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This article is cited in 4 scientific papers (total in 4 papers)
Modeling of aircraft flight through the wake vortex
A. M. Gaifullin, O. V. Animitsa, I. S. Bosnyakov, P. V. Kuzmin, Yu. N. Sviridenko, S. N. Suprunenko, K. G. Khairullin Central Aerohydrodynamic Institute, Zhukovsky, 140180, Russia
Abstract:
A mathematical model is proposed for calculating the forces and moments acting on an aircraft in the region affected by the wake vortex generated by another aircraft. This model takes into account various random factors and determines the wake vortex characteristics, as well as its shape, which depends on integral and distributed characteristics of atmospheric turbulence. The computational scheme, which involves the use of artificial neural networks, allows real-time calculation of the aerodynamic characteristics of the aircraft and to ensure training of pilots on flight simulators.
Keywords:
wake vortex, artificial neural networks, aerodynamic characteristics, flight simulators.
Received: 16.10.2018 Revised: 16.10.2018 Accepted: 29.10.2018
Citation:
A. M. Gaifullin, O. V. Animitsa, I. S. Bosnyakov, P. V. Kuzmin, Yu. N. Sviridenko, S. N. Suprunenko, K. G. Khairullin, “Modeling of aircraft flight through the wake vortex”, Prikl. Mekh. Tekh. Fiz., 60:2 (2019), 148–157; J. Appl. Mech. Tech. Phys., 60:2 (2019), 314–322
Linking options:
https://www.mathnet.ru/eng/pmtf466 https://www.mathnet.ru/eng/pmtf/v60/i2/p148
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