Stability analysis of electric power systems for ‘more electric’ aircraft

Abstract

This paper presents a comprehensive assessment of small-signal stability for a “more-electric” aircraft power system consisting of a synchronous variable-frequency generator which supplies several power electronic controlled loads via an 18-pulse autotransformer rectifier unit (ATRU) for AC-DC conversion. Functional models for key power system components and loads are derived. Numerical tools employed for the automatic calculation of linearized equations and operating points are described, and the influence of leading design and operational parameter on system stability is evaluated.

Metadata

Item Type:	Proceedings Paper
Authors/Creators:	Griffo, Antonio Wang, J.B. Howe, D.
Copyright, Publisher and Additional Information:	3rd International Conference “From Scientific Computing to Computational Engineering" 3rd IC-SCCE Athens, 9-12 July, 2008 © IC-SCCE
Keywords:	power systems, stability, linearization
Dates:	Published: July 2008
Institution:	The University of Sheffield
Academic Units:	The University of Sheffield > Faculty of Engineering (Sheffield) > Department of Electronic and Electrical Engineering (Sheffield)
Depositing User:	Dr Antonio Griffo
Date Deposited:	02 Sep 2008 12:56
Last Modified:	19 Dec 2022 13:19
Status:	Published
Refereed:	Yes
Related URLs:	http://www.scce.gr/
Open Archives Initiative ID (OAI ID):	oai:eprints.whiterose.ac.uk:4495

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Stability analysis of electric power systems for ‘more electric’ aircraft

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