2010
DOI: 10.1007/s00162-010-0184-8
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Reduced-order models for control of fluids using the eigensystem realization algorithm

Abstract: As sensors and flow control actuators become smaller, cheaper, and more pervasive, the use of feedback control to manipulate the details of fluid flows becomes increasingly attractive. One of the challenges is to develop mathematical models that describe the fluid physics relevant to the task at hand, while neglecting irrelevant details of the flow in order to remain computationally tractable. A number of techniques are presently used to develop such reduced-order models, such as proper orthogonal decompositio… Show more

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Cited by 205 publications
(152 citation statements)
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“…A systematic way to perform such a reduction is to use balanced truncation (Moore 1981); for a high-dimensional system, balanced truncation can be approximated using a snapshot-based algorithm proposed by Rowley (2005). This methodology is equivalent to a system identification method called the eigensystem realization algorithm (ERA) (Juang & Pappa 1985), as shown in Ma, Ahuja & Rowley (2011).…”
Section: Design-then-reduce Versus Reduce-then-designmentioning
confidence: 99%
“…A systematic way to perform such a reduction is to use balanced truncation (Moore 1981); for a high-dimensional system, balanced truncation can be approximated using a snapshot-based algorithm proposed by Rowley (2005). This methodology is equivalent to a system identification method called the eigensystem realization algorithm (ERA) (Juang & Pappa 1985), as shown in Ma, Ahuja & Rowley (2011).…”
Section: Design-then-reduce Versus Reduce-then-designmentioning
confidence: 99%
“…= system matrices ̃, ̃, C, D = discrete-time system matrices C l , C m = lift and pitching moment coefficients H(t) = continuous-time impulse response matrix H rs (k) = Hankel matrix of size r × s at time level k H k = Markov parameter h 1 = first order kernel of the system k = time level l g = gust length m = number of inputs in a multiple input/output system p = number of outputs in a multiple input/output system t = time U = velocity U, V = square unitary matrices v g (t) = input vector x = state vector ẋ = state vector differentiated with respect to time y = output vector y 1 = non-linear system response to a pulse input of arbitrary y 11 = non-linear system response to a pulse input of twice the magnitude as that of y 1 0 m = square identity matrix of size m × m 1 Ph.D Researcher, Department of Aerospace Engineering, Queens Building, University Walk, Bristol, England, BS8 1TR. 2 Senior Lecturer, Department of Aerospace Engineering.…”
Section: A B C Dmentioning
confidence: 99%
“…We keep the first r states, by considering the first r columns of the matrices U ∈ R m o ×m o , the first r rows of the matrix V ∈ R m c ×m c , and the first r rows and columns of Σ . The resulting matrices U r ∈ R m o ×r , V r ∈ R m c ×r and Σ r ∈ R r×r are used for finding the ROM of the system; indeed, the ROM is identified by the matrices A r ∈ R r×r , B r ∈ R r×(d+m) and C r ∈ R (k+p)×r defined as The equivalence of this procedure with balanced truncation can be shown by directly comparing the relations in A.6 with ROM obtained as projection onto a base of balanced modes (see, for more details, Ma et al 2011). The resulting ROM is in time-discrete form, but it can easily converted in continuous-time form (Glad & Ljung 2001) for running the ROM next to the main DNS simulation.…”
Section: Appendix Control Designmentioning
confidence: 99%
“…the linearized Navier-Stokes equation) and the related adjoint. In a recent application, Ma, Ahuja & Rowley (2011) propose for fluid flow control a system identification algorithm usually referred to as eigensystem realization algorithm (ERA) (see Juang & Pappa 1985); they show the equivalence between approximate balanced truncation and ERA, although using the latter algorithm neither simulations of the adjoint system nor a Galerkin projection onto the balanced mode basis are necessary to obtain low-order models. Once the low-order controller is designed, it can be tested in full direct numerical simulations (DNS) or large eddy simulations (LES).…”
mentioning
confidence: 99%
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