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.
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Original Russian Text© S.A. Ermakov, V.I. Lalabekov, S.L. Samsonovich, 2017, published in Izvestiya Vysshikh Uchebnykh Zavedenii. Aviatsionnaya Tekhnika, 2017, No. 3, pp. 86–94.
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Ermakov, S.A., Lalabekov, V.I. & Samsonovich, S.L. The adjustment of the mathematical model accuracy of the gas-hydraulic flight control actuator power circuit of an aircraft. Russ. Aeronaut. 60, 412–420 (2017). https://doi.org/10.3103/S1068799817030138
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DOI: https://doi.org/10.3103/S1068799817030138