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: 1P1-F08
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単発UAVの飛行制御の研究
久保田 悠介*西田 信一郎
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Multi-rotor UAVs are important for various applications, but they are driven by electric motors and have the limitation of short cruising time. In this study, the composition and control system of a UAV that achieves attitude control by vertical fins are proposed. The suggested UAV has a single rotor, which, using an actuator, can be converted into an internal combustion engine. Herein, the results of the dynamical simulations and tests are described.

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