Abstract
Application features of the resonant accumulator battery energy converter for high-voltage spacecraft power supply systems are considered. The analysis of the energy converter control method under the discharge limitation current of accumulator battery is done and conditions of soft switching of the converter transistors are determined. Experimental verification of the possibility of stabilizing the output load voltage and the mode of limiting the discharge current subject to a change in discharge accumulator battery voltage are conducted. It is established that the limitation of the discharge current is provided by controlling the rectifier. In the course of the studies it is found that providing a soft switching of the rectifier transistors allows to significantly increase the efficiency of the converter and provides the possibility of its practical application in the high frequency region.
| Original language | English |
|---|---|
| Title of host publication | 2018 19th International Conference of Young Specialists on Micro/Nanotechnologies and Electron Devices, EDM 2018 - Proceedings |
| Publisher | IEEE Computer Society |
| Pages | 551-554 |
| Number of pages | 4 |
| Volume | 2018-July |
| ISBN (Print) | 9781538650219 |
| DOIs | |
| Publication status | Published - 13 Aug 2018 |
| Event | 19th International Conference of Young Specialists on Micro/Nanotechnologies and Electron Devices, EDM 2018 - Erlagol, Altai, Russian Federation Duration: 29 Jun 2018 → 3 Jul 2018 |
Conference
| Conference | 19th International Conference of Young Specialists on Micro/Nanotechnologies and Electron Devices, EDM 2018 |
|---|---|
| Country | Russian Federation |
| City | Erlagol, Altai |
| Period | 29.6.18 → 3.7.18 |
Fingerprint
Keywords
- Accumulator battery
- High-voltage power supply system
- Resonant dual active bridge converter
- Soft switching
- Spacecraft
ASJC Scopus subject areas
- Electrical and Electronic Engineering
- Atomic and Molecular Physics, and Optics
Cite this
Research and development of resonant converter for high-voltage spacecraft power supply systems with accumulator battery. / Chernaya, Mariya M.; Shinyakov, Yuriy A.; Yaroslavtsev, Evgeniy V.; Burkin, Evgeniy Yu.
2018 19th International Conference of Young Specialists on Micro/Nanotechnologies and Electron Devices, EDM 2018 - Proceedings. Vol. 2018-July IEEE Computer Society, 2018. p. 551-554 8435047.Research output: Chapter in Book/Report/Conference proceeding › Conference contribution
}
TY - GEN
T1 - Research and development of resonant converter for high-voltage spacecraft power supply systems with accumulator battery
AU - Chernaya, Mariya M.
AU - Shinyakov, Yuriy A.
AU - Yaroslavtsev, Evgeniy V.
AU - Burkin, Evgeniy Yu
PY - 2018/8/13
Y1 - 2018/8/13
N2 - Application features of the resonant accumulator battery energy converter for high-voltage spacecraft power supply systems are considered. The analysis of the energy converter control method under the discharge limitation current of accumulator battery is done and conditions of soft switching of the converter transistors are determined. Experimental verification of the possibility of stabilizing the output load voltage and the mode of limiting the discharge current subject to a change in discharge accumulator battery voltage are conducted. It is established that the limitation of the discharge current is provided by controlling the rectifier. In the course of the studies it is found that providing a soft switching of the rectifier transistors allows to significantly increase the efficiency of the converter and provides the possibility of its practical application in the high frequency region.
AB - Application features of the resonant accumulator battery energy converter for high-voltage spacecraft power supply systems are considered. The analysis of the energy converter control method under the discharge limitation current of accumulator battery is done and conditions of soft switching of the converter transistors are determined. Experimental verification of the possibility of stabilizing the output load voltage and the mode of limiting the discharge current subject to a change in discharge accumulator battery voltage are conducted. It is established that the limitation of the discharge current is provided by controlling the rectifier. In the course of the studies it is found that providing a soft switching of the rectifier transistors allows to significantly increase the efficiency of the converter and provides the possibility of its practical application in the high frequency region.
KW - Accumulator battery
KW - High-voltage power supply system
KW - Resonant dual active bridge converter
KW - Soft switching
KW - Spacecraft
UR - http://www.scopus.com/inward/record.url?scp=85052376681&partnerID=8YFLogxK
UR - http://www.scopus.com/inward/citedby.url?scp=85052376681&partnerID=8YFLogxK
U2 - 10.1109/EDM.2018.8435047
DO - 10.1109/EDM.2018.8435047
M3 - Conference contribution
SN - 9781538650219
VL - 2018-July
SP - 551
EP - 554
BT - 2018 19th International Conference of Young Specialists on Micro/Nanotechnologies and Electron Devices, EDM 2018 - Proceedings
PB - IEEE Computer Society
ER -