Article-Journal

Ultra-Low Cost Hardware-In-the-Loop Simulation for CubeSat Platform: Implementation and Verification of Momentum Wheel-Based Attitude Control
Project
Enhancing Real-Time Kinematic-Based Relative Navigation for CubeSat Rendezvous: Ambiguity Dilution of Precision Perspective on Integer Ambiguity Resolution
Project
Highly Efficient Real-Time Kinematic-Based Precise Relative Navigation for Autonomous Rendezvous CubeSat
This study addresses the practical challenges associated with real-time kinematic relative navigation for cube satellites (CubeSats) …
Project Video DOI
Highly Efficient Real-Time Kinematic-Based Precise Relative Navigation for Autonomous Rendezvous CubeSat
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 …
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Development of Hardware-In-the-Loop Simulation for CubeSat Platform: Focusing on Magnetometer and Magnetorquer
Precise in-orbit relative navigation technique for rendezvous mission of CubeSats using only GPS receivers
This paper proposes a global positioning system (GPS) based relative navigation algorithm for CubeSats that perform autonomous …
Project DOI
Precise in-orbit relative navigation technique for rendezvous mission of CubeSats using only GPS receivers
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 …
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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) …
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In-Orbit Results and Attitude Analysis of the SNUGLITE Cube-Satellite