| 基于DSP的控制力矩陀螺外框驱动控制系统设计 |
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| 引用本文： | 刘承,刘向东,李黎.基于DSP的控制力矩陀螺外框驱动控制系统设计[J].电气传动,2006,36(9):29-31,43. |
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| 作者姓名： | 刘承 刘向东 李黎 |
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| 作者单位： | 北京理工大学 |
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| 摘 要： | 控制力矩陀螺是大型对地观测卫星以及空间站姿态控制系统的关键执行部件,介绍了以TMS-320LF2407为核心进行了单框架控制力矩陀螺外框驱动控制系统设计,包括了DSP控制核心及其外围电路、RS422串行通信接口设计、模拟量输出与位置测角模块硬件设计,以及整个DSP硬件系统控制系统软件设计,并成功地应用于单框架控制力矩陀螺外框驱动控制系统样机。
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| 关 键 词： | 单框架控制力矩陀螺 数字信号处理器 姿态控制 |
| 收稿时间： | 2005-08-12 |
| 修稿时间： | 2005-08-122006-04-19 |
Design and Application of the Control System of SGCMG Based on DSP |
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| Liu Cheng,Liu Xiangdong,Li Li.Design and Application of the Control System of SGCMG Based on DSP[J].Electric Drive,2006,36(9):29-31,43. |
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| Authors: | Liu Cheng Liu Xiangdong Li Li |
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| Affiliation: | Liu Cheng Liu Xiangdong Li Li |
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| Abstract: | Control moment gyro is the important part of attitude control of the space station system and the observe satellites. In this paper we introduce how to design a digital controller with DSP TMS320LF2407 in a SGCMG control system, included the particular of DSP,RS422, D/A, position measurement module and the software of the system. The controller has already been used in the prototype of control moment gyro system successfully. |
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| Keywords: | single gimbal control moment gyros(SGCMG) digital signal processor(DSP) attitude control |
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