collaborators

1 paper

eess.SY2026

Low-Thrust Trajectory Optimization for Cubesat Lunar Mission: HORYU-VI

Omer Burak Iskender, Keck Voon Ling, Mengu Cho +2

This paper presents a low-thrust trajectory optimization strategy to achieve a near-circular lunar orbit for a CubeSat injected into a lunar flyby trajectory. The 12U CubeSat HORYU…