Abstract
Today the electrification of flight is more popular than ever, creating a wide array of concept aircraft and associated power system topologies. In order to gain insights into benefits of these varying architectures, this paper introduces the development of a framework for electric aircraft power system (EAPS) optimization. The proposed framework accepts inputs from a designer in the form of component parameters and desired flight mission characteristics. A collective graph representing many architectures is formed, from which, subgraphs or power system topologies meeting the flight requirements are extracted and analyzed. An optimum topology meeting the flight requirements with minimum mass, maximum efficiency and reliability can be subsequently selected from these subgraphs. The presented results include the comparative analysis of different EAPS types with respect to the competing performance metrics of mass and efficiency.
Original language | English |
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Title of host publication | 2020 IEEE Transportation Electrification Conference and Expo, ITEC 2020 |
Pages | 809-813 |
Number of pages | 5 |
ISBN (Electronic) | 9781728146294 |
DOIs | |
State | Published - Jun 2020 |
Event | 2020 IEEE Transportation Electrification Conference and Expo, ITEC 2020 - Chicago, United States Duration: Jun 23 2020 → Jun 26 2020 |
Publication series
Name | 2020 IEEE Transportation Electrification Conference and Expo, ITEC 2020 |
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Conference
Conference | 2020 IEEE Transportation Electrification Conference and Expo, ITEC 2020 |
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Country/Territory | United States |
City | Chicago |
Period | 6/23/20 → 6/26/20 |
Bibliographical note
Funding Information:The support of this research by the National Aeronautics and Space Administration, through the NASA Grant no. KY GF-19-051, is gratefully acknowledged.
Publisher Copyright:
© 2020 IEEE.
Keywords
- electric aircraft
- graph theory
- optimization
- power systems
ASJC Scopus subject areas
- Energy Engineering and Power Technology
- Automotive Engineering
- Transportation