Lee, Sangwon, "Development of Attitude Determination and Control and Thrust Modulation Algorithms for Formation Flying of the SNIPE Nano-Satellite"
, 2018
송민섭, "Development and Performance Verification of Ephemeris Generator for Korean Pathfinder Lunar Orbiter"
, 2018
황혜원, "Precise Orbit Determination of LEO Satellites with Optical Observations Using Batch Filter"
, 2018
강석주, "SNIPE 나노위성 임무를 위한 편대 비행 시나리오 설계 및 분석"
, 2018
현정훈, "시각 센서를 이용한 위성 상대 위치/자세 추정 알고리즘 분석 및 검증"
, 2018
김민식, "시험용 달 궤도선의 정밀 궤도결정을 위한 DSN 관측 모델 개발 및 검증"
, 2018
신범준, "전자광학감시체계를 활용한 정지궤도 위성의 정밀궤도결정 및 분석"
, 2018
Lee,Jongwoo, "Relative Orbit Estimation with Laser-Based Intermittent Measurement for Formation Flying Spacecraft"
, 2018
Lee,Youngro, "Numerical analysis of the relative orbit control strategy of the CANYVAL-X mission"
, 2018
Lee, Jeongah, "Orbit Design of the Lunar Impactor CubeSat Measuring Local Magnetic Field and the Lunar Orbiter CubeSat Implementing Space Internet Technology,"
, 2017
Kim, HyunJeong, "Development of the Data Simulation Module of the Flight Dynamics Subsystem for Korea Pathfinder Lunar Orbiter,"
, 2016
Song, Youngbum, "Development of Flight Software for CANYVAL-X Cubesat Mission,"
, 2016
이은지, "Design and construction of communication system and ground station for CANYVAL-X cubesat"
, , 2015
최정민 , "Orbit determination of Korea regional navigation satellite system based on inter-satellite link"
, 2014
정승연 , "A preliminary design of a 5-DOF hardware simulator for spacecraft formation flying"
, 2014
김민희 , "Performance analysis and general-purpose module development of root-finding algorithms for spacecraft trajectory design"
, 2014
Hwang, Joo-Yeon , "Implementation of LARES spin model and its analysis"
, 2014
김경하 , "Fuel optimization for altitude maintenance of Low-Earth-Orbit(LEO) spacecraft by combining direct and indirect methods"
, 2014
Jung, Shinwon , "Relative position determination in real-time using inter-satellite laser ranging"
, 2013
Park, Jong Su , "An Analytical Method for the Altitude Maintenance of LEO Satellite with Constrained Eccentricity Using the Low-Thrust"
, 2011
