Propellant-Free Rendezvous Mission of SNUGLITE-III CubeSat: Orbit Control Using Aerodynamic Forces Mar 1, 2025· Jae Woong Hwang Hanjoon Shim Yonghwan Bae Changdon Kee , Jaegang Kim · 0 min read Last updated on Mar 1, 2025 Authors Jae Woong Hwang M.S Authors Hanjoon Shim Ph.D Authors Yonghwan Bae Ph.D Authors Changdon Kee Professor ← Onboard Implementation and Validation of RTK-Based Relative Navigation System for CubeSats Mar 1, 2025 SNUGLITE-III 큐브위성의 자율 편대비행 임무를 위한 위성 간 분리 후 상대 운동 분석 Jan 1, 2025 →