Proportional-resonant controlled NPC converter for more-electric-aircraft starter-generator

More electric aircraft (MEA) technology is achieved by exchanging various mechanical and pneumatic elements of a conventional aircraft with their equivalent electrical devices in order to increase the reliability and decrease the maintenance. This paper proposes a proportional resonant (PR) controll...

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Main Authors: Dehghani Tafti, Hossein, Lim, Ziyou, Raj, Pinkymol Harikrishna, Maswood, Ali Iftekhar, Ooi, Gabriel Heo Peng
Other Authors: School of Electrical and Electronic Engineering
Format: Conference or Workshop Item
Language:English
Published: 2015
Subjects:
Online Access:https://hdl.handle.net/10356/98052
http://hdl.handle.net/10220/38524
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Institution: Nanyang Technological University
Language: English
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spelling sg-ntu-dr.10356-980522021-01-14T07:09:28Z Proportional-resonant controlled NPC converter for more-electric-aircraft starter-generator Dehghani Tafti, Hossein Lim, Ziyou Raj, Pinkymol Harikrishna Maswood, Ali Iftekhar Ooi, Gabriel Heo Peng School of Electrical and Electronic Engineering 2015 IEEE 11th International Conference on Power Electronics and Drive Systems (PEDS 2015) Energy Research Institute @ NTU (ERI@N) DRNTU::Engineering::Electrical and electronic engineering::Power electronics More electric aircraft (MEA) technology is achieved by exchanging various mechanical and pneumatic elements of a conventional aircraft with their equivalent electrical devices in order to increase the reliability and decrease the maintenance. This paper proposes a proportional resonant (PR) controller together with the adaptive space vector modulation (ASVM) technique for the more electric aircraft (MEA) starter-generator neutral-point clamped (NPC) converter. The proposed controller is implemented in the stationary (αβ) frame where the calculated reference voltages of the PR controller can be directly fed into the ASVM. Hence, the main objectives of the proposed controller are to reduce the computational complexity and the steady state error by decreasing the required number of framework transformations units. On top of that, the ASVM technique provides a proper DC-link capacitor voltage balancing with improved output power quality. The dynamic performance of the proposed controller is evaluated under both initial starting interval and generating mode. ASTAR (Agency for Sci., Tech. and Research, S’pore) Accepted version 2015-08-26T04:16:33Z 2019-12-06T19:50:04Z 2015-08-26T04:16:33Z 2019-12-06T19:50:04Z 2015 2015 Conference Paper Dehghani Tafti, H., Maswood, A. I., Lim, Z., Ooi, G. H. P., & Raj, P. H. (2015). Proportional-resonant controlled NPC converter for more-electric-aircraft starter-generator. 2015 IEEE 11th International Conference on Power Electronics and Drive Systems. https://hdl.handle.net/10356/98052 http://hdl.handle.net/10220/38524 10.1109/PEDS.2015.7203443 en © 2015 IEEE. Personal use of this material is permitted. Permission from IEEE must be obtained for all other uses, in any current or future media, including reprinting/republishing this material for advertising or promotional purposes, creating new collective works, for resale or redistribution to servers or lists, or reuse of any copyrighted component of this work in other works. The published version is available at: [http://dx.doi.org/10.1109/PEDS.2015.7203443]. application/pdf
institution Nanyang Technological University
building NTU Library
continent Asia
country Singapore
Singapore
content_provider NTU Library
collection DR-NTU
language English
topic DRNTU::Engineering::Electrical and electronic engineering::Power electronics
spellingShingle DRNTU::Engineering::Electrical and electronic engineering::Power electronics
Dehghani Tafti, Hossein
Lim, Ziyou
Raj, Pinkymol Harikrishna
Maswood, Ali Iftekhar
Ooi, Gabriel Heo Peng
Proportional-resonant controlled NPC converter for more-electric-aircraft starter-generator
description More electric aircraft (MEA) technology is achieved by exchanging various mechanical and pneumatic elements of a conventional aircraft with their equivalent electrical devices in order to increase the reliability and decrease the maintenance. This paper proposes a proportional resonant (PR) controller together with the adaptive space vector modulation (ASVM) technique for the more electric aircraft (MEA) starter-generator neutral-point clamped (NPC) converter. The proposed controller is implemented in the stationary (αβ) frame where the calculated reference voltages of the PR controller can be directly fed into the ASVM. Hence, the main objectives of the proposed controller are to reduce the computational complexity and the steady state error by decreasing the required number of framework transformations units. On top of that, the ASVM technique provides a proper DC-link capacitor voltage balancing with improved output power quality. The dynamic performance of the proposed controller is evaluated under both initial starting interval and generating mode.
author2 School of Electrical and Electronic Engineering
author_facet School of Electrical and Electronic Engineering
Dehghani Tafti, Hossein
Lim, Ziyou
Raj, Pinkymol Harikrishna
Maswood, Ali Iftekhar
Ooi, Gabriel Heo Peng
format Conference or Workshop Item
author Dehghani Tafti, Hossein
Lim, Ziyou
Raj, Pinkymol Harikrishna
Maswood, Ali Iftekhar
Ooi, Gabriel Heo Peng
author_sort Dehghani Tafti, Hossein
title Proportional-resonant controlled NPC converter for more-electric-aircraft starter-generator
title_short Proportional-resonant controlled NPC converter for more-electric-aircraft starter-generator
title_full Proportional-resonant controlled NPC converter for more-electric-aircraft starter-generator
title_fullStr Proportional-resonant controlled NPC converter for more-electric-aircraft starter-generator
title_full_unstemmed Proportional-resonant controlled NPC converter for more-electric-aircraft starter-generator
title_sort proportional-resonant controlled npc converter for more-electric-aircraft starter-generator
publishDate 2015
url https://hdl.handle.net/10356/98052
http://hdl.handle.net/10220/38524
_version_ 1690658400031997952