Interior Stable Manifold

Author: Tianjiang Shuo

Website: https://cislunarspace.cn

Definition

The half of the stable manifold of a halo orbit that extends toward the Moon. A spacecraft on the interior stable manifold moves inward from the halo orbit and can be used to design interior transfer trajectories that pass near the Moon.

Application Value

This term在cislunar space missions中has important application value. In orbit design, it can be used foroptimizing transfer trajectories, reducing mission fuel consumption. In attitude control and dynamics analysis, it helps understandthe motion characteristics of spacecraft in complex gravitational fields, providing theoretical support for mission planning. In navigation and orbit determination, methods based on this termcan improve orbit prediction accuracy, supporting the development of autonomous navigation algorithms.

  • Periodicity Conditions in Relative Orbital Motion
  • Helix Formation
  • Energy Dissipation Method
  • Unstable Manifold

References

  • /home/ouyangjiahong/Downloads/地月空间相关/output/Parker和Born - 2008 - Direct lunar halo orbit transfers/hybrid_auto/Parker和Born - 2008 - Direct lunar halo orbit transfers.md
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Contributors: ouyangjiahong, Ou Yang Jiahong