Main approaches and features of the design of aircraft hydro-mechanical control systems
- 作者: Petrov P.V.1, Tselischev V.A.1, Kuderko D.A.2
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隶属关系:
- Ufa University of Science and Technology
- R and D Center “Technodinamika”
- 期: 卷 23, 编号 1 (2024)
- 页面: 67-79
- 栏目: AIRCRAFT AND SPACE ROCKET ENGINEERING
- URL: https://ogarev-online.ru/2542-0453/article/view/311447
- DOI: https://doi.org/10.18287/2541-7533-2024-23-1-67-79
- ID: 311447
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全文:
详细
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.
作者简介
P. Petrov
Ufa University of Science and Technology
编辑信件的主要联系方式.
Email: pgl.petrov@mail.ru
ORCID iD: 0000-0001-7901-2853
Candidate of Science (Engineering), Associate Professor of the Department of Applied Hydromechanics
俄罗斯联邦V. Tselischev
Ufa University of Science and Technology
Email: pgl.ugatu@mail.ru
Doctor of Science (Engineering), Professor, Head of Department of Applied Hydromechanics
俄罗斯联邦D. Kuderko
R and D Center “Technodinamika”
Email: dm_kuderko@mail.ru
Candidate of Science (Engineering), Head Center
俄罗斯联邦参考
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