Multiport Converter for CubeSat

Maximizing solar energy harvesting and miniaturizing DC-to-DC converters will be a difficult task for the CubeSat that operates in low earth orbit (LEO), where size weight are limited. To maximize collection, electrical power system (EPS) architectures use numerous separate DC–DC converters, which problem miniaturization of whole model because several inductors used each converter. The key purpose this article is to demonstrate topology multiport converter requires only one inductor small number components, reducing overall size. proposed have half-bridge modules with series connection, connected parallelly PV panels battery through DC-DC boost On considering 1U standards prototype verify performance case scenarios.