This paper explores feedback controller design for cavity flows based on reduced-order models derived using Proper Orthogonal Decomposition (POD) along with Galerkin projection method. Our preliminary analysis shows that the equilibrium of the POD model is unstable and a static output feedback controller cannot stabilize it. We develop Linear Quadratic (LQ) optimal state feedback controllers and LQ optimal observers for the linearized models. The linear controllers and observers are applied to the nonlinear system using simulations. The controller robustness is numerically tested with respect to different POD models generated at different forcing frequencies. An estimation for the region of attraction of the linear controllers is also provi...
This report presents results of experiments and numerical simulations studying closed-loop feedback ...
Models for understanding and controlling oscillations in the flow past a rectangular cavity are deve...
Flow over open cavities is mainly governed by a feedback mechanism due to the interaction of shear l...
In our recent work we presented preliminary results for subsonic cavity flow control using a reduce...
A benchmark problem in active aerodynamic flow control, suppression of strong pressure oscillations ...
A novel feedback control design method is proposed to tackle nonlinear fluid flow dynamics based on ...
In this paper, we present the latest results of our ongoing research activities in the development o...
A study is presented of the modeling and implementation of different concepts for linear feedback co...
One of the current three main thrust areas of the Collaborative Center of Control Science (CCCS) at ...
Feedback control of aerodynamic flows is attracting the attention of researchers from a wide spectru...
Using data from direct numerical simulations, linear models of the compressible flow past a rectangu...
International audienceThe control of separated fluid flow by reduced-order models is studied using t...
Flow over open cavities is mainly governed by a feedback mechanism due to the interaction of shear l...
Linear Quadratic Gaussian (LQG) control is a promising tool to control flows. Initially developed fo...
This work aims at understanding how the different elements involved in the feedback loop influence ...
This report presents results of experiments and numerical simulations studying closed-loop feedback ...
Models for understanding and controlling oscillations in the flow past a rectangular cavity are deve...
Flow over open cavities is mainly governed by a feedback mechanism due to the interaction of shear l...
In our recent work we presented preliminary results for subsonic cavity flow control using a reduce...
A benchmark problem in active aerodynamic flow control, suppression of strong pressure oscillations ...
A novel feedback control design method is proposed to tackle nonlinear fluid flow dynamics based on ...
In this paper, we present the latest results of our ongoing research activities in the development o...
A study is presented of the modeling and implementation of different concepts for linear feedback co...
One of the current three main thrust areas of the Collaborative Center of Control Science (CCCS) at ...
Feedback control of aerodynamic flows is attracting the attention of researchers from a wide spectru...
Using data from direct numerical simulations, linear models of the compressible flow past a rectangu...
International audienceThe control of separated fluid flow by reduced-order models is studied using t...
Flow over open cavities is mainly governed by a feedback mechanism due to the interaction of shear l...
Linear Quadratic Gaussian (LQG) control is a promising tool to control flows. Initially developed fo...
This work aims at understanding how the different elements involved in the feedback loop influence ...
This report presents results of experiments and numerical simulations studying closed-loop feedback ...
Models for understanding and controlling oscillations in the flow past a rectangular cavity are deve...
Flow over open cavities is mainly governed by a feedback mechanism due to the interaction of shear l...