Robust mode transition attitude control of tail-sitter unmanned aerial vehicles

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

Abstract

In this paper, an attitude control strategy is proposed for a class of tail-sitter aerial vehicles, which is required to achieve the desired tracking control performance during the mode transition. The resulted controller is constructed by a nominal controller and a robust compensator to reduce the effects of nonlinear dynamics and uncertainties. Theoretical analysis and numerical simulation results are given to show the effectiveness of the constructed closed-loop control system.

Original languageEnglish
Title of host publicationProceedings of the 36th Chinese Control Conference, CCC 2017
EditorsTao Liu, Qianchuan Zhao
PublisherIEEE Computer Society
Pages3198-3202
Number of pages5
ISBN (Electronic)9789881563934
DOIs
StatePublished - 7 Sep 2017
Event36th Chinese Control Conference, CCC 2017 - Dalian, China
Duration: 26 Jul 201728 Jul 2017

Publication series

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

Conference

Conference36th Chinese Control Conference, CCC 2017
Country/TerritoryChina
CityDalian
Period26/07/1728/07/17

Keywords

  • Tail-sitter aerial vehicle
  • nonlinear system
  • robust control
  • uncertain system

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