Review on gyroless attitude determination methods for small satellites

Chingiz Hajiyev*, Demet Cilden Guler

*Corresponding author for this work

Research output: Contribution to journalReview articlepeer-review

51 Citations (Scopus)

Abstract

This study surveys the developments in the gyroless attitude determination system, especially for small satellites. Two kinds of gyroless satellite attitude determination algorithms were reviewed namely, vector measurements and Kalman filter based methods. Traditional and nontraditional Kalman filters were considered in the Kalman filter based methods including Unscented Kalman Filter (UKF) and Extended Kalman Filter (EKF). Also, robust versions of those Kalman filters, which were incorporated with single, and multiple measurement noise scale factors (SMNSF, MMNSF respectively) are investigated and compared in the presence of measurement faults.

Original languageEnglish
Pages (from-to)54-66
Number of pages13
JournalProgress in Aerospace Sciences
Volume90
DOIs
Publication statusPublished - Apr 2017

Bibliographical note

Publisher Copyright:
© 2017 Elsevier Ltd

Keywords

  • Attitude determination
  • Gyroless
  • Kalman filter
  • Measurement fault
  • Single-frame method
  • Small satellite

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