Attitude determination of nanosatellites in the sun-eclipse phases

Chingiz Hajiyev; Demet Cilden-Guler; Yevgeny Somov

doi:10.1109/RAST.2017.8002990

Attitude determination of nanosatellites in the sun-eclipse phases

Chingiz Hajiyev, Demet Cilden-Guler, Yevgeny Somov

Samara State Technical University

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › peer-review

3 Citations (Scopus)

Abstract

Singular Value Decomposition (SVD) and extended Kalman filter (EKF) are integrated earlier by authors in order to estimate the satellite's angular motion parameters about center of mass. The SVD-aided EKF algorithm is used in this study for estimation of the attitude angles and angular velocities. In the eclipse period, algorithm is switched into the prediction phase for better attitude estimation of the satellite; therefore, satellite's attitude angles when no data coming from the sun sensor are improved.

Original language	English
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	397-401
Number of pages	5
ISBN (Electronic)	9781538616031
DOIs	https://doi.org/10.1109/RAST.2017.8002990
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

Conference

Conference	8th International Conference on Recent Advances in Space Technologies, RAST 2017
Country/Territory	Turkey
City	Istanbul
Period	19/06/17 → 22/06/17

Bibliographical note

Publisher Copyright:
© 2017 IEEE.

Keywords

Satellite attitude estimation
attitude prediction
extended Kalman filter
magnetometer
rate gyro
sun sensor

Access to Document

10.1109/RAST.2017.8002990

Cite this

Hajiyev, C., Cilden-Guler, D., & Somov, Y. (2017). Attitude determination of nanosatellites in the sun-eclipse phases. In M. F. Unal, A. Hacioglu, M. S. Yildiz, O. Altan, & M. Yorukoglu (Eds.), Proceedings of 8th International Conference on Recent Advances in Space Technologies, RAST 2017 (pp. 397-401). Article 8002990 (Proceedings of 8th International Conference on Recent Advances in Space Technologies, RAST 2017). Institute of Electrical and Electronics Engineers Inc.. https://doi.org/10.1109/RAST.2017.8002990

Hajiyev, Chingiz ; Cilden-Guler, Demet ; Somov, Yevgeny. / Attitude determination of nanosatellites in the sun-eclipse phases. Proceedings of 8th International Conference on Recent Advances in Space Technologies, RAST 2017. editor / M.F. Unal ; A. Hacioglu ; M.S. Yildiz ; O. Altan ; M. Yorukoglu. Institute of Electrical and Electronics Engineers Inc., 2017. pp. 397-401 (Proceedings of 8th International Conference on Recent Advances in Space Technologies, RAST 2017).

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abstract = "Singular Value Decomposition (SVD) and extended Kalman filter (EKF) are integrated earlier by authors in order to estimate the satellite's angular motion parameters about center of mass. The SVD-aided EKF algorithm is used in this study for estimation of the attitude angles and angular velocities. In the eclipse period, algorithm is switched into the prediction phase for better attitude estimation of the satellite; therefore, satellite's attitude angles when no data coming from the sun sensor are improved.",

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author = "Chingiz Hajiyev and Demet Cilden-Guler and Yevgeny Somov",

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doi = "10.1109/RAST.2017.8002990",

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Hajiyev, C , Cilden-Guler, D & Somov, Y 2017, Attitude determination of nanosatellites in the sun-eclipse phases. in MF Unal, A Hacioglu, MS Yildiz, O Altan & M Yorukoglu (eds), Proceedings of 8th International Conference on Recent Advances in Space Technologies, RAST 2017., 8002990, Proceedings of 8th International Conference on Recent Advances in Space Technologies, RAST 2017, Institute of Electrical and Electronics Engineers Inc., pp. 397-401, 8th International Conference on Recent Advances in Space Technologies, RAST 2017, Istanbul, Turkey, 19/06/17. https://doi.org/10.1109/RAST.2017.8002990

Attitude determination of nanosatellites in the sun-eclipse phases. / Hajiyev, Chingiz ; Cilden-Guler, Demet; Somov, Yevgeny.
Proceedings of 8th International Conference on Recent Advances in Space Technologies, RAST 2017. ed. / M.F. Unal; A. Hacioglu; M.S. Yildiz; O. Altan; M. Yorukoglu. Institute of Electrical and Electronics Engineers Inc., 2017. p. 397-401 8002990 (Proceedings of 8th International Conference on Recent Advances in Space Technologies, RAST 2017).

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › peer-review

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AB - Singular Value Decomposition (SVD) and extended Kalman filter (EKF) are integrated earlier by authors in order to estimate the satellite's angular motion parameters about center of mass. The SVD-aided EKF algorithm is used in this study for estimation of the attitude angles and angular velocities. In the eclipse period, algorithm is switched into the prediction phase for better attitude estimation of the satellite; therefore, satellite's attitude angles when no data coming from the sun sensor are improved.

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Hajiyev C , Cilden-Guler D, Somov Y. Attitude determination of nanosatellites in the sun-eclipse phases. In Unal MF, Hacioglu A, Yildiz MS, Altan O, Yorukoglu M, editors, Proceedings of 8th International Conference on Recent Advances in Space Technologies, RAST 2017. Institute of Electrical and Electronics Engineers Inc. 2017. p. 397-401. 8002990. (Proceedings of 8th International Conference on Recent Advances in Space Technologies, RAST 2017). doi: 10.1109/RAST.2017.8002990

Attitude determination of nanosatellites in the sun-eclipse phases

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Bibliographical note

Keywords

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