Adaptive super-twisting nonsingular fast terminal sliding mode fault tolerant control of a 2-DOF helicopter with input quantization.

Hui Bi, Tao Zou, Jincai Zhu, JiaKun Liu
{"title":"Adaptive super-twisting nonsingular fast terminal sliding mode fault tolerant control of a 2-DOF helicopter with input quantization.","authors":"Hui Bi, Tao Zou, Jincai Zhu, JiaKun Liu","doi":"10.1016/j.isatra.2025.03.003","DOIUrl":null,"url":null,"abstract":"<p><p>To address system uncertainties and external disturbances in a 2-DOF helicopter system, this paper proposes a novel adaptive super-twisting non-singular fast terminal sliding mode (NFTSM) fault-tolerant control (FTC) strategy. First, a hysteresis quantizer is utilized to mitigate chattering during the signal quantization process, and reduce energy loss. Second, a novel finite-time convergent NFTSM manifold is proposed, enabling the tracking trajectories to quickly reach the sliding mode surface, thereby endowing the controller with strong robustness. Additionally, neural networks (NNs) are employed to approximate the system's nonlinear uncertainty functions. Furthermore, to overcome the dependency of the super-twisting algorithm on boundary information regarding disturbances during the design process, an adaptive super-twisting algorithm is introduced to compensate for the effects of quantization errors and external disturbances, ensuring FTC performance. Finally, simulation and experiment results effectively validate the superiority of the proposed control strategy.</p>","PeriodicalId":94059,"journal":{"name":"ISA transactions","volume":" ","pages":""},"PeriodicalIF":0.0000,"publicationDate":"2025-03-18","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"ISA transactions","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1016/j.isatra.2025.03.003","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
引用次数: 0

Abstract

To address system uncertainties and external disturbances in a 2-DOF helicopter system, this paper proposes a novel adaptive super-twisting non-singular fast terminal sliding mode (NFTSM) fault-tolerant control (FTC) strategy. First, a hysteresis quantizer is utilized to mitigate chattering during the signal quantization process, and reduce energy loss. Second, a novel finite-time convergent NFTSM manifold is proposed, enabling the tracking trajectories to quickly reach the sliding mode surface, thereby endowing the controller with strong robustness. Additionally, neural networks (NNs) are employed to approximate the system's nonlinear uncertainty functions. Furthermore, to overcome the dependency of the super-twisting algorithm on boundary information regarding disturbances during the design process, an adaptive super-twisting algorithm is introduced to compensate for the effects of quantization errors and external disturbances, ensuring FTC performance. Finally, simulation and experiment results effectively validate the superiority of the proposed control strategy.

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:481959085
Book学术官方微信