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Using Direct Transcription to Compute Optimal Low Thrust Transfers Between Libration Point Orbits

In: Space Engineering

Author

Listed:
  • John T. Betts

    (Applied Mathematical Analysis, LLC)

Abstract

The direct transcription method has been used to solve many challenging optimal control problems. One such example involves the calculation of a low thrust orbit transfer between libration point orbits. The recent implementation of high order discretization techniques is first described and then illustrated by computing optimal low thrust trajectories between orbits about the L 1 and L 2 Earth-Moon libration points.

Suggested Citation

  • John T. Betts, 2016. "Using Direct Transcription to Compute Optimal Low Thrust Transfers Between Libration Point Orbits," Springer Optimization and Its Applications, in: Giorgio Fasano & János D. Pintér (ed.), Space Engineering, pages 49-86, Springer.
    • Handle: RePEc:spr:spochp:978-3-319-41508-6_2
    DOI: 10.1007/978-3-319-41508-6_2
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