Fault tolerant control of attitude dynamics of nanosatellites

Demet Cilden Guler; Chingiz Hajiyev; Janset Dasdemir

doi:10.1109/RAST.2017.8002964

Fault tolerant control of attitude dynamics of nanosatellites

Yildiz Technical University

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

Özet

In this paper, fault-tolerant active control of the rotational motion of the satellite has been applied. Satellite mathematical models are introduced, and the nontraditional Kalman filter is designed with the presented control algorithms. Re-adjustment control procedure has been established taking into account the identified control distribution matrix. If there are three-axis reaction wheels on the satellite, the failure of one actuator, control setting is carried out using control distribution matrix diagnostics. Extended Kalman Filter has been introduced to control the distribution estimation of matrix elements, so check back adjustment rule is applied by the fault tolerant attitude control.

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	349-353
Sayfa sayısı	5
ISBN (Elektronik)	9781538616031
DOI'lar	https://doi.org/10.1109/RAST.2017.8002964
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.

Finansman

ACKNOWLEDGMENT This work was carried out under the support of the project 113E595 of the Scientific and Technological Research Council of Turkey (TUBITAK).

Finansörler
TUBITAK
Türkiye Bilimsel ve Teknolojik Araştirma Kurumu

Belgeye Erişim

10.1109/RAST.2017.8002964

Diğer Dosyalar ve Linkler

Link to publication in Scopus

Alıntı Yap

Guler, D. C., Hajiyev, C., & Dasdemir, J. (2017). Fault tolerant control of attitude dynamics of nanosatellites. 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. 349-353). Makale 8002964 (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.2017.8002964

Guler, Demet Cilden ; Hajiyev, Chingiz ; Dasdemir, Janset. / Fault tolerant control of attitude dynamics of nanosatellites. 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. 349-353 (Proceedings of 8th International Conference on Recent Advances in Space Technologies, RAST 2017).

@inproceedings{733133e0ce0a4f7682dce56b34dc89ba,

title = "Fault tolerant control of attitude dynamics of nanosatellites",

abstract = "In this paper, fault-tolerant active control of the rotational motion of the satellite has been applied. Satellite mathematical models are introduced, and the nontraditional Kalman filter is designed with the presented control algorithms. Re-adjustment control procedure has been established taking into account the identified control distribution matrix. If there are three-axis reaction wheels on the satellite, the failure of one actuator, control setting is carried out using control distribution matrix diagnostics. Extended Kalman Filter has been introduced to control the distribution estimation of matrix elements, so check back adjustment rule is applied by the fault tolerant attitude control.",

keywords = "attitude, estimation, fault tolerant control, nanosatellite, reconfigurable control",

author = "Guler, \{Demet Cilden\} and Chingiz Hajiyev and Janset Dasdemir",

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.2017.8002964",

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series = "Proceedings of 8th International Conference on Recent Advances in Space Technologies, RAST 2017",

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

pages = "349--353",

editor = "M.F. Unal and A. Hacioglu and M.S. Yildiz and O. Altan and M. Yorukoglu",

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Guler, DC , Hajiyev, C & Dasdemir, J 2017, Fault tolerant control of attitude dynamics of nanosatellites. 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., 8002964, Proceedings of 8th International Conference on Recent Advances in Space Technologies, RAST 2017, Institute of Electrical and Electronics Engineers Inc., pp. 349-353, 8th International Conference on Recent Advances in Space Technologies, RAST 2017, Istanbul, Turkey, 19/06/17. https://doi.org/10.1109/RAST.2017.8002964

Fault tolerant control of attitude dynamics of nanosatellites. / Guler, Demet Cilden ; Hajiyev, Chingiz; Dasdemir, Janset.
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. 349-353 8002964 (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 - Fault tolerant control of attitude dynamics of nanosatellites

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N2 - In this paper, fault-tolerant active control of the rotational motion of the satellite has been applied. Satellite mathematical models are introduced, and the nontraditional Kalman filter is designed with the presented control algorithms. Re-adjustment control procedure has been established taking into account the identified control distribution matrix. If there are three-axis reaction wheels on the satellite, the failure of one actuator, control setting is carried out using control distribution matrix diagnostics. Extended Kalman Filter has been introduced to control the distribution estimation of matrix elements, so check back adjustment rule is applied by the fault tolerant attitude control.

AB - In this paper, fault-tolerant active control of the rotational motion of the satellite has been applied. Satellite mathematical models are introduced, and the nontraditional Kalman filter is designed with the presented control algorithms. Re-adjustment control procedure has been established taking into account the identified control distribution matrix. If there are three-axis reaction wheels on the satellite, the failure of one actuator, control setting is carried out using control distribution matrix diagnostics. Extended Kalman Filter has been introduced to control the distribution estimation of matrix elements, so check back adjustment rule is applied by the fault tolerant attitude control.

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KW - estimation

KW - fault tolerant control

KW - nanosatellite

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PB - Institute of Electrical and Electronics Engineers Inc.

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Guler DC , Hajiyev C, Dasdemir J. Fault tolerant control of attitude dynamics of nanosatellites. 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. 349-353. 8002964. (Proceedings of 8th International Conference on Recent Advances in Space Technologies, RAST 2017). doi: 10.1109/RAST.2017.8002964

Fault tolerant control of attitude dynamics of nanosatellites

Özet

Yayın serisi

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

Bibliyografik not

Finansman

Belgeye Erişim

Diğer Dosyalar ve Linkler

Parmak izi

Alıntı Yap