Exploiting manifolds of L-1 halo orbits for end-to-end Earth-Moon low-thrust trajectory design
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Singh, S. K., Anderson, B. D., Taheri, E., & Junkins, J. L.
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Singh, Sandeep K||Anderson, Brian D||Taheri, Ehsan||Junkins, John L
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Bi-circular Model
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Cislunar Trajectory
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Halo Orbits
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Indirect Methods
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Invariant Manifolds
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Low-thrust
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Minimum-time
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Optimal Control
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http://dx.doi.org/10.1016/j.actaastro.2021.03.017