On the regulation of a helicopter system: A trajectory planning approach for the Liouvillian model

H. Sira-Ramírez, R. Castro-Linares
{"title":"On the regulation of a helicopter system: A trajectory planning approach for the Liouvillian model","authors":"H. Sira-Ramírez, R. Castro-Linares","doi":"10.23919/ECC.1999.7099823","DOIUrl":null,"url":null,"abstract":"A feedback regulation scheme is presented which allows for a wide range of displacement maneuvers on a simplified longitudinal model of a helicopter system which is underactuated and nondifferentially flat. The system, nevertheless, is shown to be of the \"Liouvillian\" type. An off-line, open loop, trajectory planning procedure is proposed, based on the solution of differential equations for the desired attitude angle reference signal, which precisely results in the desired nominal horizontal displacement trajectory. The performance of a proposed feedback controller, which exploits the fact that the linearized system has its coefficients on a Hardy filed, is evaluated through digital computer simulations including unmodelled mid course wind gusts and initial setting errors.","PeriodicalId":117668,"journal":{"name":"1999 European Control Conference (ECC)","volume":"33 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"1999-08-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"6","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"1999 European Control Conference (ECC)","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.23919/ECC.1999.7099823","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
引用次数: 6

Abstract

A feedback regulation scheme is presented which allows for a wide range of displacement maneuvers on a simplified longitudinal model of a helicopter system which is underactuated and nondifferentially flat. The system, nevertheless, is shown to be of the "Liouvillian" type. An off-line, open loop, trajectory planning procedure is proposed, based on the solution of differential equations for the desired attitude angle reference signal, which precisely results in the desired nominal horizontal displacement trajectory. The performance of a proposed feedback controller, which exploits the fact that the linearized system has its coefficients on a Hardy filed, is evaluated through digital computer simulations including unmodelled mid course wind gusts and initial setting errors.
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
直升机系统的调节:Liouvillian模型的轨迹规划方法
针对欠驱动、无差平的直升机系统纵向简化模型,提出了一种允许大范围位移机动的反馈调节方案。然而,该系统显示为“Liouvillian”类型。在解姿态角参考信号微分方程的基础上,提出了一种离线开环弹道规划方法,该方法可以精确地得到期望的标称水平位移轨迹。利用线性化系统在Hardy场上具有其系数的事实,所提出的反馈控制器的性能通过数字计算机模拟进行评估,包括未建模的中途阵风和初始设置误差。
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
A non-conservative approach to set membership identification for control Approximating uncertainty representations using the v-GAP metric Fault-tolerant control of a ship propulsion system using model predictive control Closed-loop identification using canonical correlation analysis Subspace-based identification of MIMO bilinear systems
×
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