Fundamental numerical and experimental evaluation of attitude recovery control for a quad tilt rotor UAV against disturbance

Satoko Abiko, Kengo Tashiro

研究成果: Conference contribution

1 被引用数 (Scopus)

抄録

This paper presents attitude recovery control for a quad tilt rotor UAV. The quad tilt rotor UAV has ability of flying with completely independent 3 DOF position and 3 DOF attitude control by changing the thrust directions. This type of UAV is expected to perform better response to the disturbance by virtue of the mechanism of changing the thrust directions compared to the conventional multi-rotor UAV. This paper proposes disturbance detection method using IMU sensor and develops attitude recovery control against impact disturbance. The numerical simulation and fundamental flight experiments were carried out to evaluate the effectiveness of the proposed method compared to the conventional PID control.

本文言語English
ホスト出版物のタイトルICCAS 2016 - 2016 16th International Conference on Control, Automation and Systems, Proceedings
出版社IEEE Computer Society
ページ709-712
ページ数4
ISBN(電子版)9788993215120
DOI
出版ステータスPublished - 2017 1 24
イベント16th International Conference on Control, Automation and Systems, ICCAS 2016 - Gyeongju, Korea, Republic of
継続期間: 2016 10 162016 10 19

Other

Other16th International Conference on Control, Automation and Systems, ICCAS 2016
CountryKorea, Republic of
CityGyeongju
Period16/10/1616/10/19

ASJC Scopus subject areas

  • Artificial Intelligence
  • Computer Science Applications
  • Control and Systems Engineering
  • Electrical and Electronic Engineering

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