The adjustment of the mathematical model accuracy of the gas-hydraulic flight control actuator power circuit of an aircraft |
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| Authors: | S A Ermakov V I Lalabekov S L Samsonovich |
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| Institution: | 1.Moscow Aviation Institute (National Research University),Moscow,Russia |
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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. |
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