Spatial Bi-Circular Model, SBCM
Author: Tianjiang Shuo
Website: https://cislunarspace.cn
Definition
An analytical four-body model including gravitational forces from the Sun, Earth and Moon, assuming the Earth-Moon barycenter moves in Keplerian circular motion around the Sun, and the lunar orbital plane has an inclination of 5°9′ relative to the ecliptic plane, used for studying low-energy Earth-Moon transfer trajectories.
Application Value
This concept has application value in cislunar space research and engineering practice, helping to understand core principles of the field.
Related Concepts
- Monte Carlo Trajectory Shooting, MCTS
- Powered Lunar Flyby, PLF
- Planar Circular Restricted Three-Body Problem, PCRTBP
- Insertion Delta-V
References
- Xu 等 - 2013 - On the construction of low-energy cislunar and trans-lunar transfers based on the libration points.
