TR
EN
Minimizing deflection on the yaw axis on VTOL type air-vehicles with three rotors
Abstract
This study provides an effective solution to the problem of deflection on yaw axes of air-vehicles capable of three-rotor Vertical Take-Off and Landing (VTOL). Most VTOL aircraft are produced with five rotors in national context. Four of these rotors are used for landing and taking off and are positioned to balance each other. The other rotor is positioned to fly with fixed wings. Therefore, no deviation in the yaw axis is experienced during descent-off. Three rotor VTOL configurations are available as an alternative to five rotor VTOL air-vehicles. This study is available through the three rotor VTOL prototypes that we have developed. The biggest drawback of three rotor VTOLs is the instability due to the position of the rotors during takeoff. This instability has been eliminated and three rotor VTOLs have been more advantageous than other configurations.
Keywords
References
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Details
Primary Language
English
Subjects
Aerospace Engineering
Journal Section
Research Article
Publication Date
April 30, 2022
Submission Date
January 12, 2022
Acceptance Date
February 18, 2022
Published in Issue
Year 2022 Volume: 3 Number: 1
APA
Çiçin, K., & Yavşan, E. (2022). Minimizing deflection on the yaw axis on VTOL type air-vehicles with three rotors. International Journal of Aeronautics and Astronautics, 3(1), 1-6. https://doi.org/10.55212/ijaa.1056802
AMA
1.Çiçin K, Yavşan E. Minimizing deflection on the yaw axis on VTOL type air-vehicles with three rotors. International Journal of Aeronautics and Astronautics. 2022;3(1):1-6. doi:10.55212/ijaa.1056802
Chicago
Çiçin, Kürşat, and Emrehan Yavşan. 2022. “Minimizing Deflection on the Yaw Axis on VTOL Type Air-Vehicles With Three Rotors”. International Journal of Aeronautics and Astronautics 3 (1): 1-6. https://doi.org/10.55212/ijaa.1056802.
EndNote
Çiçin K, Yavşan E (April 1, 2022) Minimizing deflection on the yaw axis on VTOL type air-vehicles with three rotors. International Journal of Aeronautics and Astronautics 3 1 1–6.
IEEE
[1]K. Çiçin and E. Yavşan, “Minimizing deflection on the yaw axis on VTOL type air-vehicles with three rotors”, International Journal of Aeronautics and Astronautics, vol. 3, no. 1, pp. 1–6, Apr. 2022, doi: 10.55212/ijaa.1056802.
ISNAD
Çiçin, Kürşat - Yavşan, Emrehan. “Minimizing Deflection on the Yaw Axis on VTOL Type Air-Vehicles With Three Rotors”. International Journal of Aeronautics and Astronautics 3/1 (April 1, 2022): 1-6. https://doi.org/10.55212/ijaa.1056802.
JAMA
1.Çiçin K, Yavşan E. Minimizing deflection on the yaw axis on VTOL type air-vehicles with three rotors. International Journal of Aeronautics and Astronautics. 2022;3:1–6.
MLA
Çiçin, Kürşat, and Emrehan Yavşan. “Minimizing Deflection on the Yaw Axis on VTOL Type Air-Vehicles With Three Rotors”. International Journal of Aeronautics and Astronautics, vol. 3, no. 1, Apr. 2022, pp. 1-6, doi:10.55212/ijaa.1056802.
Vancouver
1.Kürşat Çiçin, Emrehan Yavşan. Minimizing deflection on the yaw axis on VTOL type air-vehicles with three rotors. International Journal of Aeronautics and Astronautics. 2022 Apr. 1;3(1):1-6. doi:10.55212/ijaa.1056802