O-Jong Kim

Latest

Operation Results of SNUGLITE-II CubeSat: Convective 3D Observation and Precise Attitude Determination Using GPS Carrier Measurements
Development of Hardware-In-the-Loop Simulation for CubeSat Platform: Focusing on Magnetometer and Magnetorquer
Result of Satellite Telemetry Analysis of SNUGLITE-I CubeSat for 4 Years
Precise in-orbit relative navigation technique for rendezvous mission of CubeSats using only GPS receivers
Rendezvous Technology of SNU CubeSat (SNUGLITE-III) Using Only GPS Receivers
Probabilistic Determination Algorithm for Detumbling and Angular Rate Convergence using a Three-Axis Magnetometer
Single Frequency GPS Relative Navigation for Autonomous Rendezvous and Docking Mission of Low-Earth Orbit Cube-Satellites
Performance Analysis of GPS/GALLILEO-Based Attitude Determination for CubeSatellite
Real-time Differential GPS Relative Navigation System Implementation and Verification of KARDSAT Cube-Satllites for Autonomous Rendezvous and Docking Missions
A Preliminary Design of SNUGLITE-II Cube-Satellite for 3D Atmospheric Remote Sensing with GPS Radio Occultation
Long-Tem Operational Results and Analysis of the SNUGLITE Cube-Satellite
In-Orbit Results and Attitude Analysis of the SNUGLITE Cube-Satellite
Verification of Space GPS Receiver Navigation Performance Using a Cube Satellite
Design of Helmholtz Cage for Verification of Attitude Determination and Control System SNUGLITE Cube-Satellite
Orbit Determination and Performance Analysis by Using Navigation Solution Received from SNUGLITE Cube Satellite
Attitude Determination of Cube-Satellite using Multiple GPS Antennas
Relative Navigation for Autonomous Rendezvous and Docking of Nano-Satellite Based on DGPS
Analysis of On-board GPS Receiver Navigation Solutions for SNUGLITE Cubesat
Attitude Determination and Control System Verification of SNUGLITE Cube-Satellite on Orbit
Development and Launch Preparation of SNUGLITE Cube-satellite Observing Space Weather and Earthquake using GNSS signals
SNUGLITE Cubesat Ground Station Communication and Control System Operation Test
운용 시나리오를 고려한 SNUGLITE 큐브위성의 자세결정 및 제어 시스템 지상환경 HILS
Development and Verification of Attitude Determination and Control Algorithm for SNUGLITE Cube Satellite
Single-Axis Hardware in the Loop Experiment Verification of ADCS for Low Earth Orbit Cube-Satellite
Single-Axis Attitude Determination and Control System HILS Considering Ground Environment of SNUGLITE Cube-Satellite using Magnetoquer
위성항법 신호를 이용하여 우주환경관측 및 지진관측 수행을 위한 저궤도 큐브위성 개발