Detail publikace

Model of Aircraft Actuator with BLAC Motor

TOMAN, J. SINGULE, V. HADAŠ, Z.

Originální název

Model of Aircraft Actuator with BLAC Motor

Typ

článek ve sborníku ve WoS nebo Scopus

Jazyk

angličtina

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

BLAC; Power bridge; EMF; PWM; PSD; Actuator

Autoři

TOMAN, J.; SINGULE, V.; HADAŠ, Z.

Rok RIV

2014

Vydáno

21. 9. 2014

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)

Edice

1

Číslo edice

1

Strany od

278

Strany do

283

Strany počet

6

URL

http://www.pemc2014.org/

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/"
}