Design of an Aeronautic Test AC Power Supply Based on MCU
DOI:
CSTR:
Author:
Affiliation:

Clc Number:

V242.2

Fund Project:

  • Article
  • |
  • Figures
  • |
  • Metrics
  • |
  • Reference
  • |
  • Related
  • |
  • Cited by
  • |
  • Materials
  • |
  • Comments
    Abstract:

    In this paper,an aeronautic tested DC/AC inverter based on a Micro-computer Unit(MCU) is introduced.The DC/DC boost unit is push-pull circuit controlled by UC3846,which can restrain the magnetic bais of the push-pull transformer and enhance the dynamic load response. The SPWM control pulses are produced by P87LPC768.This inverter has the merits of simple structure,small volume,high output-stablity and easy to be adjusted.The test waveform is present at the end of this paper.

    Reference
    Related
    Cited by
Get Citation
Related Videos

Share
Article Metrics
  • Abstract:
  • PDF:
  • HTML:
  • Cited by:
History
  • Received:April 13,2006
  • Revised:
  • Adopted:
  • Online:
  • Published:
Article QR Code