Electrical monitoring for fault detection in an EMA

L. Romeral; J. A. Rosero; A. Garcia Espinosa; J. Cusido; J. A. Ortega

doi:10.1109/MAES.2010.5463950

Electrical monitoring for fault detection in an EMA

L. Romeral^*
, J. A. Rosero
, A. Garcia Espinosa
, J. Cusido
, J. A. Ortega

^*Corresponding author for this work

Polytechnic University of Catalonia

Research output: Contribution to journal › Article › peer-review

46 Citations (Scopus)

Abstract

The concept of a More Electric Aircraft (MEA) leads, among other actions, to the substitution of hydraulic-based actuators for Electro-Mechanical ACtuators (EMA).

Original language	English
Article number	5463950
Pages (from-to)	4-9
Number of pages	6
Journal	IEEE Aerospace and Electronic Systems Magazine
Volume	25
Issue number	3
DOIs	https://doi.org/10.1109/MAES.2010.5463950
Publication status	Published - Mar 2010
Externally published	Yes

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10.1109/MAES.2010.5463950

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title = "Electrical monitoring for fault detection in an EMA",

abstract = "The concept of a More Electric Aircraft (MEA) leads, among other actions, to the substitution of hydraulic-based actuators for Electro-Mechanical ACtuators (EMA).",

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AU - Romeral, L.

AU - Rosero, J. A.

AU - Garcia Espinosa, A.

AU - Cusido, J.

AU - Ortega, J. A.

PY - 2010/3

Y1 - 2010/3

N2 - The concept of a More Electric Aircraft (MEA) leads, among other actions, to the substitution of hydraulic-based actuators for Electro-Mechanical ACtuators (EMA).

AB - The concept of a More Electric Aircraft (MEA) leads, among other actions, to the substitution of hydraulic-based actuators for Electro-Mechanical ACtuators (EMA).

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M3 - Article

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VL - 25

SP - 4

EP - 9

JO - IEEE Aerospace and Electronic Systems Magazine

JF - IEEE Aerospace and Electronic Systems Magazine

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M1 - 5463950

ER -

Electrical monitoring for fault detection in an EMA

Abstract

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