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We find that the spacecraft can use the invariant manifolds in three body model to change its orbital elements naturally and reduce the fuel consumption when capturing into a Keplerian orbit.
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This page is a summary of: Mars High Orbit Capture Using Manifolds in the Sun–Mars System, Journal of Guidance Control and Dynamics, July 2020, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.g004865.
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