Development of electromechanical actuators

Hong Guo; Wei Xing

Development of electromechanical actuators

Hong Guo^*
, Wei Xing

^*Corresponding author for this work

Research output: Contribution to journal › Article › peer-review

30 Scopus citations

Abstract

The electromechanical actuator (EMA) represents such a class of position servo systems, which directly or indirectly control the motion of load by servomotors or electric devices. This paper summarizes the application, the history of structure evolvement and the key technology development of EMA, and introduces the developing trends of EMA. Based on the summaries and analysis, some suggestions are presented on future EMA research and development in the application to aircraft.

Original language	English
Pages (from-to)	620-627
Number of pages	8
Journal	Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica
Volume	28
Issue number	3
State	Published - May 2007

Keywords

Control of aircraft
Development trend
Electromechanical actuator
High reliability

Cite this

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title = "Development of electromechanical actuators",

abstract = "The electromechanical actuator (EMA) represents such a class of position servo systems, which directly or indirectly control the motion of load by servomotors or electric devices. This paper summarizes the application, the history of structure evolvement and the key technology development of EMA, and introduces the developing trends of EMA. Based on the summaries and analysis, some suggestions are presented on future EMA research and development in the application to aircraft.",

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AU - Guo, Hong

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AB - The electromechanical actuator (EMA) represents such a class of position servo systems, which directly or indirectly control the motion of load by servomotors or electric devices. This paper summarizes the application, the history of structure evolvement and the key technology development of EMA, and introduces the developing trends of EMA. Based on the summaries and analysis, some suggestions are presented on future EMA research and development in the application to aircraft.

KW - Control of aircraft

KW - Development trend

KW - Electromechanical actuator

KW - High reliability

UR - https://www.scopus.com/pages/publications/34347248720

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SN - 1000-6893

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JF - Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica

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ER -

Development of electromechanical actuators

Abstract

Keywords

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