Multi-Revolution Solution

Author: Tianjiang Shuo

Website: https://cislunarspace.cn

Definition

Solution to Lambert's problem where the time of flight exceeds one orbital period with multiple complete revolutions.

Application Value

When flight time exceeds a single orbit period, multi-revolution Lambert problems must be solved. The number of solutions grows exponentially with revolution count, a key issue for long-time-of-flight transfer missions.

  • Finite-Time-Convergent Differentiator, FTCD
  • Prescribed Performance Control, PPC
  • Prescribed Performance Function, PPF
  • Terminal Sliding Mode Control, TSMC

References

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