Halo Orbit Insertion

Author: Tianjiang Shuo

Website: https://cislunarspace.cn

Definition

The process of applying the second impulse to introduce a spacecraft from a transfer trajectory into a target halo orbit. The insertion location and velocity components are design unknowns, determined through differential evolution optimization.

Application Value

The 光环轨道插入 concept is applied in cislunar space research, providing technical support or analytical methods for lunar exploration missions.

  • (No related concepts available)

References

  • Neelakantan和Ramanan - 2022 - Two-impulse transfer to multi-revolution halo orbits in the Earth–moon elliptic restricted three bod