{"title":"电磁飞机弹射系统的模块化控制","authors":"A. Monti, K. Patel, D. Patterson, R. Dougal","doi":"10.1109/PESC.2003.1217739","DOIUrl":null,"url":null,"abstract":"This paper describes an approach to a modular control for an electromagnetic aircraft launching system (EMALS) for the aircraft carrier of the future. The purpose is to analyze the possibility of improving the control performance using efficient evaluation of switching conditions. Different options for the basic control design are discussed and as well as the way in which these options will be tested using the virtual test bed (VTB) software.","PeriodicalId":236199,"journal":{"name":"IEEE 34th Annual Conference on Power Electronics Specialist, 2003. PESC '03.","volume":"19 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"2003-06-15","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"5","resultStr":"{\"title\":\"Modular control for electromagnetic aircraft launching system\",\"authors\":\"A. Monti, K. Patel, D. Patterson, R. Dougal\",\"doi\":\"10.1109/PESC.2003.1217739\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"This paper describes an approach to a modular control for an electromagnetic aircraft launching system (EMALS) for the aircraft carrier of the future. The purpose is to analyze the possibility of improving the control performance using efficient evaluation of switching conditions. Different options for the basic control design are discussed and as well as the way in which these options will be tested using the virtual test bed (VTB) software.\",\"PeriodicalId\":236199,\"journal\":{\"name\":\"IEEE 34th Annual Conference on Power Electronics Specialist, 2003. PESC '03.\",\"volume\":\"19 1\",\"pages\":\"0\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"2003-06-15\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"5\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"IEEE 34th Annual Conference on Power Electronics Specialist, 2003. PESC '03.\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.1109/PESC.2003.1217739\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"IEEE 34th Annual Conference on Power Electronics Specialist, 2003. PESC '03.","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/PESC.2003.1217739","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
Modular control for electromagnetic aircraft launching system
This paper describes an approach to a modular control for an electromagnetic aircraft launching system (EMALS) for the aircraft carrier of the future. The purpose is to analyze the possibility of improving the control performance using efficient evaluation of switching conditions. Different options for the basic control design are discussed and as well as the way in which these options will be tested using the virtual test bed (VTB) software.
京公网安备 11010802042870号
京ICP备2023020795号-1
分享
求助内容：
应助结果提醒方式：
扫码关注我们
