Skip to Main content Skip to Navigation
Journal articles

Multi-level integrated optimal design for power systems of more electric aircraft

Abstract : This paper proposes a multi-level optimal design method for a complex actuation system of more electric aircraft. The multilevel structure consists in sharing the optimization process in several levels, here 2, a “system level” which involves main coupling variables and a “component level” with one optimization loop for each device. The interest of this method is to separate the optimal design of each component, making easier the convergence of loops. This method is applied to a relatively complex power conversion system including a high speed permanent magnet synchronous machine (HSPMSM) supplied by a pulse width modulation (PWM) voltage source inverter (VSI) associated with a DC-link filter. Its interest is shown through a comparison with classical design approaches employed in previous works.
Document type :
Journal articles
Complete list of metadatas

Cited literature [23 references]  Display  Hide  Download

https://hal.archives-ouvertes.fr/hal-01409149
Contributor : Open Archive Toulouse Archive Ouverte (oatao) <>
Submitted on : Monday, December 5, 2016 - 4:54:25 PM
Last modification on : Wednesday, June 10, 2020 - 5:28:07 PM
Long-term archiving on: : Tuesday, March 21, 2017 - 12:10:15 AM

File

sareni_16686.pdf
Files produced by the author(s)

Identifiers

Collections

Citation

Houdhayfa Ounis, Bruno Sareni, Xavier Roboam, André de Andrade. Multi-level integrated optimal design for power systems of more electric aircraft. Mathematics and Computers in Simulation, Elsevier, 2016, vol. 130, pp. 223-235. ⟨10.1016/j.matcom.2015.08.016⟩. ⟨hal-01409149⟩

Share

Metrics

Record views

193

Files downloads

511