Main approaches and features of the design of aircraft hydro-mechanical control systems


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Abstract

The main purpose of the article is to identify the main approaches and define the concept when modeling the hydro-mechanical control systems of an aircraft. The advantages and importance of a computational experiment with the aid of a virtual test bed at the stage of constructive parametric debugging of the elements of complex hydraulic systems are emphasized. The characteristics obtained from the results of the computational experiment will allow us to determine the level of adequacy of the models and subsequently choose the most optimal design and operational parameters.

About the authors

P. V. Petrov

Ufa University of Science and Technology

Author for correspondence.
Email: pgl.petrov@mail.ru
ORCID iD: 0000-0001-7901-2853

Candidate of Science (Engineering), Associate Professor of the Department of Applied Hydromechanics

Russian Federation

V. A. Tselischev

Ufa University of Science and Technology

Email: pgl.ugatu@mail.ru

Doctor of Science (Engineering), Professor, Head of Department of Applied Hydromechanics

Russian Federation

D. A. Kuderko

R and D Center “Technodinamika”

Email: dm_kuderko@mail.ru

Candidate of Science (Engineering), Head Center

Russian Federation

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