Aeroacoustic Characteristics of a Quadcopter Impeller in Vertical Take-Off and Landing Mode

Author:

Denisenko P. V.,Bulat P. V.,Chernyshov P. S.,Volkov K. N.

Publisher

Allerton Press

Subject

Aerospace Engineering

Reference27 articles.

1. Ostroukhov, S.P., Aerodinamika vozduzhnykh vintov i vintokol’tsevykh dvizhitelei (Aerodynamics of Propellers and Impellers), Moscow: Fizmatlit, 2014.

2. Czyba, R. and Szafranski, G., Control Structure Impact on the Flying Performance of the Multi-Rotor VTOL Platform – Design, Analysis and Experimental Validation, Int. Journal of Advanced Robotic Systems, 2013, vol. 10, no. 1, URL: https://journals.sagepub.com/doi/full/10.5772/53747.

3. Hrishikeshavan, V. and Chopra, I., Performance, Flight Testing of Shrouded Rotor Micro Air Vehicle in Edgewise Gusts, Journal of Aircraft, 2012, vol. 49, no. 1, pp. 193–205.

4. Popov, N.I., Emel’yanova, O.V., and Yatsun, S.F., Simulation of the Dynamics of a Quadcopter Flight, Vestnik Voronezhskogo Instituta GPS MChS Rossii, 2014, no. 4(13), pp. 69–75.

5. Kanatnikov, A.N. and Akopyan, K.R., Quadcopter Flat Motion Control, Matematika i Matematicheskoe Modelirovanie, 2015, no. 2, pp. 23–36.

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