Shock and Vibration

Volume 2018, Article ID 3727021, 7 pages

https://doi.org/10.1155/2018/3727021

## Updating Stiffness and Hysteretic Damping Matrices Using Measured Modal Data

Correspondence should be addressed to Jiashang Jiang; moc.361@gnahsaijj

Received 30 March 2017; Accepted 21 January 2018; Published 19 February 2018

Academic Editor: Francesco Pellicano

Copyright © 2018 Jiashang Jiang and Yongxin Yuan. This is an open access article distributed under the Creative Commons Attribution License, which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.

#### Abstract

A new direct method for the finite element (FE) matrix updating problem in a hysteretic (or material) damping model based on measured incomplete vibration modal data is presented. With this method, the optimally approximated stiffness and hysteretic damping matrices can be easily constructed. The physical connectivity of the original model is preserved and the measured modal data are embedded in the updated model. The numerical results show that the proposed method works well.

#### 1. Introduction

The dynamic behavior of a mechanical system with degrees of freedom is modeled by the following set of second-order ordinary differential equations: where and are analytical mass, stiffness, and hysteretic damping matrices, respectively. is a displacement vector depending on time . In general, is symmetric and positive definite, and and are symmetric. Equation (1) is usually modeled by FE techniques and thus a FE model is a numerical model. Assuming a fundamental solution , one obtains the structural eigenproblem where

The FE method is used in many applications in engineering practice such as structural response prediction, structural control, structural health monitoring, damage detection, and reliability and risk assessment [1–6]. However, the accuracy of the FE model may be adversely affected by the inaccuracies in the model often related to material properties, modeling of joints, boundary conditions, and damping and simplifications made. As a result, a significant discrepancy may exist between the modal properties calculated by the constructed FE model and those identified from the vibration measurements of the actual structure. Many investigations show that the differences between the numerical and experimental frequencies may exceed 10% [7, 8]. The problem of how to modify a numerical model from the dynamic measurements is known as model updating in structural dynamics. Generally speaking, FE model updating involves two major applications. The first aspect is the FE model tuning, in which the goal is to update a numerical model to characterize the behavior of a real structure; the second one is damage detection, where the discrepancies in the structural dynamic properties before and after damage are identified to help locate and quantify structural damage.

FE model updating has been an active area of research for the last four decades and a lot of approaches have been established for updating structural dynamic models [5, 6]. The direct matrix updating methods were first introduced by Baruch and Bar-Itzhack [9], Baruch [10], and Berman and Nagy [11]. An optimal solution was obtained using Lagrange multipliers for minimizing the changes in the matrices subject to the orthogonality properties of the modes, the eigenvalue equation, and the symmetry of the updated matrices. The matrix mixing methods were developed by Caesar [12] and Link et al. [13]. This approach utilized experimental modal data and analytical ones to construct the inverses of the mass and stiffness matrices. An alternative approach suggested by Wei [14, 15] was to update the mass and stiffness matrices simultaneously using a measured eigenvector matrix as the reference. The control-based eigenstructure assignment techniques for FE model updating were proposed by Zimmerman and Widengren [16] and Inman and Minas [17]. These early methods are simple and computationally efficient but do not generally respect the structural connectivity in the initial FE model. To deal with this difficulty, Kabe [18] presented a stiffness matrix adjustment technique using the constrained minimization theory. The adjusted stiffness matrix can predict the measured modal data accurately and the connectivity of the original stiffness matrix is preserved. Kammer [19] proposed the projector matrix (PM) method which uses the projector matrix theory and the Moore-Penrose inverse, resulting in a more computationally efficient solution. Halevi and Bucher [20] also established a direct matrix updating method by including the connectivity constraints.

It is observed that model updating problems for linear viscously damped elastic systems (or gyroscopic systems) have been considered by many authors [21–29]. However, problems for updating hysteretic damping models have not got enough attention in these years. It is known that the principal difference between viscous and hysteretic damping models is that, for the viscous system, the energy dissipation per cycle depends linearly upon the frequency of oscillation, while for the hysteretic case it is independent of frequency. Very few authors pay attention to hysteretic damping model updating problems because the free vibration response for a system with hysteretic damping is necessarily complex, whereas the modal data of viscously damped elastic systems are closed under complex conjugation. In [30], the authors provided an extended application of the constrained eigenstructure assignment method (CEAM), which was first introduced in [31], to finite element model updating. The existing formulation was modified to accommodate larger systems by developing a quadratic optimization procedure which is unconditionally stable.

The present paper proposes an efficient direct updating method for the FE model with hysteretic (or material) damping which preserves the connectivity of the original coefficient matrices. Assume that and are real-valued symmetric -diagonal matrices; that is, and are band matrices and the nonzero elements are . The problem of updating stiffness and hysteretic damping matrices simultaneously can be stated following the inverse eigenvalue problem and an associated optimal approximation problem, leading to Problems 1 and 2.

*Problem 1. *Let and represent the diagonal matrix of measured eigenvalues and the matrix of corresponding measured eigenvectors, where Find real-valued symmetric -diagonal matrices and such that

*Problem 2. *Find such that where is the solution set of Problem 1.

This paper is divided into five sections. In Section 2, we give an explicit formula for the solution set of Problem 1 using the Kronecker product and vec operator. In Section 3, we show that the solution of Problem 2 is unique and present the expression of the unique solution of this problem. Section 4 describes and discusses the numerical results which indicate the accuracy and efficiency of the proposed algorithm. Some concluding remarks will be drawn in Section 5.

In this paper, we use the following notations. and denote the set of all complex and real matrices, and denotes the set of all symmetric matrices in . and denote the transpose and the Moore-Penrose inverse of a real matrix , respectively. represents the identity matrix of size . In space , we define an inner product as , for all ; then, is a Hilbert space and the matrix norm induced by the inner product is the Frobenius norm. Given , the Kronecker product of and is defined by Also, represents the vec operator; that is, , for the matrix , where , is the th column vector of . For convenience, the symbols and stand for the two orthogonal projectors: and , where

#### 2. The Solution of Problem 1

To solve Problem 1, we need the following lemmas.

Lemma 3 (see [32]). *Assume that and Then, the equation of has a solution if and only if . In this case, the set of all solutions of the equation is , where is an arbitrary vector.*

Lemma 4 (see [33]). *Suppose that , and Then, *

Lemma 5 (see [34]). *Let be an arbitrary partitioned matrix, where , and let Then, the generalized inverse of the matrix is *

If we denote the set of all real symmetric -diagonal matrices by , then we can easily see that is a linear subspace of , and the dimension of is Define where and , is the th column vector of Clearly, forms an orthonormal basis of the subspace ; that is, Now, if are -diagonal matrices, then can be expressed as where the real numbers , need to be determined.

Separating (3) into its real and imaginary parts yields where Substituting (9) into (10), we have Let By Lemma 4, (11) are equivalent to where , and Applying Lemma 3, the first equation of (15) with unknown vector has a solution if and only if In this case, the general solution of the equation is where is an arbitrary vector. Substituting (17) into the second equation of (15) yields Using Lemma 3 again, the equation of (18) with unknown vector has a solution if and only if where When condition (19) is satisfied, the general solution of the equation of (18) is given by where is an arbitrary vector. Substituting (20) into (17) results in By Lemma 5, we have where Using (22), we have where Using Lemma 5 again, we can get where By (22), (24), and (26), (21) can be equivalently written as where and are arbitrary vectors.

To sum up the above discussion, we can get the following result.

Theorem 6. *Assume that and are the measured eigenvalue and eigenvector matrices, where Let , and be given by (12), (13), and (14), respectively. Also, let , and . and are given by (22) and (26), respectively. If conditions (16) and (19) are satisfied, then the solution set of Problem 1 is wherewhere , and are, respectively, given by (23), (25), (27), (28), and (29), with being arbitrary vectors.*

#### 3. The Solution of Problem 2

When the set is nonempty, it is easy to check from (30) that is a closed convex subset of . It follows from the best approximation theorem (see, e.g., [35]) that there exists a unique solution in such that (4) holds.

Now, we set out to find the unique solution in . If and are real symmetric -diagonal matrices, then can be expressed as the linear combinations of the orthonormal basis ; namely, where , are uniquely determined by the elements of and . Let Then, for any in (30), by (8), (9), (32), (33), and (34), we get Substituting (21) into the relation of , we get where Notice that which implies that Therefore, Clearly, the function attains the smallest value at , which yields By substituting (40) into (28) and (29), we obtain By now, we proved the following theorem.

Theorem 7. *Suppose that the real symmetric -diagonal matrices and are given. If conditions (16) and (19) hold, then Problem 2 has a unique solution and the unique solution of Problem 2 can be expressed as where are given by (41) and (42), respectively.*

#### 4. A Numerical Example

Based on Theorems 6 and 7, we can state an algorithm for solving Problems 1 and 2 as follows.

*Algorithm 8. *(1)Input (2)Form the orthonormal basis by (7).(3)Separating and into real and imaginary parts yields , and (4)Compute according to (12), (13), and (14), respectively.(5)Compute (6)Compute by (23) and compute by (22).(7)If condition (16) is not satisfied, then stop.(8)Compute by (25) and form the matrix by (24).(9)Compute by (27) and compute by (26).(10)If condition (19) is not satisfied, then stop.(11)Form vectors by (33) and (34).(12)Compute by (31), (41), and (42), respectively.(13)Compute the unique solution of Problem 2 by (43).

*Example 1. *Consider a five-DOF system with analytical mass, damping, and stiffness matrices as follows: That is, are symmetric 3-diagonal matrices. The model used to simulate the consistent experimental data is given by , and Note that the differences between and are , and elements. The eigensolution of the model is used to create the experimental modal data. Assume that the measured eigenvalue matrix and corresponding eigenvector matrix are given by All the tests are performed on an Intel Core 3.39 GHz PC with a main memory of 2.99 GB running MATLAB 6.5. It is easy to check that conditions (16) and (19) hold , . According to Algorithm 8 with 0.1710 CPU time (in seconds), we solve the optimal approximation solution of Problem 2 as follows: We can see that Algorithm 8 works well and the updated matrices and are very close to the accurate stiffness matrix and hysteretic damping matrix with absolute errors Define By Algorithm 8, we can get the results in Table 1.

Therefore, the measured eigenvalues and eigenvectors are reproduced in the new model , and the updated matrices are also symmetric 3-diagonal matrices, which means that the structural connectivity of the original model is preserved.