A comparative study of altitude and yaw controllers for rotorcraft UAV

Alexandre Da S. Fernandes, A. Brandão, Elmer R. Llanos Villarreal
{"title":"A comparative study of altitude and yaw controllers for rotorcraft UAV","authors":"Alexandre Da S. Fernandes, A. Brandão, Elmer R. Llanos Villarreal","doi":"10.1109/RED-UAS.2015.7441034","DOIUrl":null,"url":null,"abstract":"The paper presents a brief study of quadrotor vehicle, its principle of operation and its high-level dynamic model. The proposal of altitude and yaw controllers is also presented. PID, LQR (LQRI) and Lyapunov based control techniques are here compared according to Integral Absolute Error (IAE) and Control Signal Energy criteria. The performance is analyzed in terms of the response time and energy spent to accomplish the task. The optimum controller gains are defined by simulation, after establishing the maximum value of the criteria. In the sequence, some experiments are run to validate the controllers and to compared them in real scenarios of regulation and trajectory tracking tasks.","PeriodicalId":317787,"journal":{"name":"2015 Workshop on Research, Education and Development of Unmanned Aerial Systems (RED-UAS)","volume":"14 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"2015-11-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"2","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"2015 Workshop on Research, Education and Development of Unmanned Aerial Systems (RED-UAS)","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/RED-UAS.2015.7441034","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
引用次数: 2

Abstract

The paper presents a brief study of quadrotor vehicle, its principle of operation and its high-level dynamic model. The proposal of altitude and yaw controllers is also presented. PID, LQR (LQRI) and Lyapunov based control techniques are here compared according to Integral Absolute Error (IAE) and Control Signal Energy criteria. The performance is analyzed in terms of the response time and energy spent to accomplish the task. The optimum controller gains are defined by simulation, after establishing the maximum value of the criteria. In the sequence, some experiments are run to validate the controllers and to compared them in real scenarios of regulation and trajectory tracking tasks.
查看原文
分享 分享
微信好友 朋友圈 QQ好友 复制链接
本刊更多论文
旋翼无人机高度与偏航控制器的比较研究
本文简要介绍了四旋翼飞行器的工作原理及其高级动力学模型。提出了高度控制器和偏航控制器的设计方案。本文根据积分绝对误差(IAE)和控制信号能量标准对PID、LQR (LQRI)和Lyapunov控制技术进行了比较。性能是根据完成任务所花费的响应时间和精力来分析的。在建立准则的最大值后,通过仿真确定了最优控制器增益。在此过程中,对控制器进行了实验验证,并在实际的调节和轨迹跟踪任务中进行了比较。
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 去求助
来源期刊
自引率
0.00%
发文量
0
期刊最新文献
Model identification and validation for translational movements of an octorotor UAV Vision-IMU based collaborative control of a blind UAV Velocity control of mini-UAV using a helmet system A hybrid 3D path planning method for UAVs Design of sliding mode observers for quadrotor pitch/roll angle estimation via IMU measurements
×
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
现在去查看 取消
×
提示
确定
0
微信
客服QQ
Book学术公众号 扫码关注我们
反馈
×
意见反馈
请填写您的意见或建议
请填写您的手机或邮箱
已复制链接
已复制链接
快去分享给好友吧!
我知道了
×
扫码分享
扫码分享
Book学术官方微信
Book学术文献互助
Book学术文献互助群
群 号:481959085
Book学术
文献互助 智能选刊 最新文献 互助须知 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 Book学术 All rights reserved.
ghs 京公网安备 11010802042870号 京ICP备2023020795号-1