Dual-path neural network learning method for free-return orbit integrating dynamic characteristics
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V412.4

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    Abstract:

    The free-return orbit serves as the preferred orbital scheme for crewed spacecraft in Earth-Moon transfers, yet its design involves stringent constraints and significant initial-value dependency in existing algorithms. This study addresses the Earth-Moon transfer trajectory planning for manned lunar exploration by proposing a dual-path neural network learning method to optimize free-return orbit initialization. First, a free-return orbit design framework is established, and the near-earth solution space characteristics are analyzed. Second, integrating the spatial partitioning characteristics of ascending and descending orbital phase in solution spaces, a dual-path neural network architecture designed via parameter-correlated transformation is proposed to ensure the completeness of orbital solutions. Finally, utilizing astromaster of Aerospace Tool Kit, the Earth-Moon free-return orbit planning under the dual-path network learning-based initialization method is implemented and validated through simulation. The results provide an effective reference for mitigating initial-value dependency in manned lunar mission orbit design.

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History
  • Received:March 28,2025
  • Revised:May 27,2025
  • Adopted:May 20,2025
  • Online: May 27,2025
  • Published:
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