Detail publikace
Model of Aircraft Actuator with BLAC Motor
TOMAN, J. SINGULE, V. HADAŠ, Z.
Anglický název
Model of Aircraft Actuator with BLAC Motor
Typ
Stať ve sborníku v databázi WoS či Scopus
Jazyk
en
Originální abstrakt
The paper deals with a development of control algorithms for electro-mechanical actuator in an aircraft. Contemporary technological developments within the all-electric aircraft concept lead to replacement of existing hydraulicmechanical circuits by intelligent actuators based on electrical servo drives which increase overall reliability and utility value, decrease operating costs, dimensions and weight. The article is focused on design of complex model of Brushless Alternating Current (BLAC) motor and control algorithms with respect to used two types of rotor position sensor. Commonly used an incremental encoder and discrete Hall sensors for sensing rotor position are chosen. Development includes design and verification of these models and their performance is evaluated. In all tests the initial rotor position was non-zero to prove algorithms’ ability to start up the motor from an arbitrary position.
Klíčová slova anglicky
BLAC; Power bridge; EMF; PWM; PSD; Actuator
Vydáno
2014-09-21
Nakladatel
Gazi University, Turkey
Místo
Antalya
ISBN
978-1-4799-2060-0
Kniha
16th INTERNATIONAL POWER ELECTRONICS AND MOTION CONTROL CONFERENCE AND EXPOSITION (PEMC 2014)
Strany od–do
278–283
Počet stran
6
BIBTEX
@inproceedings{BUT109889,
author="Jiří {Toman} and Vladislav {Singule} and Zdeněk {Hadaš}",
title="Model of Aircraft Actuator with BLAC Motor",
booktitle="16th INTERNATIONAL POWER ELECTRONICS AND MOTION CONTROL CONFERENCE AND EXPOSITION (PEMC 2014)",
year="2014",
series="1",
number="1",
pages="278--283",
publisher="Gazi University, Turkey",
address="Antalya",
isbn="978-1-4799-2060-0",
url="http://www.pemc2014.org/"
}