Paper-Conference

Precise GPS Relative Navigation for SNUGLITE-III CubeSat Rendezvous Mission: Overcoming Challenges in Precision and Efficiency
Project
Low-Cost Satellite Angular Velocity Determination Method through Optical Flow Tracking Based on Flownet
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
Single Frequency RTK Relative Navigation for Autonomous Formation Flying Mission of SNUGLITE-III CubeSat
This study addresses the challenge of real-time kinematics (RTK) relative navigation for CubeSats engaged in autonomous formation …
Project DOI
Verification of Space GPS Receiver Navigation Performance Based on Full-Orbit Navigation Solutions of CubeSat
This study verifies navigation performance of in-house developed space GPS receiver using full-orbit onboard navigation solutions of …
Project DOI
Verification of Space GPS Receiver Navigation Performance Using a Cube Satellite
SNUGLITE(Seoul National University GNSS Laboratory Satellite) is 2U-size Low Earth Orbit (LEO) CubeSat (U-class spacecraft). Attitude …
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Development and Verification of Attitude Determination and Control Algorithm for SNUGLITE Cube Satellite
This study demonstrates the validation of the in-house developed space GPS receiver using a cube satellite called Seoul National …
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