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Optimal Design and Synthesis of MEA Power System Architectures considering Reliability Specifications

Recalde, Angel A.; Atkin, Jason A.; Bozhko, Serhiy V.

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Authors

Angel A. Recalde

JASON ATKIN jason.atkin@nottingham.ac.uk
Associate Professor

SERHIY BOZHKO serhiy.bozhko@nottingham.ac.uk
Professor of Aircraft Electric Power Systems



Abstract

IEEE Aircraft electrification requires novel designs to supply the growing demand for electric power on-board through efficient and reliable production and distribution of electrical energy. Moreover, the aircraft power system will be a key enabler for the integration of future technologies. Pledging to these intentions, we propose a formulation to synthesize a power system architecture that complies with safety specifications following a Platform Based Design methodology that optimizes the main aerospace drivers. Due to the non-linear nature of the design problem, this paper presents reliability based MILP network design formulations for topology synthesis. The novelty of this approach relies in the adoption of network design optimization for MEA power system construction that allows explicit design formulations as MILP problems. This approach will provide an effective way to include safety specifications by introducing reliability and resiliency constraints.

Citation

Recalde, A. A., Atkin, J. A., & Bozhko, S. V. (2020). Optimal Design and Synthesis of MEA Power System Architectures considering Reliability Specifications. IEEE Transactions on Transportation Electrification, 6(4), 1801-1818. https://doi.org/10.1109/TTE.2020.3002875

Journal Article Type Article
Acceptance Date Jun 9, 2020
Online Publication Date Jun 16, 2020
Publication Date 2020-12
Deposit Date Jun 17, 2020
Publicly Available Date Jun 19, 2020
Journal IEEE Transactions on Transportation Electrification
Electronic ISSN 2332-7782
Publisher Institute of Electrical and Electronics Engineers
Peer Reviewed Peer Reviewed
Volume 6
Issue 4
Pages 1801-1818
DOI https://doi.org/10.1109/TTE.2020.3002875
Keywords optimization methods, aircraft power systems, reliability, linear programming, design methodology
Public URL https://nottingham-repository.worktribe.com/output/4668261
Publisher URL https://ieeexplore.ieee.org/document/9118967
Additional Information © 2020 IEEE.Personal use of this material is permitted. Permission from IEEE must be obtained for all other uses, in any current or future media, including reprinting/republishing this material for advertising or promotional purposes,creating new collective works, for resale or redistribution to servers or lists, or reuse of any copyrighted component of this work in other works.

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