Indirect adaptive control for attitude tracking of spacecraft with unknown reaction wheel friction
Author:
Funder
Harbin Institute of Technology
National Natural Science Foundation of China
Open Fund of National Defense Key Discipline Laboratory of Micro-Spacecraft Technology
Publisher
Elsevier BV
Subject
Aerospace Engineering
Reference16 articles.
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4. Inverse optimal adaptive control for attitude tracking of spacecraft;Luo;IEEE Trans. Autom. Control,2005
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