Robustness analysis of dynamic inversion control laws applied to nonlinear aircraft pitch-axis models

DOI10.1016/S0362-546X(97)00503-8zbMath0947.93033WikidataQ127517451 ScholiaQ127517451MaRDI QIDQ4266441

Bing-Yu Zhang, Blaise G. Morton

Publication date: 30 September 1999

Published in: Nonlinear Analysis: Theory, Methods & Applications (Search for Journal in Brave)

zbMATH Keywords

robust stabilityfeedback linearizationnonlinear aircraft pitch-axis models

Mathematics Subject Classification ID

Sensitivity (robustness) (93B35) Nonlinear systems in control theory (93C10) Application models in control theory (93C95) Design techniques (robust design, computer-aided design, etc.) (93B51)

Related Items (2)

Existence and uniqueness of solutions for the second order periodic-integrable boundary value problem ⋮ Set membership inversion and robust control from data of nonlinear systems

Cites Work

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• Further facts about input to state stabilization
• Dynamic inversion: an evolving methodology for flight control design
• Smooth stabilization implies coprime factorization
• Stability of dynamic inversion control laws applied to nonlinear aircraft pitch-axis models

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