910
DOIs
StatePublished - 26 Aug 2016
Event35th Chinese Control Conference, CCC 2016 - Chengdu, China
Duration: 27 Jul 201629 Jul 2016

Publication series

NameChinese Control Conference, CCC
Volume2016-August
ISSN (Print)1934-1768
ISSN (Electronic)2161-2927

Conference

Conference35th Chinese Control Conference, CCC 2016
Country/TerritoryChina
CityChengdu
Period27/07/1629/07/16

Keywords

  • 3-DOF Helicopter
  • Disturbance Observer
  • Input Constraint
  • Output Constraint

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