Transfer between the planar Lyapunov orbits around the Earth–Moon L2 point using low-thrust engine
Author:
Funder
China Scholarship Council
Russian Science Foundation
Publisher
Elsevier BV
Subject
Aerospace Engineering
Reference63 articles.
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3. Low-thrust trajectory design with convex optimization for libration point orbits;Kayama,2021
4. Low-Energy Lunar Trajectory Design, Vol. 12;Parker,2014
5. Design and analysis of a direct transfer trajectory from a near rectilinear halo orbit to a low lunar orbit;Lu;Adv. Space Res.,2021
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