Title :
Research on rectifier based on TMS320LF2407 and IR2130 used in the aircraft
Author :
Zhang Shutuan ; Liu Lingshun ; Hu Chunwan
Author_Institution :
Dept. of Control Eng., Naval Aeronaut. & Astronaut. Univ., Yantai, China
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.
Keywords :
PWM rectifiers; aircraft power systems; digital control; digital signal processing chips; power factor; three-term control; IR2130; SVPWM control strategy; TMS320LF2407 DSP; VSR; aircraft; digital control technology; hardware circuit; high-power factor rectifier; incremental PID regulator; mathematical model; power electronics; seven-segment space vector pulsewith modulation control strategy; three-phase voltage source PWM rectifier; Mathematical model; Rectifiers; Space vector pulse width modulation; Switches; Voltage control; Control strategy; Incremental PID regulator; Power factor; SVPWM; TMS320LF2407;
Conference_Titel :
Fuzzy Systems and Knowledge Discovery (FSKD), 2011 Eighth International Conference on
Conference_Location :
Shanghai
Print_ISBN :
978-1-61284-180-9
DOI :
10.1109/FSKD.2011.6020044
