This paper presents the implementation of a Single Ended Primary Inductance Converter (SEPIC) in Bridgeless configuration for AC-DC conversion More Electric Aircraft (MEA - More Electric Aircraft). The Bridgeless configuration allows better efficiency due to the reduction of the number of diodes and the drive control and sensing systems are simplified when operating in Discontinuous Conduction Mode (DCM). Theoretical and experimental results are presented in this paper proposal and the complete analysis will be presented in the final version.
