Pitch angle control of UAV Based on L1adaptive control law

  • Lei Zhang
  • , Feng Tian Yang
  • , Wen Ya Zhou
  • , Jun Huang
  • , Xiu Jian Su

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

Abstract

Both L1 adaptive control law and PD control law are designed to control the pitch angle of the UAV, which contains parameter uncertainty. MATLAB software is used to simulate the both. The results show that, When the time-varying unknown parameter vector is within ± 0.4, L1 adaptive control law can always control the pitch angle of UAV well. While the PD control law only works within some range, in which the time-varying unknown state parameter changing of angle of attack, pitch angle and pitch rate are equivalent to negative feedback when they are positive, and the parameter changing of velocity is the main influencing factor in PD control system.

Original languageEnglish
Title of host publicationProceedings - 2020 35th Youth Academic Annual Conference of Chinese Association of Automation, YAC 2020
PublisherInstitute of Electrical and Electronics Engineers Inc.
Pages68-72
Number of pages5
ISBN (Electronic)9781728176840
DOIs
StatePublished - 16 Oct 2020
Event35th Youth Academic Annual Conference of Chinese Association of Automation, YAC 2020 - Zhanjiang, China
Duration: 16 Oct 202018 Oct 2020

Publication series

NameProceedings - 2020 35th Youth Academic Annual Conference of Chinese Association of Automation, YAC 2020

Conference

Conference35th Youth Academic Annual Conference of Chinese Association of Automation, YAC 2020
Country/TerritoryChina
CityZhanjiang
Period16/10/2018/10/20

Keywords

  • L1 adaptive control law
  • PD control law
  • Parameter uncertainty
  • UAV

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