Yonghwan Bae

Latest

Development of an Autonomous Rendezvous Orbit Control System for SNUGLITE-III CubeSat Using Real-Time Kinematic Based Precise Relative Navigation
Efficient Integer Ambiguity Resolution Techniques for RTK-Based Relative Navigation in the SNUGLITE-III CubeSat Rendezvous Mission
Precise GPS Relative Navigation for SNUGLITE-III CubeSat Rendezvous Mission: Overcoming Challenges in Precision and Efficiency
Ultra-Low Cost Hardware-In-the-Loop Simulation for CubeSat Platform: Implementation and Verification of Momentum Wheel-Based Attitude Control
Analysis of Orbit Control System Using Aerodynamic Drag for Propellant-less Rendezvous Mission of SNUGLITE-III CubeSat
Development of Orbit Control System Using Aerodynamic Drag for Autonomous Formation Flying Mission of SNUGLITE-Ⅲ
Critical Design of SNUGLITE-III Cube-satellite for Formation Flight Mission
Development of GPS Precise Relative Navigation System for Autonomous Rendezvous-Docking Mission of SNUGLITE-III CubeSat
Verification and Hardware Implementation of Single-Frequency RTK-Based Precise Relative Navigation for SNUGLITE-III CubeSat
Analysis of Relative Motion after Inter-Satellite Separation for Formation Flying Mission of SNUGLITE-Ⅲ
Ground Experiments and Performance Analysis of SNUGLITE-Ⅲ Cube Satellite for GPS Attitude Determination
Verification Technique for the Single-Frequency RTK Relative Navigation Algorithm of SNUGLITE-III CubeSat Performing Autonomous Formation Flying
Operation Results of SNUGLITE-II CubeSat: Convective 3D Observation and Precise Attitude Determination Using GPS Carrier Measurements
Single Frequency RTK Relative Navigation for Autonomous Formation Flying Mission of SNUGLITE-III CubeSat
Critical Design of Electrical Power Subsystem of SNUGLITE-III CubeSat
Result of Satellite Telemetry Analysis of SNUGLITE-I CubeSat for 4 Years
Preliminary Design of Electrical Power Subsystem of SNUGLITE-III Cube Satellite
Preliminary Design of SNUGLITE-III Cube-satellite for Formation Flight based GPS Radio Occultation
Real-time Software Verification Technique of Attitude Determination and Control System for CubeSat
Verification of Space GPS Receiver Navigation Performance Based on Full-Orbit Navigation Solutions of CubeSat
Initial Operation Result of SNUGLITE-II Cube-Satellite
Rendezvous Technology of SNU CubeSat (SNUGLITE-III) Using Only GPS Receivers
SNUGLITE-II Cubesat Ground Station Configuration and Ground Operation Test
Integer Ambiguity Estimation for SNUGLITE-II Cube Satellite GNSS-based Attitude Determination
Quaternion-based Optimal Controller Design for SNUGLITE-II Cube Satellite Attitude Control System
Centimeter-level Precision Smartphone Navigation Using RTK
Performance Analysis of GPS/GALLILEO-Based Attitude Determination for CubeSatellite
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
Analysis of On-board GPS Receiver Navigation Solutions for SNUGLITE Cubesat
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