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-C03
会議情報
2A1-C03 マルチロータヘリコプタの操縦性能改善のための入力補正インタフェースの開発(飛行ロボット・メカトロニクス(1))
大滝 潤藤川 太郎汐月 哲夫
著者情報
会議録・要旨集 フリー

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抄録
In this paper, a model of lifting force generation system in order to perform the lifting control 4-axis aircraft is proposed. In the prior study, since it is assumed that lifting force of 4-axis aircraft can be generated by algebraic are addition and subtraction of motor duty ratio value, and time delay and coupling of dynamics are ignored. However, the ignored elements may deteriorate the performance of the actual system. In this study, I propose a model of lifting force generation system that identified on the basis of experimental data obtained by the lifting force measurement device. Finally, we perform lifting force tracking experiment by using this model.
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© 2014 一般社団法人 日本機械学会
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