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.
Convex Approach to Three-Dimensional Launch Vehicle Ascent Trajectory Optimization.Journal of Guidance, Control, and Dynamics, 44(6):1116–1131, 2021
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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.