{"title":"延迟系统识别应用于飞机通过垂直阵风的纵向飞行","authors":"F. Veysset, L. Belkoura, P. Coton, J. Richard","doi":"10.1109/MED.2006.328876","DOIUrl":null,"url":null,"abstract":"This paper deals with modelling and identification of aircraft dynamic entering a vertical gust. The identification approach initiated in (M. Fliess et al., 2003) falls under a prospect for identification from tests carried out in the Flight Analysis Laboratory of the DCSD of ONERA in Lille. The plane is considered into various elements which consist in the fuselage, the wing and the tail. The model incorporates delays linked to the aircraft passage through the atmospheric turbulence","PeriodicalId":347035,"journal":{"name":"2006 14th Mediterranean Conference on Control and Automation","volume":"229 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"2006-06-28","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"8","resultStr":"{\"title\":\"Delay system identification applied to the longitudinal flight of an aircraft through a vertical gust\",\"authors\":\"F. Veysset, L. Belkoura, P. Coton, J. Richard\",\"doi\":\"10.1109/MED.2006.328876\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"This paper deals with modelling and identification of aircraft dynamic entering a vertical gust. The identification approach initiated in (M. Fliess et al., 2003) falls under a prospect for identification from tests carried out in the Flight Analysis Laboratory of the DCSD of ONERA in Lille. The plane is considered into various elements which consist in the fuselage, the wing and the tail. The model incorporates delays linked to the aircraft passage through the atmospheric turbulence\",\"PeriodicalId\":347035,\"journal\":{\"name\":\"2006 14th Mediterranean Conference on Control and Automation\",\"volume\":\"229 1\",\"pages\":\"0\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"2006-06-28\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"8\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"2006 14th Mediterranean Conference on Control and Automation\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.1109/MED.2006.328876\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"2006 14th Mediterranean Conference on Control and Automation","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/MED.2006.328876","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
引用次数: 8
摘要
本文研究了飞机进入垂直阵风的动力学建模和识别问题。在(M. Fliess et al.， 2003)中提出的鉴定方法属于在里尔ONERA DCSD飞行分析实验室进行的测试中进行鉴定的前景。飞机被认为是由机身、机翼和尾部组成的各种元素。该模型包含了与飞机通过大气湍流有关的延迟
Delay system identification applied to the longitudinal flight of an aircraft through a vertical gust
This paper deals with modelling and identification of aircraft dynamic entering a vertical gust. The identification approach initiated in (M. Fliess et al., 2003) falls under a prospect for identification from tests carried out in the Flight Analysis Laboratory of the DCSD of ONERA in Lille. The plane is considered into various elements which consist in the fuselage, the wing and the tail. The model incorporates delays linked to the aircraft passage through the atmospheric turbulence
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