Structural damage detection based on cloud model and DempsterShafer evidence theory
Liang Tian^{1} , Huiyong Guo^{2} , Xinyu Zhou^{3} , Yushan Wang^{4}
^{1, 2, 3}Key Laboratory of New Technology for Construction of Cities in Mountain Area, Ministry of Education, Chongqing, 400045, China
^{1, 2, 3}School of Civil Engineering, Chongqing University, Chongqing, 400045, P. R. China
^{4}School of Water Conservancy and Architectural Engineering, Shihezi University, Shihezi, 832003, China
^{2}Corresponding author
Journal of Vibroengineering, Vol. 20, Issue 2, 2018, p. 909922.
https://doi.org/10.21595/jve.2017.18361
Received 20 March 2017; received in revised form 1 August 2017; accepted 10 August 2017; published 31 March 2018
JVE Conferences
Cloud model and DS theory have been widely used in uncertainty reasoning. Meanwhile, modal strain energy and Inner Product Vector are also utilized as damagesensitive features to detect structural damage. In this paper, a new structural damage identification approach is proposed based on DempsterShafer theory and cloud model. Cloud models were created to make uncertainty reasoning in damage structures by modal strain energy and the Inner Product Vector of acceleration. Then the results of the two methods were combined by using the DempsterShafer theory. Due to the classical DS theory involves counter – intuitive behavious when the high conflicting evidences exists, the distance function was introduced to correct the conflict factor $K$ and combine the evidences. Moreover, a model of simple beam was created to verify the feasibility and accuracy for the singledamage and the multipledamage. The effects of noise on damage detection were investigated simultaneously. The results show that the method has strong antinoise ability and high accuracy.
Keywords: damage identification, cloud model, DS theory, mode strain energy, inner product vector.
1. Introduction
In the past two decades, the security of building structure has received increasingly concern both at home and abroad especially the damage detection for structure itself. As a result of the structural damage, the local rigidity of the structure will descend while the modal parameters change. Therefore, most of researchers make the damage detection analysis based on modal parameters and the structural dynamic responses. Koh [1] has made damage detection in Suspension Bridge based on the modal correlation, and Shi Z. Y. [2] presented a method for structural damage localization and damage degree analysis by the incomplete modal displacement change before and after structure damaged. Fan [3] has made damage research on plate structure, using the wavelet transform of structural vibration mode and modal shape, obtained good results. S. M. Seyedpoor [4] has put forward a method which is divided into two stage to detect structural damage, based on the modal strain energy calculated by the particle swarm optimization. Guo [5] has proposed a method based on evidence theory and modal strain energy to make damage analysis. And ShaoFei Jiang [6] combined the Artificial Neural Network with the DempsterShafer theory [7, 8], and its effectiveness has also been proved in the research.
In the prior context, we find that the modal strain energy has been widely applied in structural damage detection. On the other hand, there are also some damage research based on the Inner Product Vector (IPV). The IPV is related to the mode shapes and can be directly calculated by the time domain vibration responses. Zhichun Yang [9] has proposed a method based on the changes in IPV, and damage detection experiments of shear frame structure are presented to illustrate the reliability and effectiveness of the method. Muyu Zhang [10] has formulated a new approach to detect the damage based on the auto correlation function, and the auto correlation function of the vibration response signals from different measurement points can be used to detect damage accurately even when the damage is very small. But most of above methods have difficulties with uncertainty in structural damage identification area.
In this paper, a new method is proposed to detect the structural damage based on cloud model and DempsterShafer theory. DS theory and cloud model are both effective ways to deal with uncertainty, and have been widely used in mechanical field, electronic field and medical field. In the field of structural damage identification, Qingguo Fei [11] used the modal strain energy change ratio by model shapes of different orders to locate the damage element of a fixend beam, then applied the DS theory to fuse the results of different orders. Hui Li [12] proposed a damage identification method based on the combination of ratification neural network, DS evidence theory and the Shannon entropy and used a threedimensional finite element model of the Binzhou Yellow River Highway Bridge to verify the accuracy of the method. Qifeng Zhou [13] has proposed an intelligent detection method which combined the posteriori probability support vector machines and DS theory to detect the location and extent of structural damage. Since it is difficult to solve uncertain problem in structural damage identification only by DS theory, cloud model is introduced to combine with DS theory. At present, the cloud model is seldom used in the field of structural damage identification. In this paper, firstly the cloud model is introduced, which was proposed by Deyi Li in 1995 [14]. Cloud model is an effective tool to deal with the uncertainty and can realize the conversion between qualitative concepts and quantitative values. Then the DemspsterShafer theory is introduced, which is originated from Dempster’s work on multivalued mapping in the 1960s, and has been widely used recently in the fields of uncertain reasoning. Then the modal strain energy and the acceleration IPV are used to formulate cloud models separately. Next combine the two results by modal energy and IPV with the improved DemspsterShafer theory.
Theoretically the method has strong antinoise ability and high accuracy. Firstly, multiply cloud reasoning are performed in both two cloud generators, which ensure the accuracy of the reasoning result and improve the antinoise ability. Secondly, DS theory is improved to eliminate the possibility of wrong combined results. Meanwhile, the identification results of two cloud generators are combined according to the combination rules. Damage detect of a simple beam is used to verify the method. The results show that the new method has good antinoise ability, effectiveness for damage. And as a supplement, the method based on modal strain energy dissipation rate is adopted to compare with the new method in based on cloud model and DS theory. The results show that the new method has stronger antinoise ability and higher accuracy than modal strain energy dissipation rate.
2. Cloud model
In cloud model, three numerical characteristics are used to describe the information uncertainty, Expectation $Ex$, Entropy $En$, and Excess Entropy $He$ [1517]. The detailed descriptions are listed in the following context.
$Ex$: A point that can stand the qualitative concept to the maximal degree in the whole universe space. It is also the position of the center of gravity of the cloud.
$En$: The discrete degree of cloud droplet that represents the qualitative concept can be reflected by this numerical characteristic, and it shows the connection between the randomness and fuzziness.
$He$: The measurement of the entropy. In another word, it is the entropy of the entropy. This numerical characteristic reflects the uncertainty aggregation extent of all the points that contribute to the qualitative concept $C$ in the quantitative universe $U$ and the magnitude of the randomness of the certainty degree $u\left(x\right)$.
In a word, the three numerical characteristic combine the fuzziness with the randomness perfectly, and shows the mutual mapping between the qualitative concept and the quantitative numeric. In this paper, we use the three numerical characteristic to construct a normal cloud generator to realize the transformation between the qualitative concept and the quantitative numeric.
The cloud generators can be divided into normal cloud generator and backward cloud generator. Both the position coordinates of a cloud droplet in the quantitative universe space and the qualitative extent can be obtained by inputting the three numerical characteristic ($Ex$, $En$, $He$) and the quantity of cloud droplets that need to be generated in the normal cloud generator. Similarly, the backward cloud generator is the inverse process of the normal cloud generator.
Fig. 1. Normal cloud generator and backward cloud generator
The normal cloud generator algorithm [18]:
a) Generating a normal random number $Xr$ according to the three numerical characteristic ($Ex$, $En$, $He$), and the expectation of $Xr$ is $Ex$ and the standard deviation is $En$.
b) Generating a normal random number $En$, of which the expectation is $En$ and the standard deviation is $He$.
c) Generating the cloud droplet (${x}_{r}$, ${\mu}_{r}$) by ${\mu}_{r}=\mathrm{e}\mathrm{x}\mathrm{p}\left[{\left({x}_{r}Ex\right)}^{2}/\left(2{{En}^{\text{'}}}^{2}\right)\right]$.
d) Repeat the above procedure until $N$ cloud droplets were generated.
The backward cloud generator algorithm [19]:
a) $\stackrel{}{X}=\frac{1}{N}\sum _{r=1}^{N}{x}_{r}$, ${M}_{1}^{*}=\frac{1}{N}\sum _{r=1}^{N}\left{x}_{r}\stackrel{}{X}\right$, ${S}^{2}=\frac{1}{N1}\sum _{r=1}^{N}{\left({x}_{r}\stackrel{}{X}\right)}^{2}$.
b) $\widehat{Ex}=\stackrel{}{X}$.
c) $\widehat{En}=\sqrt{\frac{\pi}{2}}\times \frac{1}{N}\sum _{r=1}^{N}\left{x}_{r}\widehat{Ex}\right$.
d) $\widehat{He}=\sqrt{\left{S}^{2}{\widehat{En}}^{2}\right}$.
Given three digital characteristics $Ex$, $En$, $He$ and a particular number ${x}_{0}$, the generator could produce the cloud droplet (${x}_{0}$, $\mu $). This kind of generators is called forward cloud generator as well as $X$ conditions cloud generators. By contrast, given the three digital characteristics and a particular $Y={u}_{i}$, the generator could produce cloud droplet (${x}_{i},{u}_{i}$). This kind of generators is called backward cloud generator as well as $Y$ conditions cloud generators.
A qualitative rule could be described as if $A$ then $B$, only single condition and single rule generators are discussed in this paper. The algorithm is listed as follows:
Input: the digital characteristics of forward cloud qualitative concept C1 (${Ex}_{a}$,${En}_{a}$,${He}_{a}$) and backward cloud qualitative concept C2 (${Ex}_{b}$, ${En}_{b}$, ${He}_{b}$), the quantitative number ${x}_{a}$ for C1.
Output: the quantitative number ${x}_{b}$ got form certainty $u$ for C2.
Detailed procedures [20]:
1) Generate a normal random number ${En}_{a}^{\text{'}}$, of which expectation is ${En}_{a}$, and standard deviation is ${He}_{a}$.
2) Calculate the certainty by $\mu =\mathrm{e}\mathrm{x}\mathrm{p}\left[{\left({x}_{a}{Ex}_{a}\right)}^{2}/\left(2{{En}_{a}^{\text{'}}}^{2}\right)\right]$.
3) Generate a normal random number ${En}_{b}^{\text{'}}$, of which expectation is ${En}_{b}$, and standard deviation is ${He}_{b}$.
4) If ${x}_{a}>{Ex}_{a}$, ${x}_{b}={Ex}_{b}+{En}_{b}^{\text{'}}\sqrt{2\mathrm{l}\mathrm{n}\mu}$.
5) If ${x}_{a}\le {Ex}_{a}$, ${x}_{b}={Ex}_{b}{En}_{b}^{\text{'}}\sqrt{2\mathrm{l}\mathrm{n}\mu}$.
From the above texts, we can know that the degree of uncertainty could be passed on by cloud generators. Firstly, a quantitative value ${x}_{a}$ was input into the forward cloud generator, so we can get the certainty $\mu $ by the cloud generator. Then the certainty $\mu $ was input into the backward cloud generator and a quantitative value ${x}_{b}$ was obtained.
3. Modal strain energy index and inner product vector of acceleration
Structural damage will change the mass, stiffness and damping properties of a structure, thus leading to the change of structural frequency and vibration mode. Therefore, various methods have been introduced to identify the damage in structure based on comparing the response data of the structure before and after damage. One of the most popular methods is that one based on using the strain energy of a structure.
Assuming that the structure is divided into $n$ elements, the modal strain energy of $j$th structural element for $i$th mode before and after damage can be expressed by a matrix notation as:
where ${\phi}_{i}$ is the $i$thorder modal vibration mode of the structure, ${\phi}_{i}^{d}$ is the $i$thorder modal vibration mode of the damaged structure, ${K}_{j}$ is the stiffness matrix of the $j$th element.
Hui Liu [21] introduced a method to identify the structural damage by modal strain energy dissipation rate. The damage coefficient of $f$th element can be expressed as:
In recent years, a new approach to detecting structure damage by using the inner product vector of the measured vibration responses was proposed. This kind of method has the advantage of high accuracy in damage detection. In this paper, the inner product is based on the cross correlation functions of displacement response under white noise excitation. Assuming that there exists a series of response measurement points in the structure, and the acceleration inner product vectors can be calculated by the inner product of the time domain vibration responses of each point under white noise excitation when the time lag equals to zero. The acceleration inner product vector ${R}_{ipv}$ is defined as [22]:
where $N$: the numbers of the response measurement points; ${X}_{ip}$: the time series of structure excitation response of measurement points; ${X}_{j}$: the time series of structure excitation response of reference point.
In this paper, the acceleration inner product vector ${R}_{ipv}$ is normalized by its maximum value:
The structural modal parameter can be changed when the structure is damaged, as well as abrupt changes in mode shapes. Therefore, the inner product vector of the damaged structure may exhibit abrupt changes. So, the damage index can be formulated as:
where ${R}_{ipv,i}^{d}$ and ${R}_{ipv,i}^{u}$ indicate the ith element in the inner product vectors of the intact and damage structures, respectively. Sometimes, the change of the inner product vector is not obvious in tiny structure damages, so a new damage index is formulated to make the damage location clear as:
4. DS evidence theory
DS evidence theory is originated from Dempster’s work on multivalued mapping in the 1960s, and has been widely used recently in the fields of uncertain reasoning.
Let ${m}_{1}$, ${m}_{2}$ be two pieces of evidence in the same frame of discernment $\mathrm{\Theta}$, and the evidence fusion rule is listed as follows [23]:
where $A$, ${A}_{i}$, ${B}_{j}\in {2}^{\mathrm{\Theta}}$, $K=1\sum _{{A}_{i}\bigcap {B}_{j}=\mathrm{\varnothing}}{m}_{1}\left({A}_{i}\right){m}_{2}\left({B}_{j}\right)$, which measure the conflict degree between the two pieces of evidence. In Eq. (8), the two pieces of evidence completely conflict when $K=0$, and in this situation the fusion rule is unavailable. If $K\ne 0$, the $m\left(A\right)$ satisfies $\sum m\left(A\right)=\text{1}$. When $K\to 0$, the two pieces of evidence are in high conflict, and an illogical result is the traditional DS fusion rule. To improve the fusion accuracy of the DS theory, distance function defined by Jousselme [24] is introduced. The distance function is defined as follows:
where $D=\left({D}_{ij}\right)$ is a matrix with order ${2}^{N}\times {2}^{N}$. And the specific calculation formula of Eq. (9) is given by:
where $\u2329{m}_{1},{m}_{2}\u232a$ is the inner product of the two vectors. Combined with the traditional conflict factor $K$ and the distance function $d\left({m}_{1},{m}_{2}\right)$, the new conflict factor between evidence is defined as follows:
5. Numerical example of cloud reasoning
To apply the above method to damage identification of structure, a simply supported beam model is used as Fig. 2. There are 20 elements of the simply beam and its overall length is 6 m, cross section area is 0.005 m^{2}, moment of inertia is 1.67 m^{4}, elastic modulus is 32 GPa, density is 2500 kg/m^{3}.
From the above information, we know the model has 39 degrees of freedom. And the paper used the Matlab software to establish finite element model, ignore the model error. Two different damage scenarios given in Table 1 are considered in the model to test the proposed method.
Fig. 2. EulerBernoulli beam
Table 1. Two different damage scenarios induced in model
Scenario 1

Scenario 2


Element number

Damage ratio

Element number

Damage ratio

8

0.2

6

0.2

14

0.2

15

0.2

Here we formulate the mapping ${f}_{1}$ to connect the element stiffness damage degree ${C}_{f}$ and the modal strain energy after structure damaged, as well as the mapping ${f}_{2}$ to connect the ${C}_{f}$ and the acceleration inner product vector after structure damaged. Forward cloud generator A1 is built by the damaged modal strain energy and A2 is built by the damaged acceleration inner product vector of every element. Meanwhile, the backward cloud generator B1 and B2 are built by the damage degree ${C}_{f}$ of every element, respectively. Then the rule base of cloud reasoning is formulated.
Suppose that the backward generator is composed of five qualitative concepts: Damage Level 1Level 5. Each digital characteristic of qualitative concept calculated by the gray cloud model is listed in Table 2.
Table 2. Digital characteristics of qualitative concept in variable degrees of damage
Level 1

Level 2

Level 3

Level 4

Level 5


Boundaries

(0, 0.1)

(0.1, 0.2)

(0.2, 0.3)

(0.3, 0.4)

(0.4, 0.5)

$Ex$

0.05

0.15

0.25

0.35

0.45

$En$

0.0167

0.0167

0.0167

0.0167

0.0167

$He$

0.0017

0.0017

0.0017

0.0017

0.0017

Then, the backward cloud generator B1 can be obtained by the forward cloud generator A1 in Matlab software.
Table 3 is the canonical matrix formulated by expectation of damaged MSE in variable degrees of damage. Entropy of damaged MSE is also necessary to formulate the cloud model, which is shown in Table 4. And the excess entropy of damaged MSE is one tenth of entropy according to the grey cloud model. The specific calculation steps are listed as follows:
1) Suppose there are m evaluation indexes and $n$ evaluation objects to formulate the canonical matrix $A=\left({a}_{rf}\right){}_{n\times m}{}^{}$.
2) Calculate the entropy of the $f$th index:
3) Calculate the soften factor of the $f$th index:
4) Give risen order to each evaluation index in matrix A and denoted by ${a}_{rf}^{\text{'}}$, by which the threshold value of the $f$th evaluation index to the $r$th gray class can be obtained, as well as the standard value interval:
${\theta}_{rf}=1.5\times {a}_{rf}^{\text{'}},f=m,$
${\theta}_{rf},L=0.95\times {a}_{rf}^{\text{'}},f=\mathrm{1,2},\dots ,m,$
${\theta}_{rf},R={\theta}_{rf},f=\mathrm{1,2},\dots ,m,$
where ${\theta}_{rf}$, $L$: the left endpoint of the standard value interval, ${\theta}_{rf}$, $R$: the right endpoint of the standard value interval.
5) Apply the canonical matrix of expectation of damaged MSE in variable degrees of damage into gray model.
Peak value ${C}_{s}$: the expectation of damaged MSE in variable degrees of damage.
Threshold value ${R}_{s}$ and ${L}_{s}$: the endpoints of the standard value interval ${\theta}_{rf}$, $L$ and ${\theta}_{rf}$, $R$.
6) $En={R}_{s}{L}_{s}/6$, $He=k=En/10$.
Table 3. Expectation of damaged MSE in variable degrees of damage
Element

Level 1

Level 2

Level 3

Level 4

Level 5

1

2841378885

3158871445

3530452308

3969275783

4493638057

2

563314131.9

661809738.9

789239381.9

958654589.8

1191963547

3

237085075.8

288903906.8

359955502.4

461228971.6

613024267

4

1054678417

1278960849

1582467110

2006951696

2625347900

5

1787482817

2139114524

2604416327

3237498089

4128365920

6

1696276664

2019134078

2443316748

3015882137

3814571320

7

979398889

1174941312

1435326045

1792675840

2301751997

8

428936988.8

518133305.4

638443741.9

806313141.2

1050811901

9

635392118.8

770379695.4

953374529.4

1210135920

1586333745

10

1394308016

1677080584

2054749396

2574626772

3317285208

11

1937283160

2312097672

2806472716

3476815011

4416841756

12

1719752427

2062122789

2516919443

3138766641

4019509302

13

944506803.7

1145417551

1417514780

1798578388

2354956160

14

391150076.7

474085023.4

586602965.3

744748265.5

977257418.2

15

661858656.9

795844411.4

975086970.6

1222576585

1578088353

16

1549034100

1842368753

2227408027

2746663012

3470412397

17

2231349792

2657722418

3217453718

3971693256

5020475115

18

2040377920

2477311705

3068119651

3892521186

5087534069

19

1075704199

1334990707

1699805390

2235530577

3066378137

20

182912446.7

228615533.4

293854012.3

391576469.5

547542094.3

So, the qualitative rule base based on the modal strain energy cloud reasoning of simply supported beam is formulated as: if ${A}_{rf}$, then ${B}_{rf}$, $r=$1, 2,…, 20, $f=$1, 2, 3, 4, 5.
The forward and backward cloud generator of qualitative rules can be regarded as qualitative concepts described with 3 digital characteristics of cloud model. For every rule in the rule base, we can construct the corresponding cloud generator and calculate by specific algorithm. In the cloud generator, many cloud droplets are produced with respective certainty degree as (${x}_{b}^{f}$, ${\mu}_{f}$), where ${x}_{b}^{f}$ is the quantitative output value of droplet in the $f$th rule activated and ${\mu}_{f}$ is the certainty. According to weighting average method [25], the results is as ${x}_{b}={\sum}_{f=1}^{m}{x}_{b}^{f}{\mu}_{f}/{\sum}_{f=1}^{m}{\mu}_{f}$.
In the Matlab software, the practical structure damage is simulated by reduction in element stiffness. Choose the first three modal vibration shape to calculate modal strain energy and measure 20 times under the 0.02 noise level. Choose the average value of the 20 times calculations results as the final identification result, so the identification effect is shown in Fig. 4 and Fig. 5 for the above two damage scenarios.
Table 4. Entropy of damaged MSE in variable degrees of damage
Element

Level 1

Level 2

Level 3

Level 4

Level 5

1

132131618

144988877.6

160223634.4

228016033.2

262125195.9

2

29644044.4

35158088.66

42603317.75

53109860.58

68872403.1

3

13481788.27

16835321.44

21731945.46

29319905.59

42062542.65

4

59369274.86

73464732.01

93551303.76

123567871.9

171175085

5

97856807.53

118790809.7

147683793.7

189167507.4

241037368.7

6

91812951.7

110679299.8

136501247

173246282.5

228108462.1

7

53896753.44

65711619.64

82766366.02

106249977.3

143336318.2

8

23949584.08

29506863.82

37418300.19

49268486.51

68241372.83

9

35754315.95

44268550.67

56459364.07

74038927.91

104365011.4

10

77155330.27

94373949.37

118471384.4

153693618.6

210125783.2

11

105448005.7

127572033.9

158004886.6

201560305.1

233302516.2

12

94542924.96

115117267.2

143684222.9

185022352.8

229838683.2

13

53173078.95

65821047.3

83313099.08

110946708.3

154096722.8

14

21994602.66

27233273.95

34754507.13

46142969.28

64640188.2

15

36601045.97

44786579.66

56295733.73

74039988.2

99796314.43

16

83698006.78

100796182.2

124178802.2

157433993.1

207090805.5

17

120936701.2

145818017.6

179543596

234252526.4

299083635.1

18

115150278.4

142581221.3

181513602.3

182662577.2

329510983.9

19

63514491.27

81313612.54

108134955.1

151172195.3

224011491.4

20

10956550.35

14191467.12

19183619.3

27473469.99

42685709.02

Fig. 3. Key flowchart of cloud reasoning based on MSE
For the cloud reasoning based on the acceleration inner product vector, this paper used a section of random white noise as the external excitation. To calculate the acceleration response of every measurement point, the Wilson$\theta $ method is adopted. Furthermore, formulate the cross correlation function in the zero delay time to construct the acceleration inner product vector and the damage index ${D}_{ipv}$. The cloud reasoning method is similar as the cloud reasoning based on modal strain energy. And the identification results are listed as Fig. 6 and Fig. 7.
Fig. 4. Average identification result for scenario 1
Fig. 5. Average identification for scenario 2
Fig. 6. Average identification result for scenario 1
Fig. 7. Average identification result for scenario 2
Apply the improved DS evidence theory into the above numerical example, the results are shown in Figs. 811.
As a supplement, the method based on modal strain energy dissipation rate is adopted to compare with the new method in based on cloud model and DS theory. The results show that the new method has stronger antinoise ability and higher accuracy.
Fig. 8. Damage identification result with 2 % noise for scenario 1
Fig. 9. Damage identification result with 2 % noise for scenario 2
Fig. 10. Damage identification results without noise for scenario 2
Fig. 11. Damage identification results with 2 % noise for scenario 2
Moreover, the original DS theory was conducted to verify the effectiveness and necessity of the improved DS theory. To save space, this paper only discussed the second damage scenario with 2 % noise. And the results are listed in Table 5 and Fig. 12.
Table 5. The comparison of the original DS and improved DS in scenario 2 with 2 % noise
Element number

Original DS

Improved DS

1

0

0

2

0

0

3

0.079996

0.123399

4

0

0

5

0

0

6

0.203831

0.218185

7

0.053918

0

8

0

0

9

0.092054

0.075543

10

0.066807

0

11

0

0

12

0.075728

0.05654

13

0

0

14

0

0

15

0.249584

0.267519

16

0

0

17

0

0

18

0

0

19

0

0

20

0

0

Fig. 12. The comparison of the original DS and improved DS in scenario 2 with 2 % noise
From the comparison results between original DS theory and improved DS theory, we can draw the conclusion that the improved DS theory is more accurate. In fact, with the numerical example becoming more complicated, the identification results of the improved DS theory are more accurate than the original DS theory.
In this paper, to assure a stable damage identification result of the structure under white noise, 20 times measurements are adopted, thus a matrix with order 20×20 is formed.
We calculated the average value, entropy value and excess entropy value of every element by the matrix to confirm the accuracy of this method. Meanwhile, the damage threshold was set at 0.005 so the element which is less than 0.005 can be neglected. Moreover, reliable index was formulated as ${R}_{i}={E}_{n}/{E}_{x}$, where the ${R}_{i}$ is less, the result is more reliable. And if the ${R}_{i}$ is more than 1, it is shows that the results are divergent. Simultaneously, formulate the ${RR}_{i}={H}_{e}/{E}_{n}$. The results of ${R}_{i}$ and ${RR}_{i}$ in two scenarios are listed in Table 6 and Table 7.
Table 6. Reliable index ${R}_{i}$ and ${RR}_{i}$ in scenario 1
Damage element

8

14

${R}_{i}$


IPV

1.2348

0.5143

Modal strain energy

0.3438

0.6083

DS

0.3404

0.4679

${RR}_{i}$


IPV

0.7995

0.6003

Modal strain energy

2.6821

0.6449

DS

1.5739

0.6855

Table 7. Reliable index ${R}_{i}$ and ${RR}_{i}$ in scenario 2
Damage element

6

15

${R}_{i}$


IPV

0.9989

0.3194

Modal strain energy

0.3822

0.8091

DS

0.3324

0.2158

${RR}_{i}$


IPV

0.4699

1.0928

Modal strain energy

0.5883

0.2818

DS

1.3718

1.7759

In the above texts, it can be easily seen that the results after DS fusion is more accuracy and stable, which shows the practicality and effectiveness of improved DS evidence theory.
6. Conclusions
Firstly, cloud models are created based on modal strain energy and acceleration Inner product vector, which can be calculated by structural vibration mode and acceleration separately. By apply the cloud models into a established simply supported beam model with white noise, the feasibility and antinoise ability of cloud models are verified. To solve the defect of traditional DS theory on fusing highly conflicting evidences, distance function is introduced and the accuracy of the improved DS theory is proved. Meanwhile, the mean value, entropy and excess entropy of the results are utilized to analyze the reliability. The ultimate results show that the developed approach in this paper can be extensively applied in structural damage detection fields. Since the structural vibration mode and acceleration are easily measured in practical engineering, there is a bright application prospect of the new method.
Acknowledgements
This work was supported by the National Natural Science Foundation of China (Grant No. 51468058, 51578094), and the Fundamental Research Funds for the Central Universities (Grant No. 106112014CDJZR200011).
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Cited By
Smart Materials and Structures
Yong Huang, Hui Li, Stephen Wu, Yongchao Yang

2018
