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Design of optimal trajectory transition controller for thrust-vectored V/STOL aircraft

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Acknowledgements

This work was supported by National Natural Science Foundation of China (Grant Nos. 61603210, 61673240).

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Authors and Affiliations

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

    Zhiqiang Cheng, Jihong Zhu, Xiaming Yuan & Xiangyang Wang

  2. Key Laboratory of Complex Ship System Simulation, Beijing, 100161, China

    Zhiqiang Cheng

Authors
  1. Zhiqiang Cheng
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  2. Jihong Zhu
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  3. Xiaming Yuan
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  4. Xiangyang Wang
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Corresponding author

Correspondence to Jihong Zhu.

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Cheng, Z., Zhu, J., Yuan, X. et al. Design of optimal trajectory transition controller for thrust-vectored V/STOL aircraft. Sci. China Inf. Sci. 64, 139201 (2021). https://doi.org/10.1007/s11432-018-9582-6

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  • DOI: https://doi.org/10.1007/s11432-018-9582-6

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