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基于FPGA的星载步进电机控制电路设计

林方 王煜 付毅宾 陆钒 常振 邱晓晗

中国空间科学技术2017,Vol.37Issue(3):77-85,9.
中国空间科学技术2017,Vol.37Issue(3):77-85,9.DOI:10.16708/j.cnki.1000-758X.2017.0022

基于FPGA的星载步进电机控制电路设计

Design of stepper motor control circuit for satellitebased on FPGA

林方 1王煜 2付毅宾 2陆钒 2常振 1邱晓晗2

作者信息

  • 1. 中国科学技术大学,合肥 230031
  • 2. 中国科学院 安徽光学精密机械研究所,合肥 230031
  • 折叠

摘要

Abstract

A design of a circuit controlling stepper motors in a wide range of moment for special characteristics of long in-orbit operation and the difficulty to replace in space equipments was proposed. This design utilizes FPGA,Xilinx chip XC3S400-208, as the core control chip and LMD18200 as the driving chip of stepper motors. On the basis of a description of the circuit, the problem of the increase of resistance moment and the solutions of output moment adjustment in space equipments by PWM control and impulse frequency were discussed.Tests verified that the design′s maximum value of output moment in range makes moment margin reach 4 and the range of adjusting matches the requests of space equipments.

关键词

航天设备/力矩可调/步进电机控制电路/FPGA/PWM控制技术

Key words

space equipments/ adjustable moment/ a circuit controlling stepper motors/ FPGA/ PWM control

分类

信息技术与安全科学

引用本文复制引用

林方,王煜,付毅宾,陆钒,常振,邱晓晗..基于FPGA的星载步进电机控制电路设计[J].中国空间科学技术,2017,37(3):77-85,9.

基金项目

国家自然科学基金(41275037),安徽省自然科学基金(1408085MKL49) (41275037)

中国空间科学技术

OA北大核心CSCDCSTPCD

1000-758X

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