Hybrid Control Strategy for VIENNA Rectifiers in More Electric Aircraft Electrical Systems
The increasing adoption of power electronics devices in the more electric aircraft (MEA) industry brings the need for advanced power quality solutions to ensure stable operation under challenging conditions such as unbalanced grids, unbalanced DC loading, arc faults, and variable grid frequencies. T...
Saved in:
| Main Authors: | , |
|---|---|
| Format: | Article |
| Language: | English |
| Published: |
IEEE
2025-01-01
|
| Series: | IEEE Access |
| Subjects: | |
| Online Access: | https://ieeexplore.ieee.org/document/10988539/ |
| Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
| _version_ | 1850269671227392000 |
|---|---|
| author | Mehmet Can Alphan Gurkan Soykan |
| author_facet | Mehmet Can Alphan Gurkan Soykan |
| author_sort | Mehmet Can Alphan |
| collection | DOAJ |
| description | The increasing adoption of power electronics devices in the more electric aircraft (MEA) industry brings the need for advanced power quality solutions to ensure stable operation under challenging conditions such as unbalanced grids, unbalanced DC loading, arc faults, and variable grid frequencies. This study introduces a hybrid controller for Vienna rectifiers to overcome the addressed power quality issues. The proposed controller strategy integrates Hysteresis Current Control (HCC), a Second Order Generalized Integrator-Phase Locked Loop (SOGI-PLL), and a Proportional Integral Resonant (PIR) controller, collectively improving grid synchronization, enhancing power quality by minimizing total harmonic distortion (THD), and ensuring stable operation during grid disturbances. The proposed strategy achieves a <inline-formula> <tex-math notation="LaTeX">$THD_{i}$ </tex-math></inline-formula> of 2.24%, significantly lower than the 4.74% reported in comparable studies, while maintaining compliance with the requirements of MIL-STD-704F. Extensive simulations validate its effectiveness, demonstrating robust performance in scenarios with unbalanced grids, unbalanced loading, and series arc faults, alongside maintaining minimal DC voltage ripple and near-unity power factor. The findings represent a significant advancement in power electronics, offering a reliable and efficient solution for dynamic and fault-prone electrical systems. |
| format | Article |
| id | doaj-art-a82325925d5042aabf96072ca385d0c2 |
| institution | OA Journals |
| issn | 2169-3536 |
| language | English |
| publishDate | 2025-01-01 |
| publisher | IEEE |
| record_format | Article |
| series | IEEE Access |
| spelling | doaj-art-a82325925d5042aabf96072ca385d0c22025-08-20T01:53:00ZengIEEEIEEE Access2169-35362025-01-0113866868670410.1109/ACCESS.2025.356711310988539Hybrid Control Strategy for VIENNA Rectifiers in More Electric Aircraft Electrical SystemsMehmet Can Alphan0https://orcid.org/0000-0002-7062-2273Gurkan Soykan1https://orcid.org/0000-0001-9516-1314Department of Electrical and Electronics Engineering, Bahçeşehir University, Istanbul, TürkiyeDepartment of Energy System Engineering, Bahçeşehir University, Istanbul, TürkiyeThe increasing adoption of power electronics devices in the more electric aircraft (MEA) industry brings the need for advanced power quality solutions to ensure stable operation under challenging conditions such as unbalanced grids, unbalanced DC loading, arc faults, and variable grid frequencies. This study introduces a hybrid controller for Vienna rectifiers to overcome the addressed power quality issues. The proposed controller strategy integrates Hysteresis Current Control (HCC), a Second Order Generalized Integrator-Phase Locked Loop (SOGI-PLL), and a Proportional Integral Resonant (PIR) controller, collectively improving grid synchronization, enhancing power quality by minimizing total harmonic distortion (THD), and ensuring stable operation during grid disturbances. The proposed strategy achieves a <inline-formula> <tex-math notation="LaTeX">$THD_{i}$ </tex-math></inline-formula> of 2.24%, significantly lower than the 4.74% reported in comparable studies, while maintaining compliance with the requirements of MIL-STD-704F. Extensive simulations validate its effectiveness, demonstrating robust performance in scenarios with unbalanced grids, unbalanced loading, and series arc faults, alongside maintaining minimal DC voltage ripple and near-unity power factor. The findings represent a significant advancement in power electronics, offering a reliable and efficient solution for dynamic and fault-prone electrical systems.https://ieeexplore.ieee.org/document/10988539/More electric aircraft (MEA)power qualityVIENNA rectifier |
| spellingShingle | Mehmet Can Alphan Gurkan Soykan Hybrid Control Strategy for VIENNA Rectifiers in More Electric Aircraft Electrical Systems IEEE Access More electric aircraft (MEA) power quality VIENNA rectifier |
| title | Hybrid Control Strategy for VIENNA Rectifiers in More Electric Aircraft Electrical Systems |
| title_full | Hybrid Control Strategy for VIENNA Rectifiers in More Electric Aircraft Electrical Systems |
| title_fullStr | Hybrid Control Strategy for VIENNA Rectifiers in More Electric Aircraft Electrical Systems |
| title_full_unstemmed | Hybrid Control Strategy for VIENNA Rectifiers in More Electric Aircraft Electrical Systems |
| title_short | Hybrid Control Strategy for VIENNA Rectifiers in More Electric Aircraft Electrical Systems |
| title_sort | hybrid control strategy for vienna rectifiers in more electric aircraft electrical systems |
| topic | More electric aircraft (MEA) power quality VIENNA rectifier |
| url | https://ieeexplore.ieee.org/document/10988539/ |
| work_keys_str_mv | AT mehmetcanalphan hybridcontrolstrategyforviennarectifiersinmoreelectricaircraftelectricalsystems AT gurkansoykan hybridcontrolstrategyforviennarectifiersinmoreelectricaircraftelectricalsystems |