Suboptimal constant output feedback and its application to modern flight control system design

DOI10.1080/00207178108922937zbMath0456.49005OpenAlexW1971983090MaRDI QIDQ3906012

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Publication date: 1981

Published in: International Journal of Control (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1080/00207178108922937

zbMATH Keywords

flight controlsuboptimal feedback

Mathematics Subject Classification ID

Numerical methods involving duality (49M29) Linear systems in control theory (93C05) Asymptotic stability in control theory (93D20) Existence theories for optimal control problems involving ordinary differential equations (49J15) Model systems in control theory (93C99)

Related Items (2)

Constrained optimal estimation and control ⋮ A design method of discrete output feedback control system based on improved optimal regulator theory

Cites Work

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• Combined Primal-Dual and Penalty Methods for Constrained Minimization
• Quadratic weights for asymptotic regulator properties
• A concise derivation of optimal constant limited state feedback gains
• On optimal output feedback

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