2009
DOI: 10.1115/1.3077635
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Input-Output Analysis and Control Design Applied to a Linear Model of Spatially Developing Flows

Abstract: A framework for the input-output analysis, model reduction and control design of spatially developing shear flows is presented using the Blasius boundary-layer flow as an example. An input-output formulation of the governing equations yields a flexible formulation for treating stability problems and for developing control strategies that optimize given objectives. Model reduction plays an important role in this process since the dynamical systems that describe most flows are discretized partial differential eq… Show more

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Cited by 154 publications
(257 citation statements)
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References 86 publications
(23 reference statements)
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“…easily recover the original characterization of the problem (Bagheri et al 2009b). In the present contribution, the dual algorithm is referred to as adjoint of adjoint-direct (AAD).…”
Section: Aim Of the Investigationmentioning
confidence: 99%
See 2 more Smart Citations
“…easily recover the original characterization of the problem (Bagheri et al 2009b). In the present contribution, the dual algorithm is referred to as adjoint of adjoint-direct (AAD).…”
Section: Aim Of the Investigationmentioning
confidence: 99%
“…Lewis & Syrmos 1995;Zhou, Doyle & Glover 2002;Bagheri et al 2009b); the aim of this section is to introduce the main relations in a concise way, as these will be needed in § 4.…”
Section: Optimal Control and Estimation: A Brief Reviewmentioning
confidence: 99%
See 1 more Smart Citation
“…Indeed, using the HSV, it is possible to evaluate a priori the theoretical error bounds when exact balanced truncation is performed (see Skogestad & Postlethwaite 2005). By assuming that the theoretical bounds of the exact balanced truncation are valid also for the approximate case when the converged modes are considered (see Bagheri et al 2009b), we kept an error bound of order O(10 −4 ) for all of the models used in this work. Transition delay in a boundary layer flow using active control…”
Section: Appendix Control Designmentioning
confidence: 99%
“…For a complete derivation of the LQG solution, we refer to Lewis & Syrmos (1995), Dullerud & Paganini (1999) and Bagheri et al (2009b). First, the controller is computed by assuming full knowledge of the state and solving the associated algebraic Riccati equation 0 = A H r X + XA r − XB 2r R −1 B H 2r X + C H 1r C 1r .…”
mentioning
confidence: 99%