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http://dx.doi.org/10.12985/ksaa.2018.26.4.122

Flying-wing Type Compound Drone Design and Mission Accuracy Analysis  

Sung, Dong-gyu (건국대학교 항공우주정보시스템공학과)
Koh, Eun-hak (건국대학교 항공우주정보시스템공학과)
Kim, Ju-chan (건국대학교 항공우주정보시스템공학과)
Nam, Yong-hyeon (건국대학교 항공우주정보시스템공학과)
Lee, Jeong-ho (건국대학교 항공우주정보시스템공학과)
Lee, Jae-seung (건국대학교 항공우주정보시스템공학과)
Lee, Chan-bin (건국대학교 항공우주정보시스템공학과)
Jeon, Yeong-bae (건국대학교 항공우주정보시스템공학과)
Choi, Cheol-kyun (건국대학교 대학원 항공우주정보시스템공학과)
Lee, Jae woo (건국대학교 항공우주정보시스템공학과)
Publication Information
Journal of the Korean Society for Aviation and Aeronautics / v.26, no.4, 2018 , pp. 122-128 More about this Journal
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.
Keywords
compound drone; lift fan; fixed wing; vertical takeoff and landing; mission accuracy;
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  • Reference
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