基于滑模控制的四轴飞行器航路点跟踪飞行控制器设计

2020 4th International Conference on Advanced Systems and Emergent Technologies (IC_ASET) Pub Date : 2020-12-15 DOI:10.1109/IC_ASET49463.2020.9318249

Helmi Abrougui, Saber Hachicha, C. Zaoui, Habib Dallagi, S. Nejim

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引用次数: 3

摘要

飞行控制系统广泛应用于现代飞机;他们帮助飞行员驾驶飞机。施加在飞行器四轴飞行器机体上的风力导致了较大的漂移角。为了解决这一问题，设计了一种基于非线性控制器的高效飞行控制器。这两个控制器是基于四轴飞行器动力学模型开发的。通过仿真验证了该方法的有效性。

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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Flight Controller Design Based on Sliding Mode Control for Quadcopter Waypoints Tracking

Flight control systems are widely used in modern aircraft; they help pilot in steering their aircrafts. The wind force applied on the aircraft quadcopter body causes large drift angles. To remedy this issue, an efficient flight controller based on nonlinear controller for both high-level and low-level regulators was designed. These tow controllers were developed based on the quadcopter dynamic model. This approach is validated through simulation to show its effectiveness.

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来源期刊

2020 4th International Conference on Advanced Systems and Emergent Technologies (IC_ASET)

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