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Attitude control of a novel tilt-wing UAV in hovering flight

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Acknowledgements

This work was supported by National Natural Science Foundation of China (Grant Nos. 62203259, 62073185, 61903216, 61973182) and China Postdoctoral Science Foundation (Grant No. 2021TQ0179).

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Authors and Affiliations

  1. Department of Precision Instrument, Tsinghua University, Beijing, 100084, China

    Jihong Zhu, Yunjie Yang & Xiaming Yuan

  2. Institute for Aero Engine, Tsinghua University, Beijing, 100084, China

    Xiangyang Wang & Xiao Yang

Authors
  1. Jihong Zhu
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  2. Yunjie Yang
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  3. Xiangyang Wang
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  4. Xiaming Yuan
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  5. Xiao Yang
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Corresponding author

Correspondence to Yunjie Yang.

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Videos and Appendixes A–C. The supporting information is available online at info.scichina.com and link.springer.com. The supporting materials are published as submitted, without typesetting or editing. The responsibility for scientific accuracy and content remains entirely with the authors.

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Attitude control of a novel tilt-wing UAV in hovering flight

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Zhu, J., Yang, Y., Wang, X. et al. Attitude control of a novel tilt-wing UAV in hovering flight. Sci. China Inf. Sci. 66, 154201 (2023). https://doi.org/10.1007/s11432-022-3605-5

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  • DOI: https://doi.org/10.1007/s11432-022-3605-5