The adjustment of the mathematical model accuracy of the gas-hydraulic flight control actuator power circuit of an aircraft
- Autores: Ermakov S.1, Lalabekov V.1, Samsonovich S.1
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Afiliações:
- Moscow Aviation Institute (National Research University)
- Edição: Volume 60, Nº 3 (2017)
- Páginas: 412-420
- Seção: 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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Resumo
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.
Sobre autores
S. Ermakov
Moscow Aviation Institute (National Research University)
Email: lalabekov.valentin@yandex.ru
Rússia, Volokolamskoe shosse 4, Moscow, 125993
V. Lalabekov
Moscow Aviation Institute (National Research University)
Autor responsável pela correspondência
Email: lalabekov.valentin@yandex.ru
Rússia, Volokolamskoe shosse 4, Moscow, 125993
S. Samsonovich
Moscow Aviation Institute (National Research University)
Email: lalabekov.valentin@yandex.ru
Rússia, Volokolamskoe shosse 4, Moscow, 125993