A MISOCP-SCP two-stage framework enables solar sail station-keeping in eLLOs for at least one year without propellant by leveraging predictable eccentricity vector behavior.
Analysis of lifetime extension capabilities for CubeSats equipped with a low-thrust propulsion system for Moon missions.Acta Astronautica, 160:558–571, July 2019
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Station-Keeping Approach for Extremely Low Lunar Orbits with Solar Sailing
A MISOCP-SCP two-stage framework enables solar sail station-keeping in eLLOs for at least one year without propellant by leveraging predictable eccentricity vector behavior.