基于并行分布式补偿的直升机鲁棒TS模糊控制器

A. Mahmoud, Munna Khan
{"title":"基于并行分布式补偿的直升机鲁棒TS模糊控制器","authors":"A. Mahmoud, Munna Khan","doi":"10.1109/CIACT.2017.7977308","DOIUrl":null,"url":null,"abstract":"A robust TS Fuzzy controller is developed for a discrete-time 2-DOF helicopter model in this work. The state feedback controller is synthesized based on fuzzy model control technique called Parallel Distributed compensation (PDC). The new algorithm control is a straightforward controller to robustly stabilize the flight attitude of 2-DOF helicopter. Thus, the proposed algorithm is used to ensure the quadratic stabilization and performance of nonlinear closed loop system and ensure robustness of fuzzy model control system. Moreover, the design conditions and criteria for the controller are formulated in the form of linear matrix inequality (LMI). The simulation response will compare the efficiency and disturbance attenuation of the designed flight controller to the other scheme.","PeriodicalId":218079,"journal":{"name":"2017 3rd International Conference on Computational Intelligence & Communication Technology (CICT)","volume":"11 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"2017-02-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":"{\"title\":\"Robust TS fuzzy controller for helicopter via parallel distributed compensation\",\"authors\":\"A. Mahmoud, Munna Khan\",\"doi\":\"10.1109/CIACT.2017.7977308\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"A robust TS Fuzzy controller is developed for a discrete-time 2-DOF helicopter model in this work. The state feedback controller is synthesized based on fuzzy model control technique called Parallel Distributed compensation (PDC). The new algorithm control is a straightforward controller to robustly stabilize the flight attitude of 2-DOF helicopter. Thus, the proposed algorithm is used to ensure the quadratic stabilization and performance of nonlinear closed loop system and ensure robustness of fuzzy model control system. Moreover, the design conditions and criteria for the controller are formulated in the form of linear matrix inequality (LMI). The simulation response will compare the efficiency and disturbance attenuation of the designed flight controller to the other scheme.\",\"PeriodicalId\":218079,\"journal\":{\"name\":\"2017 3rd International Conference on Computational Intelligence & Communication Technology (CICT)\",\"volume\":\"11 1\",\"pages\":\"0\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"2017-02-01\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"0\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"2017 3rd International Conference on Computational Intelligence & Communication Technology (CICT)\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.1109/CIACT.2017.7977308\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"2017 3rd International Conference on Computational Intelligence & Communication Technology (CICT)","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/CIACT.2017.7977308","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

针对离散二自由度直升机模型,设计了一种鲁棒TS模糊控制器。状态反馈控制器是基于并行分布补偿(PDC)模糊模型控制技术合成的。该控制算法是一种简单的二自由度直升机飞行姿态鲁棒稳定控制器。因此,该算法既保证了非线性闭环系统的二次镇定性和性能,又保证了模糊模型控制系统的鲁棒性。并以线性矩阵不等式(LMI)的形式给出了控制器的设计条件和准则。仿真响应将比较所设计的飞行控制器与其他方案的效率和干扰衰减。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Robust TS fuzzy controller for helicopter via parallel distributed compensation
A robust TS Fuzzy controller is developed for a discrete-time 2-DOF helicopter model in this work. The state feedback controller is synthesized based on fuzzy model control technique called Parallel Distributed compensation (PDC). The new algorithm control is a straightforward controller to robustly stabilize the flight attitude of 2-DOF helicopter. Thus, the proposed algorithm is used to ensure the quadratic stabilization and performance of nonlinear closed loop system and ensure robustness of fuzzy model control system. Moreover, the design conditions and criteria for the controller are formulated in the form of linear matrix inequality (LMI). The simulation response will compare the efficiency and disturbance attenuation of the designed flight controller to the other scheme.
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