DocumentCode
3511152
Title
Multiple port DC DC converter for spacecraft Power Conditioning Unit
Author
Mourra, Olivier ; Fernandez, Arturo ; Tonicello, Ferdinando ; Landstroem, Sven
Author_Institution
ESA - Eur. Space Agency, Noordwijk, Netherlands
fYear
2012
fDate
5-9 Feb. 2012
Firstpage
1278
Lastpage
1285
Abstract
In a satellite, the main function of a Power Conditioning Unit (PCU) is to manage the energy coming from several power sources (usually solar arrays and battery) and to deliver it continuously to the users in an appropriate form during the overall mission. The objective of this paper is to present an electronic switching DC-DC converter called Buck-Buck-Boost Regulator (B3R) that could be used as a modular and recurrent solution for regulated satellite power bus classes. The power conversion stages of the B3R topology are first described. Then theoretical equations and practical tests illustrate how the converter operates in term of power conversion, control loops performances and efficiency. The paper finally provides some examples of single point failure tolerant implementation using the B3R.
Keywords
DC-DC power convertors; aircraft power systems; power conversion; space vehicles; switching convertors; B3R regulator topology; battery; buck-buck-boost regulator topology; control loop efficiency; control loop performance; electronic switching DC-DC converter; multiple port DC DC converter; power conversion stage; regulated satellite power bus class; single point failure tolerant implementation; solar array; spacecraft PCU; spacecraft power conditioning unit; Batteries; Inductors; Pulse width modulation; Regulators; Switches; Voltage control; Voltage measurement;
fLanguage
English
Publisher
ieee
Conference_Titel
Applied Power Electronics Conference and Exposition (APEC), 2012 Twenty-Seventh Annual IEEE
Conference_Location
Orlando, FL
Print_ISBN
978-1-4577-1215-9
Electronic_ISBN
978-1-4577-1214-2
Type
conf
DOI
10.1109/APEC.2012.6165983
Filename
6165983
Link To Document