Low cost attitude determination system for a LEO information mini-satellite

Yevgeny Somov, Sergey Butyrin, Sergey Somov, Chingiz Hajiyev

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

Abstract

We present method for in-flight signal processing and calibration of a strap-down inertial navigation system (SINS) for the information mini-satellites at low Earth orbit. We have applied the SINS correction based on the signals of a sun-magnetic system and consider the problem at a long-term forecasting of the mini-satellite's orbital motion.

Original languageEnglish
Title of host publicationRAST 2015 - Proceedings of 7th International Conference on Recent Advances in Space Technologies
EditorsM. Fevzi Unal, Suleyman Basturk, Okyay Kaynak, Abdurrahman Hacioglu, Fuat Ince
PublisherInstitute of Electrical and Electronics Engineers Inc.
Pages725-730
Number of pages6
ISBN (Electronic)9781467377607
DOIs
Publication statusPublished - 17 Aug 2015
Event7th International Conference on Recent Advances in Space Technologies, RAST 2015 - Istanbul, Turkey
Duration: 16 Jun 201519 Jun 2015

Publication series

NameRAST 2015 - Proceedings of 7th International Conference on Recent Advances in Space Technologies

Conference

Conference7th International Conference on Recent Advances in Space Technologies, RAST 2015
Country/TerritoryTurkey
CityIstanbul
Period16/06/1519/06/15

Bibliographical note

Publisher Copyright:
© 2015 IEEE.

Keywords

  • calibration
  • mini-satellite
  • signal processing
  • SINS

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