| 中大功率航天电动伺服机构发展综述 |
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| 引用本文： | 郭洪根,王指国.中大功率航天电动伺服机构发展综述[J].导航定位于授时,2016(3):1-5. |
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| 作者姓名： | 郭洪根 王指国 |
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| 作者单位： | 中国航天科工集团伺服技术研究所,南京,210006 |
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| 摘 要： | 随着新材料、新技术的发展,电动伺服机构在电传飞机、先进飞行器、推力矢量控制中得到成功的应用.对中大功率航天电动伺服机构在国内外的研究及应用情况进行了介绍.通过分析,在国外电动伺服机构的运用已经相当成熟,在国内中大功率电动伺服机构在航天应用中已初具规模,出现逐步取代液压伺服机构的趋势.
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| 关 键 词： | 姿态控制 电动伺服机构 航天 应用现状 |
A Review of the Current Development of High-Power Aerospace EMA |
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| GUO Hong-gen and WANG Zhi-guo.A Review of the Current Development of High-Power Aerospace EMA[J].Navigation Positioning & Timing,2016(3):1-5. |
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| Authors: | GUO Hong-gen and WANG Zhi-guo |
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| Institution: | Servo technology institute of China Aerospace science & Industry Corp and Servo technology institute of China Aerospace science & Industry Corp |
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| Abstract: | With the rapid development of the new material and technology, the Electromechanical Actuator(EMA) has been successfully applied in the design of fly-by-wire aircraft, advanced space vehicle and thrust vector control systems.This paper introduces researches and applications of the High-power EMA in the world.According to the study, the EMA technology has been applied widely in foreign countries, and began to contribute to thrust vector control of Aerospace in China.We can predict that the EMA will take the place of Hydraulic Servo Mechanism in the future. |
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| Keywords: | Attitude control Electric servo mechanism Aerospace The condition of the application |
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