MIL-Standards Verification of Battery Control for More Electric Aircraft Application

Author:

Russo Antonio,Canciello Giacomo,Cavallo Alberto

Abstract

Abstract As a consequence of the increase of air traffic, the innovative topic of the More Electric Aircraft (MEA) has received increasing attention. In this paper, the control of a bidirectional DC/DC converter for battery management in the MEA framework is described. A detailed simulator and simulation campaign have been designed in order to verify the satisfaction of the MIL-STD-704F standard which regulates the behaviour of electric devices on-board the aircraft.

Publisher

IOP Publishing

Subject

General Physics and Astronomy

Reference18 articles.

1. The more electric aircraft - Assessing the benefits;Jones;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering,2002

2. The More Electric Aircraft: Technology and challenges;Wheeler;IEEE Electrification Magazine,2014

3. Robust control of aeronautical electrical generators for energy management applications;Canciello;International Journal of Aerospace Engineering,2017

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