Detail publikace

Model of Aircraft Actuator with BLAC Motor

Originální název

Model of Aircraft Actuator with BLAC Motor

Anglický název

Model of Aircraft Actuator with BLAC Motor

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.

Anglický 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.

BibTex


@inproceedings{BUT109889,
  author="Jiří {Toman} and Vladislav {Singule} and Zdeněk {Hadaš}",
  title="Model of Aircraft Actuator with BLAC Motor",
  annote="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.",
  address="Gazi University, Turkey",
  booktitle="16th INTERNATIONAL POWER ELECTRONICS AND MOTION CONTROL CONFERENCE AND EXPOSITION (PEMC 2014)",
  chapter="109889",
  edition="1",
  howpublished="electronic, physical medium",
  institution="Gazi University, Turkey",
  year="2014",
  month="september",
  pages="278--283",
  publisher="Gazi University, Turkey",
  type="conference paper"
}