Towards a High Fidelity Direct Transcription Method for Optimisation of Low-Thrust Trajectories

Details Towards a High Fidelity Direct Transcription Method for Optimisation of Low-Thrust Trajectories Towards a High Fidelity Direct Transcription Method for Optimisation of Low-Thrust Trajectories

2010-04-26

arxiv.org/abs/1004.4539v1

Mathematics

Optimization and Control

To be presented at the 4th International Conference on Astrodynamics Tools and Techniques.

Scientific paper

We build upon some new ideas in direct transcription methods developed within the Advanced Concepts Team to introduce two improvements to the Sims-Flanagan transcription for low-thrust trajectories. The obtained new algorithm is able to produce an operational trajectory accounting for the real spacecraft dynamics and adapting the segment duration on-line improving the final trajectory optimality.

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