SNUGLITE-III

Design and Ground Testing of an Electromagnetic Docking Mechanism for the SNUGLITE-III CubeSat
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System Design and Engineering Model Test Results of SNUGLITE-Ⅲ CubeSats for Formation Flying and Rendezvous-Docking Missions
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Media Report on Nov 07, 2025
  • Title: Separation and Reintegration in Orbit? The World’s First Ultra-Precision GPS-Enabled Thrustless Autonomous Orbit Control Test Satellite | SNUGLITE-III
  • Source: KARI TV (Youtube)
  • Language: Korean
  • Tag: SNUGLITE-III
Nov 7, 2025
Media Report on Nov 07, 2025
Development and Launch Preparation of SNUGLITE-III CubeSat Flight Model
Project
Enhancing Real-Time Kinematic-Based Relative Navigation for CubeSat Rendezvous: Ambiguity Dilution of Precision Perspective on Integer Ambiguity Resolution
This study addresses the practical challenges of real-time kinematic (RTK)-based precise relative navigation and integer ambiguity …
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Enhancing Real-Time Kinematic-Based Relative Navigation for CubeSat Rendezvous: Ambiguity Dilution of Precision Perspective on Integer Ambiguity Resolution
“Ground-Based Verification of GPS-Based Attitude Determination for the SNUGLITE-III Cube Satellite Engineering Model
Project
Design and Ground Testing of an Electromagnetic Docking Mechanism for the SNUGLITE-III CubeSat
Project
Implementation and Validation of High-Precision GPS-Based Relative Navigation for the SNUGLITE-III CubeSat in Autonomous Rendezvous and Docking
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Efficient GNSS-Based Attitude Determination and Integer Ambiguity Resolution for 3U CubeSats
This paper presents the design and validation of a Global Navigation Satellite System (GNSS)-based attitude determination algorithm …
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Onboard Implementation and Validation of RTK-Based Relative Navigation System for CubeSats
This paper presents the first onboard Real-Time Kinematic (RTK)-based relative navigation system designed specifically for CubeSat …
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