초소형 쿼드로터 개발을 위한 기체형상 설계변경

An ultra light quad-rotor is utilized in various areas for military and commercial purpose. Especially, the airframe shape is designed with various airframe size, weight and purpose. In this paper, the initial airframe shape of the quad-rotor was designed and manufactured. Flight test was conducted...

Full description

Saved in:
Bibliographic Details
Published in한국항공운항학회지 Vol. 25; no. 4; pp. 44 - 51
Main Authors 박대진, 이상철, 박생진, 송태훈, Park, Dae-Jin, Lee, Sangchul, Park, Saeng-Jin, Song, Tae-Hun
Format Journal Article
LanguageKorean
Published 한국항공운항학회 01.12.2017
Subjects
항공우주공학
Online AccessGet full text

Cover

More Information
Summary:An ultra light quad-rotor is utilized in various areas for military and commercial purpose. Especially, the airframe shape is designed with various airframe size, weight and purpose. In this paper, the initial airframe shape of the quad-rotor was designed and manufactured. Flight test was conducted for the quad-rotor. The design modification of airframe shape was conducted to meet design requirement. By changing design, weight of airframe structure was reduced and payloads were placed to the best position. By reinforcing ribs and reducing vehicle's legs, the durability of airframe structure was enhanced.
Bibliography:KISTI1.1003/JNL.JAKO201708260284046
ISSN:1225-9705
2466-1791