Real Force Model

Author: Tianjiang Shuo Website: https://cislunarspace.cn

Definition

A realistic force model of the Earth-Moon system that includes the Moon's orbital eccentricity and solar gravitational perturbation, closer to actual flight conditions than the CRTBP model.

Application Value

This orbital design method can be applied to transfer trajectory design, orbit keeping, and mission planning in cislunar space missions, improving spacecraft performance and mission flexibility.

References

• Liu 等 - 2014 - Application of two special orbits in the orbit determination of lunar satellites