六旋翼机自动驾驶仪滑模控制设计

2022 5th International Conference on Advanced Systems and Emergent Technologies (IC_ASET) Pub Date : 2022-03-22 DOI:10.1109/IC_ASET53395.2022.9765926

Helmi Abrougui, S. Nejim, Anis Charrada, Habib Dallagi

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引用次数: 2

摘要

提出了一种六旋翼机姿态建模与控制方法。采用滑模控制设计了自动驾驶仪。它由一个用于姿态稳定的低级控制器和一个用于位置跟踪控制的高级控制器组成。仿真结果表明了所设计的自动驾驶仪的有效性。

本文章由计算机程序翻译，如有差异，请以英文原文为准。

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Sliding Mode Control for Hexacopter Autopilot design

This paper proposes an approach for modeling and controlling the attitude of a hexacopter. An autopilot is designed using sliding mode control. It consists of a low-level controller for attitude stabilization and a high-level controller for position tracking control. Simulations are carried out to show the effectiveness of the designed autopilot.

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来源期刊

2022 5th International Conference on Advanced Systems and Emergent Technologies (IC_ASET)

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