Adaptive Closed-Loop Separation Control on a High-Lift Configuration Using Extremum Seeking

By Ralf Becker, R. King, R. Petz, Wolfgang Nitsche. 2006

218 citations recorded by the source corpus.

Subfields: Aerospace Engineering, Computational Mechanics, Control and Systems Engineering

View Paper: https://www.semanticscholar.org/paper/41017cefec53479fae3d75d723f667ee03b48944

How researchers see this paper

The researchers whose trusted networks rank it highest, strongest advocate first. Every researcher gets a different order.

In Aerospace Engineering

1. Bernd R. Noack
2. Igor V. Adamovich
3. Mohammad Samimy
4. J. Little
5. M. Nishihara
6. Clarence W. Rowley
7. Saman Rashidi
8. Miroslav Krstic

In Computational Mechanics

1. Bernd R. Noack
2. Steven L. Brunton
3. Clarence W. Rowley
4. Maziar S. Hemati
5. J. Nathan Kutz
6. Louis N. Cattafesta
7. Igor V. Adamovich
8. Eric A. Deem

In Control and Systems Engineering

1. Dragan Nesic
2. Bernd R. Noack
3. R. King
4. Maziar S. Hemati
5. Azad Ghaffari
6. Tamer Basar
7. Paul Frihauf
8. Miroslav Krstic

Citations in the corpus

• Multivariable Newton-based extremum seeking (2011, background): “INTRODUCTION a) Motivation: Dramatic advances have occurred over the past decade both in the theory [2], [3], [7], [12], [16], [17], [18], [19], [20], [21] and in applications [4], [5], [6], [8], [9], [10], [11], [13], [22], [23] of extremum seeking control.”
• Adaptive separation control of a laminar boundary layer using online dynamic mode decomposition (2020, methodology): “These approaches have been utilized in separation control studies (Becker et al. 2007; Benard et al. 2010).”
• Feedback shear layer control for bluff body drag reduction (2008, background): “A case in point is the saturated effect of an actuation amplitude on the separation region and flow reattachment over an aircraft wing (Becker et al. 2007).”
• High-lift airfoil trailing edge separation control using a single dielectric barrier discharge plasma actuator (2010, background): “Control of flow separation over simple flaps on high-lift airfoils has been investigated in both open-loop (Kiedaisch et al. 2006; Melton et al. 2006) and closed-loop (Becker et al. 2007) configurations using synthetic jets and more recently with plasma actuators (Mabe et al. 2009).”
• Vortex shedding suppression and wake control: A review (2016, background): “Becker and King (2006) controlled the separation on a high-lift configuration by using extremum seeking control.”
• Nash Equilibrium Seeking in Noncooperative Games (2012, background): “Many works have used extremum seeking, which performs non-model based gradient estimation, for a variety of applications, such as steering vehicles toward a source in GPS-denied environments [34]–[36], optimizing the control of homogeneous charge-compression ignition (HCCI) engines [37] and nonisoth”