What is it about?
designing and applying Super twisting and terminal sliding mode controller and observer for the spacecraft attitude control subsystem simulator. the closed loop stability is proved.
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Why is it important?
the spacecraft simulator modeling the closed loop stability
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This page is a summary of: Hardware-in-the-loop attitude control via a high-order sliding mode controller/observer, Proceedings of the Institution of Mechanical Engineers Part G Journal of Aerospace Engineering, May 2017, SAGE Publications,
DOI: 10.1177/0954410017706992.
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