Dynamics Modeling and Induced Vibration Analysis of Momentum Wheel for Control Moment Gyros von PARK, Jong-Oh, OH, Shi-Hwan, YONG, Ki-Lyuk, IM, Young-Do

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Three-axis attitude determination using incomplete vector observations von Lee, Seon-Ho, Ahn, Hyo-Sung, Yong, Ki-Lyuk

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Feasibility study & system conceptual design for the spherical actuator von Geeyong Park, Hyungjoo Yoon, Dae-kwan Kim, Ki-Lyuk Yong, Petrov, S. E.

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Simulation Model Development Environment using 3 Dimensional Model-Based Approach von Hoon-Hee Lee, Cheol-Hea Koo, Ki-Lyuk Yong, Irvine, M.

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저궤도 위성용 저정밀 태양센서 선행모델 및 인증모델 개발 von 김용복, 조영준, 용기력, 우형제, Kim, Yong-Bok, Jo, Young-Jun, Yong, Ki-Lyuk, Woo, Hyung-Je

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반작용휠 속도측정방법의 오차 분석 von 오시환, 이혜진, 이선호, 용기력, Oh, Shi-Hwan, Lee, Hye-Jin, Lee, Seon-Ho, Yong, Ki-Lyuk

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Development of Path finder Model and Qualified Model of Coarse Sun Sensor Assembly for Low Earth Orbit Satellite von Kim, Yong-Bok, Jo, Young-Jun, Yong, Ki-Lyuk, Woo, Hyung-Je

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Error Analysis of Reaction Wheel Speed Detection Methods von Oh, Shi-Hwan, Lee, Hye-Jin, Lee, Seon-Ho, Yong, Ki-Lyuk

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정상 임무운용 상태에서 다목적실용위성 2호 탑재체에 대한 태양 입사각 분석 von 김응현, 용기력, 이상률, Eunghyun Kim, Ki-Lyuk Yong, Sang-Ryool Lee

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Sun Incidence Angle Analysis of KOMPSAT-2 Payload during Normal Mission Operations von Eunghyun Kim, Ki-Lyuk Yong, Sang-Ryool Lee

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KOMPSAT-1 Satellite Orbit Control using GPS Data von Jin-Ho Lee, Myung-Jin Baek, Ja-Chun Koo, Ki-Lyuk Yong, Young-Keun Chang

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저궤도 위성용 저정밀 태양센서 선행모델 및 인증모델 개발 von 김용복, 조영준, 용기력, 우형제, Kim, Yong-Bok, Jo, Young-Jun, Yong, Ki-Lyuk, Woo, Hyung-Je

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반작용휠 속도측정방법의 오차 분석 von 오시환, 이혜진, 이선호, 용기력, Oh, Shi-Hwan, Lee, Hye-Jin, Lee, Seon-Ho, Yong, Ki-Lyuk

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Method for improving maneuverability and controllability by simultaneously applying both reaction wheel-based attitude controller and thruster-based attitude controller von Seo, Hyun Ho, Yong, Ki Lyuk, Oh, Shi Hwan, Choi, Hong Taek, Lee, Seon Ho, Yim, Jo Ryeong, Kim, Yong Bok, Lee, Hye Jin

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Method for improving maneuverability and controllability by simultaneously applying both reaction wheel-based attitude controller and thruster-based attitude controller von SEO, HYUN HO, YIM, JO RYEONG, LEE, SEON HO, YONG, KI LYUK, OH, SHI HWAN, CHOI, HONG TAEK, KIM, YONG BOK, LEE, HYE JIN

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Method for improving maneuverability and controllability by simultaneously applying both reaction wheel-based attitude controller and thruster-based attitude controller von SEO, HYUN HO, YIM, JO RYEONG, LEE, SEON HO, YONG, KI LYUK, OH, SHI HWAN, CHOI, HONG TAEK, KIM, YONG BOK, LEE, HYE JIN

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System for improving maneuverability and controllability by simultaneously applying both reaction wheel-based attitude controller and thruster-based attitude controller von SEO, HYUN HO, YIM, JO RYEONG, LEE, SEON HO, YONG, KI LYUK, OH, SHI HWAN, CHOI, HONG TAEK, KIM, YONG BOK, LEE, HYE JIN

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Three-dimensional misalignment correction method of attitude angle sensor using single image von SEO, HYUN HO, YIM, JO RYEONG, LEE, SEON HO, YONG, KI LYUK, OH, SHI HWAN, LEE, HYE JIN, KIM, YONG BOK, CHOI, HONG TAEK

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Method for improving maneuverability and controllability by simultaneously applying both reaction wheel-based attitude controller and thruster-based attitude controller von CHOI HONG TAEK, YIM JO RYEONG, LEE HYE JIN, SEO HYUN HO, LEE SEON HO, OH SHI HWAN, YONG KI LYUK, KIM YONG BOK

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Method for improving maneuverability and controllability by simultaneously applying both reaction wheel-based attitude controller and thruster-based attitude controller von SEO, HYUN HO, YIM, JO RYEONG, LEE, SEON HO, YONG, KI LYUK, OH, SHI HWAN, CHOI, HONG TAEK, KIM, YONG BOK, LEE, HYE JIN

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