Abstract
We consider some principal problems on precise attitude determination of the maneuvering land-survey satellites placed on the orbit altitudes from 600 up to 1000 km. We present onboard discrete algorithms for signal processing, calibration and alignment of astroinertial attitude determination system which is a part of the strapdown inertial navigation system.
Original language | English |
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Title of host publication | Proceedings of 8th International Conference on Recent Advances in Space Technologies, RAST 2017 |
Editors | M.F. Unal, A. Hacioglu, M.S. Yildiz, O. Altan, M. Yorukoglu |
Publisher | Institute of Electrical and Electronics Engineers Inc. |
Pages | 409-413 |
Number of pages | 5 |
ISBN (Electronic) | 9781538616031 |
DOIs | |
Publication status | Published - 4 Aug 2017 |
Event | 8th International Conference on Recent Advances in Space Technologies, RAST 2017 - Istanbul, Turkey Duration: 19 Jun 2017 → 22 Jun 2017 |
Publication series
Name | Proceedings of 8th International Conference on Recent Advances in Space Technologies, RAST 2017 |
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Conference
Conference | 8th International Conference on Recent Advances in Space Technologies, RAST 2017 |
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Country/Territory | Turkey |
City | Istanbul |
Period | 19/06/17 → 22/06/17 |
Bibliographical note
Publisher Copyright:© 2017 IEEE.
Funding
ACKNOWLEDGMENTS This work was supported by RFBR (Russian Foundation for Basic Research, Grant nos. 14-08-91373, 17-08-01708 and 17-48-630637) and TUBITAK (The Scientific and Technological Research Council of Turkey, Grant no. 113E595), and also Division on the Energy, Mechanics, Machine building and Control Processes (EMMCP) of Russian Academy of Sciences (Program no. 13 on Basic Research).
Funders | Funder number |
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TUBITAK | |
Russian Foundation for Basic Research | 14-08-91373, 17-48-630637, 17-08-01708 |
Russian Academy of Sciences | 13 |
Türkiye Bilimsel ve Teknolojik Araştirma Kurumu | 113E595 |