The document develops a functional model of symmetrical multi pulse autotransformer rectifier units (ATRUs) for use in more-electric aircraft applications. Currently, there is no model of ATRUs suitable for unbalanced or faulty conditions. This paper aims to fill that gap by developing functional models for ATRUs that work for both balanced and unbalanced operating conditions. The functional models are validated through simulation and experiment, and show significant improvements in simulation efficiency over detailed switching models, especially under balanced operating conditions.