Email this article The adjustment of the mathematical model accuracy of the gas-hydraulic flight control actuator power circuit of an aircraft
- Authors: Ermakov S.A.1, Lalabekov V.I.1, Samsonovich S.L.1
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Affiliations:
- Moscow Aviation Institute (National Research University)
- Issue: Vol 60, No 3 (2017)
- Pages: 412-420
- Section: Aircraft and Rocket Engine Theory
- URL: https://journals.rcsi.science/1068-7998/article/view/230200
- DOI: https://doi.org/10.3103/S1068799817030138
- ID: 230200
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Abstract
The methodology is proposed and the mathematical model is developed for the purpose of numerical simulation of the power circuit of the gas-hydraulic actuator with displacing power source for the gimbaled nozzle control. It provides the highest power efficiency factor of the actuator as a part of aircraft by means of pulling together the profiles of available and required power.
About the authors
S. A. Ermakov
Moscow Aviation Institute (National Research University)
Email: lalabekov.valentin@yandex.ru
Russian Federation, Volokolamskoe shosse 4, Moscow, 125993
V. I. Lalabekov
Moscow Aviation Institute (National Research University)
Author for correspondence.
Email: lalabekov.valentin@yandex.ru
Russian Federation, Volokolamskoe shosse 4, Moscow, 125993
S. L. Samsonovich
Moscow Aviation Institute (National Research University)
Email: lalabekov.valentin@yandex.ru
Russian Federation, Volokolamskoe shosse 4, Moscow, 125993
