Orbital Boundary Value Problem

Author: Tianjiang Shuo

Website: https://cislunarspace.cn

Definition

The problem of finding an orbit given initial and terminal states; fundamental in trajectory design, including classic cases such as Lambert's problem.

Application Value

This concept is fundamental to cislunar orbital mechanics and mission analysis, providing essential theoretical support for trajectory design and operational planning.

  • Retrograde Motion
  • Absolute Phase Bias
  • Relative Attitude Quaternion
  • Radial-Tangential-Normal Coordinate System, RTN

References

  • 航天动力学的数学方法（修订版）/Richard H. Battin - 2018 - 航天动力学的数学方法（修订版）.md
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Contributors: ouyangjiahong, Ou Yang Jiahong