Robust stability analysis for a cruise missile

DOI10.1016/S1004-4132(08)60154-1zbMath1228.93092OpenAlexW173503494MaRDI QIDQ3087695

Hongzhong Ma, Guangfu Ma, Yingjing Shi

Publication date: 16 August 2011

Published in: Journal of Systems Engineering and Electronics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/s1004-4132(08)60154-1

zbMATH Keywords

robust controlaircraft controlquadratic stabilizationleast square

Mathematics Subject Classification ID

Design techniques (robust design, computer-aided design, etc.) (93B51) Linear systems in control theory (93C05) Automated systems (robots, etc.) in control theory (93C85) Robust stability (93D09) Control/observation systems governed by ordinary differential equations (93C15)

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A TIME-FUEL OPTIMAL CONTROL PROBLEM OF A CRUISE MISSILE BASED ON AN IMPROVED SLIDING MODE VARIABLE STRUCTURE MODEL

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