基于动态反演的非线性飞行控制器设计

Y. Baba, L. Takano, M. Sano
{"title":"基于动态反演的非线性飞行控制器设计","authors":"Y. Baba, L. Takano, M. Sano","doi":"10.1109/SICE.1995.526734","DOIUrl":null,"url":null,"abstract":"This paper deals with a synthesis for a nonlinear flight controller using a nonlinear state feedback. This method is called a dynamic inversion theory and is widely used to design a nonlinear flight controller. We show how to choose the control gains for the controller designed by a dynamic inversion theory when inversion is not exact due to the actuator lags.","PeriodicalId":344374,"journal":{"name":"SICE '95. Proceedings of the 34th SICE Annual Conference. International Session Papers","volume":"29 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"1995-07-26","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"2","resultStr":"{\"title\":\"Design of a nonlinear flight controller based on dynamic inversion\",\"authors\":\"Y. Baba, L. Takano, M. Sano\",\"doi\":\"10.1109/SICE.1995.526734\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"This paper deals with a synthesis for a nonlinear flight controller using a nonlinear state feedback. This method is called a dynamic inversion theory and is widely used to design a nonlinear flight controller. We show how to choose the control gains for the controller designed by a dynamic inversion theory when inversion is not exact due to the actuator lags.\",\"PeriodicalId\":344374,\"journal\":{\"name\":\"SICE '95. Proceedings of the 34th SICE Annual Conference. International Session Papers\",\"volume\":\"29 1\",\"pages\":\"0\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"1995-07-26\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"2\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"SICE '95. Proceedings of the 34th SICE Annual Conference. International Session Papers\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.1109/SICE.1995.526734\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"SICE '95. Proceedings of the 34th SICE Annual Conference. International Session Papers","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/SICE.1995.526734","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
引用次数: 2

摘要

研究了一种基于非线性状态反馈的非线性飞行控制器的综合问题。这种方法被称为动态反演理论,广泛应用于非线性飞行控制器的设计。我们展示了当由于执行器滞后而导致反转不精确时,如何选择由动态反转理论设计的控制器的控制增益。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Design of a nonlinear flight controller based on dynamic inversion
This paper deals with a synthesis for a nonlinear flight controller using a nonlinear state feedback. This method is called a dynamic inversion theory and is widely used to design a nonlinear flight controller. We show how to choose the control gains for the controller designed by a dynamic inversion theory when inversion is not exact due to the actuator lags.
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