摘要
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.
| 源语言 | 英语 |
|---|---|
| 页(从-至) | 620-627 |
| 页数 | 8 |
| 期刊 | Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica |
| 卷 | 28 |
| 期 | 3 |
| 出版状态 | 已出版 - 5月 2007 |
指纹
探究 'Development of electromechanical actuators' 的科研主题。它们共同构成独一无二的指纹。引用此
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