DocumentCode :
1673231
Title :
Stability assessment of electric power systems for ‘more electric’ aircraft
Author :
Griffo, Antonio ; Wang, Jiabin
Author_Institution :
Dept. of Electron. & Electr. Eng., Univ. of Sheffield, Sheffield, UK
fYear :
2009
Firstpage :
1
Lastpage :
10
Abstract :
This paper presents a comprehensive assessment of small-signal stability for a ldquomore-electricrdquo 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.
Keywords :
AC-DC power convertors; aircraft power systems; autotransformers; power system stability; pulse transformers; rectifying circuits; synchronous generators; 18-pulse autotransformer rectifier unit; AC-DC conversion; linearized equations; more-electric aircraft power system; power electronics; small-signal stability assessment; synchronous variable-frequency generator; Aerospace control; Aerospace electronics; Aircraft; Automatic generation control; Power electronics; Power generation; Power supplies; Power system modeling; Power system stability; Synchronous generators; Aerospace; Converter circuit; Modelling; Simulation;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Power Electronics and Applications, 2009. EPE '09. 13th European Conference on
Conference_Location :
Barcelona
Print_ISBN :
978-1-4244-4432-8
Electronic_ISBN :
978-90-75815-13-9
Type :
conf
Filename :
5279220
Link To Document :
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