Aircraft flight controls design using output feedback

DOI10.2514/3.20824zbMath0749.93035OpenAlexW2038783476MaRDI QIDQ4006392

Frank L. Lewis, Fouad M. AL-Sunni, B. L. Stevens

Publication date: 26 September 1992

Published in: Journal of Guidance, Control, and Dynamics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.2514/3.20824

zbMATH Keywords

optimal controllinear quadratic output-feedback techniques

Mathematics Subject Classification ID

Design techniques (robust design, computer-aided design, etc.) (93B51)

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