DocumentCode :
2542245
Title :
New Power Conditioning System for Battery-free Satellite Buses with Maximum Power Point Tracking
Author :
Maset, E. ; Sanchis-Kilders, E. ; Ejea, J.B. ; Ferreres, A. ; Blanes, J.M. ; Garrigós, A. ; Carrasco, J.A. ; Weinberg, A.H.
Author_Institution :
Dpt. IngenierÃ\xada Electrónica, E.T.S.E. / Universidad de Valencia, E-46100 Burjassot, SPAIN. emaset@uv.es
fYear :
2007
fDate :
Feb. 25 2007-March 1 2007
Firstpage :
1299
Lastpage :
1305
Abstract :
The purpose of this paper is describe a new conception of Power Conditioning Unit (PCU) developed to fulfill the requirements of BepiColombo Electronic Propulsion module. This load bus has very tough specification especially regarding transient response during total load switch-off ("beam out") which has to be less than 2% of the bus voltage. The conception we propose, is the new Sequential Switching Shunt Maximum Power Regulator (S3MPR) consisting in a S3R, to keep the SA voltage at its Maximum Power Point (MPP) followed by a Boost regulator to produce a constant 100V to supply the Electronic Propulsion (EP). This concept may also be of interest for other future missions involving high power/high voltage power busses. The PCU has been verified by means of testing on a scaled-down Power Subsystem of 1kW output power.
Keywords :
Moon; Power conditioning; Power systems; Propulsion; Regulators; Satellites; Sun; Temperature; Testing; Voltage;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Applied Power Electronics Conference, APEC 2007 - Twenty Second Annual IEEE
Conference_Location :
Anaheim, CA, USA
ISSN :
1048-2334
Print_ISBN :
1-4244-0713-3
Type :
conf
DOI :
10.1109/APEX.2007.357683
Filename :
4195886
Link To Document :
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