SNUGLITE-III

Development of an Autonomous Rendezvous Orbit Control System for SNUGLITE-III CubeSat Using Real-Time Kinematic Based Precise Relative Navigation
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Efficient Integer Ambiguity Resolution Techniques for RTK-Based Relative Navigation in the SNUGLITE-III CubeSat Rendezvous Mission
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Precise GPS Relative Navigation for SNUGLITE-III CubeSat Rendezvous Mission: Overcoming Challenges in Precision and Efficiency
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Enhancing Real-Time Kinematic-Based Relative Navigation for CubeSat Rendezvous: Ambiguity Dilution of Precision Perspective on Integer Ambiguity Resolution
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Media Report on Sep 26, 2024
  • Title: SNUGLITE-III CubeSat Release
  • Source: Newsis; 머니투데이; 세계일보; 연합뉴스; 이데일리
  • Language: Korean
  • Tag: SNUGLITE-III
Sep 26, 2024 12:00 AM
Media Report on Sep 26, 2024
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
PDF Project
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
PDF Project