Journal of Aerospace System Engineering (항공우주시스템공학회지)
- Volume 3 Issue 3
- /
- Pages.13-16
- /
- 2009
- /
- 1976-6300(pISSN)
- /
- 2508-7150(eISSN)
Implementation and Application of the Control Surface Deflection Angle measuring device for UAV using Potentiometer
전위차계를 이용한 무인항공기 조종면 변위 측정 장치 구현 및 적용
- Kim, Ji-Chul ;
- Choi, Il-Gyu ;
- Gong, Sung-Chul ;
- Cheon, Dong-Ik ;
-
Lee, Sangchul
;
-
Oh, Hwa-Suk
;
- Kang, Min-young
- 김지철 (한국항공대학교 항공우주공학과) ;
- 최일규 (한국항공대학교 항공우주공학과) ;
- 공성철 (한국항공대학교 항공우주공학과) ;
- 전동익 (한국항공대학교 항공우주공학과) ;
-
이상철
(한국항공대학교 기계공학부)
;
-
오화석
(한국항공대학교 기계공학부)
;
- 강민영 ((주) 인텔레인)
- Published : 2009.09.30
Abstract
Aircraft flight control surfaces which are one of the most important elements of safety allow a pilot to adjust and control the aircraft's flight attitude. This paper is described of the control surface deflection angle measuring device. Data analysis through ground test and flight test can provide reliability of this device using the present system. It is also shown that measuring system is capable of detecting failure of control surfaces.