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Displaced orbits around $L_2$ point in Earth-Moon system are useful for lunar far-side communications. We design hybrid sail displaced orbits in the Earth-Moon elliptic restricted three-body system and propose a backstepping controller for orbital maintenance while the overall propellant consumption of the solar electric thruster is minimized.

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This page is a summary of: Hybrid Sail Displaced Orbits Around L2 Point in the Elliptic Earth-Moon System, Journal of Guidance Control and Dynamics, February 2019, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.g003748.
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