Quadcopter attitude and altitude tracking by using improved PD controllers

K. E. Hamidi, Mostafa Mjahed, A. E. Kari, H. Ayad
{"title":"Quadcopter attitude and altitude tracking by using improved PD controllers","authors":"K. E. Hamidi, Mostafa Mjahed, A. E. Kari, H. Ayad","doi":"10.1504/IJNDC.2019.098688","DOIUrl":null,"url":null,"abstract":"The quadcopter is a complex coupled nonlinear system with unstable behaviour, which makes it difficult to control. Therefore, in this paper, we present an effective control method based on neural network gain-scheduled PD (NNGS-PD) and model reference controller-based PD (MRC-PD) for quadcopter attitude stabilisation and altitude tracking. Both nonlinear and linear methods verified the stability and robustness of the proposed controllers. The simulation results illustrate that the synthesis control methods have good performance in terms of attitude and altitude tracking when faced with external disturbances.","PeriodicalId":249374,"journal":{"name":"International Journal of Nonlinear Dynamics and Control","volume":"27 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"2019-04-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"5","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"International Journal of Nonlinear Dynamics and Control","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1504/IJNDC.2019.098688","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
引用次数: 5

Abstract

The quadcopter is a complex coupled nonlinear system with unstable behaviour, which makes it difficult to control. Therefore, in this paper, we present an effective control method based on neural network gain-scheduled PD (NNGS-PD) and model reference controller-based PD (MRC-PD) for quadcopter attitude stabilisation and altitude tracking. Both nonlinear and linear methods verified the stability and robustness of the proposed controllers. The simulation results illustrate that the synthesis control methods have good performance in terms of attitude and altitude tracking when faced with external disturbances.
采用改进PD控制器的四轴飞行器姿态和高度跟踪
四轴飞行器是一个复杂的非线性耦合系统,具有不稳定的特性,控制难度很大。因此,本文提出了一种基于神经网络增益调度PD (NNGS-PD)和基于模型参考控制器PD (MRC-PD)的四轴飞行器姿态稳定和高度跟踪的有效控制方法。非线性和线性方法验证了所提控制器的稳定性和鲁棒性。仿真结果表明,该综合控制方法在面对外界干扰时具有良好的姿态和高度跟踪性能。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
求助全文
约1分钟内获得全文 求助全文
来源期刊
自引率
0.00%
发文量
0
×
引用
GB/T 7714-2015
复制
MLA
复制
APA
复制
导出至
BibTeX EndNote RefMan NoteFirst NoteExpress
×
提示
您的信息不完整,为了账户安全,请先补充。
现在去补充
×
提示
您因"违规操作"
具体请查看互助需知
我知道了
×
提示
确定
请完成安全验证×
copy
已复制链接
快去分享给好友吧!
我知道了
右上角分享
点击右上角分享
0
联系我们:info@booksci.cn Book学术提供免费学术资源搜索服务,方便国内外学者检索中英文文献。致力于提供最便捷和优质的服务体验。 Copyright © 2023 布克学术 All rights reserved.
京ICP备2023020795号-1
ghs 京公网安备 11010802042870号
Book学术文献互助
Book学术文献互助群
群 号:604180095
Book学术官方微信