DocumentCode
39645
Title
In this issue - Technically
Volume
28
Issue
12
fYear
2013
fDate
Dec. 2013
Firstpage
2
Lastpage
2
Abstract
Growing electrical load demands in the aircraft industry has resulted in an increase of DC voltage levels. As a consequence, new technologies like the solid state power controller (SSPC) have been introduced that both connect loads to the main electrical bus and protect the electrical installations from overloads and short circuits. In order to analyze the infuence of these new protection devices on the onboard power distribution system (PDS) and to predict either failures or malfunctions, models of SSPC have to be developed. This article presents and analyses a behavioral model for SSPC.
fLanguage
English
Journal_Title
Aerospace and Electronic Systems Magazine, IEEE
Publisher
ieee
ISSN
0885-8985
Type
jour
DOI
10.1109/MAES.2013.6693661
Filename
6693661
Link To Document