PhD in Aerospace Engineering with strong interpersonal skills developed through extensive team project experiences. Demonstrated ability to lead teams effectively and collaborate as a valuable team member.Special expertise in the following areas:
Interests
- GPS Applications in LEO
- RTK Relative Navigation
- CubeSat
- Attitude Orbit Control System (AOCS)
- Hardware-In-the-Loop Simulation (HILS)
Education
PhD in Aerospace Engineering, 2024
Seoul National University, Seoul, Korea
MSc in Mechanical and Aerospace Engineering, 2019
Seoul National University, Seoul, Korea
BSc in Mechanical and Control Engineering, 2016
Handong Global University, Pohang, Korea
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
- Low-Cost Satellite Angular Velocity Determination Method through Optical Flow Tracking Based on Flownet
- Ultra-Low Cost Hardware-In-the-Loop Simulation for CubeSat Platform: Implementation and Verification of Momentum Wheel-Based Attitude Control
- Enhancing Real-Time Kinematic-Based Relative Navigation for CubeSat Rendezvous: Ambiguity Dilution of Precision Perspective on Integer Ambiguity Resolution
- Precise GPS Relative Navigation for CubeSat Rendezvous
- Analysis of Orbit Control System Using Aerodynamic Drag for Propellant-less Rendezvous Mission of SNUGLITE-III CubeSat
- Highly Efficient Real-Time Kinematic-Based Precise Relative Navigation for Autonomous Rendezvous 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
- Development of Hardware-In-the-Loop Simulation for CubeSat Platform: Focusing on Magnetometer and Magnetorquer
- 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
- Precise in-orbit relative navigation technique for rendezvous mission of CubeSats using only GPS receivers
- 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
- Probabilistic Determination Algorithm for Detumbling and Angular Rate Convergence using a Three-Axis Magnetometer
- HILS Verification of SNUGLITE-II Cube-Satellite Attitude Control System Equipped with Reaction Wheel and Magnetorquer
- SNUGLITE-II 큐브위성의 전력계 분석
- Single Frequency GPS Relative Navigation for Autonomous Rendezvous and Docking Mission of Low-Earth Orbit Cube-Satellites
- 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
- 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
- HILS Verification of Low Earth Orbit Cube-Satellite Attitude Determination and Control System Using Helmholtz Cage
- 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
- Altitude Estimation by Integrating Barometer with Accelerometer
- 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
- Vertical Channel Damping Loop Design for Autonomous Vehicle with Altitude Controller