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

Samara State Technical University

Araştırma sonucu: Kitap/Rapor/Konferans Bildirisinde Bölüm › Konferans katkısı › bilirkişi

3 Atıf (Scopus)

Özet

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.

Orijinal dil	İngilizce
Ana bilgisayar yayını başlığı	Proceedings of 8th International Conference on Recent Advances in Space Technologies, RAST 2017
Editörler	M.F. Unal, A. Hacioglu, M.S. Yildiz, O. Altan, M. Yorukoglu
Yayınlayan	Institute of Electrical and Electronics Engineers Inc.
Sayfalar	397-401
Sayfa sayısı	5
ISBN (Elektronik)	9781538616031
DOI'lar	https://doi.org/10.1109/RAST.2017.8002990
Yayın durumu	Yayınlandı - 4 Ağu 2017
Etkinlik	8th International Conference on Recent Advances in Space Technologies, RAST 2017 - Istanbul, Turkey Süre: 19 Haz 2017 → 22 Haz 2017

Yayın serisi

Adı	Proceedings of 8th International Conference on Recent Advances in Space Technologies, RAST 2017

???event.eventtypes.event.conference???

???event.eventtypes.event.conference???	8th International Conference on Recent Advances in Space Technologies, RAST 2017
Ülke/Bölge	Turkey
Şehir	Istanbul
Periyot	19/06/17 → 22/06/17

Bibliyografik not

Publisher Copyright:
© 2017 IEEE.

Finansman

The work was jointly supported by TUBITAK (The Scientific and Technological Research Council of Turkey), Grant 113E595, and RFBR (Russian Foundation for Basic Research), Grant 14-08-91373.

Finansörler	Finansör numarası
TUBITAK
Russian Foundation for Basic Research	14-08-91373
Türkiye Bilimsel ve Teknolojik Araştirma Kurumu	113E595

Belgeye Erişim

10.1109/RAST.2017.8002990

Diğer Dosyalar ve Linkler

Link to publication in Scopus

Alıntı Yap

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). Makale 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. editör / 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).

@inproceedings{5851f3fd83874681ab7a12bab4b2d742,

title = "Attitude determination of nanosatellites in the sun-eclipse phases",

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.",

keywords = "Satellite attitude estimation, attitude prediction, extended Kalman filter, magnetometer, rate gyro, sun sensor",

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

note = "Publisher Copyright: {\textcopyright} 2017 IEEE.; 8th International Conference on Recent Advances in Space Technologies, RAST 2017 ; Conference date: 19-06-2017 Through 22-06-2017",

year = "2017",

month = aug,

day = "4",

doi = "10.1109/RAST.2017.8002990",

language = "English",

series = "Proceedings of 8th International Conference on Recent Advances in Space Technologies, RAST 2017",

publisher = "Institute of Electrical and Electronics Engineers Inc.",

pages = "397--401",

editor = "M.F. Unal and A. Hacioglu and M.S. Yildiz and O. Altan and M. Yorukoglu",

booktitle = "Proceedings of 8th International Conference on Recent Advances in Space Technologies, RAST 2017",

address = "United States",

}

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).

Araştırma sonucu: Kitap/Rapor/Konferans Bildirisinde Bölüm › Konferans katkısı › bilirkişi

TY - GEN

T1 - Attitude determination of nanosatellites in the sun-eclipse phases

AU - Hajiyev, Chingiz

AU - Cilden-Guler, Demet

AU - Somov, Yevgeny

PY - 2017/8/4

Y1 - 2017/8/4

N2 - 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.

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.

KW - Satellite attitude estimation

KW - attitude prediction

KW - extended Kalman filter

KW - magnetometer

KW - rate gyro

KW - sun sensor

UR - https://www.scopus.com/pages/publications/85030266149

U2 - 10.1109/RAST.2017.8002990

DO - 10.1109/RAST.2017.8002990

M3 - Conference contribution

AN - SCOPUS:85030266149

T3 - Proceedings of 8th International Conference on Recent Advances in Space Technologies, RAST 2017

SP - 397

EP - 401

BT - Proceedings of 8th International Conference on Recent Advances in Space Technologies, RAST 2017

A2 - Unal, M.F.

A2 - Hacioglu, A.

A2 - Yildiz, M.S.

A2 - Altan, O.

A2 - Yorukoglu, M.

PB - Institute of Electrical and Electronics Engineers Inc.

T2 - 8th International Conference on Recent Advances in Space Technologies, RAST 2017

Y2 - 19 June 2017 through 22 June 2017

ER -

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, editörler, 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

Özet

Yayın serisi

???event.eventtypes.event.conference???

Bibliyografik not

Finansman

Belgeye Erişim

Diğer Dosyalar ve Linkler

Parmak izi

Alıntı Yap