The adjustment of the mathematical model accuracy of the gas-hydraulic flight control actuator power circuit of an aircraft

被引：0
作者：
Ermakov S.A. [1 ]
Lalabekov V.I. [1 ]
Samsonovich S.L. [1 ]
机构：
[1] Moscow Aviation Institute (National Research University), Volokolamskoe shosse 4, Moscow
来源：
Russian Aeronautics | 2017年 / 60卷 / 3期
关键词：
elastic joint; gas pressure regulator; gas-hydraulic actuator; gimbaled control nozzle; servo unit; solid-fuel gas generator;
D O I：
10.3103/S1068799817030138
中图分类号：
学科分类号：
摘要：
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. © 2017, Allerton Press, Inc.
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页码：412 / 420
页数：8
相关论文
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Antonov V.V., Grebenkin V.I., Kuznetsov N.P., Mokrushin B.S., Cherepov V.I., Khramov S.N., Organy upravleniya vectorom tyagi tverdotoplivnykh raket, (2006)
[3]  
Lalabekov V.I., Samsonovich S.L., Mathematical Model of Gas-Hydraulic Actuator with Displacing Power Source, Izv. TulGU. Tekhnicheskie Nauki, 6, 1, pp. 362-373, (2015)
[4]  
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