Spacecraft electrical power systems (EPS) using the Flyback converters

Abstract

The paper depicts generation of solar power by the charge controller skills to charge the battery bank at a persnickety voltage during the sunbeams by the Flyback converter to make use of this power at spacecraft power systems during the orbital night or when the load demand goes beyond the solar booth or array capacity. All bits and pieces are supervised by the Flyback power supply entity as light weight, high power density, solid size, least cost, stumpy silhouette, low volume, tight regulations, fine design, high reliability, least failure rate and high efficiency as EPS of a spacecraft.