AUTOMATIC CONTROL SYSTEM FOR REGULATED HIGH TEMPERATURE MAIN COMBUSTION CHAMBER OF MANEUVERABLE AIRCRAFT MULTIMODE GAS TURBINE ENGINE

The paper describes choosing and substantiating the control laws, forming the appearance the automatic control system for regulated high temperature main combustion chamber of maneuverable aircraft multimode gas turbine engine aimed at sustainable and effective functioning of main combustion chamber...

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Main Authors: T. V. Gras’Ko, S. A. Мayatsky
Format: Article
Language:Russian
Published: Moscow State Technical University of Civil Aviation 2016-11-01
Series:Научный вестник МГТУ ГА
Subjects:
Online Access:https://avia.mstuca.ru/jour/article/view/212
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author T. V. Gras’Ko
S. A. Мayatsky
author_facet T. V. Gras’Ko
S. A. Мayatsky
author_sort T. V. Gras’Ko
collection DOAJ
description The paper describes choosing and substantiating the control laws, forming the appearance the automatic control system for regulated high temperature main combustion chamber of maneuverable aircraft multimode gas turbine engine aimed at sustainable and effective functioning of main combustion chamber within a broad operation range.
format Article
id doaj-art-3db3be900096403bbd894515b0ac18e6
institution Kabale University
issn 2079-0619
2542-0119
language Russian
publishDate 2016-11-01
publisher Moscow State Technical University of Civil Aviation
record_format Article
series Научный вестник МГТУ ГА
spelling doaj-art-3db3be900096403bbd894515b0ac18e62025-08-20T03:35:43ZrusMoscow State Technical University of Civil AviationНаучный вестник МГТУ ГА2079-06192542-01192016-11-0102066875212AUTOMATIC CONTROL SYSTEM FOR REGULATED HIGH TEMPERATURE MAIN COMBUSTION CHAMBER OF MANEUVERABLE AIRCRAFT MULTIMODE GAS TURBINE ENGINET. V. Gras’Ko0S. A. Мayatsky1ВУНЦ ВВС «Военно-воздушная академия им. проф. Н.Е. Жуковского и Ю.А. Гагарина»ВУНЦ ВВС «Военно-воздушная академия им. проф. Н.Е. Жуковского и Ю.А. Гагарина»The paper describes choosing and substantiating the control laws, forming the appearance the automatic control system for regulated high temperature main combustion chamber of maneuverable aircraft multimode gas turbine engine aimed at sustainable and effective functioning of main combustion chamber within a broad operation range.https://avia.mstuca.ru/jour/article/view/212human factorinformation support system of taking decisionflight safetycatastrophic factornoncatastrophic factorairborne computerautomatic flight control system
spellingShingle T. V. Gras’Ko
S. A. Мayatsky
AUTOMATIC CONTROL SYSTEM FOR REGULATED HIGH TEMPERATURE MAIN COMBUSTION CHAMBER OF MANEUVERABLE AIRCRAFT MULTIMODE GAS TURBINE ENGINE
Научный вестник МГТУ ГА
human factor
information support system of taking decision
flight safety
catastrophic factor
noncatastrophic factor
airborne computer
automatic flight control system
title AUTOMATIC CONTROL SYSTEM FOR REGULATED HIGH TEMPERATURE MAIN COMBUSTION CHAMBER OF MANEUVERABLE AIRCRAFT MULTIMODE GAS TURBINE ENGINE
title_full AUTOMATIC CONTROL SYSTEM FOR REGULATED HIGH TEMPERATURE MAIN COMBUSTION CHAMBER OF MANEUVERABLE AIRCRAFT MULTIMODE GAS TURBINE ENGINE
title_fullStr AUTOMATIC CONTROL SYSTEM FOR REGULATED HIGH TEMPERATURE MAIN COMBUSTION CHAMBER OF MANEUVERABLE AIRCRAFT MULTIMODE GAS TURBINE ENGINE
title_full_unstemmed AUTOMATIC CONTROL SYSTEM FOR REGULATED HIGH TEMPERATURE MAIN COMBUSTION CHAMBER OF MANEUVERABLE AIRCRAFT MULTIMODE GAS TURBINE ENGINE
title_short AUTOMATIC CONTROL SYSTEM FOR REGULATED HIGH TEMPERATURE MAIN COMBUSTION CHAMBER OF MANEUVERABLE AIRCRAFT MULTIMODE GAS TURBINE ENGINE
title_sort automatic control system for regulated high temperature main combustion chamber of maneuverable aircraft multimode gas turbine engine
topic human factor
information support system of taking decision
flight safety
catastrophic factor
noncatastrophic factor
airborne computer
automatic flight control system
url https://avia.mstuca.ru/jour/article/view/212
work_keys_str_mv AT tvgrasko automaticcontrolsystemforregulatedhightemperaturemaincombustionchamberofmaneuverableaircraftmultimodegasturbineengine
AT samayatsky automaticcontrolsystemforregulatedhightemperaturemaincombustionchamberofmaneuverableaircraftmultimodegasturbineengine