Coupling of RTBPs

Author: Tianjiang Shuo

Website: https://cislunarspace.cn

Definition

Decoupling a four-body problem into two coupled restricted three-body problems (e.g., Sun-Earth+Moon system) for analysis.

Application Value

This concept provides fundamental support in cislunar space research and mission design. In practical applications, the appropriate analysis method should be selected based on specific mission scenarios and constraints.

References

  • Belló 等 - 2010 - Invariant manifolds, Lagrangian trajectories and space mission design
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Contributors: ouyangjiahong, Ou Yang Jiahong