Attitude filtering with uncertain process and measurement noise covariance using SVD‐aided adaptive UKF

Author:

Hajiyev Chingiz1ORCID,Cilden‐Guler Demet2ORCID

Affiliation:

1. Department of Aeronautical Engineering, Faculty of Aeronautics and Astronautics Istanbul Technical University Istanbul Turkey

2. Department of Astronautical Engineering, Faculty of Aeronautics and Astronautics Istanbul Technical University Istanbul Turkey

Publisher

Wiley

Subject

Electrical and Electronic Engineering,Industrial and Manufacturing Engineering,Mechanical Engineering,Aerospace Engineering,Biomedical Engineering,General Chemical Engineering,Control and Systems Engineering

Reference43 articles.

1. NPSAT1 Parameter Estimation Using Unscented Kalman Filtering

2. Estimation of Pico satellite attitude dynamics and external torques via unscented Kalman filter;Soken HE;J Aerospace Technol Manage,2014

3. Flight results of a low-cost attitude determination system

4. Inexpensive Cubesat attitude estimation using quaternions and unscented Kalman filtering;Vinther K;Autom Control Aerosp,2011

5. Estimation of Pico satellite attitude dynamics and external torques via unscented Kalman filter;Söken HE;J Aerosp Technol Manage,2014

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