An Integrated Design Methodology for Architecture Solutions to Shimmy Reduction Subsystems in All Electric Aircraft
No Thumbnail Available
Access rights
openAccess
acceptedVersion
URL
Journal Title
Journal ISSN
Volume Title
A1 Alkuperäisartikkeli tieteellisessä aikakauslehdessä
This publication is imported from Aalto University research portal.
View publication in the Research portal (opens in new window)
View/Open full text file from the Research portal (opens in new window)
Other link related to publication (opens in new window)
View publication in the Research portal (opens in new window)
View/Open full text file from the Research portal (opens in new window)
Other link related to publication (opens in new window)
Date
2024
Major/Subject
Mcode
Degree programme
Language
en
Pages
13
Series
IEEE Transactions on Transportation Electrification, Volume 10, issue 4, pp. 10428-10440
Abstract
This article investigates the search for architecture solutions to a novel shimmy reduction subsystem in the nose wheel steering system (NWSS) of all-electric aircraft (AEA). Since the traditional trial-and-error and empirical methods are inefficient and infeasible in this study, respectively, a new methodology for system architecture design is needed. The integrated methodology combines the systems engineering engine method and V-model to explore the design space of the shimmy reduction subsystem, defines the parameters of the low-level product using general morphological analysis (GMA), eliminates incompatible alternatives through cross-consistency assessment (CCA), and, after morphological analysis, subjects the solutions that satisfy the optimal design set to a single-objective decision based on cost-effectiveness analysis (CEA). Furthermore, a product realization of the final selected design solution is presented, along with the implementation and verification processes. The methodology deals with the problem in the design of the shimmy reduction subsystem in AEA.Description
Publisher Copyright: IEEE
Keywords
Aircraft, All electric aircraft, Damping, Gears, Nose, Shock absorbers, System analysis and design, Wheels, electromagnetic damper, morphological analysis, shimmy reduction and system design, electromagnetic damper (EMD), All electric aircraft (AEA)
Other note
Citation
She, C, Zhang, M, Hinkkanen, M & Yang, Y 2024, ' An Integrated Design Methodology for Architecture Solutions to Shimmy Reduction Subsystems in All Electric Aircraft ', IEEE Transactions on Transportation Electrification, vol. 10, no. 4, pp. 10428-10440 . https://doi.org/10.1109/TTE.2024.3376973