STUDY ON CONTROL PERFORMANCE OF A NEW TYPE OF TILT-ROTOR AIRCRAFT

Kazusa Miyabe, Mai Bando, Shinji Hokamoto

研究成果: ジャーナルへの寄稿会議記事査読

抄録

A new type of tilt-rotor aircraft is introduced in this study, whose rotors are tilted by arm-mechanisms. The effect and benefits of the arm-mechanisms are explained by comparing with the standard tilt-rotor aircraft. The most evaluable feature is that the new tilt-rotor aircraft can enhance the stability during the transitional mode between its vertical take-off/landing and cruising modes by reducing the interference between the rotor-wakes and the fixed-wing. In addition, simple control strategy is effective because independent control for the three attitude motions is possible for the tilt-rotor aircraft.

本文言語英語
ジャーナルICAS Proceedings
出版ステータス出版済み - 2024
イベント34th Congress of the International Council of the Aeronautical Sciences, ICAS 2024 - Florence, イタリア
継続期間: 9月 9 20249月 13 2024

!!!All Science Journal Classification (ASJC) codes

  • 航空宇宙工学
  • 制御およびシステム工学
  • 電子工学および電気工学
  • 材料科学一般

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