屋外におけるスライディングモード制御を用いた小型ドローンの自律飛行制御
小野山 博之, 中西 喬希, 内田 達也, 深尾 隆則
pp. 209-216
DOI:
10.5687/iscie.35.209抄録
In this paper, we designed an attitude controller for a quadcopter based on sliding mode control. Autonomous flight experiments on a straight line path were conducted in the outdoors. The control performance of the conventional PID control method and the sliding mode control method designed in this paper was compared at a wind speed of 3 m/s. In the case of PID control, the maximum errors of the lateral direction, roll angle, pitch angle, and yaw angle were 34.6 cm, 2.59 deg, 5.61 deg, and 15.02 deg, respectively, on the other hand, in the case of sliding mode control, they were 20.5 cm, 1.49 deg, 1.43 deg, and 5.62 deg, respectively. Therefore, under a wind speed of 3.0 m/s, the results of position and attitude angle errors indicate that sliding mode control is effective in improving the robustness of the system.
他の人はこちらも検索
材料と環境 Vol.71(2022), No.10
鋼構造論文集 Vol.29(2022), No.115
日本エネルギー学会誌 Vol.101(2022), No.11