Planar Circular Restricted Three-Body Problem, PCRTBP
Author: Tianjiang Shuo
Website: https://cislunarspace.cn
Definition
A dynamics problem where two primary bodies move in coplanar circular orbits, and the spacecraft moves in the same plane under the gravitational action of both.
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
- Insertion Delta-V
- Momentum Integral, MI
References
- Chao 等 - 2022.