Sliding mode-based fault tolerant control designs for quadrotor UAVs-A comparative study

Seema Mallavalli, A. Fekih
{"title":"Sliding mode-based fault tolerant control designs for quadrotor UAVs-A comparative study","authors":"Seema Mallavalli, A. Fekih","doi":"10.1109/ICCA.2017.8003051","DOIUrl":null,"url":null,"abstract":"This paper provides a comparative study of three Sliding Mode Control (SMC)-based fault tolerant controllers for trajectory tracking of a quadrotor UAV subject to actuator faults. Conventional SMC, Integral (ISMC) and Integral Terminal SMC (ITSMC) designs are designed and implemented to a quadrator UAV. The controllers' performance along with their respective robustness was assessed using various faulty conditions. Stability analysis was carried over using the Lyapunov approach. A thorough discussion of the controllers' respective performance in light of the obtained results was also performed and presented in the paper.","PeriodicalId":379025,"journal":{"name":"2017 13th IEEE International Conference on Control & Automation (ICCA)","volume":"103 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"2017-07-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"13","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"2017 13th IEEE International Conference on Control & Automation (ICCA)","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/ICCA.2017.8003051","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
引用次数: 13

Abstract

This paper provides a comparative study of three Sliding Mode Control (SMC)-based fault tolerant controllers for trajectory tracking of a quadrotor UAV subject to actuator faults. Conventional SMC, Integral (ISMC) and Integral Terminal SMC (ITSMC) designs are designed and implemented to a quadrator UAV. The controllers' performance along with their respective robustness was assessed using various faulty conditions. Stability analysis was carried over using the Lyapunov approach. A thorough discussion of the controllers' respective performance in light of the obtained results was also performed and presented in the paper.
基于滑模的四旋翼无人机容错控制设计——比较研究
对三种基于滑模控制的四旋翼无人机执行器故障轨迹跟踪容错控制器进行了比较研究。设计并实现了常规SMC、积分SMC和积分终端SMC。在不同的故障条件下,对控制器的性能及其鲁棒性进行了评估。稳定性分析采用李雅普诺夫方法进行。根据所获得的结果,对控制器各自的性能进行了深入的讨论,并在文中进行了介绍。
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