基于最优整定的线性自抗扰控制在四轴飞行器中的应用

S. A. Suhail, M. A. Bazaz, Shoeb Hussain
{"title":"基于最优整定的线性自抗扰控制在四轴飞行器中的应用","authors":"S. A. Suhail, M. A. Bazaz, Shoeb Hussain","doi":"10.1109/ICONAT53423.2022.9725873","DOIUrl":null,"url":null,"abstract":"This paper proposes a novel control approach called the Active Disturbance Rejection Control (ADRC) for the altitude and attitude control of an unmanned quadcopter with disturbances. The quadcopter is an underactuated system subject to parametric perturbations, non-linearity, unmodeled dynamics, strong coupling, and external disturbances. Linear Quadratic Regulator (LQR), an optimal control method, is used for the tuning of ADRC. The proposed control scheme is verified in simulation studies with the presence of sensor noise and external disturbances. The simulation results show that the proposed algorithm can significantly reduce the chattering phenomenon, owing to the estimation capability of the Extended State Observer (ESO). The proposed method also improves the robustness against modeling errors and disturbances and smoothly tracks the reference trajectory compared to PID and sliding mode control (SMC).","PeriodicalId":377501,"journal":{"name":"2022 International Conference for Advancement in Technology (ICONAT)","volume":"42 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"2022-01-21","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":"{\"title\":\"Optimal Tuning Based Linear Active Disturbance Rejection Control Applied to a Quadcopter\",\"authors\":\"S. A. Suhail, M. A. Bazaz, Shoeb Hussain\",\"doi\":\"10.1109/ICONAT53423.2022.9725873\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"This paper proposes a novel control approach called the Active Disturbance Rejection Control (ADRC) for the altitude and attitude control of an unmanned quadcopter with disturbances. The quadcopter is an underactuated system subject to parametric perturbations, non-linearity, unmodeled dynamics, strong coupling, and external disturbances. Linear Quadratic Regulator (LQR), an optimal control method, is used for the tuning of ADRC. The proposed control scheme is verified in simulation studies with the presence of sensor noise and external disturbances. The simulation results show that the proposed algorithm can significantly reduce the chattering phenomenon, owing to the estimation capability of the Extended State Observer (ESO). The proposed method also improves the robustness against modeling errors and disturbances and smoothly tracks the reference trajectory compared to PID and sliding mode control (SMC).\",\"PeriodicalId\":377501,\"journal\":{\"name\":\"2022 International Conference for Advancement in Technology (ICONAT)\",\"volume\":\"42 1\",\"pages\":\"0\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"2022-01-21\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"0\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"2022 International Conference for Advancement in Technology (ICONAT)\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.1109/ICONAT53423.2022.9725873\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"2022 International Conference for Advancement in Technology (ICONAT)","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/ICONAT53423.2022.9725873","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
引用次数: 0

摘要

针对具有扰动的无人四轴飞行器的高度和姿态控制问题,提出了一种新的自抗扰控制方法。四轴飞行器是一个欠驱动系统,受参数扰动、非线性、未建模动力学、强耦合和外部干扰的影响。采用线性二次型调节器(LQR)作为最优控制方法对自抗扰控制器进行整定。在存在传感器噪声和外界干扰的情况下,对所提出的控制方案进行了仿真研究。仿真结果表明,由于扩展状态观测器(ESO)的估计能力,该算法可以显著降低抖振现象。与PID和滑模控制(SMC)相比,该方法还提高了对建模误差和干扰的鲁棒性,并能平滑地跟踪参考轨迹。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Optimal Tuning Based Linear Active Disturbance Rejection Control Applied to a Quadcopter
This paper proposes a novel control approach called the Active Disturbance Rejection Control (ADRC) for the altitude and attitude control of an unmanned quadcopter with disturbances. The quadcopter is an underactuated system subject to parametric perturbations, non-linearity, unmodeled dynamics, strong coupling, and external disturbances. Linear Quadratic Regulator (LQR), an optimal control method, is used for the tuning of ADRC. The proposed control scheme is verified in simulation studies with the presence of sensor noise and external disturbances. The simulation results show that the proposed algorithm can significantly reduce the chattering phenomenon, owing to the estimation capability of the Extended State Observer (ESO). The proposed method also improves the robustness against modeling errors and disturbances and smoothly tracks the reference trajectory compared to PID and sliding mode control (SMC).
求助全文
通过发布文献求助,成功后即可免费获取论文全文。 去求助
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:481959085
Book学术官方微信