| 惯性飞轮电机力矩伺服控制系统 |
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| 引用本文： | 杜坤梅,李铁才.惯性飞轮电机力矩伺服控制系统[J].电机与控制学报,2001,5(2):119-120,132. |
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| 作者姓名： | 杜坤梅 李铁才 |
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| 作者单位： | 1. 哈尔滨理工大学,
2. 哈尔滨工业大学, |
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| 摘 要： | 惯性飞轮是航天空间飞行器姿态控制系统的执行元件。姿态控制需要对惯性飞轮做四象限力矩伺服控制。本文采用双重电流闭环方法，即同时进行桥壁脉宽调幅与三相半桥脉宽调制综合控制，实现了飞轮电机的四象限精确力矩伺服控制。
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| 关 键 词： | 力矩伺服控制系统 惯性飞轮 电机 航天空间飞行器 |
| 文章编号： | 1007-449(2001)02-0119-02 |
Controlling system of inertial fly-wheel through torque servo motor |
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| DU Kun-mei,LI Tie-cai.Controlling system of inertial fly-wheel through torque servo motor[J].Electric Machines and Control,2001,5(2):119-120,132. |
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| Authors: | DU Kun-mei LI Tie-cai |
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| Abstract: | Fly-wheel is the implementary element of the poser controlling system of the space vehicle. The poser controlling system of the fly-wheel needs to be realized by means of four-quadrant torque servo control. This article adopts the double closed-loop current controlling method. That is adopting the bridge-arm pulse-amplitude modulation, and three-phase half-bridge pulse-width modulation simultaneously. With this method, this arti-cle realizes the accurate four-quadrant torque-servo control of the fly-wheel motor. |
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| Keywords: | fly-wheel motor torque servo control closed-loop current controlling |
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