Main approaches and features of the design of aircraft hydro-mechanical control systems
- Authors: Petrov P.V.1, Tselischev V.A.1, Kuderko D.A.2
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Affiliations:
- Ufa University of Science and Technology
- R and D Center “Technodinamika”
- Issue: Vol 23, No 1 (2024)
- Pages: 67-79
- Section: AIRCRAFT AND SPACE ROCKET ENGINEERING
- URL: https://journals.rcsi.science/2542-0453/article/view/311447
- DOI: https://doi.org/10.18287/2541-7533-2024-23-1-67-79
- ID: 311447
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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 FederationV. 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 FederationD. A. Kuderko
R and D Center “Technodinamika”
Email: dm_kuderko@mail.ru
Candidate of Science (Engineering), Head Center
Russian FederationReferences
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