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Lunar landing trajectory design based on invariant manifold

โœ Scribed by Sheng-ping Gong; Jun-feng Li; He-xi Baoyin; Yun-feng Gao


Book ID
106345995
Publisher
Springer
Year
2007
Tongue
English
Weight
564 KB
Volume
28
Category
Article
ISSN
0253-4827

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The safety of astronauts would be severely threatened if the lunar-landing spacecraft were under an emergency during the near moon phase of flight, which was far from the Earth. For the problem of mission abort caused by the main engine (service propulsion system, SPS) failure during lunar orbit ins