A fault tolerant control supervisory system development procedure for small satellites - The AAUSAT-II case

Roozbeh Izadi-Zamanabadi*, Jesper A. Larsen

*Corresponding author for this work

Research output: Contribution to book/anthology/report/conference proceedingArticle in proceedingResearchpeer-review

5 Citations (Scopus)

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.

Original languageEnglish
Title of host publicationACA' 2007 - 17th IFAC Symposium on Automatic Control in Aerospace - Proceedings
Number of pages6
Publication date1 Dec 2007
EditionPART 1
Pages289-294
ISBN (Print)9783902661241
Publication statusPublished - 1 Dec 2007
Event17th IFAC Symposium on Automatic Control in Aerospace, ACA' 2007 - Toulouse, France
Duration: 25 Jun 200729 Jun 2007

Conference

Conference17th IFAC Symposium on Automatic Control in Aerospace, ACA' 2007
Country/TerritoryFrance
CityToulouse
Period25/06/200729/06/2007
SeriesIFAC Proceedings Volumes (IFAC-PapersOnline)
NumberPART 1
Volume17
ISSN1474-6670

Keywords

  • AAUSAT-II
  • Decision logic
  • Fault tolerance
  • Pico satellite
  • Structural analysis

Fingerprint

Dive into the research topics of 'A fault tolerant control supervisory system development procedure for small satellites - The AAUSAT-II case'. Together they form a unique fingerprint.

Cite this