Composite model of a research flight simulator for a helicopter with the hingeless main rotor


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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.

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


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