{"title":"俯仰解耦VTOL/FW飞机:首飞","authors":"J. Apkarian","doi":"10.1109/RED-UAS.2017.8101676","DOIUrl":null,"url":null,"abstract":"A novel Pitch-Decoupled Tilt Rotor aircraft is introduced that dramatically deviates from all tilt rotor systems developed to date. This new design does not require a complex transition algorithm and is continuously stable and operable in all its rotor pitch configurations.","PeriodicalId":299104,"journal":{"name":"2017 Workshop on Research, Education and Development of Unmanned Aerial Systems (RED-UAS)","volume":"1 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"2017-10-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"7","resultStr":"{\"title\":\"Pitch-decoupled VTOL/FW aircraft: First flights\",\"authors\":\"J. Apkarian\",\"doi\":\"10.1109/RED-UAS.2017.8101676\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"A novel Pitch-Decoupled Tilt Rotor aircraft is introduced that dramatically deviates from all tilt rotor systems developed to date. This new design does not require a complex transition algorithm and is continuously stable and operable in all its rotor pitch configurations.\",\"PeriodicalId\":299104,\"journal\":{\"name\":\"2017 Workshop on Research, Education and Development of Unmanned Aerial Systems (RED-UAS)\",\"volume\":\"1 1\",\"pages\":\"0\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"2017-10-01\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"7\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"2017 Workshop on Research, Education and Development of Unmanned Aerial Systems (RED-UAS)\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.1109/RED-UAS.2017.8101676\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"2017 Workshop on Research, Education and Development of Unmanned Aerial Systems (RED-UAS)","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/RED-UAS.2017.8101676","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
A novel Pitch-Decoupled Tilt Rotor aircraft is introduced that dramatically deviates from all tilt rotor systems developed to date. This new design does not require a complex transition algorithm and is continuously stable and operable in all its rotor pitch configurations.