Attitude and gyro bias estimation by SVD-aided EKF

Author:

Hajiyev Chingiz,Cilden-Guler Demet

Funder

Istanbul Technical University Scientific Research Projects Coordination Unit

Istanbul Teknik Üniversitesi

Publisher

Elsevier BV

Subject

Applied Mathematics,Electrical and Electronic Engineering,Condensed Matter Physics,Instrumentation

Reference49 articles.

1. A Vector Measurement-based Angular Velocity Estimation Scheme for Maneuvering Spacecraft;Jo;J. Astronaut. Sci.,2017

2. Review on Gyroless Attitude Determination Methods for Small Satellites;Hajiyev;Prog. Aerosp. Sci.,2017

3. Three-axis attitude determination via Kalman filtering of magnetometer data;Psiaki;J. Guid. Control Dyn.,1990

4. P. Sekhavat, Q. Gong, I.M. Ross, NPSAT 1 Parameter Estimation using Unscented Kalman Filter, in: Proc. 2007 Am. Control Conf., New York, USA, 2007: pp. 4445–4451. doi:10.1109/ACC.2007.4283031.

5. H.E. Soken, C. Hajiyev, Unscented Kalman Filter Based Attitude Estimation of ITU-PSAT I Satellite Using Magnetometer Measurements, in: Proc. Int. Work. Small Satell. New Mission. New Technol., Istanbul, TURKEY, 2008: pp. 72–76.

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