具有扰动的无人四旋翼飞行器加速度多环控制

Y. He, H. Zhou, H. Yue, G. T. Qiu, Z. Z. Lin
{"title":"具有扰动的无人四旋翼飞行器加速度多环控制","authors":"Y. He, H. Zhou, H. Yue, G. T. Qiu, Z. Z. Lin","doi":"10.1109/CGNCC.2016.7828976","DOIUrl":null,"url":null,"abstract":"Over the last decade, considerable interest has been shown from government, academia, military and business circles to the design of unmanned quadrotor autonomous control. This paper uses a multiple-loop control strategy with disturbance compensation by the acceleration measurement for an unmanned quadrotor. The outer-loop control uses dynamic surface control method with disturbance compensation by use of acceleration measurement. The middle-loop uses P control and the inner-loop uses PID control. This structure does not need know the quadrotor parameters and can be applied into practice easily. The simulation and experiment results also show that the good performance of position tracking and extern disturbance (wind gust) rejection.","PeriodicalId":426650,"journal":{"name":"2016 IEEE Chinese Guidance, Navigation and Control Conference (CGNCC)","volume":"7 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"2016-08-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":"{\"title\":\"Acceleration-based multiple-loop control of unmanned quadrotors with disturbances\",\"authors\":\"Y. He, H. Zhou, H. Yue, G. T. Qiu, Z. Z. Lin\",\"doi\":\"10.1109/CGNCC.2016.7828976\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"Over the last decade, considerable interest has been shown from government, academia, military and business circles to the design of unmanned quadrotor autonomous control. This paper uses a multiple-loop control strategy with disturbance compensation by the acceleration measurement for an unmanned quadrotor. The outer-loop control uses dynamic surface control method with disturbance compensation by use of acceleration measurement. The middle-loop uses P control and the inner-loop uses PID control. This structure does not need know the quadrotor parameters and can be applied into practice easily. The simulation and experiment results also show that the good performance of position tracking and extern disturbance (wind gust) rejection.\",\"PeriodicalId\":426650,\"journal\":{\"name\":\"2016 IEEE Chinese Guidance, Navigation and Control Conference (CGNCC)\",\"volume\":\"7 1\",\"pages\":\"0\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"2016-08-01\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"0\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"2016 IEEE Chinese Guidance, Navigation and Control Conference (CGNCC)\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.1109/CGNCC.2016.7828976\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"2016 IEEE Chinese Guidance, Navigation and Control Conference (CGNCC)","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/CGNCC.2016.7828976","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

在过去的十年中,相当大的兴趣已经显示从政府,学术界,军方和商界的无人驾驶四旋翼自主控制的设计。针对无人四旋翼飞行器的加速度测量,提出了一种带有扰动补偿的多回路控制策略。外环控制采用动态面控制方法,利用加速度测量进行扰动补偿。中回路采用P控制,内回路采用PID控制。这种结构不需要知道四旋翼的参数,可以很容易地应用于实际。仿真和实验结果表明,该系统具有良好的位置跟踪和抗外界干扰(阵风)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。
Acceleration-based multiple-loop control of unmanned quadrotors with disturbances
Over the last decade, considerable interest has been shown from government, academia, military and business circles to the design of unmanned quadrotor autonomous control. This paper uses a multiple-loop control strategy with disturbance compensation by the acceleration measurement for an unmanned quadrotor. The outer-loop control uses dynamic surface control method with disturbance compensation by use of acceleration measurement. The middle-loop uses P control and the inner-loop uses PID control. This structure does not need know the quadrotor parameters and can be applied into practice easily. The simulation and experiment results also show that the good performance of position tracking and extern disturbance (wind gust) rejection.
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:604180095
Book学术官方微信