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...
Saved in:
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 |
Similar Items
-
Design and testing of a solid-state power controller control and protection card for aerospace application
by: Singh, Davinder
Published: (2019) -
Development of power converter for aerospace applications
by: Tan, Melvin Yu Fei
Published: (2023) -
Development of DC/AC power controller in aerospace power system
by: Ang, Cheryl Hui Miin
Published: (2021) -
Solid state power controller
by: Ng, Tze Wei
Published: (2021) -
Exploring electrification in the aerospace industry and development of Aerospace Power System Evaluation Tool (APSET)
by: Ong, Cody Wai Kiat
Published: (2019)