Attitude Control of Quadrotor in Consideration of the Effects of a Pole Based on Limited Pole Placement

Yasunori Sugawara; Akira Shimada

doi:10.1002/eej.22882

Attitude Control of Quadrotor in Consideration of the Effects of a Pole Based on Limited Pole Placement

Yasunori Sugawara, Akira Shimada

研究成果: Article

2 引用（Scopus）

抜粋

This paper introduces an attitude control technique for a quadrotor aircraft. Considering that the nonlinear characteristics of the aircraft makes it difficult to stabilize, a quadrotor controlled with an adaptive algorithm. Accordingly, we proposed a quadrotor application with backstepping based on the Lyapunov function. Furthermore, we designed a separate actuator control to be mounted on the aircraft for the control of the quadrotor. This approach is often used in industrial equipment. In particular, the limited pole placement (LPP) method is applied to design the controller considering the characteristics of the actuator. The representative simulation results are presented and discussed.

元の言語	English
ページ（範囲）	34-44
ページ数	11
ジャーナル	Electrical Engineering in Japan (English translation of Denki Gakkai Ronbunshi)
巻	198
発行部数	1
DOI	https://doi.org/10.1002/eej.22882
出版物ステータス	Published - 2017 1 1

ASJC Scopus subject areas

Energy Engineering and Power Technology
Electrical and Electronic Engineering

文献にアクセス

10.1002/eej.22882

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これを引用

Sugawara, Y., & Shimada, A. (2017). Attitude Control of Quadrotor in Consideration of the Effects of a Pole Based on Limited Pole Placement. Electrical Engineering in Japan (English translation of Denki Gakkai Ronbunshi), 198(1), 34-44. https://doi.org/10.1002/eej.22882

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