ロボティクス・メカトロニクス講演会講演概要集
Online ISSN : 2424-3124
セッションID: 2A1-F09
会議情報
2A1-F09 ティルトロータ型無人航空機に関する考察 : Tri-Copter型ティルトロータUAVの構想
今村 彰隆三輪 昌史
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会議録・要旨集 フリー

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抄録
The mobility and the large area are evaluated, and tilt rotor type vertical takeoff and landing (VTOL) machine is being expected by not only the army but also the private organization. A lot of same shape types are demanded unmanned aerial vehicle (UAV) in addition. However, because the tilt structure and the head structure of the rotor are complex, Osprey is unsuitable to cheap UAV. It aims to simplify the structure when tilt rotor type VTOL machine is made UAV and to research and develop the method that is appropriate for UAV in the present study. It pays attention to three rotor type with easy structure in this report, and do the study of making of tilt rotor type VTOL UAV.
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