In-flight calibration of magnetometer and attitude determination system for land-survey mini-satellite

Yevgeny Somov; Sergey Butyrin; Chingiz Hajiyev

doi:10.1109/MetroAeroSpace.2015.7180668

In-flight calibration of magnetometer and attitude determination system for land-survey mini-satellite

Yevgeny Somov
, Sergey Butyrin
, Chingiz Hajiyev

Uçak Mühendisliği Bölümü

Samara State Technical University

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

3 Atıf (Scopus)

Özet

Magnetometers are widely used for attitude determination of low Earth orbit (LEO) information satellites. In order to estimate the satellite attitude accurately, bias of magnetometer must be estimated. In this study a Linear Kalman Filter (LKF) based algorithm for the estimation of magnetometer biases is proposed. Proposed algorithms are simulated through attitude dynamics of a small satellite. We shortly present also discrete algorithms for in-flight calibration and alignment of a low cost strap-down inertial navigation system with correction by signals from the Sun and magnetic sensors.

Orijinal dil	İngilizce
Ana bilgisayar yayını başlığı	2nd IEEE International Workshop on Metrology for Aerospace, MetroAeroSpace 2015 - Proceedings
Yayınlayan	Institute of Electrical and Electronics Engineers Inc.
Sayfalar	277-282
Sayfa sayısı	6
ISBN (Elektronik)	9781479975693
DOI'lar	https://doi.org/10.1109/MetroAeroSpace.2015.7180668
Yayın durumu	Yayınlandı - 5 Ağu 2015
Etkinlik	2nd IEEE International Workshop on Metrology for Aerospace, MetroAeroSpace 2015 - Benevento, Italy Süre: 3 Haz 2015 → 5 Haz 2015

Yayın serisi

Adı	2nd IEEE International Workshop on Metrology for Aerospace, MetroAeroSpace 2015 - Proceedings

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

???event.eventtypes.event.conference???	2nd IEEE International Workshop on Metrology for Aerospace, MetroAeroSpace 2015
Ülke/Bölge	Italy
Şehir	Benevento
Periyot	3/06/15 → 5/06/15

Bibliyografik not

Publisher Copyright:
© 2015 IEEE.

Belgeye Erişim

10.1109/MetroAeroSpace.2015.7180668

Diğer Dosyalar ve Linkler

Link to publication in Scopus

Alıntı Yap

Somov, Y., Butyrin, S., & Hajiyev, C. (2015). In-flight calibration of magnetometer and attitude determination system for land-survey mini-satellite. In 2nd IEEE International Workshop on Metrology for Aerospace, MetroAeroSpace 2015 - Proceedings (pp. 277-282). Makale 7180668 (2nd IEEE International Workshop on Metrology for Aerospace, MetroAeroSpace 2015 - Proceedings). Institute of Electrical and Electronics Engineers Inc.. https://doi.org/10.1109/MetroAeroSpace.2015.7180668

Somov, Yevgeny ; Butyrin, Sergey ; Hajiyev, Chingiz. / In-flight calibration of magnetometer and attitude determination system for land-survey mini-satellite. 2nd IEEE International Workshop on Metrology for Aerospace, MetroAeroSpace 2015 - Proceedings. Institute of Electrical and Electronics Engineers Inc., 2015. pp. 277-282 (2nd IEEE International Workshop on Metrology for Aerospace, MetroAeroSpace 2015 - Proceedings).

@inproceedings{8a11b0f466c541e6ba73c34e6ed5e5f6,

title = "In-flight calibration of magnetometer and attitude determination system for land-survey mini-satellite",

abstract = "Magnetometers are widely used for attitude determination of low Earth orbit (LEO) information satellites. In order to estimate the satellite attitude accurately, bias of magnetometer must be estimated. In this study a Linear Kalman Filter (LKF) based algorithm for the estimation of magnetometer biases is proposed. Proposed algorithms are simulated through attitude dynamics of a small satellite. We shortly present also discrete algorithms for in-flight calibration and alignment of a low cost strap-down inertial navigation system with correction by signals from the Sun and magnetic sensors.",

author = "Yevgeny Somov and Sergey Butyrin and Chingiz Hajiyev",

note = "Publisher Copyright: {\textcopyright} 2015 IEEE.; 2nd IEEE International Workshop on Metrology for Aerospace, MetroAeroSpace 2015 ; Conference date: 03-06-2015 Through 05-06-2015",

year = "2015",

month = aug,

day = "5",

doi = "10.1109/MetroAeroSpace.2015.7180668",

language = "English",

series = "2nd IEEE International Workshop on Metrology for Aerospace, MetroAeroSpace 2015 - Proceedings",

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

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booktitle = "2nd IEEE International Workshop on Metrology for Aerospace, MetroAeroSpace 2015 - Proceedings",

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}

Somov, Y, Butyrin, S & Hajiyev, C 2015, In-flight calibration of magnetometer and attitude determination system for land-survey mini-satellite. in 2nd IEEE International Workshop on Metrology for Aerospace, MetroAeroSpace 2015 - Proceedings., 7180668, 2nd IEEE International Workshop on Metrology for Aerospace, MetroAeroSpace 2015 - Proceedings, Institute of Electrical and Electronics Engineers Inc., pp. 277-282, 2nd IEEE International Workshop on Metrology for Aerospace, MetroAeroSpace 2015, Benevento, Italy, 3/06/15. https://doi.org/10.1109/MetroAeroSpace.2015.7180668

In-flight calibration of magnetometer and attitude determination system for land-survey mini-satellite. / Somov, Yevgeny; Butyrin, Sergey; Hajiyev, Chingiz.
2nd IEEE International Workshop on Metrology for Aerospace, MetroAeroSpace 2015 - Proceedings. Institute of Electrical and Electronics Engineers Inc., 2015. p. 277-282 7180668 (2nd IEEE International Workshop on Metrology for Aerospace, MetroAeroSpace 2015 - Proceedings).

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

TY - GEN

T1 - In-flight calibration of magnetometer and attitude determination system for land-survey mini-satellite

AU - Somov, Yevgeny

AU - Butyrin, Sergey

AU - Hajiyev, Chingiz

PY - 2015/8/5

Y1 - 2015/8/5

N2 - Magnetometers are widely used for attitude determination of low Earth orbit (LEO) information satellites. In order to estimate the satellite attitude accurately, bias of magnetometer must be estimated. In this study a Linear Kalman Filter (LKF) based algorithm for the estimation of magnetometer biases is proposed. Proposed algorithms are simulated through attitude dynamics of a small satellite. We shortly present also discrete algorithms for in-flight calibration and alignment of a low cost strap-down inertial navigation system with correction by signals from the Sun and magnetic sensors.

AB - Magnetometers are widely used for attitude determination of low Earth orbit (LEO) information satellites. In order to estimate the satellite attitude accurately, bias of magnetometer must be estimated. In this study a Linear Kalman Filter (LKF) based algorithm for the estimation of magnetometer biases is proposed. Proposed algorithms are simulated through attitude dynamics of a small satellite. We shortly present also discrete algorithms for in-flight calibration and alignment of a low cost strap-down inertial navigation system with correction by signals from the Sun and magnetic sensors.

UR - https://www.scopus.com/pages/publications/84941349031

U2 - 10.1109/MetroAeroSpace.2015.7180668

DO - 10.1109/MetroAeroSpace.2015.7180668

M3 - Conference contribution

AN - SCOPUS:84941349031

T3 - 2nd IEEE International Workshop on Metrology for Aerospace, MetroAeroSpace 2015 - Proceedings

SP - 277

EP - 282

BT - 2nd IEEE International Workshop on Metrology for Aerospace, MetroAeroSpace 2015 - Proceedings

PB - Institute of Electrical and Electronics Engineers Inc.

T2 - 2nd IEEE International Workshop on Metrology for Aerospace, MetroAeroSpace 2015

Y2 - 3 June 2015 through 5 June 2015

ER -

Somov Y, Butyrin S, Hajiyev C. In-flight calibration of magnetometer and attitude determination system for land-survey mini-satellite. In 2nd IEEE International Workshop on Metrology for Aerospace, MetroAeroSpace 2015 - Proceedings. Institute of Electrical and Electronics Engineers Inc. 2015. p. 277-282. 7180668. (2nd IEEE International Workshop on Metrology for Aerospace, MetroAeroSpace 2015 - Proceedings). doi: 10.1109/MetroAeroSpace.2015.7180668

In-flight calibration of magnetometer and attitude determination system for land-survey mini-satellite

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Diğer Dosyalar ve Linkler

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