Modeling and Simulation of Power Distribution System in More Electric Aircraft
The More Electric Aircraft concept is a fast-developing trend in modern aircraft industry. With this new concept, the performance of the aircraft can be further optimized and meanwhile the operating and maintenance cost will be decreased effectively. In order to optimize the power system integrity a...
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| Main Authors: | , , , |
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| Format: | Article |
| Language: | English |
| Published: |
Wiley
2015-01-01
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| Series: | Journal of Electrical and Computer Engineering |
| Online Access: | http://dx.doi.org/10.1155/2015/847624 |
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| _version_ | 1832556659915882496 |
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| author | Zhangang Yang Junchao Qu Yingchuan Ma Xudong Shi |
| author_facet | Zhangang Yang Junchao Qu Yingchuan Ma Xudong Shi |
| author_sort | Zhangang Yang |
| collection | DOAJ |
| description | The More Electric Aircraft concept is a fast-developing trend in modern aircraft industry. With this new concept, the performance of the aircraft can be further optimized and meanwhile the operating and maintenance cost will be decreased effectively. In order to optimize the power system integrity and have the ability to investigate the performance of the overall system in any possible situations, one accurate simulation model of the aircraft power system will be very helpful and necessary. This paper mainly introduces a method to build a simulation model for the power distribution system, which is based on detailed component models. The power distribution system model consists of power generation unit, transformer rectifier unit, DC-DC converter unit, and DC-AC inverter unit. In order to optimize the performance of the power distribution system and improve the quality of the distributed power, a feedback control network is designed based on the characteristics of the power distribution system. The simulation result indicates that this new simulation model is well designed and it works accurately. Moreover, steady state performance and transient state performance of the model can fulfill the requirements of aircraft power distribution system in the realistic application. |
| format | Article |
| id | doaj-art-1d486daca08d47b6a1d33d5d1a0b33c7 |
| institution | Kabale University |
| issn | 2090-0147 2090-0155 |
| language | English |
| publishDate | 2015-01-01 |
| publisher | Wiley |
| record_format | Article |
| series | Journal of Electrical and Computer Engineering |
| spelling | doaj-art-1d486daca08d47b6a1d33d5d1a0b33c72025-02-03T05:44:36ZengWileyJournal of Electrical and Computer Engineering2090-01472090-01552015-01-01201510.1155/2015/847624847624Modeling and Simulation of Power Distribution System in More Electric AircraftZhangang Yang0Junchao Qu1Yingchuan Ma2Xudong Shi3Aeronautical Automation College, Civil Aviation University of China, Tianjin 300300, ChinaAeronautical Automation College, Civil Aviation University of China, Tianjin 300300, ChinaAeronautical Automation College, Civil Aviation University of China, Tianjin 300300, ChinaAeronautical Automation College, Civil Aviation University of China, Tianjin 300300, ChinaThe More Electric Aircraft concept is a fast-developing trend in modern aircraft industry. With this new concept, the performance of the aircraft can be further optimized and meanwhile the operating and maintenance cost will be decreased effectively. In order to optimize the power system integrity and have the ability to investigate the performance of the overall system in any possible situations, one accurate simulation model of the aircraft power system will be very helpful and necessary. This paper mainly introduces a method to build a simulation model for the power distribution system, which is based on detailed component models. The power distribution system model consists of power generation unit, transformer rectifier unit, DC-DC converter unit, and DC-AC inverter unit. In order to optimize the performance of the power distribution system and improve the quality of the distributed power, a feedback control network is designed based on the characteristics of the power distribution system. The simulation result indicates that this new simulation model is well designed and it works accurately. Moreover, steady state performance and transient state performance of the model can fulfill the requirements of aircraft power distribution system in the realistic application.http://dx.doi.org/10.1155/2015/847624 |
| spellingShingle | Zhangang Yang Junchao Qu Yingchuan Ma Xudong Shi Modeling and Simulation of Power Distribution System in More Electric Aircraft Journal of Electrical and Computer Engineering |
| title | Modeling and Simulation of Power Distribution System in More Electric Aircraft |
| title_full | Modeling and Simulation of Power Distribution System in More Electric Aircraft |
| title_fullStr | Modeling and Simulation of Power Distribution System in More Electric Aircraft |
| title_full_unstemmed | Modeling and Simulation of Power Distribution System in More Electric Aircraft |
| title_short | Modeling and Simulation of Power Distribution System in More Electric Aircraft |
| title_sort | modeling and simulation of power distribution system in more electric aircraft |
| url | http://dx.doi.org/10.1155/2015/847624 |
| work_keys_str_mv | AT zhangangyang modelingandsimulationofpowerdistributionsysteminmoreelectricaircraft AT junchaoqu modelingandsimulationofpowerdistributionsysteminmoreelectricaircraft AT yingchuanma modelingandsimulationofpowerdistributionsysteminmoreelectricaircraft AT xudongshi modelingandsimulationofpowerdistributionsysteminmoreelectricaircraft |