Dynamic output feedback sliding mode control for spacecraft hovering without velocity measurements

DOI10.1016/J.JFRANKLIN.2019.01.030zbMath1409.93018OpenAlexW2912296983WikidataQ128585798 ScholiaQ128585798MaRDI QIDQ1730063

Guang-Ren Duan, Ming-Da Ma, Kai Zhang

Publication date: 11 March 2019

Published in: Journal of the Franklin Institute (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/j.jfranklin.2019.01.030

zbMATH Keywords

finite-time stabilityoutput feedback sliding mode controlspacecraft hovering

Mathematics Subject Classification ID

Feedback control (93B52) Application models in control theory (93C95) Lyapunov and other classical stabilities (Lagrange, Poisson, (L^p, l^p), etc.) in control theory (93D05) Variable structure systems (93B12)

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