直升飞机纵向动力学的调节:一种Liouvillian系统方法

H. Sira-Ramírez, R. Castro-Linares, E. Licéaga-Castro
{"title":"直升飞机纵向动力学的调节:一种Liouvillian系统方法","authors":"H. Sira-Ramírez, R. Castro-Linares, E. Licéaga-Castro","doi":"10.1109/ACC.1999.786571","DOIUrl":null,"url":null,"abstract":"A feedback regulation scheme is presented for a wide range of horizontal and vertical displacement manoeuvres on a simplified longitudinal model of a helicopter system. The approach is based on the \"Liouvillian\" property of the helicopter model, rather than its differential flatness, thus requiring only a static, though time-varying, state feedback controller which tracks an off-line planned trajectory planning for the attitude angle reference signal computed in terms of the desired horizontal and vertical displacements. The controller performance is evaluated through digital computer simulations which include initial setting errors and an unmodelled mid course wind gust perturbation of significant magnitude.","PeriodicalId":441363,"journal":{"name":"Proceedings of the 1999 American Control Conference (Cat. No. 99CH36251)","volume":"150 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"1999-12-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"9","resultStr":"{\"title\":\"Regulation of the longitudinal dynamics of an helicopter: a Liouvillian systems approach\",\"authors\":\"H. Sira-Ramírez, R. Castro-Linares, E. Licéaga-Castro\",\"doi\":\"10.1109/ACC.1999.786571\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"A feedback regulation scheme is presented for a wide range of horizontal and vertical displacement manoeuvres on a simplified longitudinal model of a helicopter system. The approach is based on the \\\"Liouvillian\\\" property of the helicopter model, rather than its differential flatness, thus requiring only a static, though time-varying, state feedback controller which tracks an off-line planned trajectory planning for the attitude angle reference signal computed in terms of the desired horizontal and vertical displacements. The controller performance is evaluated through digital computer simulations which include initial setting errors and an unmodelled mid course wind gust perturbation of significant magnitude.\",\"PeriodicalId\":441363,\"journal\":{\"name\":\"Proceedings of the 1999 American Control Conference (Cat. No. 99CH36251)\",\"volume\":\"150 1\",\"pages\":\"0\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"1999-12-01\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"9\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"Proceedings of the 1999 American Control Conference (Cat. No. 99CH36251)\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.1109/ACC.1999.786571\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"Proceedings of the 1999 American Control Conference (Cat. No. 99CH36251)","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/ACC.1999.786571","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
引用次数: 9

摘要

在简化的直升机系统纵向模型上,提出了一种适用于大范围水平和垂直位移机动的反馈调节方案。该方法基于直升机模型的“Liouvillian”属性,而不是其差分平面,因此只需要一个静态的,尽管时变的状态反馈控制器,该控制器跟踪离线规划的轨迹规划,根据期望的水平和垂直位移计算姿态角参考信号。通过数字计算机模拟来评估控制器的性能,其中包括初始设置误差和未建模的显著量级的中途阵风扰动。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Regulation of the longitudinal dynamics of an helicopter: a Liouvillian systems approach
A feedback regulation scheme is presented for a wide range of horizontal and vertical displacement manoeuvres on a simplified longitudinal model of a helicopter system. The approach is based on the "Liouvillian" property of the helicopter model, rather than its differential flatness, thus requiring only a static, though time-varying, state feedback controller which tracks an off-line planned trajectory planning for the attitude angle reference signal computed in terms of the desired horizontal and vertical displacements. The controller performance is evaluated through digital computer simulations which include initial setting errors and an unmodelled mid course wind gust perturbation of significant magnitude.
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