Dong-gyu Sung, Eun-hak Koh, Ju-Chan Kim, Y. Nam, Jeong-ho Lee, Jae-seung Lee, Chan-bin Lee, Yeong-bae Jeon, Cheol-kyun Choi, Jae-Woo Lee
{"title":"Flying-wing Type Compound Drone Design and Mission Accuracy Analysis","authors":"Dong-gyu Sung, Eun-hak Koh, Ju-Chan Kim, Y. Nam, Jeong-ho Lee, Jae-seung Lee, Chan-bin Lee, Yeong-bae Jeon, Cheol-kyun Choi, Jae-Woo Lee","doi":"10.12985/ksaa.2018.26.4.122","DOIUrl":null,"url":null,"abstract":"A compound drone that combines a fixed wing and a rotary wing is an aircraft that can take off and landing vertically, and can increase flight time and fly faster with fixed wings. The compound drones are divided into many types depending on the method of adding the thrust vectoring or the lift fan and the position of the rotor. In this study, we designed and fabricated a composite drone with four V-TOL motors in a fixed-wing, and assigned missions to the aviation body, hence judged mission accuracy using the actual flight test. The design process and the mission evaluation process employed in this study can be utilized on the development of various unmanned aerial vehicle.","PeriodicalId":132579,"journal":{"name":"Journal of the Korean Society for Aviation and Aeronautics","volume":"204 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"2018-12-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"Journal of the Korean Society for Aviation and Aeronautics","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.12985/ksaa.2018.26.4.122","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
引用次数: 0
Abstract
A compound drone that combines a fixed wing and a rotary wing is an aircraft that can take off and landing vertically, and can increase flight time and fly faster with fixed wings. The compound drones are divided into many types depending on the method of adding the thrust vectoring or the lift fan and the position of the rotor. In this study, we designed and fabricated a composite drone with four V-TOL motors in a fixed-wing, and assigned missions to the aviation body, hence judged mission accuracy using the actual flight test. The design process and the mission evaluation process employed in this study can be utilized on the development of various unmanned aerial vehicle.