SNUGLITE-I

Development of Hardware-In-the-Loop Simulation for CubeSat Platform: Focusing on Magnetometer and Magnetorquer
This study is aimed at addressing the practical challenges of conducting hardware-in-the-loop simulation (HILS) for a CubeSat attitude …
PDF Project DOI
Development of Hardware-In-the-Loop Simulation for CubeSat Platform: Focusing on Magnetometer and Magnetorquer
Probabilistic Determination Algorithm for Detumbling and Angular Rate Convergence using a Three-Axis Magnetometer
This paper proposes an algorithm to determine the convergence of angular rate by using B-dot measurements from a 3-axis magnetometer …
PDF Project DOI
Long-Tem Operational Results and Analysis of the SNUGLITE Cube-Satellite
PDF Project
In-Orbit Results and Attitude Analysis of the SNUGLITE Cube-Satellite
SNUGLITE (Seoul National University Global navigation satellite system Laboratory satellITE) is a two-unit cube satellite (CubeSat) …
PDF Project DOI
In-Orbit Results and Attitude Analysis of the SNUGLITE Cube-Satellite
Verification of Space GPS Receiver Navigation Performance Using a Cube Satellite
SNUGLITE(Seoul National University GNSS Laboratory Satellite) is 2U-size Low Earth Orbit (LEO) CubeSat (U-class spacecraft). Attitude …
Project DOI
Design of Helmholtz Cage for Verification of Attitude Determination and Control System SNUGLITE Cube-Satellite
PDF Project
Orbit Determination and Performance Analysis by Using Navigation Solution Received from SNUGLITE Cube Satellite
PDF Project
Analysis of On-board GPS Receiver Navigation Solutions for SNUGLITE Cubesat
PDF Project
Attitude Determination and Control System Verification of SNUGLITE Cube-Satellite on Orbit
PDF Project
Development and Launch Preparation of SNUGLITE Cube-satellite Observing Space Weather and Earthquake using GNSS signals
PDF Project