Design of a Half-Bridge Current-Source Inverter Topology for Avionic Systems
This paper analyses a new half-bridge current–source inverter for avionic systems. In the circuit, two 28 V batteries are used as inputs. These voltage sources are connected to inductors which create a constant current source. Then only two high-frequency switches are used to waveshape the positive...
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| Hauptverfasser: | , |
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| Format: | Artigo |
| Sprache: | Inglês |
| Veröffentlicht: |
MDPI AG
2022-07-01
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| Schriftenreihe: | Aerospace |
| Schlagworte: | |
| Online-Zugang: | https://www.mdpi.com/2226-4310/9/7/354 |
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