Stability assessment of a droop-controlled multi-generator electrical power system in the more electric aircraft using parameter space approach

This paper investigates the dynamic stability of a droop-controlled multi-generator system in the more electric aircraft (MEA). Based on the developed state-space model of the potential dc electrical power system (EPS) architecture, the stability boundaries of EPS operation depending on parameter va...

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Main Authors: Gao, Fei, Zheng, Xiancheng, Bozhko, Serhiy
Format: Conference or Workshop Item
Published: 2017
Subjects:
Online Access:https://eprints.nottingham.ac.uk/35009/
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author Gao, Fei
Zheng, Xiancheng
Bozhko, Serhiy
author_facet Gao, Fei
Zheng, Xiancheng
Bozhko, Serhiy
author_sort Gao, Fei
building Nottingham Research Data Repository
collection Online Access
description This paper investigates the dynamic stability of a droop-controlled multi-generator system in the more electric aircraft (MEA). Based on the developed state-space model of the potential dc electrical power system (EPS) architecture, the stability boundaries of EPS operation depending on parameter variations including component parameters and operating conditions are investigated. The effect of multiple parametric uncertainties on EPS stability is graphically illustrated by stability regions maps. In addition, the effect of the droop coefficient on the stability is discussed from the impedance point of view. The detailed mathematical models and analytical results of stability assessment are verified by time domain simulation studies.
first_indexed 2025-11-14T19:24:50Z
format Conference or Workshop Item
id nottingham-35009
institution University of Nottingham Malaysia Campus
institution_category Local University
last_indexed 2025-11-14T19:24:50Z
publishDate 2017
recordtype eprints
repository_type Digital Repository
spelling nottingham-350092020-05-04T18:34:27Z https://eprints.nottingham.ac.uk/35009/ Stability assessment of a droop-controlled multi-generator electrical power system in the more electric aircraft using parameter space approach Gao, Fei Zheng, Xiancheng Bozhko, Serhiy This paper investigates the dynamic stability of a droop-controlled multi-generator system in the more electric aircraft (MEA). Based on the developed state-space model of the potential dc electrical power system (EPS) architecture, the stability boundaries of EPS operation depending on parameter variations including component parameters and operating conditions are investigated. The effect of multiple parametric uncertainties on EPS stability is graphically illustrated by stability regions maps. In addition, the effect of the droop coefficient on the stability is discussed from the impedance point of view. The detailed mathematical models and analytical results of stability assessment are verified by time domain simulation studies. 2017-02-16 Conference or Workshop Item PeerReviewed Gao, Fei, Zheng, Xiancheng and Bozhko, Serhiy (2017) Stability assessment of a droop-controlled multi-generator electrical power system in the more electric aircraft using parameter space approach. In: 8th Annual IEEE Energy Conversion Congress & Exposition (ECCE 2016), 18-22 September 2016, Milwaukee, USA. Parameter space method stability droop control constant power load more electric aircraft multi-generator system http://ieeexplore.ieee.org/document/7855459/
spellingShingle Parameter space method
stability
droop control
constant power load
more electric aircraft
multi-generator system
Gao, Fei
Zheng, Xiancheng
Bozhko, Serhiy
Stability assessment of a droop-controlled multi-generator electrical power system in the more electric aircraft using parameter space approach
title Stability assessment of a droop-controlled multi-generator electrical power system in the more electric aircraft using parameter space approach
title_full Stability assessment of a droop-controlled multi-generator electrical power system in the more electric aircraft using parameter space approach
title_fullStr Stability assessment of a droop-controlled multi-generator electrical power system in the more electric aircraft using parameter space approach
title_full_unstemmed Stability assessment of a droop-controlled multi-generator electrical power system in the more electric aircraft using parameter space approach
title_short Stability assessment of a droop-controlled multi-generator electrical power system in the more electric aircraft using parameter space approach
title_sort stability assessment of a droop-controlled multi-generator electrical power system in the more electric aircraft using parameter space approach
topic Parameter space method
stability
droop control
constant power load
more electric aircraft
multi-generator system
url https://eprints.nottingham.ac.uk/35009/
https://eprints.nottingham.ac.uk/35009/