Relative CR3BP Dynamics

Author: Tianjiang Shuo

Website: https://cislunarspace.cn

Definition

Modeling and analysis of relative orbital motion between two spacecraft within the Circular Restricted Three-Body Problem framework.

Application Value

In orbit design and optimization, this concept is used to analyze spacecraft motion characteristics in the cislunar multi-body gravitational field, providing a theoretical basis for low-energy transfer trajectory design.

  • Lorillo Stability Criterion
  • Stable Eigenvector
  • Lunar Fly-by Method
  • Reachability Set

References

  • Cuevas del Valle 等 - 2023 - Optimal floquet stationkeeping under the relative dynamics of the three-body problem
Improve this page
Last Updated:
Contributors: ouyangjiahong, Ou Yang Jiahong