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. / Master of Science
| Identifer | oai:union.ndltd.org:VTETD/oai:vtechworks.lib.vt.edu:10919/42369 |
| Date | 30 April 2009 |
| Creators | Shum, Kin E. |
| Contributors | Electrical Engineering, Lee, Fred C., Chen, Dan Y., Sable, Daniel M. |
| Publisher | Virginia Tech |
| Source Sets | Virginia Tech Theses and Dissertation |
| Language | English |
| Detected Language | English |
| Type | Thesis, Text |
| Format | 92 leaves, BTD, application/pdf, application/pdf |
| Rights | In Copyright, http://rightsstatements.org/vocab/InC/1.0/ |
| Relation | OCLC# 30502932, LD5655.V855_1994.S566.pdf |
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