Attitude and attitude rate estimation for a nanosatellite using SVD and UKF

Demet Cilden; Chingiz Hajiyev; Halil Ersin Soken

doi:10.1109/RAST.2015.7208431

Attitude and attitude rate estimation for a nanosatellite using SVD and UKF

Demet Cilden
, Chingiz Hajiyev
, Halil Ersin Soken

JAXA Institute of Space and Astronautical Science

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

21 Atıf (Scopus)

Özet

Singular value decomposition (SVD) method and unscented Kalman filter (UKF) are integrated to estimate the attitude and attitude rates of a nanosatellite recursively. First the SVD method minimizes the Wahba's loss function to find the optimal solution for the attitude on the basis of magnetometer and sun sensor vector measurements. Then the UKF uses this attitude information as the measurements for providing more accurate attitude estimates even when the satellite is in eclipse. The 'rotation angle error covariance matrix' calculated for the estimations of the SVD method are regarded as the measurement noise covariance for the UKF. Discussions for the UKF tuning are included specifically for the eclipse period where the SVD method fails and practically there is no measurements incoming to the filter.

Orijinal dil	İngilizce
Ana bilgisayar yayını başlığı	RAST 2015 - Proceedings of 7th International Conference on Recent Advances in Space Technologies
Editörler	M. Fevzi Unal, Suleyman Basturk, Okyay Kaynak, Abdurrahman Hacioglu, Fuat Ince
Yayınlayan	Institute of Electrical and Electronics Engineers Inc.
Sayfalar	695-700
Sayfa sayısı	6
ISBN (Elektronik)	9781467377607
DOI'lar	https://doi.org/10.1109/RAST.2015.7208431
Yayın durumu	Yayınlandı - 17 Ağu 2015
Etkinlik	7th International Conference on Recent Advances in Space Technologies, RAST 2015 - Istanbul, Türkiye Süre: 16 Haz 2015 → 19 Haz 2015

Yayın serisi

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

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

???event.eventtypes.event.conference???	7th International Conference on Recent Advances in Space Technologies, RAST 2015
Ülke/Bölge	Türkiye
Şehir	Istanbul
Periyot	16/06/15 → 19/06/15

Bibliyografik not

Publisher Copyright:
© 2015 IEEE.

Belgeye Erişim

10.1109/RAST.2015.7208431

Diğer Dosyalar ve Linkler

Link to publication in Scopus

Alıntı Yap

Cilden, D., Hajiyev, C., & Soken, H. E. (2015). Attitude and attitude rate estimation for a nanosatellite using SVD and UKF. In M. F. Unal, S. Basturk, O. Kaynak, A. Hacioglu, & F. Ince (Eds.), RAST 2015 - Proceedings of 7th International Conference on Recent Advances in Space Technologies (pp. 695-700). Makale 7208431 (RAST 2015 - Proceedings of 7th International Conference on Recent Advances in Space Technologies). Institute of Electrical and Electronics Engineers Inc.. https://doi.org/10.1109/RAST.2015.7208431

Cilden, Demet ; Hajiyev, Chingiz ; Soken, Halil Ersin. / Attitude and attitude rate estimation for a nanosatellite using SVD and UKF. RAST 2015 - Proceedings of 7th International Conference on Recent Advances in Space Technologies. editör / M. Fevzi Unal ; Suleyman Basturk ; Okyay Kaynak ; Abdurrahman Hacioglu ; Fuat Ince. Institute of Electrical and Electronics Engineers Inc., 2015. pp. 695-700 (RAST 2015 - Proceedings of 7th International Conference on Recent Advances in Space Technologies).

@inproceedings{324beaa8e9c64950b601b0bb0824c8d2,

title = "Attitude and attitude rate estimation for a nanosatellite using SVD and UKF",

abstract = "Singular value decomposition (SVD) method and unscented Kalman filter (UKF) are integrated to estimate the attitude and attitude rates of a nanosatellite recursively. First the SVD method minimizes the Wahba's loss function to find the optimal solution for the attitude on the basis of magnetometer and sun sensor vector measurements. Then the UKF uses this attitude information as the measurements for providing more accurate attitude estimates even when the satellite is in eclipse. The 'rotation angle error covariance matrix' calculated for the estimations of the SVD method are regarded as the measurement noise covariance for the UKF. Discussions for the UKF tuning are included specifically for the eclipse period where the SVD method fails and practically there is no measurements incoming to the filter.",

keywords = "SVD, UKF, attitude estimation, nanosatellite",

author = "Demet Cilden and Chingiz Hajiyev and Soken, \{Halil Ersin\}",

note = "Publisher Copyright: {\textcopyright} 2015 IEEE.; 7th International Conference on Recent Advances in Space Technologies, RAST 2015 ; Conference date: 16-06-2015 Through 19-06-2015",

year = "2015",

month = aug,

day = "17",

doi = "10.1109/RAST.2015.7208431",

language = "English",

series = "RAST 2015 - Proceedings of 7th International Conference on Recent Advances in Space Technologies",

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

pages = "695--700",

editor = "Unal, \{M. Fevzi\} and Suleyman Basturk and Okyay Kaynak and Abdurrahman Hacioglu and Fuat Ince",

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Cilden, D , Hajiyev, C & Soken, HE 2015, Attitude and attitude rate estimation for a nanosatellite using SVD and UKF. in MF Unal, S Basturk, O Kaynak, A Hacioglu & F Ince (eds), RAST 2015 - Proceedings of 7th International Conference on Recent Advances in Space Technologies., 7208431, RAST 2015 - Proceedings of 7th International Conference on Recent Advances in Space Technologies, Institute of Electrical and Electronics Engineers Inc., pp. 695-700, 7th International Conference on Recent Advances in Space Technologies, RAST 2015, Istanbul, Türkiye, 16/06/15. https://doi.org/10.1109/RAST.2015.7208431

Attitude and attitude rate estimation for a nanosatellite using SVD and UKF. / Cilden, Demet ; Hajiyev, Chingiz; Soken, Halil Ersin.
RAST 2015 - Proceedings of 7th International Conference on Recent Advances in Space Technologies. ed. / M. Fevzi Unal; Suleyman Basturk; Okyay Kaynak; Abdurrahman Hacioglu; Fuat Ince. Institute of Electrical and Electronics Engineers Inc., 2015. p. 695-700 7208431 (RAST 2015 - Proceedings of 7th International Conference on Recent Advances in Space Technologies).

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

TY - GEN

T1 - Attitude and attitude rate estimation for a nanosatellite using SVD and UKF

AU - Cilden, Demet

AU - Hajiyev, Chingiz

AU - Soken, Halil Ersin

PY - 2015/8/17

Y1 - 2015/8/17

N2 - Singular value decomposition (SVD) method and unscented Kalman filter (UKF) are integrated to estimate the attitude and attitude rates of a nanosatellite recursively. First the SVD method minimizes the Wahba's loss function to find the optimal solution for the attitude on the basis of magnetometer and sun sensor vector measurements. Then the UKF uses this attitude information as the measurements for providing more accurate attitude estimates even when the satellite is in eclipse. The 'rotation angle error covariance matrix' calculated for the estimations of the SVD method are regarded as the measurement noise covariance for the UKF. Discussions for the UKF tuning are included specifically for the eclipse period where the SVD method fails and practically there is no measurements incoming to the filter.

AB - Singular value decomposition (SVD) method and unscented Kalman filter (UKF) are integrated to estimate the attitude and attitude rates of a nanosatellite recursively. First the SVD method minimizes the Wahba's loss function to find the optimal solution for the attitude on the basis of magnetometer and sun sensor vector measurements. Then the UKF uses this attitude information as the measurements for providing more accurate attitude estimates even when the satellite is in eclipse. The 'rotation angle error covariance matrix' calculated for the estimations of the SVD method are regarded as the measurement noise covariance for the UKF. Discussions for the UKF tuning are included specifically for the eclipse period where the SVD method fails and practically there is no measurements incoming to the filter.

KW - SVD

KW - UKF

KW - attitude estimation

KW - nanosatellite

UR - https://www.scopus.com/pages/publications/84959864587

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DO - 10.1109/RAST.2015.7208431

M3 - Conference contribution

AN - SCOPUS:84959864587

T3 - RAST 2015 - Proceedings of 7th International Conference on Recent Advances in Space Technologies

SP - 695

EP - 700

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

A2 - Unal, M. Fevzi

A2 - Basturk, Suleyman

A2 - Kaynak, Okyay

A2 - Hacioglu, Abdurrahman

A2 - Ince, Fuat

PB - Institute of Electrical and Electronics Engineers Inc.

T2 - 7th International Conference on Recent Advances in Space Technologies, RAST 2015

Y2 - 16 June 2015 through 19 June 2015

ER -

Cilden D , Hajiyev C, Soken HE. Attitude and attitude rate estimation for a nanosatellite using SVD and UKF. In Unal MF, Basturk S, Kaynak O, Hacioglu A, Ince F, editörler, RAST 2015 - Proceedings of 7th International Conference on Recent Advances in Space Technologies. Institute of Electrical and Electronics Engineers Inc. 2015. p. 695-700. 7208431. (RAST 2015 - Proceedings of 7th International Conference on Recent Advances in Space Technologies). doi: 10.1109/RAST.2015.7208431

Attitude and attitude rate estimation for a nanosatellite using SVD and UKF

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