NDLI: Research on rectifier based on TMS320LF2407 and IR2130 used in the aircraft

Content Provider	IEEE Xplore Digital Library
Author	Zhang Shutuan Liu Lingshun Hu Chunwan
Copyright Year	2011
Description	Author affiliation: Department of Control Engineering, Naval Aeronautical and Astronautical University, Yantai, Shandong Province 264001, China (Zhang Shutuan; Liu Lingshun; Hu Chunwan)
Abstract	In order to improve the power factor of the rectifier used in the aircraft, the study of the high power factor rectifier adopted new digital control technology is the hotspot in the field of power electronics. The design and implement of the three-phase voltage source PWM rectifier, which adopt seven-segment space vector pulse-with modulation (SVPWM) control strategy, based on TMS320LF2407 DSP and IR2130 is introduced in this paper. The mathematical model and the hardware circuit of the rectifier are established. The design of three-phase voltage source rectifier (VSR) adopts the SVPWM control technology and incremental PID regulator, can help to realize the characters of high power factor and digital control. The experimental results show that the input voltage and current of rectifier has the same phase, and the rectifier designed in this paper can realize high power factor.
Starting Page	2391
Ending Page	2394
File Size	303857
Page Count	4
File Format	PDF
ISBN	9781612841809
e-ISBN	9781612841816
DOI	10.1109/FSKD.2011.6020044
Language	English
Publisher	Institute of Electrical and Electronics Engineers, Inc. (IEEE)
Publisher Date	2011-07-26
Publisher Place	China
Access Restriction	Subscribed
Rights Holder	Institute of Electrical and Electronics Engineers, Inc. (IEEE)
Subject Keyword	Space vector pulse width modulation Rectifiers Switches TMS320LF2407 SVPWM Power factor Incremental PID regulator Mathematical model Control strategy Voltage control
Content Type	Text
Resource Type	Article

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