Design, implementation and characterization of a novel bi-directional energy conversion system on DC motor drive using super-capacitors

Sun, L; Zhang, N

Design, implementation and characterization of a novel bi-directional energy conversion system on DC motor drive using super-capacitors

Sun, L

Zhang, N

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Publication Type:: Journal Article
Citation:: European Space Agency, (Special Publication) ESA SP, 2002, 153C pp. 101 - 111
Issue Date:: 2002-01-01

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Field	Value	Language
dc.contributor.author	Sun, L https://orcid.org/0000-0003-2054-6695	en_US
dc.contributor.author	Zhang, N https://orcid.org/0000-0001-6408-0044	en_US
dc.date.issued	2002-01-01	en_US
dc.identifier.citation	European Space Agency, (Special Publication) ESA SP, 2002, 153C pp. 101 - 111	en_US
dc.identifier.issn	0379-6566	en_US
dc.identifier.uri	http://hdl.handle.net/10453/35269
dc.description.abstract	With the increase of the digital processing capability of the experiment/payload units on board scientific satellites and Space Station, the number of different voltage output (with low voltage variation tolerance) has increased but their operating powers have decreased. They more and more required low power converters (5-15 Watts) with more than 2 output voltages. This paper will present the work carried out under an ESTEC Contract about two Low Power Converters, one of 5 Watts and one of 10 Watts both of different topologies.	en_US
dc.relation.ispartof	European Space Agency, (Special Publication) ESA SP	en_US
dc.relation.isbasedon	10.1016/j.apenergy.2014.06.084	en_US
dc.subject.classification	Energy	en_US
dc.title	Design, implementation and characterization of a novel bi-directional energy conversion system on DC motor drive using super-capacitors	en_US
dc.type	Journal Article
utslib.citation.volume	153C	en_US
utslib.for	0902 Automotive Engineering	en_US
utslib.for	091304 Dynamics, Vibration and Vibration Control	en_US
utslib.for	09 Engineering	en_US
utslib.for	14 Economics	en_US
pubs.embargo.period	Not known	en_US
pubs.organisational-group	/University of Technology Sydney
pubs.organisational-group	/University of Technology Sydney/Faculty of Engineering and Information Technology
pubs.organisational-group	/University of Technology Sydney/Faculty of Engineering and Information Technology/School of Mechanical and Mechatronic Engineering
utslib.copyright.status	closed_access
pubs.publication-status	Published	en_US
pubs.volume	153C	en_US

Abstract:

With the increase of the digital processing capability of the experiment/payload units on board scientific satellites and Space Station, the number of different voltage output (with low voltage variation tolerance) has increased but their operating powers have decreased. They more and more required low power converters (5-15 Watts) with more than 2 output voltages. This paper will present the work carried out under an ESTEC Contract about two Low Power Converters, one of 5 Watts and one of 10 Watts both of different topologies.

Please use this identifier to cite or link to this item:

http://hdl.handle.net/10453/35269