A Fault tolerant Control Supervisory System development Procedurefor Small Satellites: The AAUSAT-II case

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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
Publication date2007
Number of pages6
Publication statusPublished - 2007
EventIFAC Symposium on Automatic Control in Aerospace - Toulouse, France
Duration: 25 Jun 200729 Jun 2007
Conference number: 17

Conference

ConferenceIFAC Symposium on Automatic Control in Aerospace
Number17
CountryFrance
CityToulouse
Period25/06/200729/06/2007

Keywords

  • Supervisory Control
  • Small satellite
  • AAUSAT-II

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