State-Dependent Riccati Equation for Control of Aeroelastic Flutter

descriptionPublicationkeyboard_double_arrow_right Article 01 Nov 2003 English Publisher:American Institute of Aeronautics and Astronautics (AIAA)Journal:Journal of Guidance, Control, and Dynamics, volume 26, pages 914-917 (issn: 0731-5090, eissn: 1533-3884,

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Authors: M. Tadi;

doi: 10.2514/2.6918

State-Dependent Riccati Equation for Control of Aeroelastic Flutter

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Abstract

Feedback control design for suppression of flutter in an aeroelastic system is studied. Feedback control laws based on the state-dependent Riccati equation are derived. Two control laws are studied: one formulation uses an observer to estimate the states after which it uses the estimated states to generate feedback law; the other formulation uses partial observation to directly generate the control law.

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University of Colorado Denver
United States

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