Lambert Flight Time Theorem

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

Definition

Theorem describing the relationship between transfer orbit flight time and orbital parameters between two given points

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

• 任萱 - 1988 - 人造地球卫星轨道力学