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Published in 2022 at "IEEE Control Systems Letters"
DOI: 10.1109/lcsys.2021.3137714
Abstract: This letter considers a robust sliding mode control method for a spacecraft attitude control. The design of the control law is based on the reaching law approach for continuous-time systems. A novel method is proposed…
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Keywords:
reaching law;
control law;
law;
based smc ... See more keywords