Low cost attitude determination system for a LEO information mini-satellite

Yevgeny Somov; Sergey Butyrin; Sergey Somov; Chingiz Hajiyev

doi:10.1109/RAST.2015.7208436

Low cost attitude determination system for a LEO information mini-satellite

Yevgeny Somov
, Sergey Butyrin
, Sergey Somov
, Chingiz Hajiyev

Uçak Mühendisliği Bölümü

Samara State Technical University
Samara National Research University

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

Özet

We present method for in-flight signal processing and calibration of a strap-down inertial navigation system (SINS) for the information mini-satellites at low Earth orbit. We have applied the SINS correction based on the signals of a sun-magnetic system and consider the problem at a long-term forecasting of the mini-satellite's orbital motion.

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	725-730
Sayfa sayısı	6
ISBN (Elektronik)	9781467377607
DOI'lar	https://doi.org/10.1109/RAST.2015.7208436
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.2015.7208436

Diğer Dosyalar ve Linkler

Link to publication in Scopus

Alıntı Yap

Somov, Y., Butyrin, S., Somov, S., & Hajiyev, C. (2015). Low cost attitude determination system for a LEO information mini-satellite. 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. 725-730). Makale 7208436 (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.2015.7208436

Somov, Yevgeny ; Butyrin, Sergey ; Somov, Sergey et al. / Low cost attitude determination system for a LEO information mini-satellite. 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. 725-730 (RAST 2015 - Proceedings of 7th International Conference on Recent Advances in Space Technologies).

@inproceedings{e32392fa5a784bd193efada6b3dc081d,

title = "Low cost attitude determination system for a LEO information mini-satellite",

abstract = "We present method for in-flight signal processing and calibration of a strap-down inertial navigation system (SINS) for the information mini-satellites at low Earth orbit. We have applied the SINS correction based on the signals of a sun-magnetic system and consider the problem at a long-term forecasting of the mini-satellite's orbital motion.",

keywords = "SINS, calibration, mini-satellite, signal processing",

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

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.2015.7208436",

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 = "725--730",

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

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

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Somov, Y, Butyrin, S, Somov, S & Hajiyev, C 2015, Low cost attitude determination system for a LEO information mini-satellite. 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., 7208436, RAST 2015 - Proceedings of 7th International Conference on Recent Advances in Space Technologies, Institute of Electrical and Electronics Engineers Inc., pp. 725-730, 7th International Conference on Recent Advances in Space Technologies, RAST 2015, Istanbul, Türkiye, 16/06/15. https://doi.org/10.1109/RAST.2015.7208436

Low cost attitude determination system for a LEO information mini-satellite. / Somov, Yevgeny; Butyrin, Sergey; Somov, Sergey et al.
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. 725-730 7208436 (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 - Low cost attitude determination system for a LEO information mini-satellite

AU - Somov, Yevgeny

AU - Butyrin, Sergey

AU - Somov, Sergey

AU - Hajiyev, Chingiz

PY - 2015/8/17

Y1 - 2015/8/17

N2 - We present method for in-flight signal processing and calibration of a strap-down inertial navigation system (SINS) for the information mini-satellites at low Earth orbit. We have applied the SINS correction based on the signals of a sun-magnetic system and consider the problem at a long-term forecasting of the mini-satellite's orbital motion.

AB - We present method for in-flight signal processing and calibration of a strap-down inertial navigation system (SINS) for the information mini-satellites at low Earth orbit. We have applied the SINS correction based on the signals of a sun-magnetic system and consider the problem at a long-term forecasting of the mini-satellite's orbital motion.

KW - SINS

KW - calibration

KW - mini-satellite

KW - signal processing

UR - https://www.scopus.com/pages/publications/84959884699

U2 - 10.1109/RAST.2015.7208436

DO - 10.1109/RAST.2015.7208436

M3 - Conference contribution

AN - SCOPUS:84959884699

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

SP - 725

EP - 730

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 -

Somov Y, Butyrin S, Somov S, Hajiyev C. Low cost attitude determination system for a LEO information mini-satellite. 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. 725-730. 7208436. (RAST 2015 - Proceedings of 7th International Conference on Recent Advances in Space Technologies). doi: 10.1109/RAST.2015.7208436

Low cost attitude determination system for a LEO information mini-satellite

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Yayın serisi

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Bibliyografik not

Belgeye Erişim

Diğer Dosyalar ve Linkler

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