Lambert's Three-Body Problem, L3BP

Author: Tianjiang Shuo

Website: https://cislunarspace.cn

Definition

The problem of finding a transfer trajectory given initial point, final point and time of flight within the R3BP framework.

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
• Planar Circular Restricted Three-Body Problem, PCRTBP
• Insertion Delta-V

References

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