Enhancing Disturbance Rejection in Minisatellite Attitude Control: A Comparative Study
Author:
Affiliation:
1. Istanbul Technical University,Aeronautical Engineering Department,Istanbul,Türkiye
Publisher
IEEE
Link
http://xplorestaging.ieee.org/ielx7/10197839/10197652/10197865.pdf?arnumber=10197865
Reference21 articles.
1. Quaternion based linear time-varying model predictive attitude control for satellites with two reaction wheels
2. MPC for coupled station keeping, attitude control, and momentum management of low-thrust geostationary satellites
3. Satellite dynamics and control in a quaternion formulation;blanke;Technical University of Denmark Department of Electrical Engineering Tech Rep 2010,0
4. Incorporating delayed star tracker measurements in Gokturk-2 satellite attitude filter
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