NDLI: Accelerated functional-level modeling of more-electric aircraft electrical power system

Content Provider	IEEE Xplore Digital Library
Author	Bozhko, S.V. Wu, T. Asher, G.M. Wheeler, P.W.
Copyright Year	2010
Description	Author affiliation: The University of Nottingham, Nottingham NG7 2RD, United Kingdom (Bozhko, S.V.; Wu, T.; Asher, G.M.; Wheeler, P.W.)
Abstract	The more-electric aircraft concept (MEA) is one of the major trends in modern aircraft electric power system (EPS) engineering that results in a significantly increased number of onboard loads driven by power-electronics. Development of appropriate EPS architectures requires intensive simulations to ensure the system integrity, requested quality and performance under possible normal and abnormal scenarios. At the same time, the increased use of tightly-controlled motor drives and power electronic converters can make the simulation of the large-scale EPS impractical due to enormous computation time or numerical non-convergence due to the model complexity. This paper addresses the development of a functional models library capable of significant improvement in simulation time whilst maintaining good accuracy up to a specified frequency range. The library application is demonstrated on the example study of the performance of a twin-generator example EPS under both normal and faulty regimes.
Starting Page	1
Ending Page	6
File Size	364767
Page Count	6
File Format	PDF
ISBN	9781424490929
e-ISBN	9781424490943
DOI	10.1109/ESARS.2010.5665198
Language	English
Publisher	Institute of Electrical and Electronics Engineers, Inc. (IEEE)
Publisher Date	2010-10-19
Publisher Place	Italy
Access Restriction	Subscribed
Rights Holder	Institute of Electrical and Electronics Engineers, Inc. (IEEE)
Subject Keyword	Computational modeling Atmospheric modeling Benchmark testing Steady-state Circuit faults Aircraft Load modeling
Content Type	Text
Resource Type	Article

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