Trajectory Tracking Control of Quadrotor Based on Fractional-Order S-Plane Model

Author:

Li Jiacheng1ORCID,Chen Pengyun1ORCID,Chang Zhe1,Zhang Guobing1,Guo Luji1,Zhao Chenbo1

Affiliation:

1. School of Aerospace Engineering, North University of China, Taiyuan 030051, China

Abstract

Quadrotors possess traits such as under-actuation, nonlinearity, and strong coupling. Quaternions are primarily used for attitude calculations in drones, with error quaternions seldom being employed directly in the control of specific quadcopter drones. This paper focuses on the low tracking accuracy and weak anti-interference ability of quadcopter drones in trajectory-tracking control. By establishing the quadcopter quaternion model, a controller based on quaternion error is designed through a combination of fractional-order PID control with S-plane control. Trajectory-tracking experiments demonstrate that, in comparison with fractional-order PID, this method exhibits strong wind disturbance resistance and high tracking accuracy.

Funder

Key Research and Development Program of Shanxi Province

National Natural Science Foundation of China

Fundamental Research Program of Shanxi Province

Postgraduate Science and Technology Project of NUC

Publisher

MDPI AG

Subject

Electrical and Electronic Engineering,Industrial and Manufacturing Engineering,Control and Optimization,Mechanical Engineering,Computer Science (miscellaneous),Control and Systems Engineering

Reference29 articles.

1. Li, J., and Li, Y. (2011, January 7–10). Dynamic analysis and PID control for a quadrotor. Proceedings of the 2011 IEEE International Conference on Mechatronics and Automation, Beijing, China.

2. Timis, D.D., Muresan, C.I., and Dulf, E.H. (2022). Design and Experimental Results of an Adaptive Fractional-Order Controller for a Quadrotor. Fractal Fract., 6.

3. Design of fractional-order backstepping sliding mode control for quadrotor UAV;Shi;Asian J. Control,2019

4. Han, J. (2008). Active Disturbance Rejection Control Technique—The Technique for Estimating and Compensating the Uncertainties, National Defense Industry Press.

5. Wang, C., Chen, Z., Sun, Q., and Zhang, Q. (2016, January 28–30). Design of PID and ADRC based quadrotor helicopter control system. Proceedings of the 2016 Chinese Control and Decision Conference (CCDC), Yinchuan, China.

Cited by 2 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

同舟云学术

1.学者识别学者识别

2.学术分析学术分析

3.人才评估人才评估

"同舟云学术"是以全球学者为主线,采集、加工和组织学术论文而形成的新型学术文献查询和分析系统,可以对全球学者进行文献检索和人才价值评估。用户可以通过关注某些学科领域的顶尖人物而持续追踪该领域的学科进展和研究前沿。经过近期的数据扩容,当前同舟云学术共收录了国内外主流学术期刊6万余种,收集的期刊论文及会议论文总量共计约1.5亿篇,并以每天添加12000余篇中外论文的速度递增。我们也可以为用户提供个性化、定制化的学者数据。欢迎来电咨询!咨询电话:010-8811{复制后删除}0370

www.globalauthorid.com

TOP

Copyright © 2019-2024 北京同舟云网络信息技术有限公司
京公网安备11010802033243号  京ICP备18003416号-3