Nontraditional UKF based nanosatellite attitude estimation with the process and measurement noise covariances adaptation

Chingiz Hajiyev; Demet Cilden Guler; Halil Ersin Soken

doi:10.1109/RAST.2017.8003009

Nontraditional UKF based nanosatellite attitude estimation with the process and measurement noise covariances adaptation

Chingiz Hajiyev
, Demet Cilden Guler
, Halil Ersin Soken

Japan Aerospace Exploration Agency

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

2 Atıf (Scopus)

Özet

In this study, we add on to our previous researches for non-traditional filtering the investigation of measurement and process noise covariance adaptation and propose an Adaptive Unscented Kalman Filter (AUKF) for nanosatellite attitude estimation. Singular Value Decomposition (SVD) method runs using the magnetometer and sun sensor measurements as the first stage of the algorithm and estimates the attitude of the nanosatellite giving one estimate at a single-frame. Then these estimated attitude terms are given as input to the AUKF. In the result, the attitude and attitude rates of the satellite are estimated reliably in the whole orbital period.

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	381-386
Sayfa sayısı	6
ISBN (Elektronik)	9781538616031
DOI'lar	https://doi.org/10.1109/RAST.2017.8003009
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.

Belgeye Erişim

10.1109/RAST.2017.8003009

Diğer Dosyalar ve Linkler

Link to publication in Scopus

Alıntı Yap

Hajiyev, C., Guler, D. C., & Soken, H. E. (2017). Nontraditional UKF based nanosatellite attitude estimation with the process and measurement noise covariances adaptation. 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. 381-386). Makale 8003009 (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.2017.8003009

Hajiyev, Chingiz ; Guler, Demet Cilden ; Soken, Halil Ersin. / Nontraditional UKF based nanosatellite attitude estimation with the process and measurement noise covariances adaptation. 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. 381-386 (Proceedings of 8th International Conference on Recent Advances in Space Technologies, RAST 2017).

@inproceedings{11ba827cee104ce1b51f46ac3e7867ae,

title = "Nontraditional UKF based nanosatellite attitude estimation with the process and measurement noise covariances adaptation",

abstract = "In this study, we add on to our previous researches for non-traditional filtering the investigation of measurement and process noise covariance adaptation and propose an Adaptive Unscented Kalman Filter (AUKF) for nanosatellite attitude estimation. Singular Value Decomposition (SVD) method runs using the magnetometer and sun sensor measurements as the first stage of the algorithm and estimates the attitude of the nanosatellite giving one estimate at a single-frame. Then these estimated attitude terms are given as input to the AUKF. In the result, the attitude and attitude rates of the satellite are estimated reliably in the whole orbital period.",

keywords = "Attitude estimation, adaptive unscented Kalman filter, nanosatellite, single-frame estimator",

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

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.2017.8003009",

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 = "381--386",

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",

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Hajiyev, C , Guler, DC & Soken, HE 2017, Nontraditional UKF based nanosatellite attitude estimation with the process and measurement noise covariances adaptation. 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., 8003009, Proceedings of 8th International Conference on Recent Advances in Space Technologies, RAST 2017, Institute of Electrical and Electronics Engineers Inc., pp. 381-386, 8th International Conference on Recent Advances in Space Technologies, RAST 2017, Istanbul, Turkey, 19/06/17. https://doi.org/10.1109/RAST.2017.8003009

Nontraditional UKF based nanosatellite attitude estimation with the process and measurement noise covariances adaptation. / Hajiyev, Chingiz ; Guler, Demet Cilden; Soken, Halil Ersin.
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. 381-386 8003009 (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 - Nontraditional UKF based nanosatellite attitude estimation with the process and measurement noise covariances adaptation

AU - Hajiyev, Chingiz

AU - Guler, Demet Cilden

AU - Soken, Halil Ersin

PY - 2017/8/4

Y1 - 2017/8/4

N2 - In this study, we add on to our previous researches for non-traditional filtering the investigation of measurement and process noise covariance adaptation and propose an Adaptive Unscented Kalman Filter (AUKF) for nanosatellite attitude estimation. Singular Value Decomposition (SVD) method runs using the magnetometer and sun sensor measurements as the first stage of the algorithm and estimates the attitude of the nanosatellite giving one estimate at a single-frame. Then these estimated attitude terms are given as input to the AUKF. In the result, the attitude and attitude rates of the satellite are estimated reliably in the whole orbital period.

AB - In this study, we add on to our previous researches for non-traditional filtering the investigation of measurement and process noise covariance adaptation and propose an Adaptive Unscented Kalman Filter (AUKF) for nanosatellite attitude estimation. Singular Value Decomposition (SVD) method runs using the magnetometer and sun sensor measurements as the first stage of the algorithm and estimates the attitude of the nanosatellite giving one estimate at a single-frame. Then these estimated attitude terms are given as input to the AUKF. In the result, the attitude and attitude rates of the satellite are estimated reliably in the whole orbital period.

KW - Attitude estimation

KW - adaptive unscented Kalman filter

KW - nanosatellite

KW - single-frame estimator

UR - https://www.scopus.com/pages/publications/85030214320

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

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

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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 , Guler DC, Soken HE. Nontraditional UKF based nanosatellite attitude estimation with the process and measurement noise covariances adaptation. 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. 381-386. 8003009. (Proceedings of 8th International Conference on Recent Advances in Space Technologies, RAST 2017). doi: 10.1109/RAST.2017.8003009

Nontraditional UKF based nanosatellite attitude estimation with the process and measurement noise covariances adaptation

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