A feedback linearization and saturated control structure for quadrotor UAV

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9 Citations (Scopus)

Abstract

In this paper,attitude controller and position controller are investigated for a small quadrotor unmanned aerial vehicle (UAV). A feedback linearization method is proposed to design attitude tracking control of UAV, with linear extended state observer(LESO)to estimate and compensate for the disturbances. Meanwhile, a saturated control law with arc tangent functions is adopted as the position controller. Then the convergence of LESO, stability of attitude system and position system are proved. Finally, experiment results are given to illustrate the effectiveness of the proposed method.

Original languageEnglish
Title of host publicationProceedings of the 38th Chinese Control Conference, CCC 2019
EditorsMinyue Fu, Jian Sun
PublisherIEEE Computer Society
Pages8277-8282
Number of pages6
ISBN (Electronic)9789881563972
DOIs
Publication statusPublished - Jul 2019
Event38th Chinese Control Conference, CCC 2019 - Guangzhou, China
Duration: 27 Jul 201930 Jul 2019

Publication series

NameChinese Control Conference, CCC
Volume2019-July
ISSN (Print)1934-1768
ISSN (Electronic)2161-2927

Conference

Conference38th Chinese Control Conference, CCC 2019
Country/TerritoryChina
CityGuangzhou
Period27/07/1930/07/19

Keywords

  • Feedback linearization control
  • LESO
  • UAV

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