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Integral-backstepping-based Attitude Control for UAH with Immeasurable States

  • Harbin Institute of Technology
  • Aerofugia Technology Co. LTD.

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

Abstract

In this paper, a new control scheme is proposed for the attitude control of unmanned autonomous helicopter (UAH) with immeasurable states. For the design of the control scheme, the attitude model of UAH considering flapping dynamics which is used to illustrate the change of flapping angles is established firstly. However, it is unpractical to install a sensor on the rotor to measure the flapping angles in actual system. In order to get the flapping angles in real time, a high-gain observer is applied. Meanwhile, the integral-backstepping algorithm is adopted to design the controller. By using Lyapunov theory, the stability of the closed-loop system is illustrated. Besides, the effectiveness of the proposed method is verified by numerical simulations, compared with the results obtained by the linear extend state observer.

Original languageEnglish
Title of host publicationProceedings of the 40th Chinese Control Conference, CCC 2021
EditorsChen Peng, Jian Sun
PublisherIEEE Computer Society
Pages7622-7626
Number of pages5
ISBN (Electronic)9789881563804
DOIs
StatePublished - 26 Jul 2021
Event40th Chinese Control Conference, CCC 2021 - Shanghai, China
Duration: 26 Jul 202128 Jul 2021

Publication series

NameChinese Control Conference, CCC
Volume2021-July
ISSN (Print)1934-1768
ISSN (Electronic)2161-2927

Conference

Conference40th Chinese Control Conference, CCC 2021
Country/TerritoryChina
CityShanghai
Period26/07/2128/07/21

Keywords

  • Flapping dynamics
  • High-gain observer
  • Integral-backstepping
  • UAH

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