Electrical braking in matrix converter for more electric aircraft: bi-directional switch and input power clamp methods
Current aircraft power quality specifications do not allow regeneration onto the power bus. Therefore, the inherent regeneration available from Matrix Converter (MC) is not desirable in More Electric Aircraft (MEA) aerospace applications. In this paper, novel methods to avoid regeneration from the M...
| Main Authors: | , |
|---|---|
| Format: | Article |
| Language: | English |
| Published: |
American Scientific Publishers
2015
|
| Online Access: | http://eprints.nottingham.ac.uk/34477/ http://eprints.nottingham.ac.uk/34477/ http://eprints.nottingham.ac.uk/34477/ http://eprints.nottingham.ac.uk/34477/1/Electrical%20Braking%20in%20Matrix%20Converter%20for%20More%20Electric%20Aircraft%20BDS%20and%20IPC%20Methods.pdf |