In-flight calibration of magnetometers and low-cost SINS for small land-survey satellite

Yevgeny Somov, Chingiz Hajiyev

Research output: Chapter in Book/Report/Conference proceedingConference contributionpeer-review

2 Citations (Scopus)

Abstract

Magnetometers are widely used for attitude determination of the low Earth orbit satellites. In order to estimate the satellite attitude accurately, bias of magnetometer must be estimated. In this study a linear Kalman filter based algorithm for estimation of magnetometer biases is proposed. We present computer technology for onboard signal processing and in-flight calibration of a low-cost strap-down inertial navigation system (SINS) for small land-survey satellite. For the system with small financial expenditures on practical implementation, the requirements are not severe on accuracy of the attitude determination. In this situation, we have applied the SINS correction based on signals of a Sun optoelectronic sensor and magnetometer.

Original languageEnglish
Title of host publicationProceedings of the 2014 6th International Conference on Electronics, Computers and Artificial Intelligence, ECAI 2014
PublisherInstitute of Electrical and Electronics Engineers Inc.
Pages1-7
Number of pages7
ISBN (Electronic)9781479954780
DOIs
Publication statusPublished - 2014
Event6th International Conference on Electronics, Computers and Artificial Intelligence, ECAI 2014 - Pitesti, Romania
Duration: 23 Oct 201425 Oct 2014

Publication series

NameProceedings of the 2014 6th International Conference on Electronics, Computers and Artificial Intelligence, ECAI 2014

Conference

Conference6th International Conference on Electronics, Computers and Artificial Intelligence, ECAI 2014
Country/TerritoryRomania
CityPitesti
Period23/10/1425/10/14

Bibliographical note

Publisher Copyright:
© 2014 IEEE.

Keywords

  • attitude determination
  • in-flight calibration
  • magnetometer
  • small satellite
  • strap-down inertial navigation system
  • sun and magnetic sensors

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