Propellant-Free Rendezvous Mission of SNUGLITE-III CubeSat: Orbit Control Using Aerodynamic ForcesMar 1, 2025·Jae Woong HwangHanjoon ShimYonghwan BaeChangdon Kee,Jaegang Kim· 0 min readLast updated on Mar 1, 2025 AuthorsJae Woong HwangM.SAuthorsHanjoon ShimPh.DAuthorsYonghwan BaePh.DAuthorsChangdon KeeProfessor Emeritus← Onboard Implementation and Validation of RTK-Based Relative Navigation System for CubeSats Mar 1, 2025SNUGLITE-III 큐브위성의 자율 편대비행 임무를 위한 위성 간 분리 후 상대 운동 분석 Jan 1, 2025 →