Modeling of helicopter flight imitation in the vortex ring state
- Authors: Toropov M.Y.1, Stepanov S.Y.1
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Affiliations:
- Tupolev Kazan National Research Technical University
- Issue: Vol 59, No 4 (2016)
- Pages: 517-522
- Section: Flight Dynamics and Control of Flight Vehicles
- URL: https://journal-vniispk.ru/1068-7998/article/view/229879
- DOI: https://doi.org/10.3103/S1068799816040127
- ID: 229879
Cite item
Abstract
A method of imitating the helicopter flight on a flight simulator is proposed for the vortex ring state hover flight. Algorithms of artificial neural networks are used for the modeling. The method allows modeling the characteristics of the main rotor's loading during a dangerous descent of the helicopter.
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About the authors
M. Yu. Toropov
Tupolev Kazan National Research Technical University
Author for correspondence.
Email: otosoft@yandex.ru
Russian Federation, ul. Karla Marksa 10, Kazan, Tatarstan, 420111
S. Ya. Stepanov
Tupolev Kazan National Research Technical University
Email: otosoft@yandex.ru
Russian Federation, ul. Karla Marksa 10, Kazan, Tatarstan, 420111
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