Angel A. Recalde
Optimal Design and Synthesis of MEA Power System Architectures considering Reliability Specifications
Recalde, Angel A.; Atkin, Jason A.; Bozhko, Serhiy V.
Authors
Dr JASON ATKIN JASON.ATKIN@NOTTINGHAM.AC.UK
ASSOCIATE PROFESSOR
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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