High-order expansions of multi-revolution elliptic Halo orbits in the elliptic restricted three-body problem

Key Points

• High-order expansions provide significant accuracy for predicting halo orbit trajectories and stability.
• The findings highlight novel solutions relevant for satellite missions and space exploration.
• Analysis employs mathematical modeling of the elliptic restricted three-body problem to derive new orbits.
• Anticipated advancements could enhance mission design, but require further investigation in complex orbital dynamics.