Optimal Output Feedback Controllers for Spacecraft Attitude Tracking
Author:
Affiliation:
1. Department of Mathematics, Faculty of Applied Science; King Mongkut's University of Technology North Bangkok; Bangkok; 10800; Thailand
Publisher
Wiley
Subject
Control and Systems Engineering
Reference41 articles.
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4. Robust attitude and vibration control of a nonlinear flexible spacecraft;Malekzadeh;Asian J. Control,2012
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