Direct Single Shooting

Author: Tianjiang Shuo

Website: https://cislunarspace.cn

Definition

A method that treats the entire transfer trajectory as a single optimization segment, with all unknown initial conditions and parameters as design variables, solving the TPBVP via direct maximization of the objective function.

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

  • Ozimek和Howell 2010
Improve this page
Last Updated:
Contributors: ouyangjiahong, Ou Yang Jiahong