Signal processing and calibration of low-cost strap-down inertial navigation system for land-survey mini-satellite

Yevgeny Somov; Sergey Butyrin; Chingiz Hajiyev

doi:10.1063/1.4904677

Signal processing and calibration of low-cost strap-down inertial navigation system for land-survey mini-satellite

Yevgeny Somov
, Sergey Butyrin
, Chingiz Hajiyev

Uçak Mühendisliği Bölümü

Samara State Technical University

Araştırma çıktısı: Kitap/Rapor/Konferans Bildirisinde Bölüm › Konferans katkısı › Hakem

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 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	10th International Conference on Mathematical Problems in Engineering, Aerospace and Sciences, ICNPAA 2014
Editörler	Seenith Sivasundaram
Yayınlayan	American Institute of Physics Inc.
Sayfalar	1028-1037
Sayfa sayısı	10
ISBN (Elektronik)	9780735412767
DOI'lar	https://doi.org/10.1063/1.4904677
Yayın durumu	Yayınlandı - 10 Ara 2014
Etkinlik	10th International Conference on Mathematical Problems in Engineering, Aerospace and Sciences, ICNPAA 2014 - Narvik, Norway Süre: 15 Tem 2014 → 18 Tem 2014

Yayın serisi

Adı	AIP Conference Proceedings
Hacim	1637
ISSN (Basılı)	0094-243X
ISSN (Elektronik)	1551-7616

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

???event.eventtypes.event.conference???	10th International Conference on Mathematical Problems in Engineering, Aerospace and Sciences, ICNPAA 2014
Ülke/Bölge	Norway
Şehir	Narvik
Periyot	15/07/14 → 18/07/14

Bibliyografik not

Publisher Copyright:
© 2014 AIP Publishing LLC.

Belgeye Erişim

10.1063/1.4904677

Diğer Dosyalar ve Linkler

Link to publication in Scopus

Alıntı Yap

Somov, Y., Butyrin, S., & Hajiyev, C. (2014). Signal processing and calibration of low-cost strap-down inertial navigation system for land-survey mini-satellite. In S. Sivasundaram (Ed.), 10th International Conference on Mathematical Problems in Engineering, Aerospace and Sciences, ICNPAA 2014 (pp. 1028-1037). (AIP Conference Proceedings; Hac. 1637). American Institute of Physics Inc.. https://doi.org/10.1063/1.4904677

Somov, Yevgeny ; Butyrin, Sergey ; Hajiyev, Chingiz. / Signal processing and calibration of low-cost strap-down inertial navigation system for land-survey mini-satellite. 10th International Conference on Mathematical Problems in Engineering, Aerospace and Sciences, ICNPAA 2014. editör / Seenith Sivasundaram. American Institute of Physics Inc., 2014. pp. 1028-1037 (AIP Conference Proceedings).

@inproceedings{47028baf47f14912a5e6390e58b73e57,

title = "Signal processing and calibration of low-cost strap-down inertial navigation 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 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.",

keywords = "attitude determination, calibration, mini-satellite, signal processing",

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

note = "Publisher Copyright: {\textcopyright} 2014 AIP Publishing LLC.; 10th International Conference on Mathematical Problems in Engineering, Aerospace and Sciences, ICNPAA 2014 ; Conference date: 15-07-2014 Through 18-07-2014",

year = "2014",

month = dec,

day = "10",

doi = "10.1063/1.4904677",

language = "English",

series = "AIP Conference Proceedings",

publisher = "American Institute of Physics Inc.",

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editor = "Seenith Sivasundaram",

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Somov, Y, Butyrin, S & Hajiyev, C 2014, Signal processing and calibration of low-cost strap-down inertial navigation system for land-survey mini-satellite. in S Sivasundaram (ed.), 10th International Conference on Mathematical Problems in Engineering, Aerospace and Sciences, ICNPAA 2014. AIP Conference Proceedings, hac. 1637, American Institute of Physics Inc., pp. 1028-1037, 10th International Conference on Mathematical Problems in Engineering, Aerospace and Sciences, ICNPAA 2014, Narvik, Norway, 15/07/14. https://doi.org/10.1063/1.4904677

Signal processing and calibration of low-cost strap-down inertial navigation system for land-survey mini-satellite. / Somov, Yevgeny; Butyrin, Sergey; Hajiyev, Chingiz.
10th International Conference on Mathematical Problems in Engineering, Aerospace and Sciences, ICNPAA 2014. ed. / Seenith Sivasundaram. American Institute of Physics Inc., 2014. p. 1028-1037 (AIP Conference Proceedings; Hac. 1637).

Araştırma çıktısı: Kitap/Rapor/Konferans Bildirisinde Bölüm › Konferans katkısı › Hakem

TY - GEN

T1 - Signal processing and calibration of low-cost strap-down inertial navigation system for land-survey mini-satellite

AU - Somov, Yevgeny

AU - Butyrin, Sergey

AU - Hajiyev, Chingiz

PY - 2014/12/10

Y1 - 2014/12/10

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 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 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.

KW - attitude determination

KW - calibration

KW - mini-satellite

KW - signal processing

UR - https://www.scopus.com/pages/publications/84941333667

U2 - 10.1063/1.4904677

DO - 10.1063/1.4904677

M3 - Conference contribution

AN - SCOPUS:84941333667

T3 - AIP Conference Proceedings

SP - 1028

EP - 1037

BT - 10th International Conference on Mathematical Problems in Engineering, Aerospace and Sciences, ICNPAA 2014

A2 - Sivasundaram, Seenith

PB - American Institute of Physics Inc.

T2 - 10th International Conference on Mathematical Problems in Engineering, Aerospace and Sciences, ICNPAA 2014

Y2 - 15 July 2014 through 18 July 2014

ER -

Somov Y, Butyrin S, Hajiyev C. Signal processing and calibration of low-cost strap-down inertial navigation system for land-survey mini-satellite. In Sivasundaram S, editör, 10th International Conference on Mathematical Problems in Engineering, Aerospace and Sciences, ICNPAA 2014. American Institute of Physics Inc. 2014. p. 1028-1037. (AIP Conference Proceedings). doi: 10.1063/1.4904677

Signal processing and calibration of low-cost strap-down inertial navigation system for land-survey mini-satellite

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