Orbit Design Elements of Chang’e 5 Mission
Keyword(s):
The three key orbit design technologies employed in the Chang’e 5 mission are identified and discussed in this paper: orbit design for lunar orbit rendezvous and docking, orbit design for precision lunar landing and inclination optimization, and orbit design for Moon-to-Earth transfer. First, an overview of the Chang’e 5 mission profile is presented, which is followed by detailed discussions of the three key orbit design technologies, including an introduction of the tracking-based orbit design methodology. Flight data are provided to demonstrate the correctness of the designs.
2016 ◽
Vol 88
(6)
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pp. 866-872
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Keyword(s):
Keyword(s):
2021 ◽
Vol ahead-of-print
(ahead-of-print)
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2017 ◽
Vol 10
(1)
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pp. 40-65
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2016 ◽
Vol 29
(6)
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pp. 04016043
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2018 ◽
Vol 90
(2)
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pp. 302-311
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2020 ◽
Vol ahead-of-print
(ahead-of-print)
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