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.
NanoSail-D: A solar sail demonstration mission.Acta Astronautica, 68(5):571–575, March 2011
2 Pith papers cite this work. Polarity classification is still indexing.
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UNVERDICTED 2representative citing papers
Simulation study finds a size-dependent relation between solar sail area and asteroid diameter for the frequency of attitude changes needed to station-keep around irregular gravity fields using a decision-tree guidance agent.
citing papers explorer
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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.
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A study on station-keeping over irregularly shaped asteroids with different sized solar sails
Simulation study finds a size-dependent relation between solar sail area and asteroid diameter for the frequency of attitude changes needed to station-keep around irregular gravity fields using a decision-tree guidance agent.