An Adaptive Control Scheme for Longitudinal Dynamics of A Twin Otter Aircraft

Yang Haiping, Zhang Yanjun*, Zhang Zhengqiang

*Corresponding author for this work

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

Abstract

This paper proposes a feedback linearization based adaptive control scheme for longitudinal dynamics of a twin otter aircraft system established in [1]. For the aircraft system with two different output vectors, two relevant relative degree dependent formulations are developed to realize parametrizations of output dynamics. Then, the stability and output tracking performance is analyzed for the two cases based on the Lyapunov method and the gradient method, respectively. In particular, the singularity problems of the adaptive control gain matrices are analyzed for the two cases. The simulation results verify the validity of the proposed control method.

Original languageEnglish
Title of host publicationProceedings of the 40th Chinese Control Conference, CCC 2021
EditorsChen Peng, Jian Sun
PublisherIEEE Computer Society
Pages2275-2279
Number of pages5
ISBN (Electronic)9789881563804
DOIs
Publication statusPublished - 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

  • Adaptive control
  • aircraft control
  • output tracking
  • relative degree

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