Publication detail

Model of Aircraft Actuator with BLAC Motor

TOMAN, J. SINGULE, V. HADAŠ, Z.

Original Title

Model of Aircraft Actuator with BLAC Motor

Type

conference paper

Language

English

Original Abstract

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.

Keywords

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

Authors

TOMAN, J.; SINGULE, V.; HADAŠ, Z.

RIV year

2014

Released

21. 9. 2014

Publisher

Gazi University, Turkey

Location

Antalya

ISBN

978-1-4799-2060-0

Book

16th INTERNATIONAL POWER ELECTRONICS AND MOTION CONTROL CONFERENCE AND EXPOSITION (PEMC 2014)

Edition

1

Edition number

1

Pages from

278

Pages to

283

Pages count

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/"
}