Development of solid-state power controller for aerospace applications

There is a developing pattern towards progressively more electric aircraft (MEA) design and system with an expanded number of converters/inverters and electronic circuits. As the electronic system has a favourable position over the conventional mechanical system, the pressure-driven system as far as...

Full description

Saved in:
Bibliographic Details
Main Author: Low, Adrian Wei Chuan
Other Authors: Su Rong
Format: Final Year Project
Language:English
Published: Nanyang Technological University 2020
Subjects:
Online Access:https://hdl.handle.net/10356/139776
Tags: Add Tag
No Tags, Be the first to tag this record!
Institution: Nanyang Technological University
Language: English