Comparison between system design optimization strategies for more electric aircraft network

Issue title: Special Supplement Issue: Selected papers from the 13th International Workshop on Optimization and Inverse Problems in Electromagnetism (OIPE 2014)

Guest editors: Domenico Lahaye

Article type: Research Article

Authors: Hadbi, Djamel^{a; b; *} | Retière, Nicolas^a | Wurtz, Frederic^a | Roboam, Xavier^b | Sareni, Bruno^b

Affiliations: [a] University Grenoble Alpes, Grenoble F-38000, France | [b] Université de Toulouse, Toulouse 31071, France

Correspondence: [*] Corresponding author: Djamel Hadbi, University Grenoble Alpes, CNRS, G2Elab, F-38000 Grenoble, France. E-mail:[email protected]

Abstract: The aircraft electric network is a complex system, consisting of many different elements integrated to form a unique entity, designed to perform a well-defined mission. In the current state, the network conceptual design is based on standards defined by the aircraft manufacturer. As a consequence, electric subsystem suppliers are doing local optimizations to fulfill these standards in a separated way through a ``mechanistic approach''. This results in a set of optimized subsystems which is not necessarily ``optimal'' with respect to the network level. To overcome this problem, we present a design approach called EPFM (Extended Pareto Front Method) based on separated subsystem optimizations which aims at finding an optimal configuration of the electrical network at the system level. The EPFM is discussed with regard to the computational cost and the collaboration requirements in the aeronautical industrial context and compared with the classical mechanistic approach.

Keywords: System design, integrated optimal design, multilevel optimization, embedded electrical system

DOI: 10.3233/JAE-140174

Journal: International Journal of Applied Electromagnetics and Mechanics, vol. 53, no. S2, pp. S289-S305, 2017