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Adaptive Flight Control Design for Fixed-wing UAV based on Neural Network

  • Jinhua Liu
  • , Xiaoli Wang*
  • , Peiqi Zhao
  • *Corresponding author for this work
  • School of Information Science and Engineering, Harbin Institute of Technology Weihai

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

Abstract

This paper presents an adaptive flight control approach based on dynamic inversion and neural network with sliding mode technique for a fixed-wing unmanned aerial vehicle (UAV). A nonlinear dynamic model which has been decoupled into three independent single-input single-output channels is investigated. Unknown certainties of the aircraft dynamic are estimated by the neural network, which adaptively provides online parameter regulation, and the close stability analysis is also derived by using Lyapunov theory. Simulation and experiment results indicate that the proposed control scheme can perform well in tracking problem.

Original languageEnglish
Title of host publicationProceedings of the 41st Chinese Control Conference, CCC 2022
EditorsZhijun Li, Jian Sun
PublisherIEEE Computer Society
Pages2363-2368
Number of pages6
ISBN (Electronic)9789887581536
DOIs
StatePublished - 2022
Externally publishedYes
Event41st Chinese Control Conference, CCC 2022 - Hefei, China
Duration: 25 Jul 202227 Jul 2022

Publication series

NameChinese Control Conference, CCC
Volume2022-July
ISSN (Print)1934-1768
ISSN (Electronic)2161-2927

Conference

Conference41st Chinese Control Conference, CCC 2022
Country/TerritoryChina
CityHefei
Period25/07/2227/07/22

Keywords

  • Adaptive control
  • Fixed-wing UAV
  • Neural network
  • Trajectory tracking

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