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Control of a BLDC motor for electromechanical actuator

  • Harbin Institute of Technology

Research output: Chapter in Book/Report/Conference proceedingConference contributionpeer-review

Abstract

Since the aircraft has the special requirements for the electromechanical actuator (EMA), the electrical servo control system using brushless DC (BLDC) motor is designed to fulfill these requirements in this paper. An angular position detecting method of helm is proposed to overcome the electromagnetic interference from the PWM inverter. This method combines motor's discrete Hall sensors signal with a potentiometer signal to determine the position information. In order to realize the fast response of the system, and eliminate the DC-Link voltage pumping-up phenomenon, an improved reverse braking method is applied, which can realize the torque control. In order to improve the system response, the current controller and the position controller is applied. Experimental results show that the tracking performance of the proposed control system can fulfill the requirements.

Original languageEnglish
Title of host publicationProceedings of the 11th International Conference on Electrical Machines and Systems, ICEMS 2008
Pages3266-3269
Number of pages4
StatePublished - 2008
Event11th International Conference on Electrical Machines and Systems, ICEMS 2008 - Wuhan, China
Duration: 17 Oct 200820 Oct 2008

Publication series

NameProceedings of the 11th International Conference on Electrical Machines and Systems, ICEMS 2008

Conference

Conference11th International Conference on Electrical Machines and Systems, ICEMS 2008
Country/TerritoryChina
CityWuhan
Period17/10/0820/10/08

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