A Battery Charge-Discharge regulator (BCDR) intended to interface a 12V bus with a single-cell Li-ion battery for power levels in the 100W range is presented. It may be useful in small space vehicles, and especially in the cases when battery sizing is driven by the need to complement the power provided by primary power sources during high peaks of load, with comparatively small energy amounts. In particular, the Bidirectional Three Level Neutral Point Clamped (TLNPC) converter configuration was selected, and a prototype was designed, built and tested. After providing a rationale of the single-battery-cell approach, and of the criteria adopted to select the TLNPC converter circuit, the paper reports the principles of operation of the converter and indicates the design criteria for the main circuit parameters. Extensive characterization of the prototype completes the work. © 2012 IEEE.

Bidirectional converter for single-cell Li-ion batteries in a small space vehicle / Macellari, Michele; Palmerini, Giovanni Battista; Schirone, Luigi. - ELETTRONICO. - (2012), pp. 1-9. (Intervento presentato al convegno 2012 IEEE Aerospace Conference tenutosi a Big Sky, MT nel 3 March 2012 through 10 March 2012) [10.1109/aero.2012.6187247].

Bidirectional converter for single-cell Li-ion batteries in a small space vehicle

MACELLARI, MICHELE;PALMERINI, Giovanni Battista;SCHIRONE, Luigi
2012

Abstract

A Battery Charge-Discharge regulator (BCDR) intended to interface a 12V bus with a single-cell Li-ion battery for power levels in the 100W range is presented. It may be useful in small space vehicles, and especially in the cases when battery sizing is driven by the need to complement the power provided by primary power sources during high peaks of load, with comparatively small energy amounts. In particular, the Bidirectional Three Level Neutral Point Clamped (TLNPC) converter configuration was selected, and a prototype was designed, built and tested. After providing a rationale of the single-battery-cell approach, and of the criteria adopted to select the TLNPC converter circuit, the paper reports the principles of operation of the converter and indicates the design criteria for the main circuit parameters. Extensive characterization of the prototype completes the work. © 2012 IEEE.
2012
2012 IEEE Aerospace Conference
bcdr; bidirectional; li-ion; power conversion; space vehicle
04 Pubblicazione in atti di convegno::04b Atto di convegno in volume
Bidirectional converter for single-cell Li-ion batteries in a small space vehicle / Macellari, Michele; Palmerini, Giovanni Battista; Schirone, Luigi. - ELETTRONICO. - (2012), pp. 1-9. (Intervento presentato al convegno 2012 IEEE Aerospace Conference tenutosi a Big Sky, MT nel 3 March 2012 through 10 March 2012) [10.1109/aero.2012.6187247].
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Utilizza questo identificativo per citare o creare un link a questo documento: https://hdl.handle.net/11573/439069
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