Seamless 90-degree attitude transition flight of a quad tilt-rotor UAV under full position control

Tomoyuki Magariyama, Satoko Abiko

研究成果: Conference contribution

1 被引用数 (Scopus)

抄録

This paper proposes a seamless 90-degree attitude transition flight of a quad tilt-rotor UAV under full position control. The quad tilt-rotor UAV enables independent position and attitude control by additional actuators for changing the thrust directions. Therefore, the quad tilt-rotor UAV can hover with different attitudes. However, in the previous research, because the two attitude controls are switched in large attitude transition, the difficulty in certain tilting attitudes were observed. This study aims at developing a control method for realizing a seamless attitude transition flight under full position control. The flight experiment verifies the proposed method.

本文言語English
ホスト出版物のタイトル2020 IEEE/ASME International Conference on Advanced Intelligent Mechatronics, AIM 2020
出版社Institute of Electrical and Electronics Engineers Inc.
ページ839-844
ページ数6
ISBN(電子版)9781728167947
DOI
出版ステータスPublished - 2020 7
イベント2020 IEEE/ASME International Conference on Advanced Intelligent Mechatronics, AIM 2020 - Boston, United States
継続期間: 2020 7 62020 7 9

出版物シリーズ

名前IEEE/ASME International Conference on Advanced Intelligent Mechatronics, AIM
2020-July

Conference

Conference2020 IEEE/ASME International Conference on Advanced Intelligent Mechatronics, AIM 2020
CountryUnited States
CityBoston
Period20/7/620/7/9

ASJC Scopus subject areas

  • Electrical and Electronic Engineering
  • Control and Systems Engineering
  • Computer Science Applications
  • Software

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