Modelling of Aircraft DC Generator Voltage Regulation
The result's identifiers
Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F60162694%3AG43__%2F12%3A00479353" target="_blank" >RIV/60162694:G43__/12:00479353 - isvavai.cz</a>
Result on the web
<a href="http://vavtest.unob.cz/registr" target="_blank" >http://vavtest.unob.cz/registr</a>
DOI - Digital Object Identifier
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Alternative languages
Result language
angličtina
Original language name
Modelling of Aircraft DC Generator Voltage Regulation
Original language description
This article describes aircraft DC generator voltage regulation. The basic principles of an aircraft DC generator and a carbon-pile voltage regulator are explained. The experimental part starts with the creation of a mathematical model of both the aircraft generator and the voltage regulator. Then a simulation of the generator-regulator system in the MATLAB-Simulink program was done. The results of this simulation, represented by the generator?s external load characteristics and the voltage-time characteristics of the generator-regulator system are then presented in this paper.
Czech name
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Czech description
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Classification
Type
D - Article in proceedings
CEP classification
KA - Militarism
OECD FORD branch
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Result continuities
Project
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Continuities
I - Institucionalni podpora na dlouhodoby koncepcni rozvoj vyzkumne organizace
Others
Publication year
2012
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů
Data specific for result type
Article name in the collection
Proceedings of 15th International Conference on Mechatronics ? Mechatronika 2012
ISBN
978-80-01-04987-7
ISSN
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e-ISSN
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Number of pages
6
Pages from-to
209-214
Publisher name
Czech Technical University in Prague
Place of publication
Prague
Event location
Praha
Event date
Jan 1, 2012
Type of event by nationality
WRD - Celosvětová akce
UT code for WoS article
000324949300039