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Robust Saturated Finite Time Output Feedback Attitude Stabilization for Rigid Spacecraft / Qinglei Hu; Boyan Jiang; Michael Friswell

Journal of Guidance, Control, and Dynamics, Volume: 37, Issue: 6, Pages: 1914 - 1929

Swansea University Author: Michael, Friswell

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DOI (Published version): 10.2514/1.G000153

Published in: Journal of Guidance, Control, and Dynamics
Published: 2014
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College: College of Engineering
Issue: 6
Start Page: 1914
End Page: 1929