Virtual Design of Advanced Control Algorithms for Small Turbojet Engines

Kód výsledku v IS VaVaI

<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F00216275%3A25510%2F19%3A39915695" target="_blank" >RIV/00216275:25510/19:39915695 - isvavai.cz</a>

Výsledek na webu

<a href="http://uni-obuda.hu/journal/Fozo_Andoga_Kovacs_Schreiner_Beneda_Savka_Sousek_97.pdf" target="_blank" >http://uni-obuda.hu/journal/Fozo_Andoga_Kovacs_Schreiner_Beneda_Savka_Sousek_97.pdf</a>

DOI - Digital Object Identifier

<a href="http://dx.doi.org/10.12700/APH.16.10.2019.10.7" target="_blank" >10.12700/APH.16.10.2019.10.7</a>

Jazyk výsledku

angličtina

Název v původním jazyce

Virtual Design of Advanced Control Algorithms for Small Turbojet Engines

Popis výsledku v původním jazyce

Advanced control in the area of turbojet engines defines many different applied complex control strategies. Highly theoretical approaches and designs are often presented in this area. The article is aimed at practical aspects of adaptive controller design for a class of small turbojet engines in triple loop control architecture. The article presents a non-linear dynamic model of a small turbojet engine taking in account the environmental conditions, which it operates in. The designed triple loop control architecture shows increased precision of control keeping acceleration schedule of the simulated engine and is not susceptible to outer disturbances. The article shows pilot dynamic simulation tests, showing feasibility of the taken approach. It can also be used for other classes of turbojet engines as well other similar technical systems.

Název v anglickém jazyce

Virtual Design of Advanced Control Algorithms for Small Turbojet Engines

Popis výsledku anglicky

Advanced control in the area of turbojet engines defines many different applied complex control strategies. Highly theoretical approaches and designs are often presented in this area. The article is aimed at practical aspects of adaptive controller design for a class of small turbojet engines in triple loop control architecture. The article presents a non-linear dynamic model of a small turbojet engine taking in account the environmental conditions, which it operates in. The designed triple loop control architecture shows increased precision of control keeping acceleration schedule of the simulated engine and is not susceptible to outer disturbances. The article shows pilot dynamic simulation tests, showing feasibility of the taken approach. It can also be used for other classes of turbojet engines as well other similar technical systems.

Druh

J_imp - Článek v periodiku v databázi Web of Science

CEP obor

—

OECD FORD obor

20104 - Transport engineering

Projekt

—

Návaznosti

I - Institucionalni podpora na dlouhodoby koncepcni rozvoj vyzkumne organizace

Rok uplatnění

2019

Kód důvěrnosti údajů

S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů

Název periodika

Acta polytechnica hungarica

ISSN

1785-8860

e-ISSN

—

Svazek periodika

16

Číslo periodika v rámci svazku

10

Stát vydavatele periodika

HU - Maďarsko

Počet stran výsledku

17

Strana od-do

101-117

Kód UT WoS článku

000506635900007

EID výsledku v databázi Scopus

2-s2.0-85078953543