"Fixed final time three-axis satellite attitude control with thrusters ..."

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DOI: —

access: open

type: Withdrawn Item

metadata version: 2020-08-12

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  - electronic edition @ arxiv.org (open access)
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  dblp key:
  - journals/corr/abs-1908-10677
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  - https://dblp.org/rec/journals/corr/abs-1908-10677
(Withdrawn) Fixed final time three-axis satellite attitude control with thrusters based on dynamic programming and neural networks. CoRR abs/1908.10677 (2019)

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