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-F04
会議情報
2A2-F04 4ロータ型飛行ロボットのホバリング時における機体の安定化(飛行ロボット・メカトロニクス(2))
木下 敬介大内 祐介渡辺 桂吾永井 伊作
著者情報
会議録・要旨集 フリー

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抄録
UAVs have been actively researched as a means of collecting information during disasters. In particular, helicopter-type UAVs using four rotors are often called an X4-Flyer, and it has been attracting attention. The X4-Flyer has excellent maneuverability, compared to conventional helicopters that change the angle of attack of the rotor. Therefore it can be used at a space such as indoor or low altitude in which many obstacles exist. When the X4-Flyer is used at such a space, it needs to fly not so as to collide with obstacles, and so the precise control of the X4-Flyer is required. The objective of this research is to develop the X4-Flyer that can fly while detecting and avoiding obstacles. This paper presents the attitude and altitude stabilization of the X4-Flyer. We describe on measuring of the physical parameters related to the rotors and on correcting individual differences in motors, and finally conduct a hovering experiment.
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© 2014 一般社団法人 日本機械学会
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