Design, Modeling, and Testing of Hybrid-Electric Fixed-Wing VTOL Aircraft Propulsion System
Author:
Publisher
Springer Nature Singapore
Link
https://link.springer.com/content/pdf/10.1007/978-981-97-1107-9_59
Reference25 articles.
1. Gu, H., Lyx, X., Li, Z., et al.: Development and experimental verification of a hybrid vertical take-off and landing (VTOL) unmanned aerial vehicle (UAV). In: International Conference on Unmanned Aircraft Systems, ICUAS (2017)
2. Saeed, A.S., Younes, A.B., Cai, C., et al.: A survey of hybrid unmanned aerial vehicles. Prog. Aerosp. Sci. 98(April), 91–105 (2018)
3. Zong, J., Zhu, B., Hou, Z., et al.: Sizing and mission profile analysis of the hybrid-electric propulsion system for retrofitting a fixed wing VTOL aircraft. Int. J. Aerosp. Eng. 2022, 1–10 (2022)
4. Ausserer, J., Harmon, F.: Integration, validation, and testing of a hybrid-electric propulsion system for a small remotely piloted aircraft. In:10th International Energy Conversion Engineering Conference (2012)
5. An, J.H., Kwon, D.Y., Jeon, K.S., et al.: Advanced sizing methodology for a multi-mode eVTOL UAV powered by a hydrogen fuel cell and battery. Aerospace 9(2), 71 (2022)
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