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: 2A2-F03
会議情報
2A2-F03 可変ノズルを用いたテイルシッタ型VTOL機の開発
丸橋 伸也三輪 昌史
著者情報
会議録・要旨集 フリー

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抄録
Recently, R/C helicopter is used in field of aerial photography and investigation. But helicopter rotor blades are not covered, and the thrust is generated by very high rotational speed. So R/C helicopter has high risk. In this study, we developed a new flying object like the inverted pendulum that using two ducted fans instead of rotor blades. And we named it "Ducted fan Flying Object ver.3 (DFO3)". Each ducted fans have Gimbals mechanism of 2 degree of freedom as thrust vectoring mechanism. We try 3-axis (roll, pitch, yaw axis) attitude control by PI-D control and VTOL. PID gain has calculated by pole placement method and its simulation. We succeeded attitude control. However, control precision falls because of simulation precision problem and some mechanism problems. Therefore, we improvement "Ducted fan Flying Object ver.4 (DFO4)" basis of the DFO3 to solve the problems. DFO4 has nozzle mechanism instead of Gimbal mechanism.
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© 2015 一般社団法人 日本機械学会
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