Pico satellite attitude estimation via Robust Unscented Kalman Filter in the presence of measurement faults

Author:

Soken Halil Ersin,Hajiyev Chingiz

Publisher

Elsevier BV

Subject

Applied Mathematics,Control and Systems Engineering,Electrical and Electronic Engineering,Computer Science Applications,Instrumentation

Reference19 articles.

1. Kalman filtering for spacecraft attitude estimation;Lefferts;Journal of Guidance, Control, and Dynamics,1982

2. Three-axis attitude determination via Kalman filtering of magnetometer data;Psiaki;Journal of Guidance, Control, and Dynamics,1990

3. A new approach for filtering nonlinear systems;Julier,1995

4. Unscented filtering and nonlinear estimation;Julier;Proceedings of IEEE,2004

5. A new method for the nonlinear transformation of means and covariances in filters and estimators;Julier;IEEE Transactions on Automatic Control,2000

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