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Journal of Automation and Information Sciences
SJR: 0.275 SNIP: 0.59 CiteScore™: 0.8

ISSN Druckformat: 1064-2315
ISSN Online: 2163-9337

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Journal of Automation and Information Sciences

DOI: 10.1615/JAutomatInfScien.v42.i6.20
pages 30-42

Identifying Failures in Sensors of a Spacecraft Attitude Control System

Dmitriy V. Lebedev
International Research and Training Center of Information Technologies and Systems of National Academy of Sciences of Ukraine and Ministry of Education and Science of Ukraine, Kyiv

ABSTRAKT

A problem of failure detection and identification in sensors of a spacecraft attitude control system under condition of their minimum number or minimum redundancy is investigated. The effectiveness of procedures under consideration is illustrated via angular rate sensors and Sun sensor as examples.

REFERENZEN

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  4. Deyst J.J., Harrison J.V., Gai E., Daly K.C., Fault detection, identification and reconfiguration for spacecraft systems.

  5. Frank P.M., Fault diagnosis in dynamic systems using analytical and knowledge-based redundancy – a survey and some new results.

  6. Lebedev D.V., Identification of failures in a unit of sensing elements of inertial navigation system.

  7. Gantmakher F.R., Matrix theory.

  8. Chow E.Y., Willsky A.S., Analytical redundancy and the design of robust failure detection systems.

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  11. Lebedev D.V., Tkachenko A.I., Navigation and control of attitude of small spacecrafts.


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