A low ripple bi-directional battery charger/discharger using coupled inductor

There are two important issues about a spacecraft power conversion system: low ripple current flowing through both battery and bus, and bi-directional power flow to and from the battery. This thesis introduces a novel low ripple current bi-directional battery charge/discharge converter using coupled-inductor. Bi-directional switch structures and proper control scheme make it possible for the power to flow through the same converter in both directions: charging and discharging the battery. Meanwhile, the coupled-inductor is designed in such a way that all the magnetizing current (ripple current) is confined within the converter, yielding "zero-current-ripple" (ZCR) on both battery side and bus side. ZCR condition analysis, topological comparison with similar approach, and circuit design guide line are given in this thesis. Circuit operation and performance, bi-directional control strategy, and small signal characteristics of the converter are also presented along with experimental verification.

Name thesis:degree_name

Master of Science

Level thesis:degree_level

masters

Discipline thesis:degree_discipline

Electrical Engineering

Department dc:contributor.department

Electrical Engineering

Grantor dc:publisher

Virginia Tech

Year dc:date.issued

1994

Author dc:creator

• Shum, Kin E.

Chair dc:contributor.committeechair

• Lee, Fred C.

Committee members dc:contributor.committeemember

• Chen, Dan Y.
• Sable, Daniel M.

Statement dc:rights

• In Copyright

Licence dc:rights.uri

• http://rightsstatements.org/vocab/InC/1.0/

Language dc:language.iso

en

Dc Identifier Other

etd-04302009-040332

OAI identifier oai:identifier

oai:vtechworks.lib.vt.edu:10919/42369