A Tri-Ducted Fan Tilting VTOL UAV: Conceptual Design and Aerodynamic Analysis
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Publisher
Springer Nature Singapore
Link
https://link.springer.com/content/pdf/10.1007/978-981-97-1306-6_10
Reference8 articles.
1. Liu Z, He Y, Yang L, Han J (2017) Control techniques of tilt rotor unmanned aerial vehicle systems: a review. Chin J Aeronaut 30(1):135–148. Chinese Journal of Aeronautics. https://doi.org/10.1016/j.cja.2016.11.001
2. Kamal AM, Ramirez-Serrano A (2020) Conceptual design of a highly-maneuverable transitional vtol uav with new maneuver and control capabilities. In: AIAA Scitech 2020 forum, american institute of aeronautics and astronautics Inc, AIAA. https://doi.org/10.2514/6.2020-1733
3. Sharma S, Sharma R, Kumar V, Chandel S (2021) Analysis of a tiltrotor vertical take-off and landing unmanned aerial vehicle: CFD approach. IOP Conf Ser Mater Sci Eng 1116(1):012096. https://doi.org/10.1088/1757-899x/1116/1/012096
4. Panigrahi S, Krishna YSS, Thondiyath A (2021) Design, analysis, and testing of a hybrid vtol tilt-rotor uav for increased endurance. Sensors 21(18). https://doi.org/10.3390/s21185987
5. Çakici F, Leblebicioǧlu MK (2012) Modeling and simulation of a small-sized tiltrotor UAV. J Def Model Simul 9(4):335–345. https://doi.org/10.1177/1548512911414951
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