NDLI: A virtual electrical test bench for more electrical aircraft architecture verification and energy management development

Content Provider	IEEE Xplore Digital Library
Author	Bester, J.E. Mabwe, A.M. El Hajjaji, A.
Copyright Year	2015
Description	Author affiliation: MIS Lab., Univ. of Picardy Jules Verne, Amiens, France (Bester, J.E.; Mabwe, A.M.; El Hajjaji, A.)
Abstract	The shift towards More Electrical Aircraft is bringing with it many new technologies and a redesign of the existing aircraft electrical network, both of which require thorough testing before their implementation. This led to the creation of the Copper Bird® test bench which recreates the aircraft electrical system and is used for equipment evaluation and validation. This paper details the development of an accompanying virtual electrical test bench; modelling and real-time simulation of the operation of an aircraft electrical system for conducting verification activities over different aircraft electrical architectures and developing energy management strategies. In this paper particular attention is given to the PEM fuel cell model which has been characterized and validated using a scaled version of the electrical test bench. The model shows good accuracy, giving an average error of less than ±350mV and a max error of only ±3%. Fuzzy logic-based energy management was then developed for a fuel cell and battery-based auxiliary power unit with the fuel cell supplying average load power (whilst acting as a current source) and the battery handling load transients and overload situations. The energy management attains its goals of operating the fuel cell at its average power, in order to extend its lifetime, whilst maintaining the battery state of charge between 50% and 90%, also in order to extend its lifetime as well as maintaining its ability to absorb excess generated power.
Starting Page	1
Ending Page	10
File Size	415797
Page Count	10
File Format	PDF
e-ISBN	9789075815221
DOI	10.1109/EPE.2015.7309227
Language	English
Publisher	Institute of Electrical and Electronics Engineers, Inc. (IEEE)
Publisher Date	2015-09-08
Publisher Place	Switzerland
Access Restriction	Subscribed
Rights Holder	EPE Association and IEEE
Subject Keyword	Fuel cell system Fuzzy control Atmospheric modeling Power management Aerospace Fuel cells Computer architecture Modelling Batteries Aircraft manufacture Aircraft Aircraft propulsion
Content Type	Text
Resource Type	Article

Sl.	Authority	Responsibilities	Communication Details
1	Ministry of Education (GoI), Department of Higher Education	Sanctioning Authority	https://www.education.gov.in/ict-initiatives
2	Indian Institute of Technology Kharagpur	Host Institute of the Project: The host institute of the project is responsible for providing infrastructure support and hosting the project	https://www.iitkgp.ac.in
3	National Digital Library of India Office, Indian Institute of Technology Kharagpur	The administrative and infrastructural headquarters of the project	Dr. B. Sutradhar bsutra@ndl.gov.in
4	Project PI / Joint PI	Principal Investigator and Joint Principal Investigators of the project	Dr. B. Sutradhar bsutra@ndl.gov.in Prof. Saswat Chakrabarti will be added soon
5	Website/Portal (Helpdesk)	Queries regarding NDLI and its services	support@ndl.gov.in
6	Contents and Copyright Issues	Queries related to content curation and copyright issues	content@ndl.gov.in
7	National Digital Library of India Club (NDLI Club)	Queries related to NDLI Club formation, support, user awareness program, seminar/symposium, collaboration, social media, promotion, and outreach	clubsupport@ndl.gov.in
8	Digital Preservation Centre (DPC)	Assistance with digitizing and archiving copyright-free printed books	dpc@ndl.gov.in
9	IDR Setup or Support	Queries related to establishment and support of Institutional Digital Repository (IDR) and IDR workshops	idr@ndl.gov.in

Fuzzy Logic control strategy for Fuel Cell/Battery aerospace propulsion system

Dynamic control of fuel cell air supply system with power management

Design of an electrical distribution test rig for validation of equipment for more electrical aircraft

Concept analysis of an electrical fuel cell integration in modern aircraft

Analytical Solution of the Energy Management for Fuel Cell Hybrid Propulsion Systems

Fuzzy logic controller development of a hybrid fuel cell-battery auxiliary power unit for remote applications

Multiple model control for hybrid power system of Fuel Cell Electric Vehicle

Propulsion System Architecture and Power Conditioning Topologies for Fuel Cell Vehicles

Test bench for the simulation of a hybrid power train

A virtual electrical test bench for more electrical aircraft architecture verification and energy management development

Similar Documents

Fuzzy Logic control strategy for Fuel Cell/Battery aerospace propulsion system

Dynamic control of fuel cell air supply system with power management

Design of an electrical distribution test rig for validation of equipment for more electrical aircraft

Concept analysis of an electrical fuel cell integration in modern aircraft

Analytical Solution of the Energy Management for Fuel Cell Hybrid Propulsion Systems

Fuzzy logic controller development of a hybrid fuel cell-battery auxiliary power unit for remote applications

Multiple model control for hybrid power system of Fuel Cell Electric Vehicle

Propulsion System Architecture and Power Conditioning Topologies for Fuel Cell Vehicles

Test bench for the simulation of a hybrid power train

A virtual electrical test bench for more electrical aircraft architecture verification and energy management development