Nonlinear performance of a PI controlled missile: an explanation

DOI<485::AID-RNC417>3.0.CO;2-4 10.1002/(SICI)1099-1239(19990715)9:8<485::AID-RNC417>3.0.CO;2-4zbMath0937.93033OpenAlexW2178149309MaRDI QIDQ4267018

G. Ferreres, Gérard Scorletti, Vincent Fromion

Publication date: 23 November 1999

Full work available at URL: https://doi.org/10.1002/(sici)1099-1239(19990715)9:8<485::aid-rnc417>3.0.co;2-4

zbMATH Keywords

linear matrix inequalitiesnonlinear dynamical systemsconvex optimization problemsmissilequantitative robustnessincremental performance

Mathematics Subject Classification ID

Convex programming (90C25) Sensitivity (robustness) (93B35) Linear inequalities of matrices (15A39) Nonlinear systems in control theory (93C10) Application models in control theory (93C95) Design techniques (robust design, computer-aided design, etc.) (93B51)

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Uses Software

• LMITOOL
• LMI toolbox

Cites Work

• Unnamed Item
• Set-valued system of fractional differential equations with hysteresis
• Linear Matrix Inequalities in System and Control Theory
• On the -Boundedness of Solutions of Nonlinear Functional Equations

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