Trajectory tracking of a quadrotor using TID controller

Kranthi Kumar Deveerasetty, Yimin Zhou, B. Han
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引用次数: 1

Abstract

In this paper, a TID controller is applied for the trajectory tracking of a quadrotor. The mathematical model of the control system is derived and compared with the traditional PD (Proportional-Derivative) controller. In order to improve the control precision of the UAV, the controller is designed by selecting the proper tuning parameters. To explore the effectiveness of the proposed controller, dynamic responses of a UAV obtained by using the TID controller and the validation of the results compared with the PD controller. The control performances are analysed by using MATLAB/Simulink model.
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基于TID控制器的四旋翼飞行器轨迹跟踪
本文将TID控制器应用于四旋翼飞行器的轨迹跟踪。推导了控制系统的数学模型,并与传统的比例导数控制器进行了比较。为了提高无人机的控制精度,通过选择合适的整定参数对控制器进行了设计。为了验证所提控制器的有效性,利用TID控制器获得了无人机的动态响应,并将结果与PD控制器进行了对比验证。利用MATLAB/Simulink模型对其控制性能进行了分析。
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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