Abstract
The viscoelastic relaxation spectrum provides deep insights into the complex behavior of polymers. The spectrum is not directly measurable and must be recovered from oscillatory shear or relaxation stress data. The paper deals with the problem of recovery of the relaxation spectrum of linear viscoelastic materials from discrete-time noise-corrupted measurements of relaxation modulus obtained in the stress relaxation test. A class of robust algorithms of approximation of the continuous spectrum of relaxation frequencies by finite series of orthonormal functions is proposed. A quadratic identification index, which refers to the measured relaxation modulus, is adopted. Since the problem of relaxation spectrum identification is an ill-posed inverse problem, Tikhonov regularization combined with generalized cross-validation is used to guarantee the stability of the scheme. It is proved that the accuracy of the spectrum approximation depends both on measurement noises and the regularization parameter and on the proper selection of the basis functions. The series expansions using the Laguerre, Legendre, Hermite and Chebyshev functions were studied in this paper as examples. The numerical realization of the scheme by the singular value decomposition technique is discussed and the resulting computer algorithm is outlined. Numerical calculations on model data and relaxation spectrum of polydisperse polymer are presented. Analytical analysis and numerical studies proved that by choosing an appropriate model through selection of orthonormal basis functions from the proposed class of models and using a developed algorithm of least-square regularized identification, it is possible to determine the relaxation spectrum model for a wide class of viscoelastic materials. The model is smoothed and robust on measurement noises; small model approximation errors are obtained. The identification scheme can be easily implemented in available computing environments.
Keywords: viscoelasticity, relaxation spectrum, linear relaxation modulus, identification algorithm, orthonormal functions, Tikhonov regularization, singular value decomposition
1. Introduction
Viscoelasticity denotes the joint property of elasticity and viscosity and, hence, describes materials with both fluid and solid properties at the same time. Viscoelastic relaxation or retardation spectra are commonly used to describe, analyze, compare and improve the mechanical properties of polymers [1,2,3,4,5]. The spectra are vital for constitutive models and for the insight into the properties of a viscoelastic material, since, from the relaxation or retardation spectrum, other material functions used to describe rheological properties of various polymers can be uniquely determined [6,7,8,9]. However, the spectra are not directly accessible by measurement. The relaxation and retardation spectra can be recovered from oscillatory shear data and from the time measurements of the relaxation modulus or creep compliance obtained in standard stress relaxation or retardation experiments [1,2,7]. Many different methods have been proposed during the last five decades for relaxation spectrum computation using data from dynamic modulus tests. Baumgaertel and Winter [10] applied a nonlinear regression for identification of discrete relaxation and retardation time spectra based on dynamic data, in which the number of relaxation times adjusts during the iterative calculations to avoid ill-posedness and to improve the model fit; regularization is not applied here. Honerkamp and Weese [11,12], for relaxation spectrum identification, combined nonlinear regression with Tikhonov regularization and proposed a specific viscoelastic model described by the two-mode log-normal function. Malkin [13] approximated a continuous relaxation spectrum using three constants: the maximum relaxation time, slope in the logarithmic scale and form factor. Malkin et al. [14] derived a method of continuous relaxation spectrum calculations using the Mellin integral transform. An approach proposed by Stadler and Bailly [15] is based on the relaxation spectrum approximation by a piecewise cubic Hermite spline. In turn, Davies and Goulding [16] approximated the relaxation spectrum by a sum of scaling kernel functions located at appropriately chosen points. The algorithm for the relaxation time spectrum approximation by power series was developed by Cho [17]. Anderssen et al. [1] proposed a derivative-based algorithm for continuous spectrum recovery, being also appropriate for the experimental situation where the oscillatory shear data are only available for a finite range of frequencies. These works, but also many others, using different models, approaches, algorithms and computational techniques, have opened new directions of research on discrete and continuous relaxation spectra identification based on dynamic moduli data, which are still being conducted [2,18,19,20,21].
However, a classical manner of studying viscoelasticity is also through a two-phase stress relaxation test, where time-dependent shear stress is studied for the step increase in strain [4,6,7]. There are only a few papers, e.g., [22,23,24,25,26,27,28], that deal with the spectrum determination from time measurements of the relaxation modulus; additionally, only some of them are addressed to polymers. Therefore, the computationally efficient algorithms to determine the relaxation spectrum applied to time measurements of the relaxation modulus are still desirable. The objective of the present paper was to develop a class of models and an identification algorithm for the continuous relaxation spectrum determination based on discrete-time measurements of the relaxation modulus, which, taking into account the ill-posedness of the original problem of the spectrum recovery, will provide: (a) good approximation of the relaxation spectrum and modulus; (b) smoothness of the spectrum fluctuations, even for noise-corrupted measurements; (c) noise robustness; (d) applicability to a wide range of viscoelastic materials due to the choice of respective model from the considered set of models; (e) ease of implementation of the models and identification algorithm in available computing packages. Thus, the goal of this work was the synthesis of the respective models and general identification scheme, and the analysis of their properties. Approximation errors, convergence, noise robustness, smoothness and the applicability ranges were studied analytically. Further, the numerical verification of the models and algorithm for exemplary theoretical relaxation spectrum, and their applicability to spectrum of real material, polydisperse polymer, was the purpose of this work.
The approach proposed is based on the approximation of the spectrum by a finite linear combination of the basis orthonormal functions. A quadratic identification index, related to the data of the relaxation modulus, is adopted as a measure of the model quality. As a result, the primary infinite dimensional dynamic inverse problem of the continuous relaxation spectrum identification is reduced to the static linear-quadratic programming task. Next, Tikhonov regularization is used to guarantee the well-posed solution. Thus, the approach proposed integrates the technique of an expansion of a function into a series in an orthogonal basis with the least-squares regularized identification [29].
It is demonstrated that due to the choice of appropriate special functions as the basis functions for the unknown relaxation spectrum model, the components in the relaxation modulus model are given by compact analytical or recursive formulas. The technique of expanding an unknown viscoelastic function into a series of orthogonal functions or polynomials has already been used to describe various rheological models of polymers, especially in the time domain. For example, Aleksandrov et al. [30] applied Laguerre polynomials to describe experimentally obtained polyethylene deformation in the creep under diffusion in a liquid environment. Cao et al. [31] used orthogonal expansion based on shifted Legendre polynomials to solve a fractional-order viscoelastic model of polymethyl methacrylate. Abbaszadeh and Dehghan [32] employed a new class of basis based upon the Legendre polynomials to solve a two-dimensional viscoelastic equation. Kim et al. [33] used Chebyshev polynomials for direct conversion of creep data to dynamic moduli.
The idea of using a series of orthogonal functions has also been used to approximate the relaxation spectrum. Lee et al. [34] used the Chebyshev polynomials of the first kind to approximate dynamic moduli data. Stankiewicz [27,28,35] applied orthogonal functions for relaxation spectrum recovery from the stress relaxation data, but these articles use a different definition of the relaxation modulus, according to which the modulus is directly given by the Laplace integral of the spectrum. In this paper, it is shown, for the dominant literature definition of the relaxation spectrum, that the application of the concept of expanding the unknown relaxation spectrum into a series of orthonormal basis functions combined with the least-squares regularized identification allows one to determine the smoothed model of the relaxation spectrum, robust on the measurement noises, with small approximation errors of the relaxation spectrum and modulus. The selection of appropriate orthonormal basis functions, the selection of their time-scale factor and the determination of the optimal regularization parameter using standard generalized cross-validation technique enables the application of the proposed approach to a wide class of viscoelastic materials.
2. Materials and Methods
2.1. Relaxation Spectrum
The uniaxial, nonaging and isothermal stress–strain equation for a linear viscoelastic material can be represented by a Boltzmann superposition integral [7]:
(1) |
where and denote the stress and strain at the time t and is the linear relaxation modulus. Modulus is given by [1,7,36,37]:
(2) |
or equivalently by
(3) |
where and characterize the distributions of relaxation times and relaxation frequencies , respectively. The continuous relaxation spectra and , related by , are generalizations of the discrete Maxwell spectrum [1,7] to a continuous function of the relaxation times and frequencies . Although other definitions of the relaxation spectrum are used in the literature, for example, in [5,13,28,38], the definition introduced by Equation (2) dominates. The main symbols are summarized in Nomenclature, Appendix C.
The problem of relaxation spectrum determination is the practical problem of re-constructing the solution of the Fredholm integral equation of the first kind (2) or (3) from discrete-time measured data. Time measurements of the relaxation modulus data are considered in this paper. This problem is known to be severely Hadamard ill-posed [39,40]. In particular, small changes in the measured relaxation modulus can lead to arbitrarily large changes in the determined relaxation spectrum. In remedy, some reduction of the set of admissible solutions or appropriate regularization of the original problem can be used. Here, both techniques are used simultaneously.
2.2. Models
The modified spectrum is introduced:
(4) |
where the upper index of means ‘modified’. Then, (3) can be rewritten as
(5) |
i.e., the modulus is directly the Laplace integral of the spectrum .
Assume that , where is the space of real-valued square-integrable functions on the interval . The respective sufficient conditions are given by Theorem 3 in [41]. Assume that the set of the linearly independent orthonormal functions form a basis of the space . Thus, the modified relaxation spectrum can be expressed as
(6) |
where the Fourier coefficients are [42]
For practical reasons and in order to reduce the set of admissible solutions, it is convenient to replace the infinite summation in Equation (6) with a finite one of K terms, i.e., to approximate the relaxation spectrum by a model of the form
(7) |
where the lower index of is the number K of model summands. Then, using (5), the respective model of the relaxation modulus is described by:
(8) |
where the functions
(9) |
Note, that function is Laplace transform of for real argument t, i.e.,
with the notation used for Laplace transform. For basis functions, applied in the developed algorithms, the components of the relaxation modulus model are given by analytical or recursive formulas. This avoids quadrature errors occurring in the numerical calculation of the integrals (9). The following special functions are considered as basis functions: Laguerre, Legendre, Chebyshev and Hermite. The respective basis functions and are described in Section 3.3, Section 3.4, Section 3.5 and Section 3.6. All basis functions depend on one parameter—time-scaling factor .
2.3. Identification Problem
Identification consists of selecting, within the given class of models defined by (7), (8) such a model, which ensures the best fit to the measurement results. Suppose a certain identification experiment (stress relaxation test [4,6,7]) performed on the specimen of the material under investigation resulted in a set of measurements of the relaxation modulus at the sampling instants , , where is additive measurement noise. It is assumed that the number of measurements . As a measure of model (8) accuracy, the square index is taken
(10) |
where is a K-element vector of unknown coefficients of the models (7) and (8). Using the vector-matrix notation
(11) |
the identification index (10) can be rewritten in compact form as
(12) |
where denotes the square norm in the real Euclidean space . Thus, the optimal identification of relaxation spectrum in the class of functions defined by (7) and (8) consists of solving, with respect to the model parameter , the following least-squares problem:
(13) |
The matrix is usually ill-conditioned. Thus, the optimization problem (13) is still, like the original problem of solving Fredholm’s equation of the 1st kind (3), incorrectly posed in the sense of Hadamard. Consequently, the solution of (13) is not unique, i.e., there exist many optimal model parameters minimizing the identification index (12). However, even the normal (with the lowest Euclidean norm) solution of (13) is non-continuous and unbounded function of the measurement vector . This means that when the data are noisy, even small changes in would lead to arbitrarily large artefacts in any optimal model parameter. To deal with the ill posedness, the Tikhonov regularization method is used, as presented below.
2.4. Regularization
Regularization aims to replace the ill-posed problem with a nearby well-posed problem. Tikhonov regularization [43] strives to stabilize the computation of the least-squares solution by minimizing a modified square functional of the form:
(14) |
where is a regularization parameter. The above problem is well-posed; that is, the solution always exists, is unique, and continuously depends on both the matrix and on the measurement data . The parameter vector minimizing (14) is given by:
(15) |
where is dimensional identity matrix.
The choice of regularization parameter is crucial to identify the best model parameters. Here, we apply the generalized cross-validation GCV [39,44], which does not depend on a priori knowledge about the noise variance. The GCV technique relies on choosing, as a regularization parameter, , which minimizes the GCV functional defined by [44]
(16) |
where the matrix
and
are the residual vector for the regularized solution (15); denotes the trace of . The problem of choosing the optimal regularization parameter
(17) |
has a unique solution and the resulting parameter differs the least from the normal solution of problem (14) that we would obtain for the ideal (not noise corrupted) measurements of the relaxation modulus [44].
2.5. Algebraic Background
Formula (15) is generally unsuitable for computational purposes. The singular value decomposition (SVD, [45]) technique will be used. Let SVD of the dimensional matrix take the form [45]:
(18) |
where is diagonal matrix containing the non-zero singular values of the matrix [45], matrices and are orthogonal and . Taking advantage of the diagonal structure of and the matrices and orthogonality, it may be simply proved that the regularized optimal parameter (15) is given by
(19) |
where diagonal matrix is as follows:
(20) |
Using SVD (18) and introducing dimensional vector , the GCV function (16) can be expressed by a convenient analytical formula
(21) |
as a function of the singular values and elements of the vector . The function is differentiable for any ; thus, an arbitrary gradient optimization method can be implemented to solve the GCV minimization task (17).
3. Results and Discussion
In this section, a general scheme of the relaxation spectrum identification is given. The most important results for the evaluation of the effectiveness of the algorithm and models are presented, concerning the smoothing of the models, their accuracy for ideal and noisy measurements of the relaxation modulus and the linear convergence to the model that we would obtain for the noise-free measurements. Next, examples of orthonormal basis functions and corresponding functions are given.
3.1. Identification Algorithm
The determination of the model of relaxation spectrum involves the following steps.
Perform the experiment (stress relaxation test [4,7,46,47]) and record the measurements , , of the relaxation modulus at times .
Choose the time-scaling factor and the number of model components comparing, for different values of , a few first functions from the sequence with the experiment results .
Compute the matrix (11) and next determine SVD (18).
Determine GCV function (21), and next compute the optimal regularization parameter minimizing , i.e., solving the optimization task (17).
Compute the regularized solution according to (19) for .
- For , using computed above, determine the modified spectrum of relaxation frequencies according to:
(22) - Determine the spectrum of relaxation frequencies according to
(23)
Two Remarks
Only the SVD of the matrix, , of computational complexity [45] is a space- and time-consuming task of the scheme. However, the SVD must be computed only once and is accessible in the form of optimized numerical procedures in most commonly used computational packets.
The matrix depends on the choice of the basis functions as well as the measurement points ; however, it does not depend on the relaxation modulus measurements . Thus, when the identification scheme is applied for successive samples of the same material, step 3 should not be repeated while the same time instants are kept and the same model parameters and are selected in step 2.
3.2. Analysis
In the context of the ill-posed inverse problem, for which the model quality index refers to the measured relaxation modulus but not directly to the unknown relaxation spectrum and the modified spectrum (4), we cannot estimate the error directly. As a reference point for the determined model (22), we will consider several characteristics, as follows:
-
(a)
The model of the relaxation spectrum that we would obtain on the basis of ideal (undisturbed) measurements of the relaxation modulus:
(24) |
where is the vector of regularized solution of (14)
(25) |
for noise-free measurements of relaxation modulus ; c.f., Equation (11)
-
(b)
The model of the relaxation spectrum that we obtain on the basis of the normal solution of the linear-quadratic problem (13) for noise measurements of the relaxation modulus:
(26) |
where is the Moore–Penrose pseudoinverse [48] of matrix , and is the elements of the vector
-
(c)
The model of the relaxation spectrum that we would obtain on the basis of the normal solution of the linear-quadratic problem (13) for noise-free measurements of the relaxation modulus:
(27) |
Most of the results are formulated in terms of algebraic tools of the algorithm, i.e., SVD decomposition (18) of the matrix . Such an analysis enables a deeper insight into the properties of the algorithm and the resulting model. It shows not only the influence of the regularization parameter and measurement errors, but also the impact and significance of the selection of the basis functions, including their parameters and measurement points , on which the singular values of the matrix depend.
3.2.1. Smoothness
The purpose of Tikhonov regularization relies on stabilization of the resulting vector . Due to the orthonormality of the basis functions in the Hilbert space , for an arbitrary of the form (22), the following equality holds
(28) |
where means the square norm, both in the real Euclidean space as well as in . Therefore, the smoothness of the optimal solution of discrete problem (14) guarantees that the fluctuations in the respective spectrum of relaxation, in particular the resulting spectrum of relaxation (22), are also bounded. In view of the above, due to orthonormality of the elements the basis system , the function is the approximation of the real modified spectrum in the class of functions (7), optimal in the sense of the square identification index (10) of the bounded norm.
For any regularized (19), bearing in mind the definition of the vector and orthogonality of , we have . Thus, due to the diagonal structure of (20) and based on (28), the model smoothing efficiency can be evaluated by the following relation:
(29) |
which holds for an arbitrary regularization parameter , where the spectrum is given by (26). The last equality in (29) holds, since for (18), the Moore–Penrose pseudoinverse is , where matrix . Keeping in mind (26) and (28), the above result can be derived directly from the following inequality, proved in [28]:
where are the non-zero singular values of the matrix and are elements of the dimensional vector , since and .
The first equality in (29) illustrates the mechanism of stabilization. The following rule holds: the greater the regularization parameter is, the more highly bounded the fluctuations of the spectrum are. Thus, due to orthogonality of the basis functions, the regularization parameter controls the smoothness, not only of the parameter but also of the model . The non-zero singular values of the matrix and the vector of measurement data also affect the smoothness of the spectrum model.
3.2.2. Convergence
Relaxation spectrum (22) is only an approximation of that spectrum, which can be obtained in the class of models (7) by direct minimization (without regularization) of the quadratic index (12) for noise-free measurements, i.e., the approximation of the function (27). Since
where is vector of measurement noises, based on (28); the diagonal structure of and using the Schwarz inequality [49], the following bound of the relaxation spectrum approximation error can be derived:
(30) |
The inequality (30) yields that the accuracy of the spectrum approximation depends both on the measurement noises and the regularization parameter and on the singular values of the matrix , which, in turn, depend on the selection of the basis orthogonal functions . Using (30), the regularized vector converges to the noise-free normal solution linearly with respect to the norm , as and , simultaneously. Therefore, the upper bound in (30) guarantees that the spectrum tends to in each point , at which they are both continuous, as and , simultaneously.
3.2.3. Noise Robustness
The influence of disturbances in the measurements of the relaxation modulus on the regularized solution was analyzed in detail in a two-part paper [27,50]. From Property 2 in [50], the following inequalities result:
Thus, the regularized vector converges to the noise-free regularized solution (25), and the relaxation spectrum tends to the noise-free spectrum (24) in each point , where they are both continuous, linearly with respect to the norm , as . From the above estimations, it is also evident that the accuracy of the spectrum approximation measured by depends both on the measurement noises and the regularization parameter and on the singular values of the matrix .
3.3. Legendre Model
Let us assume a basis function
(31) |
with the time-scaling factor , where is Legendre polynomials [51,52,53] defined by Rodrigue’s formula
The polynomials form a complete set of orthonormal basis in the interval with the weight [51,53]. Thus, using the substitution , it is easy to observe that the functions defined by (31) form a complete orthonormal basis in [49]. The relaxation modulus basis functions (9) are as follows:
(32) |
where the product is equal to 1 when . The proof by induction is presented in Appendix A.1. The above formula can be equivalently expressed in recurrent form as
starting with
Five first basis functions are shown in Figure 1a,b for two different values of the time-scaling factor . Figure 1c,d show the related functions. From the last figure, it is seen that the basis functions for the relaxation modulus model are in good agreement with the real relaxation modulus obtained in the experiment.
3.4. Laguerre Model
The Laguerre polynomials can be defined via Rodrigue’s formula [51,54]:
(33) |
where is a time-scaling factor [55]. The continuous Laguerre function is the product of the Laguerre polynomial and the square root of the exponential weight function [56], i.e.,
(34) |
The Laguerre functions form a complete orthonormal basis in [51,56]. In Appendix A.2, the following formula is derived for the modulus basis functions:
(35) |
The above formula is given by Wang and Cluett [55], but as there are several definitions of the Laguerre functions in the literature, and, as a result, several formulas of the Laplace transforms, for example, in [57], the derivation of (35) is given in Appendix A.2 to avoid doubts.
A few first basis functions are shown in Figure 2a,b for two different values of the time-scaling factor ; the corresponding functions are plotted in Figure 2c,d.
3.5. Chebyshev Model
The Chebyshev polynomials of the first kind defined by the recursion relation [58,59]:
(36) |
starting with
(37) |
are orthogonal in the interval with the weight function [58]. Specifically,
Thus, using the substitution , it is easy to demonstrate that the set of functions
(38) |
with the first function defined as
(39) |
form an orthonormal basis in the space . Here, as previously, is a positive time-scaling factor. The relaxation modulus basis functions (9) are described by a useful recursive formula
(40) |
and for are given by:
(41) |
(42) |
(43) |
where is the Euler’s gamma function [60]. The proof is given in Appendix A.3, where two alternative formulas (A11) and (A12) for and , respectively, are also derived. A few first basis functions are shown in Figure 3a,b for two values of the factor ; the corresponding functions are plotted in Figure 3c,d. An earlier version of the model was presented in the paper [61].
3.6. Hermite Model
The Hermite functions defined as [52,62,63]
(44) |
where is time-scaling factor and are the Hermite polynomials, which satisfy recursion formula [52]:
(45) |
with the initial
(46) |
constitute an orthonormal system in the space [52,63]. The relaxation modulus basis functions (9) are described by the recursive formula:
(47) |
and for are given by
(48) |
and
(49) |
where the complementary error function is defined by [64]:
(50) |
The derivation of the above formulas is given in Appendix A.4. The initial values of Hermite polynomials are specified by [52]:
(51) |
A few first basis functions are shown in Figure 4a,b for two factors . The related functions are plotted in Figure 4c,d. The function , and, in consequence of the recursive Formula (47), all functions , depend on the exponential multiplier rapidly moving towards infinity. The following asymptotic properties were proved in Appendix A.5 for any :
(52) |
(53) |
However, in numerical computations, the limited values of can be guaranteed only for , where depends on the maximal real number accessible in the computing environment. For example, in Matlab, the largest finite floating-point number in IEEE double precision . Thus, in view of (48), the range of numerical applicability of the Hermite model in the time domain, determined by the inequality
is as follows
(54) |
Smoothness
Since the basis functions of the Hermite model presented above form an orthonormal basis of the space of square integrable functions on , for Hermite model estimation (28) can be replaced by
Therefore, for the Hermite model, the algorithm may (but does not have to) provide a stronger limitation of the fluctuation in the determined relaxation spectrum than for the other models.
3.7. Choice of the Basis Functions
In the models proposed above, the parameter is the time-scaling factor. The following rule holds: the lower the parameter is, the shorter the relaxation times are, i.e., the greater the relaxation frequencies are. The above is illustrated by Figure 1, Figure 2, Figure 3 and Figure 4. Through the optimal choice of the scaling factor, the best fit of the model to the experimental data can be achieved. However, in practice, a simple rough rule for choosing the factor , based on the comparison of a few first functions from the sequence for different values of with the experimentally obtained function , is quite enough. In the same manner, the number of the series (8) elements can be initially evaluated. This rough selection strategy of the model parameters was used in the examples presented below. Thus, the choice of the number and the parameter must be carried out a posteriori, after the preliminary experiment data analysis.
The ranges of applicability of the four classes of models described above in the relaxation times t domain and the relaxation frequencies domain for different values of are summarized in Table A1 in Appendix A.6. It was assumed that the range of applicability for times is determined by the value of time , for which the first basis functions no longer permanently exceed, i.e., for any , of its maximum value. Specifically,
(55) |
where
Similarly, the range of applicability for the relaxation frequencies was defined on the basis of the variability in the basis functions . Here,
(56) |
with defined by
In view of the problems described above concerning the numerical determination of the basis functions only for , with defined in (54), for the Hermite model, was assumed.
3.8. Example 1
Consider viscoelastic material of relaxation spectrum described by Gauss-like distribution [11]
(57) |
The corresponding modified spectrum (4) is:
(58) |
and, therefore, using (5), the ‘real’ relaxation modulus is
(59) |
where is defined by (50). In the experiment, 0 sampling instants were generated with the constant period in the time interval seconds selected in view of the course of the modulus (59). Additive measurement noises were selected independently by random choice with uniform distribution on the interval , i.e., maximally 6.1% of the mean value of in the interval defined as the average value of the integral of over , which is equal to . The time-scaling factors are selected by comparison for different values of a few first functions with the experiment results . Only for the Chebyshev model, the rough selection of required several attempts; for the remaining classes of models, it was enough to review the data from Table A1. The basis functions and were simulated in Matlab R2022a using special functions erfc, legendreP, chebyshevT, and hermiteH. For the singular value decomposition procedure, svd was applied. For ,11, and sometimes also for , the regularization parameters were determined and are given in Table 1. Next, the vectors of optimal model parameters (19) were computed and are given in Table A2 in Appendix B. Only for the Laguerre models, some elements of the vectors of optimal parameters are negative; for the remaining classes of models, all the parameter vectors are positive. The optimal modified spectra of relaxation frequencies (22) and the ‘real’ spectrum (58) are plotted in Figure 5 for selected values of , while in Figure 6, the spectra (23) and (57) are presented. The optimal models of the relaxation modulus computed for according to (8) are plotted in Figure A1 in Appendix B, where the measurements are also marked. Since the optimal models (8) fitted the data extremely well, as indicated especially by the mean-square model errors , which vary between and , models for different practically coincide with the measurement points and with each other (see Figure A1). The norms and , as the measures of the solution smoothness, and the identification index (10), being a measure of the errors of the relaxation modulus models, are also given in Table 1. For the ‘real’ modified spectrum (58), the norm . The distance between the ‘real’ spectrum (58) and their models (22) was estimated by integral square error, defined as:
(60) |
and is given in the last column of Table 1.
Table 1.
Model |
|
||||||
---|---|---|---|---|---|---|---|
Legendre model | 6 | 1 | 0.03378 | 0.0088 | 1.5518 | 1.5518 | 2.0782 |
8 | 1 | 0.03239 | 0.0083 | 1.4833 | 1.4833 | 2.0643 | |
9 | 1 | 0.03186 | 0.0084 | 1.4657 | 1.4657 | 2.0597 | |
10 | 1 | 0.03139 | 0.0087 | 1.4537 | 1.4537 | 2.0559 | |
11 | 1 | 0.03098 | 0.0089 | 1.4452 | 1.4452 | 2.0529 | |
12 | 1 | 0.03062 | 0.0091 | 1.4391 | 1.4391 | 2.0505 | |
Laguerre model | 6 | 6 | 0.03259 | 0.0084 | 1.4929 | 1.4929 | 1.9914 |
8 | 6 | 0.02744 | 0.0093 | 1.4222 | 1.4222 | 2.0414 | |
9 | 6 | 0.02560 | 0.0092 | 1.4240 | 1.4240 | 2.0435 | |
10 | 6 | 0.0239 | 0.0089 | 1.4262 | 1.4262 | 2.0448 | |
11 | 6 | 0.02256 | 0.0088 | 1.4253 | 1.4253 | 2.0444 | |
Chebyshev model | 6 | 1.5 | 0.03103 | 0.00992 | 1.5215 | 1.5215 | 2.1119 |
8 | 1.5 | 0.03077 | 0.00981 | 1.4677 | 1.4677 | 2.0811 | |
9 | 1.5 | 0.03062 | 0.0101 | 1.4543 | 1.4543 | 2.0668 | |
10 | 1.6 | 0.03165 | 0.0089 | 1.4875 | 1.4875 | 2.0864 | |
11 | 1.6 | 0.03148 | 0.0091 | 1.47492 | 1.4749 | 2.0775 | |
12 | 1.6 | 0.03126 | 0.009246 | 1.4651 | 1.4651 | 2.0713 | |
Hermite model | 6 | 1 | 0.00625 | 0.0117 | 1.6405 | 1.6029 | 2.0529 |
8 | 1 | 0.00588 | 0.0081 | 1.5077 | 1.4891 | 2.0674 | |
9 | 1 | 0.00599 | 0.0080 | 1.4731 | 1.4639 | 2.0592 | |
10 | 1 | 0.00599 | 0.0080 | 1.4611 | 1.4569 | 2.0607 | |
11 | 1 | 0.00566 | 0.0080 | 1.4600 | 1.4561 | 2.0654 |
3.9. Example 2
Consider the spectrum of relaxation times introduced by Baumgaertel, Schausberger and Winter [36,37],
which is known to be effective in describing polydisperse polymer melts [17,34], with the parameters [34]: , , , , and . The related spectra of relaxation frequencies and (4) are well posed for . The modified spectrum is described by
(61) |
and depicted in Figure 7; the corresponding ‘real’ relaxation modulus is defined by (5). In the experiment, 0 time instants were sampled according to the square rule s, with parameter , where , in the time interval is selected in view of the course of the modulus . Due to the numerical problems described above related to determining the basis functions , Equations (47)–(49), for the Hermite model the experiment was simulated in a shorter time interval using the same sampling formula. Additive measurement noises were selected independently by random choice with uniform distribution on the interval . Here, for the selection of parameter , which guarantees a satisfactory accuracy of the modulus approximation, several or even a dozen or so attempts were necessary. This means that it will be advisable to further extend the algorithm by the level of optimal selection of the time-scaling factors. For ,12,14, and also for , the regularization parameters were determined and are given in Table 2. Only for the Laguerre and Legendre models, the accuracy of the modulus approximation measured by , Equation (10), is comparable to that obtained in Example 1. Thus, the vectors of optimal model parameters (19) for Legendre and Laguerre models are given in Table A3 in Appendix B; for the remaining models, they were omitted. The optimal spectra (22) and the ‘real’ spectrum (58) are plotted in Figure 7 for Laguerre and Legendre models; a logarithmic scale is used for the frequencies and a linear scale for the spectrum. For Legendre and Laguerre models, the optimal models computed for are plotted in Figure 8, where the measurements are also marked and logarithmic scale is applied for time axis. The norms , and the identification index are given in Table 2. For the ‘real’ modified spectrum (58), the norm . The distance between the ‘real’ spectrum (58) and its models (22) was estimated by the integral square errors , defined in (60) and given in Table 2, only for Legendre and Laguerre models. For the Chebyshev and Hermite models, a satisfactory quality of approximation was not obtained, despite the research carried out for a wide range of values. The best found and related identification indices are given in Table 2, but other indices are omitted. The optimal Legendre and Laguerre models (8) were well fitted to the experimental data, see Figure 8a,b, as also indicated by the mean-square model errors , which vary in a range from to . For the Chebyshev and Hermite models, even increasing the number of model summands does not improve the poor approximation of the relaxation modulus data (see Figure 8c,d and the values of from Table 2). In particular, the course of the model from Figure 8c shows that it is not too few components of the model but the properties of the Chebyshev model that make it ineffective for approximating the relaxation spectrum (61).
Table 2.
Model |
|
||||||
---|---|---|---|---|---|---|---|
Legendre model | 6 | 950 | 2.72 × 10−6 | 0.003261 | 62.717 | 62.717 | 80.604 |
8 | 620 | 4.968 × 10−6 | 0.00135 | 58.9351 | 58.9351 | 79.7444 | |
10 | 500 | 6.372 × 10−6 | 0.0007138 | 57.4422 | 57.4422 | 79.7170 | |
12 | 400 | 7.754 × 10−6 | 0.000557 | 56.8251 | 56.8251 | 79.7917 | |
14 | 300 | 9.226 × 10−6 | 0.000575 | 56.6390 | 56.6390 | 79.8353 | |
Laguerre model | 8 | 8500 | 2.524 × 10−6 | 0.002722 | 63.0250 | 63.0250 | 82.4674 |
10 | 8000 | 3.668 × 10−6 | 0.001494 | 59.7092 | 59.7092 | 81.0828 | |
12 | 7500 | 4.840 × 10−6 | 0.0009379 | 58.3032 | 58.3032 | 80.6344 | |
14 | 8000 | 5.294 × 10−6 | 0.000711 | 57.3277 | 57.3277 | 80.3069 | |
16 | 6000 | 7.498 × 10−6 | 0.000699 | 57.39886 | 57.39886 | 80.4441 | |
18 | 6500 | 7.686 × 10−6 | 0.000527 | 56.7967 | 56.7967 | 80.1877 | |
Chebyshev model | 6 | 31,000 | 6.0 × 10−7 | 0.8259 | 289.32 | 289.32 | |
8 | 31,500 | 6.0 × 10−7 | 0.7115 | 346.30 | 346.30 | ||
10 | 32,000 | 5.0 × 10−7 | 0.6504 | 376.6564 | 376.66 | ||
12 | 33,000 | 5.0 × 10−7 | 0.6344 | 379.0402 | 379.04 | ||
14 | 33,000 | 5.0 × 10−7 | 0.6029 | 375.3072 | 375.31 | ||
16 | 34,500 | 5.0 × 10−7 | 0.6136 | 382.0129 | 382.01 | ||
Hermite model | 6 | 27,000 | 1.8 × 10−6 | 3.0971 | 390.24 | 387.13 | |
8 | 26,800 | 1.6 × 10−6 | 2.1911 | 452.31 | 445.67 | ||
10 | 26,750 | 1.6 × 10−6 | 1.9010 | 440.42 | 436.32 | ||
12 | 26,700 | 1.8 × 10−6 | 1.8148 | 389.93 | 378.76 | ||
14 | 26,600 | 0.999 × 10−6 | 2.9235 | 472.33 | 467.32 | ||
16 | 26,600 | 0.994 × 10−6 | 2.7767 | 467.45 | 461.56 |
3.10. Remarks
The example orthogonal basis functions for relaxation spectrum models have been assumed as the products of exponentials and Legendre, Laguerre, Chebyshev and Hermite polynomials. For Legendre and Laguerre models, the basis functions of the relaxation modulus are rational functions; for the Chebyshev model, they are determined by the quotient of the Euler’s gamma functions, which is a generalization of the factorial of a non-negative integer for the no-integer argument, while, for the Hermite model, these functions are based on the complementary error function. From Figure 1c,d and Figure 2c,d, it is evident that the basis functions for the relaxation modulus of Legendre and Laguerre models are in good agreement with the real relaxation modulus obtained in the experiment. However, Figure 3c,d and Figure 4c,d show that, for the Chebyshev and Hermite models, so good agreement is not achieved for individual functions . Hence, a significantly worse fit of the Chebyshev and Hermite models to the measurement data for the spectrum from Example 2, which has a much wider range of relaxation frequencies, results.
Both examples show that, generally, increasing the number of model summands improves the model quality, provided that the assumed series can provide a good approximation of the relaxation modulus. If a given series of special functions is not suitable for approximation of the relaxation modulus for a given material, then, as shown by the research conducted for the Chebyshev and Hermite models in the second example, increasing the number of series components does not improve the quality of the model.
4. Conclusions
In this paper, a class of algorithms for the relaxation spectrum identification, which combines the technique of an expansion of a function into a series in an orthonormal basis with the least-squares regularized identification, was derived. It was demonstrated that due to the choice of an appropriate special functions (Legendre, Laguerre, Chebyshev, Hermite) as the basis functions for the relaxation spectrum model, the basis functions of the relaxation modulus model are given by compact analytical or recursive formulas. Due to the choice of orthonormal basis, the smoothness of the vector of the optimal model parameters implies equivalent smoothness of the fluctuations in the model of the relaxation spectrum.
The proposed approach based on the expansion of the relaxation spectrum into a function series can be applied for arbitrary basis functions. The proven convergence and noise robustness properties of the optimal models will be retained, but the smoothing of the spectrum model will require separate analysis. As part of further research, the algorithm can be extended with a superior level of optimal selection of the time-scaling factor, so as to obtain a better fit to the measurement data. The presented scheme of the relaxation spectrum identification can be easily modified for the retardation spectrum recovery from the creep compliance measurements obtained in the standard creep test.
Nomenclature
noise corrupted | |
relaxation modulus model corresponding to | |
dimensional vector of the measurements , Equation (11) | |
dimensional vector of noise-free measurements | |
parameters of the , | |
(8) | |
solution of regularized task (14) given for regularization parameter by (15) or (19) | |
solution of regularized task (14) for ideal measurements, Equation (25) | |
vector of optimal model parameters determined by GCV method | |
normal solutions of least-squares problem (13) for noise and noise-free measurements of the relaxation modulus | |
continuous spectrum of relaxation frequencies | |
model of | |
model of | |
model of obtained for ideal measurements, | |
models of obtained for the normal solutions | |
basis functions of the , | |
dimensional identity matrix | |
number of summands, Equation (7), – | |
number of measurements in the stress relaxation test, – | |
square identification index defined by (10), | |
number of non-zero singular values of , – | |
time interval from which the sampling instants were generated | |
orthogonal matrices of singular value decomposition of , Equation (18) | |
the GCV functional defined by (16) and expressed by (21) | |
dimensional vector | |
dimensional vector , | |
time-scaling factor of the basis functions | |
regularization parameter introduced in the optimization task (14), – | |
optimal regularization parameter determined by GCV method, Equation (17) | |
diagonal matrix defined by (20) | |
the non-zero singular values of , Equation (18) | |
diagonal matrix of singular values of , Equation (18) | |
matrix defined by (11) basis for least-squares task (13) | |
integral square error of approximation, Equation (60), |
Appendix A
Appendix A.1. Derivation of the Formula (32)
Mathematical induction will be used. In the proof, the following recurrence representation of the Legendre polynomials [52,53]:
(A1) |
is used, where the two first polynomials are as follows
(A2) |
and
(A3) |
In the base case of the proof by induction, for and , Formula (32) follows immediately from definition (9) and properties (A2), (A3). For , by (9) (31) and (A2) the basis function :
while for , applying (A3), we obtain:
For , in the induction step, combining definitions (9) and (31), we have:
(A4) |
where, substituting given by recurrence Equation (A1) and having in mind (A4), we obtain:
Via the induction hypothesis, and are given by (32); thus, the basis function can be rewritten as:
(A5) |
Since
function (A5) is given by
and, after algebraic manipulations, can be expressed as:
Hence, the direct Formula (32) follows immediately.
Appendix A.2. Derivation of Formula (35)
To derive the basis function (35), we start with the alternative formula of the Laguerre polynomials (33) given by [65]:
(A6) |
An easy consequence of (A6) is
where, using the well-known formula for the Laplace transform
the basis functions defined by (9) are given by
for . Hence, by binomial theorem, we have
where Formula (35) follows. This formula is known in [55] and coincides with that given in [66].
Appendix A.3. Derivation of Formulas (40)–(43)
Suppose . Let us first derive Formulas (41), (42). For by (39) and (9), we have
(A7) |
which, after substitution , is equivalent to
whereby, due to the well-known Euler–Poisson integral [60]:
we immediately obtain (41).
For , by (38) and (9) for the polynomial , the integral is given by
(A8) |
and, keeping in mind the last expression in (A7), can be rewritten as
Then, from Equation (41), we obtain
(A9) |
Using the well-known property of the Gamma function [60]:
(A10) |
Equation (A9), after algebraic manipulations, can be expressed as
(A11) |
or in equivalent form as Formula (42).
For , by (36), (37) and (9), we have
which, keeping in mind (A8) and (A7), can be rewritten as follows
and where, by (41), (A11) and (A10), after algebraic manipulations, we obtain
(A12) |
or, equivalently, Equation (43).
Now, it remains to show that (40) holds for any . Recalling the identity (36) and using (38) for , we have
where, bearing in mind definition (9), we obtain (40), which concludes the proof.
Appendix A.4. Derivation of Formulas (47)–(49)
Let us first derive the formulas (48) and (49). Since , for , by applying in the integral the substitution , we have:
(A13) |
where, by definition (50) of the complementary error function, Formula (48) is immediately obtained.
For , the polynomial ; then, the integral is as follows
Comparing the first integral in Formula (A13) and the integral , it is easy to notice that
(A14) |
Since by (50), we have
(A15) |
Equations (A14) and (48) yield
where the next formula follows
(A16) |
and, in view of (48), Formula (49) results.
The proof of the recursive Equation (47) is based on (45), which, by definitions (44) and (9) for , yields
(A17) |
By the integration by parts, the first integral in (A17) is as follows
which, bearing in mind that
and taking into account the known property of Hermite polynomials [52]:
and definitional Formulas (44), (9), can be expressed as
which, combined with (A17), finally yields
where, after algebraic manipulations, Formula (47) follows.
Appendix A.5. Proof of Formulas (52) and (53)
Mathematical induction will be used again. In the base step, we prove (52) and (53), successively, for , and . By (48), we have
(A18) |
where both the numerator and denominator of the expression on the right hand side of (A18) become zero when . Thus, using the L’Hospital’s rule, and taking into account (A15), we obtain
Analogically,
(A19) |
where, since by (51) the initial condition , we have
Now, by (A19) and (49), we have
In order to prove (53) for , it is enough to prove that , when , since by (51), the initial condition . On the basis of (A16), we have
(A20) |
Thus, using the L’Hospital’s rule and keeping in mind (A15), we obtain
where, since based on (47) and (51), we have
(A21) |
we immediately obtain . By (A21) and (A19), the limit
(A22) |
Based on (A16)
Hence, similarly as in the case of (A20), using the L’Hospital’s rule and including Formula (A15), after simple transformations, we obtain
(A23) |
Next, substituting (A23) into (A22) yields
and bearing in mind that by (51) , Equation (53) is proved for .
Now, in the induction step, let us assume that Formulas (52) and (53) hold for , and , where We prove that they hold also for . Consider the recursive Formula (47). By the induction hypothesis, including (52) for and (53) for , from (47), we immediately have
It is only necessary to prove the correctness of Formula (53) for . The limit can be rewritten equivalently as follows
(A24) |
where both the numerator and denominator of the expression on the right expression of (A24) become zero, when . Using the L’Hospital’s rule, we have
(A25) |
On the basis of (47):
(A26) |
To determine the derivative , note that based on (9) and (44), we have
(A27) |
Since by (45)
(A28) |
Equation (A27) can be expreseed as
where, in view of (44) and (9), after algebraic manipulations, the next formula results
(A29) |
Similarly, for , we have
(A30) |
Now, combining (A26), (A30) and (A29), after algebraic manipulations, yields
(A31) |
Substituting the derivative (A31) into (A25), and bearing in mind that , and tend to zero as , we obtain
By induction hypothesis, (53) holds for . Thus, we have
(A32) |
where, since by (45), the initial conditions are related by , the correctness of Formula (53) for immediately follows from (A32).
Appendix A.6. Applicability of the Models for Various Time-Scale Parameters
Table A1.
Model | Time-Scale Factor | Range 1 of Relaxation Frequency | Range 1 of Time |
---|---|---|---|
Legendre model | 0.001 | 5301 | 3.615 |
0.01 | 530 | 36.15 | |
0.1 | 53 | 361.5 | |
1 | 5.3 | 3614.6 | |
10 | 0.53 | 36,144.5 | |
100 | 0.05301 | 361,445 | |
1000 | 0.005301 | 3,614,450 | |
10,000 | 0.0005301 | 36,144,500 | |
Laguerre model | 0.01 | 5256 | 0.995 |
0.1 | 525.36 | 9.95 | |
1 | 52.5359 | 99.5 | |
10 | 5.2536 | 995 | |
100 | 0.528 | 9950 | |
1000 | 0.0526 | 99,500 | |
10,000 | 0.00526 | 995,000 | |
100,000 | 0.000526 | 9,950,000 | |
Chebyshev model | 0.001 | 10,020 | 0.34125 |
0.01 | 1002 | 3.4125 | |
0.1 | 100.2 | 34.125 | |
1 | 10.02 | 341.25 | |
10 | 1.002 | 3412.5 | |
100 | 0.1002 | 34,125 | |
1000 | 0.01002 | 341,250 | |
10,000 | 0.001002 | 3,412,500 | |
100,000 | 0.0001002 | 34,125,000 | |
Hermite model | 0.001 | 4797.5 | 0.037639 |
0.01 | 479.75 | 0.376394 | |
0.1 | 47.975 | 3.7639 | |
1 | 4.7975 | 37.63944 | |
10 | 0.47975 | 376.3944 | |
100 | 0.047975 | 3763.944 | |
1000 | 0.0047975 | 37,639.443 | |
10,000 | 0.00047975 | 376,394.436 | |
100,000 | 0.000047975 | 3,763,944.359 |
1 Only the upper bounds (55) and (56) of the respective intervals and are given.
Appendix B
Table A2.
Model | ||||||
---|---|---|---|---|---|---|
Legendre model | 0.8222 | 0.8225 | 0.8229 | 0.8232 | 0.8235 | 0.8238 |
0.7699 | 0.7695 | 0.7705 | 0.7714 | 0.7723 | 0.7731 | |
0.6138 | 0.5979 | 0.5963 | 0.5959 | 0.5963 | 0.5970 | |
0.5299 | 0.4503 | 0.4347 | 0.4263 | 0.4215 | 0.4188 | |
0.5448 | 0.3564 | 0.3215 | 0.3021 | 0.2889 | 0.2801 | |
0.4300 | 0.3190 | 0.2887 | 0.2647 | 0.2490 | 0.2378 | |
0.2807 | 0.2442 | 0.2227 | 0.2074 | 0.1966 | ||
0.2520 | 0.2185 | 0.1945 | 0.1781 | 0.1663 | ||
0.1973 | 0.1742 | 0.1578 | 0.1462 | |||
0.1562 | 0.1398 | 0.1280 | ||||
0.1264 | 0.1146 | |||||
0.1030 | ||||||
Laguerre model | 0.3277 | 0.3265 | 0.3265 | 0.3266 | 0.3267 | |
−0.5817 | −0.5814 | −0.5804 | −0.5795 | −0.5805 | ||
0.7416 | 0.7908 | 0.7897 | 0.7891 | 0.7856 | ||
−0.6558 | −0.7164 | −0.7193 | −0.7163 | −0.7109 | ||
0.7138 | 0.5043 | 0.5076 | 0.5013 | 0.5015 | ||
−0.5418 | −0.36570 | −0.3658 | −0.3777 | −0.3717 | ||
0.2063 | 0.2083 | 0.2121 | 0.2282 | |||
−0.0935 | −0.0918 | −0.1178 | −0.1254 | |||
−0.0054 | 0.0122 | 0.0446 | ||||
0.0517 | 0.0269 | |||||
−0.0712 | ||||||
Chebyshev model | 0.8227 | 0.8265 | 0.8316 | 0.7988 | 0.8023 | 0.7991 |
0.8350 | 0.8226 | 0.8139 | 0.7962 | 0.7905 | 0.7944 | |
0.5313 | 0.5312 | 0.5382 | 0.5234 | 0.5287 | 0.5248 | |
0.5168 | 0.4545 | 0.4362 | 0.4502 | 0.4397 | 0.4416 | |
0.4625 | 0.3392 | 0.3233 | 0.3549 | 0.3426 | 0.3294 | |
0.4209 | 0.2912 | 0.2623 | 0.3195 | 0.2992 | 0.2828 | |
0.2444 | 0.2138 | 0.2768 | 0.2542 | 0.2403 | ||
0.2148 | 0.1899 | 0.2509 | 0.2317 | 0.2146 | ||
0.1603 | 0.2270 | 0.2047 | 0.1899 | |||
0.2112 | 0.1917 | 0.1752 | ||||
0.1734 | 0.1585 | |||||
0.1487 | ||||||
Hermite model | 0.5504 | 0.6391 | 0.5909 | 0.6044 | 0.6051 | |
0.7337 | 0.7670 | 0.8046 | 0.8004 | 0.8009 | ||
0.7965 | 0.6140 | 0.6703 | 0.6826 | 0.6853 | ||
0.6881 | 0.5241 | 0.4749 | 0.5005 | 0.5075 | ||
0.4916 | 0.5137 | 0.4089 | 0.3846 | 0.3885 | ||
0.7075 | 0.4046 | 0.3715 | 0.2971 | 0.2875 | ||
0.2833 | 0.2769 | 0.2366 | 0.2181 | |||
0.3419 | 0.2239 | 0.2318 | 0.2207 | |||
0.2576 | 0.2218 | 0.2178 | ||||
0.1315 | 0.1381 | |||||
0.0236 |
Table A3.
Model | ||||||
---|---|---|---|---|---|---|
Legendre model | 43.80739 | 39.6666 | 37.4618 | 35.1566 | 32.2127 | |
−29.51378 | −31.6618 | −32.1025 | −32.1325 | −31.6435 | ||
8.10418 | 15.9237 | 19.1145 | 21.6308 | 23.8515 | ||
−2.20279 | −6.1369 | −8.1839 | −10.9840 | −14.3753 | ||
−3.819709 | 0.0198 | 1.5667 | 3.9792 | 7.5618 | ||
32.529089 | 10.4212 | 5.8515 | 2.9019 | −0.9375 | ||
−10.2725 | −5.9794 | −4.2456 | −1.7853 | |||
19.8011 | 11.2957 | 8.1554 | 5.3793 | |||
−8.6168 | −6.9530 | −5.7798 | ||||
12.6105 | 9.3899 | 7.7029 | ||||
−7.0433 | −6.9429 | |||||
8.7841 | 7.9943 | |||||
−6.6946 | ||||||
7.3213 | ||||||
Laguerre model | 53.0965 | 53.0609 | 53.0093 | 53.0664 | 52.5153 | 52.7585 |
−1.4762 | 0.2502 | 1.8283 | 0.4988 | 6.3911 | 4.8727 | |
6.9102 | 6.5809 | 6.4712 | 5.2459 | 8.0061 | 6.8685 | |
−0.2900 | −3.7059 | −4.5349 | −6.4194 | −2.4884 | −4.0192 | |
−10.8544 | −6.2248 | −3.8522 | −3.7269 | −0.8334 | −1.5307 | |
−10.7846 | −6.6303 | −6.0659 | −6.4034 | −4.9840 | −5.6574 | |
−8.9629 | −8.7827 | −7.0219 | −6.1421 | −4.2199 | −4.2360 | |
−28.0790 | −12.2858 | −8.2334 | −6.5918 | −6.1999 | −6.0076 | |
−6.1049 | −6.7165 | −5.7225 | −5.4599 | −4.9298 | ||
−18.5624 | −10.7187 | −7.3355 | −6.9589 | −6.0759 | ||
−4.8687 | −4.0801 | −5.6896 | −4.7692 | |||
−13.0786 | −8.3498 | −7.4589 | −6.0712 | |||
−2.0153 | −5.4359 | −4.2447 | ||||
−9.4015 | −7.7715 | −6.0352 | ||||
−4.9662 | −3.5890 | |||||
−7.9368 | −5.9731 | |||||
−2.9159 | ||||||
−5.8840 |
Appendix C
Mathematical Terminology and Special Functions
complementary error function, Equation (50) | |
Hermite polynomials, , Equations (45) and (46) | |
Laguerre polynomials, , Equation (33) | |
Legendre polynomials, , Equations (A1)–(A3) | |
Chebyshev polynomials of the first kind, , Equations (36) and (37) | |
space of real-valued square-integrable functions on the interval | |
Laplace transform of the function | |
Euler’s gamma function | |
square norm in the real Euclidean space and in | |
find the value of , which minimizes the function |
Institutional Review Board Statement
Not applicable.
Informed Consent Statement
Not applicable.
Data Availability Statement
Not applicable.
Conflicts of Interest
The author declares no conflict of interest.
Funding Statement
This research received no external funding.
Footnotes
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