DocumentCode
631259
Title
Design criteria for electrical power subsystem´s topology selection
Author
Shekoofa, Omid ; Karbasian, Shahab
Author_Institution
Satellite Res. Inst. (SRI), ISRC, Tehran, Iran
fYear
2013
fDate
12-14 June 2013
Firstpage
559
Lastpage
564
Abstract
Choosing an appropriate topology is a key step in the process of electrical power subsystem design. This selection should be done based on the design requirements implied from higher level like mission, system and subsystem levels. In this study the essential criteria selecting a suitable topology are discussed. This paper starts with an overview on EPS design process with emphasizing on EPS architecture and topology selection. Two concepts of energy transfer, i.e. Direct Energy Transfer and Peak Power Tracker, are reviewed and compared in details. For each concept different methods of main bus voltage regulation, like unregulated bus, regulated bus, semi-regulated bus, quasi-regulated bus and hybrid bus are discussed. They have been evaluated by comparing their advantages, disadvantages, and their applications in different space missions. These comparisons are carried out based on essential criteria for EPS design such as efficiency, complexity, reliability, weight and cost.
Keywords
aircraft power systems; maximum power point trackers; voltage control; EPS architecture; EPS design process; bus voltage regulation; direct energy transfer; electrical power subsystem; hybrid bus; peak power tracker; quasiregulated bus; semiregulated bus; space missions; topology selection; unregulated bus; Batteries; Energy exchange; Regulators; Reliability; Satellites; Topology; Voltage control; Criteria; EPS Design; Electrical Power Subsystem; Satellite; Topology;
fLanguage
English
Publisher
ieee
Conference_Titel
Recent Advances in Space Technologies (RAST), 2013 6th International Conference on
Conference_Location
Istanbul
Print_ISBN
978-1-4673-6395-2
Type
conf
DOI
10.1109/RAST.2013.6581274
Filename
6581274
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