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.

引用

页码：412 / 420

页数：8

共 9 条

[1] Mathematical Model of the Gas-Hydraulic Control Actuator for the Swiveling Nozzle of the Solid Propellant Fuel Propulsion System with Flexible Joint
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Russian Aeronautics, 2019, 62 (02): : 222 - 228
[2] FAILSAFE HYDRAULIC ACTUATOR FLIGHT CONTROL FOR JET AIRCRAFT
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[3] MATHEMATICAL-MODEL AND STABILITY OF FEEDBACK HYDRAULIC ACTUATOR WITH JET VALVE CONTROL
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[9] Mathematical Model of High Speed Actuating Hydraulic Drive for Power Unit Control Systems.
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