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 language | English |
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Pages (from-to) | 54-66 |
Number of pages | 13 |
Journal | Progress in Aerospace Sciences |
Volume | 90 |
DOIs | |
Publication status | Published - Apr 2017 |
Bibliographical note
Publisher Copyright:© 2017 Elsevier Ltd
Keywords
- Attitude determination
- Gyroless
- Kalman filter
- Measurement fault
- Single-frame method
- Small satellite