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Star Visibility Analysis for a Low Earth Orbit Satellite
Yim, Jo-Ryeong,Lee, Seon-Ho,Yong, Ki-Lyuk 한국우주과학회 2008 한국우주과학회보 Vol.17 No.2
Recently, star sensors have been successfully used as main attitude sensors for attitude control in many satellites. This research presents the star visibility analysis for star trackers and the goal of this analysis is to make sure that the star tracker
LIGHT CURVE ANALYSIS OF CW CEPHEI
YIM Jo RYEONG,KIM CHUN-HWEY,HAN WONYONG The Korean Astronomical Society 1996 Journal of The Korean Astronomical Society Vol.29 No.suppl1
The UBV observations of the close binary system CW Cephei were made from August 198:3 to December 1984 during 25 nights using the 61cm Boller and Chivens reflector at the Sobaeksan Astronomy Observatory. The new UBV light curves were analyzed with the recent Wilson-Devinney binary model. Our photometric solution for CW Cep were well consistent with those of Clausen &. Gimenez (1991). Using our photometric solution and Popper & Hill (1991) spectroscopic one, each absolute masses and radii of components for CW Cep were derived as 13.63 M$\bigodot$ and 5.83 R$\bigodot$ for the primary, and 12.18 M$\bigodot$ and 5.14 R$\bigodot$ for the secondary, respectively.
임조령(Jo Ryeong Yim),최홍택(Hong-Taek Choi) 한국항공우주연구원 2012 항공우주기술 Vol.11 No.2
본 기술논문에서는 고기동 고정밀 위성의 별 추적기 초기 점검 원격측정 데이터가 분석되었다. 최근에 발사된 위성은 고기동 고정밀 위성이므로 고도의 요구조건을 만족하기 위해 광학계, 전자부, 배플이 분리된 형태로 광학계 부분의 온도를 20 degC 근처로 유지하면서 저주파 오차 성능을 향상 시킨 프랑스 SODERN사의 SED36을 사용하였다. 본 논문에서는 위성으로부터 내려 받은 원격측정 데이터의 처리를 통해 초기 점검 상태, 요구 조건 만족 여부, 이상 현상 및 주요 임무 기동에서의 별 추적기 잡음각 성능 분석 결과를 제시하였다. This technical paper describes the analysis results of telemetry data for the initial activation of star trackers for an agile high accuracy low earth orbit satellite. The satellite was recently launched and is in the Launch and Early Operation Phases. It uses two SED36 star trackers manufactured by SODERN. The star tracker is separated by three parts, an optical head, an electronics box, and a baffle with maintaining optical head base plate temperature 20 degC in order to achieve the better performance in low frequency error. This paper presents the initial activation status, requirements and performance, anomaly occurrence, and noise equivalent angle performance analysis during the mission mode by processing the telemetry data.