Design and Experimental Verification of a Roll Control Strategy for Large Wingspan Flapping-Wing Aerial Vehicle
Author:
Funder
National Natural Science Foundation of China
ND Basic Research Funds under Grants
Key Research and Development Projects of Shaanxi Province
Publisher
Springer Science and Business Media LLC
Link
https://link.springer.com/content/pdf/10.1007/s42235-024-00532-4.pdf
Reference45 articles.
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2. Platzer, M., Jones, K., Young, J., & Lai, J. (2008). Flapping wing aerodynamics: Progress and challenges. AIAA Journal, 46(9), 2136–2149.
3. Bie, D., Zhang, Y., & Shen, T. (2022). Research progress in bat-inspired flapping wing aerial vehicle. In Proceedings of 2021 International Conference on Autonomous Unmanned Systems (pp. 1495–1504). Singapore.
4. Meng, R., Song, B., Xuan, J., & Yang, X. (2023). Design and verification of a large-scaled flapping-wing aircraft named “cloud owl.” Applied Sciences, 13(9), 5667.
5. Yang, W., Wang, L., & Song, B. (2018). Dove: A biomimetic flapping-wing micro air vehicle. International Journal of Micro Air Vehicles, 10(1), 70–84.
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