Adaptive Output Feedback Control of a Nonlinear Aeroelastic Structure
- 1 November 2000
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Guidance, Control, and Dynamics
- Vol. 23 (6), 1109-1116
- https://doi.org/10.2514/2.4662
Abstract
No abstract availableThis publication has 14 references indexed in Scilit:
- Adaptive Control of Aeroelastic Instabilities in Transonic Flow and Its ScalingJournal of Guidance, Control, and Dynamics, 1997
- Nonlinear Control of a Prototypical Wing Section with Torsional NonlinearityJournal of Guidance, Control, and Dynamics, 1997
- Fundamental Mechanisms of Aeroelastic Control with Control Surface and Strain ActuationJournal of Guidance, Control, and Dynamics, 1995
- Flutter and stall response of a helicopter blade with structural nonlinearityJournal of Aircraft, 1992
- Chaotic motions of an airfoil with non-linear stiffness in incompressible flowJournal of Sound and Vibration, 1990
- Reduced-Order Optimal Feedback Control Law Synthesis for Flutter SuppressionJournal of Guidance, Control, and Dynamics, 1982
- Design for Active Flutter Suppression and Gust Alleviation Using State-Space Aeroelastic ModelingJournal of Aircraft, 1982
- Practical gust load alleviation and flutter suppression control laws based on a LQG methodologyPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1981
- Unsteady aerodynamic modeling for arbitrary motionsAIAA Journal, 1979
- An Elementary Explanation of the Flutter Mechanism with Active Feedback ControlsJournal of Aircraft, 1979