발사대 유도전동기 제어를 위한 드라이버 모듈 개발

Development of IGBT Driver Module for Control of Launcher Induction Motor

초록

This paper describes the design and fabrication of an IGBT (Insulated Gate Bipolar Transistor) drivermodule for controlling launcher induction motors. The IGBT driver module converts digital voltage levelswitching signals from a microcontroller into gate control signals for the IGBT. It employs a Half Bridgetype IGBT driver and integrates a PNP (Positive-Negative-Positive) transistor circuit for on/off functionality. Toprotect peripheral devices from surge voltages generated during high-capacity power switching, the moduleincorporates an isolated DC/DC converter and a photocoupler circuit. The fabricated IGBT driver moduleunderwent testing in conjunction with an IGBT module equipped with IGBTs, and experimental resultsvalidated the smooth operation of the driver module. Therefore, the proposed IGBT driver module is suitablefor application in motor controllers for launcher induction motor control.

키워드

IGBT Driver(절연 게이트 양극성 트랜지스터 드라이버); Launcher Induction Motor(발사대 유도전동기); Motor Controller(모터제어장치); Electronic Circuit(전자회로)
제목
발사대 유도전동기 제어를 위한 드라이버 모듈 개발
제목 (타언어)
Development of IGBT Driver Module for Control of Launcher Induction Motor
저자
서세욱; 김희숙; 김갑순
DOI
10.14775/ksmpe.2024.23.08.040
발행일
2024-08
저널명
한국기계가공학회지
권
23
호
8
페이지
40 ~ 48