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Transfers Orbit Design from Lunar Frozen Orbit to Near Rectilinear Halo Orbit

LIANG Guoliang YANG Hongwei

深空探测学报(中英文)2026，Vol.13Issue(2)：P.151-161,11.

深空探测学报(中英文)2026，Vol.13Issue(2)：P.151-161,11.DOI:10.3724/j.issn.2096-9287.2026.20250106

LIANG Guoliang ¹YANG Hongwei¹

作者信息

1. College of Astronautics,Nanjing University of Aeronautics and Astronautics,Nanjing 211106,China
折叠

trajectory design and optimization/Lunar Frozen Orbit/Near Rectilinear Halo Orbit

航空航天

LIANG Guoliang,YANG Hongwei..Transfers Orbit Design from Lunar Frozen Orbit to Near Rectilinear Halo Orbit[J].深空探测学报(中英文),2026,13(2):P.151-161,11.

Supported by the National Natural Science Foundation of China(12372046) （12372046）

Natural Science Foundation of Jiangsu Province(BK20220130)。（BK20220130）

ISSN：2096-9287

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