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A fault tolerant control supervisory system development procedure for small satellites: The AAUSAT-II case
Automatic Control in Aerospace, Volume # 17 | Part# 1
Location: ICT, Universitas Studii Tolosana, France
National Organizing Committee Chair: Imbert, Nicole,
Alazard, Daniel
International Program Committee Chair: Siguerdidjane, Houria,
Mauffrey, Sophie
Conference Editor: Siguerdidjane, Houria
Authors
Izadi-Zamanabadi, Roozbeh; Larsen, Jesper A.
Digital Object Identifier (DOI)
10.3182/20070625-5-FR-2916.00050
Page Numbers:
289-294
Index Terms
Pico satellite,structural analysis,fault tolerance,decision logic,AAUSAT-II
Abstract
The paper presents a stepwise procedure to develop a fault tolerant control system for small satellites. The procedure is illustrated through implementation on the AAUSAT-II spacecraft. As it is shown the presented procedure requires expertise from several disciplines that are nevertheless necessary for obtaining a complete and consistent solution.
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