In-orbit calibration of attitude determination systems for land-survey micro-satellites

Ye Somov, C. Hacizade, S. Butyrin

Araştırma sonucu: ???type-name???Konferans katkısıbilirkişi

4 Atıf (Scopus)

Özet

Contemporary land-survey micro-satellites have general mass up to 100 kg and are placed on the orbit altitudes from 600 up to 800 km. For such spacecraft some principle problems on attitude determination, in-flight calibration and alignment are considered and elaborated methods are presented for their solving. We present discrete algorithms for calibration and alignment of the low cost strap-down inertial navigation systems with correction by signals from multi-head Sun sensor, magnetic sensor and the GPS/GLONASS satellites.

Orijinal dilİngilizce
Ana bilgisayar yayını başlığı19th IFAC World Congress IFAC 2014, Proceedings
EditörlerEdward Boje, Xiaohua Xia
YayınlayanIFAC Secretariat
Sayfalar7941-7946
Sayfa sayısı6
ISBN (Elektronik)9783902823625
DOI'lar
Yayın durumuYayınlandı - 2014
Etkinlik19th IFAC World Congress on International Federation of Automatic Control, IFAC 2014 - Cape Town, South Africa
Süre: 24 Ağu 201429 Ağu 2014

Yayın serisi

AdıIFAC Proceedings Volumes (IFAC-PapersOnline)
Hacim19
ISSN (Basılı)1474-6670

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???event.eventtypes.event.conference???19th IFAC World Congress on International Federation of Automatic Control, IFAC 2014
Ülke/BölgeSouth Africa
ŞehirCape Town
Periyot24/08/1429/08/14

Bibliyografik not

Publisher Copyright:
© IFAC.

Finansman

★This work was supported by TUBITAK (The Scientific and Technological Research Council of Turkey, Grant 113E595), RFBR (Russian Foundation for Basic Research, Grant 14-08-91373), and also by Division on EMMCP of the RAS (Program 14)

FinansörlerFinansör numarası
TUBITAK
Royal Astronomical Society
Russian Foundation for Basic Research14-08-91373
Türkiye Bilimsel ve Teknolojik Araştirma Kurumu113E595

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