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 language | English |
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Title of host publication | RAST 2015 - Proceedings of 7th International Conference on Recent Advances in Space Technologies |
Editors | M. Fevzi Unal, Suleyman Basturk, Okyay Kaynak, Abdurrahman Hacioglu, Fuat Ince |
Publisher | Institute of Electrical and Electronics Engineers Inc. |
Pages | 725-730 |
Number of pages | 6 |
ISBN (Electronic) | 9781467377607 |
DOIs | |
Publication status | Published - 17 Aug 2015 |
Event | 7th International Conference on Recent Advances in Space Technologies, RAST 2015 - Istanbul, Turkey Duration: 16 Jun 2015 → 19 Jun 2015 |
Publication series
Name | RAST 2015 - Proceedings of 7th International Conference on Recent Advances in Space Technologies |
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Conference
Conference | 7th International Conference on Recent Advances in Space Technologies, RAST 2015 |
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Country/Territory | Turkey |
City | Istanbul |
Period | 16/06/15 → 19/06/15 |
Bibliographical note
Publisher Copyright:© 2015 IEEE.
Keywords
- calibration
- mini-satellite
- signal processing
- SINS