Desing of a Chattering-Free Sliding Mode Control System for Robust Position Control of a Quadrotor

Aydin Can, Harry Efstathiades, A. Montazeri
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引用次数: 4

Abstract

In this paper, the major components of an unmanned aerial vehicle (UAV), including the flight control system, mechanical design, as well as the embedded electronic systems are reported. The ultimate aim is to use the developed platform in nuclear environments for decommissioning applications. Due to the hazards and uncertainties present in these nuclear environments, a more basic control system may be unable to reliably control the UAV. Therefore, the main focus of this study is on the development of a robust multi-channel control system, based on sliding mode control (SMC), for nested position and attitude control of a quadrotor UAV in 3D space. The robustness of the control systems is evaluated under parameter disturbance in the form of payload uncertainties. The final developed platform shall be capable of autonomous Simultaneous Localisation and Mapping (SLAM), however, this will be the subject of a separate study.
四旋翼飞行器鲁棒位置控制的无抖振滑模控制系统设计
本文介绍了无人机的主要组成部分,包括飞控系统、机械设计和嵌入式电子系统。最终目标是将开发的平台用于核环境中的退役应用。由于这些核环境中存在的危险和不确定性,一个更基本的控制系统可能无法可靠地控制无人机。因此,本研究的主要重点是开发基于滑模控制(SMC)的鲁棒多通道控制系统,用于四旋翼无人机在三维空间的嵌套位置和姿态控制。在载荷不确定性形式的参数扰动下,评估了控制系统的鲁棒性。最终开发的平台应能够自主同步定位和绘图(SLAM),然而,这将是一个单独研究的主题。
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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