Perturbed Lambert's Problem

Author: Tianjiang Shuo

Website: https://cislunarspace.cn

Definition

Lambert's problem solved under perturbations from sources such as Earth's oblateness, third-body gravity, and solar radiation pressure, with boundary conditions specified by initial position, final position, and time of flight.

Application Value

This term has significant application value in cislunar space missions。In the orbital design phase, engineers use relevant theories for trajectory optimization；In navigation and orbit determination, it is used to improve measurement accuracy；In attitude control and orbit maintenance tasks, it ensures stable spacecraft operation。In practical applications, parameter optimization and algorithm adaptation can be combined with mission requirements to improve mission success rate and resource utilization efficiency。

  • Characteristic Exponents
  • Capture Docking Phase
  • Lunar Flyby Transfer

References

  • Criscola等 - 2024
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Contributors: ouyangjiahong, Ou Yang Jiahong