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Using the method of invariant ellipsoids for linear robust output stabilization of spacecraft - MaRDI portal

Using the method of invariant ellipsoids for linear robust output stabilization of spacecraft

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Publication:647768

DOI10.1134/S0005117911030064zbMath1229.93138OpenAlexW2051244054MaRDI QIDQ647768

S. Gonzalez-Garcia, A. E. Polyakov, Alexander S. Poznyak

Publication date: 24 November 2011

Published in: Automation and Remote Control (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1134/s0005117911030064




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