Design and Attitude Control of a Quad-Rotor Tail-Sitter Vertical Takeoff and Landing Unmanned Aerial Vehicle

Author:

Oosedo Atsushi1,Konno Atsushi2,Matsumoto Takaaki3,Go Kenta4,Masuko Koji5,Uchiyama Masaru6

Affiliation:

1. a Department of Aerospace Engineering, Graduate School of Engineering, Tohoku University, 6-6-01, Aramaki-aza-Aoba, Aoba-ku, Sendai 980-8579, Japan;, Email: oosedo@space.mech.tohoku.ac.jp

2. b Department of Aerospace Engineering, Graduate School of Engineering, Tohoku University, 6-6-01, Aramaki-aza-Aoba, Aoba-ku, Sendai 980-8579, Japan

3. c Department of Aerospace Engineering, Graduate School of Engineering, Tohoku University, 6-6-01, Aramaki-aza-Aoba, Aoba-ku, Sendai 980-8579, Japan

4. d Department of Aerospace Engineering, Graduate School of Engineering, Tohoku University, 6-6-01, Aramaki-aza-Aoba, Aoba-ku, Sendai 980-8579, Japan

5. e Department of Aerospace Engineering, Graduate School of Engineering, Tohoku University, 6-6-01, Aramaki-aza-Aoba, Aoba-ku, Sendai 980-8579, Japan

6. f Department of Aerospace Engineering, Graduate School of Engineering, Tohoku University, 6-6-01, Aramaki-aza-Aoba, Aoba-ku, Sendai 980-8579, Japan

Publisher

Informa UK Limited

Subject

Computer Science Applications,Hardware and Architecture,Human-Computer Interaction,Software,Control and Systems Engineering

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3. Micro aerial vehicle with basic risk of operation;Scientific Reports;2022-07-27

4. Double Hybrid Tailsitter Unmanned Aerial Vehicle With Vertical Takeoff and Landing;IEEE Access;2022

5. Modeling and control of a quadrotor tail-sitter unmanned aerial vehicles;Proceedings of the Institution of Mechanical Engineers, Part I: Journal of Systems and Control Engineering;2021-10-06

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