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Adaptive feedback linearization for the control of a typical wing section with structural nonlinearity - MaRDI portal

Adaptive feedback linearization for the control of a typical wing section with structural nonlinearity (Q1307800)

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scientific article; zbMATH DE number 1360016
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English
Adaptive feedback linearization for the control of a typical wing section with structural nonlinearity
scientific article; zbMATH DE number 1360016

    Statements

    Adaptive feedback linearization for the control of a typical wing section with structural nonlinearity (English)
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    19 November 2000
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    aeroelasticity
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    aeroservoelasticity
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    adaptive nonlinear feedback control
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    parameterization
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    structural nonlinearity
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    Lie algebraic methods
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    closed loop stability
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    La Salle's invariance principle
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