I. Introduction
As public and private agencies look towards electric aircraft as the future of air travel, several technical challenges in vehicle power systems have been identified. One such challenge is the development of a robust, high-efficiency and high-energy density converter to drive the electric machines used for propulsion [1], [2]. The flying capacitor multilevel (FCML) inverter is a promising topology that can meet these performance requirements [3]–[5], with recent advances in control through closed-loop, phase-shifted pulse width modulation (PSPWM) demonstrated in [6], [7].