Automated stability assessment of more electric aircraft electrical power systems

Author

Hill, Christopher Ian ; Areerak, Kongpan ; Tao Yang ; Bozhko, Serhiy ; Odavic, Milijana

Author_Institution

Power Electron. Machines & Control Res. Group, Univ. of Nottingham, Nottingham, UK

fYear

2015

fDate

3-5 March 2015

Firstpage

1

Lastpage

6

Abstract

This paper has details the theoretical background, development and application of a newly developed Automated Stability Assessment Tool for More Electric Aircraft Electrical Power Systems. This tool is shown to provide an easy to use and extremely flexible way for system designers to analyze Electrical Power System stability. It is shown how system parameters can be easily varied in order to investigate their impact on Electrical Power System stability. This methodology could therefore save significant time and money, both by accelerating the design process, and by helping design engineers to select the lowest cost components needed to ensure Electrical Power System stability.

Keywords

aircraft power systems; eigenvalues and eigenfunctions; power system stability; automated stability assessment; eigenvalues; electrical power system stability; more electric aircraft; Aerospace electronics; Aircraft; Eigenvalues and eigenfunctions; Mathematical model; Power system stability; Rectifiers; Stability analysis; ASAT; Eigenvalues; Electrical Power System; More Electric Aircraft; Stability;

fLanguage

English

Publisher

ieee

Conference_Titel

Electrical Systems for Aircraft, Railway, Ship Propulsion and Road Vehicles (ESARS), 2015 International Conference on

Conference_Location

Aachen

Type

conf

DOI

10.1109/ESARS.2015.7101426

Filename

7101426