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

Research output: Contribution to conference without publisher/journalPaper without publisher/journalResearchpeer-review

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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

Fingerprint

Spacecraft
Satellites
Control systems

Keywords

  • Supervisory Control
  • Small satellite
  • AAUSAT-II

Cite this

Izadi-Zamanabadi, R., & Larsen, J. A. (2007). A Fault tolerant Control Supervisory System development Procedurefor Small Satellites: The AAUSAT-II case. Paper presented at IFAC Symposium on Automatic Control in Aerospace, Toulouse, France.
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Izadi-Zamanabadi, R & Larsen, JA 2007, 'A Fault tolerant Control Supervisory System development Procedurefor Small Satellites: The AAUSAT-II case', Paper presented at IFAC Symposium on Automatic Control in Aerospace, Toulouse, France, 25/06/2007 - 29/06/2007.

A Fault tolerant Control Supervisory System development Procedurefor Small Satellites : The AAUSAT-II case. / Izadi-Zamanabadi, Roozbeh; Larsen, Jesper Abildgaard.

2007. Paper presented at IFAC Symposium on Automatic Control in Aerospace, Toulouse, France.

Research output: Contribution to conference without publisher/journalPaper without publisher/journalResearchpeer-review

TY - CONF

T1 - A Fault tolerant Control Supervisory System development Procedurefor Small Satellites

T2 - The AAUSAT-II case

AU - Izadi-Zamanabadi, Roozbeh

AU - Larsen, Jesper Abildgaard

PY - 2007

Y1 - 2007

N2 - 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.

AB - 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.

KW - Supervisory Control

KW - Small satellite

KW - AAUSAT-II

M3 - Paper without publisher/journal

ER -

Izadi-Zamanabadi R, Larsen JA. A Fault tolerant Control Supervisory System development Procedurefor Small Satellites: The AAUSAT-II case. 2007. Paper presented at IFAC Symposium on Automatic Control in Aerospace, Toulouse, France.