Composite model of a research flight simulator for a helicopter with the hingeless main rotor
- Authors: Ledyankina O.A.1, Mikhailov S.A.1
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Affiliations:
- Tupolev Kazan National Research Technical University
- Issue: Vol 59, No 4 (2016)
- Pages: 495-499
- Section: Flight Dynamics and Control of Flight Vehicles
- URL: https://journals.rcsi.science/1068-7998/article/view/229859
- DOI: https://doi.org/10.3103/S1068799816040097
- ID: 229859
Cite item
Abstract
This paper presents a composite model of a flight simulator. This simulator is intended for carrying out investigative tests of flight dynamics imitation models of a hingeless rotor helicopter. A schematic diagram, composition and operation channels of the flight simulator software are presented. A possibility of applying the control lag is estimated.
Keywords
About the authors
O. A. Ledyankina
Tupolev Kazan National Research Technical University
Author for correspondence.
Email: OALedyankina@kai.ru
Russian Federation, ul. Karla Marksa 10, Kazan, Tatarstan, 420111
S. A. Mikhailov
Tupolev Kazan National Research Technical University
Email: OALedyankina@kai.ru
Russian Federation, ul. Karla Marksa 10, Kazan, Tatarstan, 420111