Publication detail

Design of universal control unit for brushless DC motors

TOMAN, J. HRBÁČEK, J. SINGULE, V.

Original Title

Design of universal control unit for brushless DC motors

English Title

Design of universal control unit for brushless DC motors

Type

conference paper

Language

en

Original Abstract

The paper presents the design of both power and control electronics used to develop a universal BLDC (brushless DC) motor control unit intended for an aircraft fuel metering pump. The controller allows employing various methods for sensor and sensor-less control including frequency, trapezoidal, sinusoidal and fielding oriented control. The power subsystem provides three power totempole switches as well as a wide range of input and auxiliary circuitry. As needed by the target aircraft industry standards, conclusions of a thorough FMECA analysis of the resulting device are given.

English abstract

The paper presents the design of both power and control electronics used to develop a universal BLDC (brushless DC) motor control unit intended for an aircraft fuel metering pump. The controller allows employing various methods for sensor and sensor-less control including frequency, trapezoidal, sinusoidal and fielding oriented control. The power subsystem provides three power totempole switches as well as a wide range of input and auxiliary circuitry. As needed by the target aircraft industry standards, conclusions of a thorough FMECA analysis of the resulting device are given.

Keywords

BLDC motor, control unit, model based design

RIV year

2012

Released

12.05.2012

Publisher

Institute of Theoretical and Applied Mechanics

Location

Praha

ISBN

978-80-86246-40-6

Book

Engineering Mechanics 2012, Book of extended abstracts

Pages from

342

Pages to

343

Pages count

2

BibTex


@inproceedings{BUT92775,
  author="Jiří {Toman} and Jan {Hrbáček} and Vladislav {Singule}",
  title="Design of universal control unit for brushless DC motors",
  annote="The paper presents the design of both power and control electronics used to develop a universal BLDC (brushless DC) motor control unit intended for an aircraft fuel metering pump. The controller allows employing various methods for sensor and sensor-less control including frequency, trapezoidal, sinusoidal and fielding oriented control. The power subsystem provides three power totempole switches as well as a wide range of input and auxiliary circuitry. As needed by the target aircraft industry standards, conclusions of a thorough FMECA analysis of the resulting device are given.",
  address="Institute of Theoretical and Applied Mechanics",
  booktitle="Engineering Mechanics 2012, Book of extended abstracts",
  chapter="92775",
  howpublished="print",
  institution="Institute of Theoretical and Applied Mechanics",
  year="2012",
  month="may",
  pages="342--343",
  publisher="Institute of Theoretical and Applied Mechanics",
  type="conference paper"
}