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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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 |
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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 |
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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. |
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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 |
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1690658400031997952 |