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An Approach for Utilizing Power Flow Modeling for Simulations of Hybrid Electric Propulsion Systems
Author(s) -
Jeffryes W. Chapman,
Jonathan S. Litt
Publication year - 2018
Publication title -
nasa sti repository (national aeronautics and space administration)
Language(s) - English
Resource type - Conference proceedings
DOI - 10.2514/6.2018-5018
Subject(s) - propulsion , power flow , computer science , electrically powered spacecraft propulsion , power (physics) , aerospace engineering , flow (mathematics) , modelica , electric power system , automotive engineering , engineering , simulation , physics , mechanics , quantum mechanics
This paper describes an approach to creating simulations of the electric components for a hybrid electric propulsion system. The proposed modeling technique is based on power/load flow modeling and is designed to provide a modular framework that includes buses, lines, and other electrical components that can be connected together to form the electrical distribution system. The purpose of this paper is to detail an electric distribution system modeling technique and to demonstrate how these models may be integrated with turbomachinery simulations. These general modeling techniques were created to be utilized for system and control design studies. Additionally, steady-state and dynamic performance for a proposed model example is compared with data from a hardware in the loop simulation.

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