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In-flight calibration of an integrated attitude determination system for a small information satellite

  • Yevgeny Somov
  • , Sergey Buryrin
  • , Sergey Somov
  • , Victor Fedosov
  • , Chingiz Hajiyev
  • , Akhmet Sofyali
  • Samara State Technical University
  • Czech Space Engineering Institute
  • Istanbul Technical University

Araştırma sonucu: Kitap/Rapor/Konferans Bildirisinde BölümKonferans katkısıbilirkişi

3 Atıf (Scopus)

Özet

Contemporary information mini-satellites have general mass up to 500 kg and are placed onto the orbit altitudes from 500 up to 1500 km. For such spacecraft some principle problems on precise attitude determination and in-flight calibration are considered and elaborated methods are presented for their solving. Original multiple discrete algorithms for filtering, integration and calibration of a strapped-down inertial navigation system for precise determining the spacecraft attitude, are presented. This system contains electrostatic micro-accelerometer, an inertial measurement unit based on the gyro sensors, an astronomical system based on star trackers, multi-head Sun sensor and magnetic sensor, the that are fixed to the spacecraft body.

Orijinal dilİngilizce
Ana bilgisayar yayını başlığıRAST 2013 - Proceedings of 6th International Conference on Recent Advances in Space Technologies
Sayfalar1103-1108
Sayfa sayısı6
DOI'lar
Yayın durumuYayınlandı - 2013
Etkinlik6th International Conference on Recent Advances in Space Technologies, RAST 2013 - Istanbul, Türkiye
Süre: 12 Haz 201314 Haz 2013

Yayın serisi

AdıRAST 2013 - Proceedings of 6th International Conference on Recent Advances in Space Technologies

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???event.eventtypes.event.conference???6th International Conference on Recent Advances in Space Technologies, RAST 2013
Ülke/BölgeTürkiye
ŞehirIstanbul
Periyot12/06/1314/06/13

Finansman

★ The work was supported by RFBR (Grants 11-08-01037, 13-08-97000) and by Division on EMMCP of the RAS (Program 14)

FinansörlerFinansör numarası
Division on EMMCP
Rochester Academy of Science
Russian Foundation for Basic Research13-08-97000, 11-08-01037

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