SNUGLITE-III

Propellant-Free Rendezvous Mission of SNUGLITE-III CubeSat: Orbit Control Using Aerodynamic Forces
This paper addresses a challenging orbit control problem for in-orbit demonstration of propellant-free Rendezvous Proximity Operation …
Project DOI
Analysis of Relative Motion after Inter-Satellite Separation for SNUGLITE-III Autonomous Formation Flying Mission
Project DOI
Development of an Autonomous Rendezvous Orbit Control System for SNUGLITE-III CubeSat Using Real-Time Kinematic Based Precise Relative Navigation
Project
Efficient Integer Ambiguity Resolution Techniques for RTK-Based Relative Navigation in the SNUGLITE-III CubeSat Rendezvous Mission
Project
Development and Test Results of the SNUGLITE-III Cube-satellite Engineering Model
Project
Precise GPS Relative Navigation for SNUGLITE-III CubeSat Rendezvous Mission: Overcoming Challenges in Precision and Efficiency
Project
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
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