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Condicionador eletrônico de potência para barramento de tensão CC em sistema elétrico aeronaútico

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Author(s):
Mateus Pinheiro Dias
Total Authors: 1
Document type: Master's Dissertation
Institution: Universidade Estadual de Campinas (UNICAMP). Faculdade de Engenharia Elétrica e de Computação
Defense date:
Examining board members:
Flávio Alessandro Serrão Gonçalves; João Inácio Yutaka Ota
Advisor: José Antenor Pomilio
Abstract

This project deals with the Electric Power Quality (PQ) in aeronautical environments. The More Electric Aircraft (MEA) concept focuses in the replacement of pneumatic and hy-draulic actuators by electromechanical actuators and increases the electric power demand in the aircraft. The master project aims to the study and the implementation of a Power Electronic Conditioner (PEC) to mitigate the unwanted effects found in the DC aircraft internal feeders. The PEC must deal with the current unbalance between the positive and negative poles of the DC bus to comply with the standards. The specific objectives are the development of a mathematical dynamic model for the current redistributor used as PEC and the study of control strategies for this aircraft electrical environment. Digital control solutions, with DSPs, FPGAs were studied along the project development. The appendixes provide the paper published in Cobep/Spec 2019 and experimental Setup (AU)

FAPESP's process: 17/11623-0 - DC bus power electronic conditioner for aircraft electric system
Grantee:Mateus Pinheiro Dias
Support type: Scholarships in Brazil - Master