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Pitch angle control of UAV Based on L1adaptive control law

  • Lei Zhang
  • , Feng Tian Yang
  • , Wen Ya Zhou
  • , Jun Huang
  • , Xiu Jian Su
  • Liaoning General Aviation Academy
  • Dalian University of Technology

科研成果: 书/报告/会议事项章节会议稿件同行评审

摘要

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.

源语言英语
主期刊名Proceedings - 2020 35th Youth Academic Annual Conference of Chinese Association of Automation, YAC 2020
出版商Institute of Electrical and Electronics Engineers Inc.
68-72
页数5
ISBN(电子版)9781728176840
DOI
出版状态已出版 - 16 10月 2020
活动35th Youth Academic Annual Conference of Chinese Association of Automation, YAC 2020 - Zhanjiang, 中国
期限: 16 10月 202018 10月 2020

出版系列

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

会议

会议35th Youth Academic Annual Conference of Chinese Association of Automation, YAC 2020
国家/地区中国
Zhanjiang
时期16/10/2018/10/20

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