Structural integrity assessment and optimization of control surfaces in coaxial unmanned aerial vehicles: A case study of a micro coaxial UAV
Author:
Affiliation:
1. Center for Research and Innovation in Aerospace Engineering, Faculty of Mechanical and Electrical Engineering, Autonomous University of Nuevo Leon, Apodaca, Nuevo Leon, Mexico;
2. La Laguna Institute of Technology-TecNM, Torreon, Coahuila, Mexico
Funder
Office of Naval Research Global
Publisher
Informa UK Limited
Link
https://www.tandfonline.com/doi/pdf/10.1080/15397734.2024.2379520
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3. Chen R. X. Zhu Z. Zhou Z. Wang and T. Zhang. 2018. “Study on the Structure Design of Solar Powered UAV.” 2018 IEEE International Conference on Prognostics and Health Management (ICPHM 2018). Seattle WA USA.
4. Design Methodology of a UAV Propeller Implemented in Monitoring Activities;Cruzatty C.;Materials Today Proceedings,2022
5. De Vivo L. D. Tran and F. Kuester. 2019. “Towards Design of a 3D Printable Prandtl Box-Wing Unmanned Aerial Vehicle.” IEEE Aerospace Conference Proceedings. Big Sky MT USA.
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