Precise GPS Relative Navigation for SNUGLITE-III CubeSat Rendezvous Mission: Overcoming Challenges in Precision and EfficiencyOct 1, 2024·Hanjoon ShimBu-gyeom KimYonghwan BaeChangdon Kee,In Hoi Koo· 0 min readLast updated on Oct 1, 2024 AuthorsHanjoon ShimPh.DAuthorsBu-gyeom KimPh.DAuthorsYonghwan BaePh.DAuthorsChangdon KeeProfessor Emeritus← Low-Cost Satellite Angular Velocity Determination Method through Optical Flow Tracking Based on Flownet Oct 1, 2024Expanding Network RTK Coverage Using an Ionospheric-Free Combination and Kriging for Tropospheric Delay Sep 1, 2024 →