An improvement of flight performance in the level flight of tilted quadrotors by attaching a fixed-wing

Yoshikazu Nakamura, Atsushi Arakawa, Keigo Watanabe, Isaku Nagai

Research output: Contribution to journalArticle

Abstract

Wide range information is required to be collected by unmanned aerial vehicles (UAVs) and the area for its take-off and landing is limited in the event of a disaster. Therefore, research on the development of a specific UAV, which has two functions of a long distance flight like a fixed-wing aircraft and of a hovering like a rotorcraft, is drawing attention recently. In this study, we focus on a hybrid tilted quadrotor, in which four rotors are tiltable and a wing is fixed. It is clarified, from a simulation comparison in a level flight mode, that the flight performance is effectively improved by adding a fixed-wing, where a tilted quadrotor is assumed to take a level flight by using a controller for a vertical-flight mode and by controlling the angles of some tiltable rotors. It is shown finally that adding a fixed-wing can save the rotor thrust about 77% per flight distance.

Original languageEnglish
JournalArtificial Life and Robotics
DOIs
Publication statusAccepted/In press - Jan 1 2019

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Fixed wings
Flight dynamics
Aircraft
Disasters
Rotors
Unmanned aerial vehicles (UAV)
Research
Takeoff
Landing
Controllers

Keywords

  • Fixed-wing
  • Quadrotor
  • Tilt rotor
  • UAV

ASJC Scopus subject areas

  • Biochemistry, Genetics and Molecular Biology(all)
  • Artificial Intelligence

Cite this

An improvement of flight performance in the level flight of tilted quadrotors by attaching a fixed-wing. / Nakamura, Yoshikazu; Arakawa, Atsushi; Watanabe, Keigo; Nagai, Isaku.

In: Artificial Life and Robotics, 01.01.2019.

Research output: Contribution to journalArticle

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