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 |
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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 2024 → 9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