SNUGLITE-III

Analysis of Orbit Control System Using Aerodynamic Drag for Propellant-less Rendezvous Mission of SNUGLITE-III CubeSat
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 Orbit Control System Using Aerodynamic Drag for Autonomous Formation Flying Mission of SNUGLITE-Ⅲ
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Critical Design of SNUGLITE-III Cube-satellite for Formation Flight Mission
PDF Project
Development of GPS Precise Relative Navigation System for Autonomous Rendezvous-Docking Mission of SNUGLITE-III CubeSat
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Media Report on Mar 13, 2024
  • Title: Launching Ceremony of the Republic of Korea Space Industry Cluster (Invited Event)
  • Source: Ministry of Science and ICT, Republic of Korea)
  • Language: Korean
  • Tag: SNUGLITE-III
Mar 13, 2024
Media Report on Mar 13, 2024
Verification and Hardware Implementation of Single-Frequency RTK-Based Precise Relative Navigation for SNUGLITE-III CubeSat
In this paper, we address the verification and hardware implementation challenges of real-time kinematics (RTK)-based precise relative …
Project DOI
Analysis of Relative Motion after Inter-Satellite Separation for Formation Flying Mission of SNUGLITE-Ⅲ
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Ground Experiments and Performance Analysis of SNUGLITE-Ⅲ Cube Satellite for GPS Attitude Determination
PDF Project
Verification Technique for the Single-Frequency RTK Relative Navigation Algorithm of SNUGLITE-III CubeSat Performing Autonomous Formation Flying
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