Bicircular Restricted Four-Body Problem, BCR4BP
Author: Tianjiang Shuo
Website: https://cislunarspace.cn
Definition
A four-body model that introduces perturbation of a third body (such as the Moon or Sun) on the restricted three-body problem. In this model, two primary bodies orbit each other while a third body moves in a circular orbit around one primary, making the system non-autonomous. The paper uses two variants: the Sun-Earth-Moon BCR4BP and the Earth-Moon-Sun BCR4BP.
Application Value
This provides a fundamental theoretical framework for cislunar dynamics modeling and analysis, serving as a mathematical tool for studying spacecraft motion.
Related Concepts
- Monte Carlo Trajectory Shooting, MCTS
- Powered Lunar Flyby, PLF
- Planar Circular Restricted Three-Body Problem, PCRTBP
- Insertion Delta-V
References
- Campana 等 - 2024 - Low-energy earth–moon transfers via theory of functional connections and homotopy.
