Missile aerodynamic design using reinforcement learning and transfer learning

Science China Information Sciences volume 61, Article number: 119204 (2018) Cite this article

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Acknowledgements

This work was supported by National Natural Science Foundation of China (Grant No. 61603210) and Aeronautical Science Foundation of China (Grant No. 20160758001).

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Affiliations

  1. Department of Computer Science and Technology, Tsinghua University, Beijing, 100084, China

    Xinghui Yan, Jihong Zhu, Minchi Kuang & Xiangyang Wang

  2. State Key Laboratory of Intelligent Technology and System, Tsinghua University, Beijing, 100084, China

    Xinghui Yan, Jihong Zhu, Minchi Kuang & Xiangyang Wang

Authors
  1. Xinghui Yan
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  2. Jihong Zhu
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  3. Minchi Kuang
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  4. Xiangyang Wang
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Correspondence to Jihong Zhu.

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Yan, X., Zhu, J., Kuang, M. et al. Missile aerodynamic design using reinforcement learning and transfer learning. Sci. China Inf. Sci. 61, 119204 (2018). https://doi.org/10.1007/s11432-018-9463-x

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