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-G05
会議情報
2A1-G05 外殻機構を用いた空陸両用球体飛行ロボットの開発
山本 旭人矢野 聖矢林 憲玉
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会議録・要旨集 フリー

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抄録
This paper describe the air-ground use flying robot. This flying robot consists of spherical outer frames, coaxial rotors, rudders and a body system. Its weight is 1311 [g], its diameter is 400[mm], and its maximum thrust is 1950[gf]. The outer frame structure can reduce collision force when the robot lands and be used to drive on the ground. The flying robot has ultrasonic distance sensor and inertial measurement unit sensor (IMU) to measure its height and attitude. Its yaw angle is controlled by using two rotors, and pitch and roll angle are controlled by using rudders. Through a hovering experiment, the effectiveness of the mechanism was verified.
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© 2015 一般社団法人 日本機械学会
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