CN111523203B - Structure reliability high-efficiency failure probability calculation method based on self-adaptive double-truncation important sampling - Google Patents

Structure reliability high-efficiency failure probability calculation method based on self-adaptive double-truncation important sampling Download PDF

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CN111523203B
CN111523203B CN202010226503.6A CN202010226503A CN111523203B CN 111523203 B CN111523203 B CN 111523203B CN 202010226503 A CN202010226503 A CN 202010226503A CN 111523203 B CN111523203 B CN 111523203B
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张建国
吴洁
游令非
叶楠
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Beihang University
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Abstract

The invention provides a high-efficiency failure probability calculation method based on self-adaptive double-truncation important sampling, which comprises the following steps of: firstly, the method comprises the following steps: determination of the structural Primary random variable X = (X) 1 ,X 2 ,...,X n ) And converting the original random variable into a random variable Y = (Y) in a standard normal space 1 ,Y 2 ,...,Y n ) The corresponding extreme state function is converted to g (Y) (conversion is not required if the extreme state function is implicit); II, secondly: the iteration number l =1, and a checking point y is determined *(1) And a radius beta of a beta sphere (a hypersphere with an origin as a sphere center and a reliability index beta as a radius) (1) (ii) a Thirdly, the method comprises the following steps: generating sample points subject to truncation importance distribution by using screening method
Figure DDA0002427843430000011
Fourthly, the method comprises the following steps: calculating failure probability estimates
Figure DDA0002427843430000012
Fifthly: calculating variance
Figure DDA0002427843430000013
And coefficient of variation
Figure DDA0002427843430000014
Sixthly, the method comprises the following steps: updating the checking point and the radius of the beta sphere; seventhly, the method comprises the following steps: judgment of
Figure DDA0002427843430000015
(epsilon is a preset precision requirement) or not; if the precision is insufficient, l = l +1, and the step three is carried out until the precision requirement is met.

Description

Structure reliability high-efficiency failure probability calculation method based on self-adaptive double-truncation important sampling
Technical Field
The invention relates to a high-efficiency failure probability calculation method based on self-adaptive double-truncation important sampling, and belongs to the technical field of structural reliability analysis.
Background
The calculation of failure probability is an important subject of structural reliability analysis. The Monte Carlo method has more accurate calculation result, can also be used for the situation that the extreme state equation is more complex, and has wider application. However, to ensure sufficient accuracy, a large number of samples are required in a practical engineering problem with a low probability of failure. The important sampling method is a method for improving sampling efficiency on the premise of ensuring calculation accuracy, and the basic idea is to construct an important sampling density function to enable the extracted samples to fall into a failure domain more, so that failure probability is improved.
On the basis of the traditional important sampling method, some scholars propose a truncation important sampling method. The method further reduces the sampling area, thereby improving the sampling efficiency. However, the following disadvantages still exist in the existing truncation significant sampling method: (1) Under the condition of unknown check points (or reliability indexes), the method cannot be independently used, and the application range of the method is limited. (2) If the order moment method is adopted to determine the checking point and the reliability index, because the error of the order moment method is larger when the extreme state function is nonlinear, an ideal approximate result of the checking point and the reliability index cannot be obtained. If the obtained reliability index is too small, the high efficiency of the algorithm is difficult to embody; if the obtained reliability index is too large, the sample point originally in the failure domain is erroneously determined to be in the security domain, so that the calculation result is inaccurate.
Disclosure of Invention
The invention aims to provide a high-efficiency failure probability calculation method based on self-adaptive double-truncation important sampling aiming at the defects of the truncation important sampling method in the prior art, so that the calculation efficiency is improved on the premise of ensuring the precision when the structural reliability is analyzed.
In order to achieve the purpose, the invention adopts the following technical scheme:
the invention provides a high-efficiency failure probability calculation method based on self-adaptive double-truncation important sampling, which comprises the following steps of:
the method comprises the following steps: determination of the structural Primary random variable X = (X) 1 ,X 2 ,...,X n ) And converting the original random variable into a random variable Y = (Y) in a standard normal space 1 ,Y 2 ,...,Y n ) The corresponding extreme state function is converted to g (Y) (no conversion is needed if the extreme state function is implicit);
step two: the iteration number l =1, and a checking point y is determined *(1) And a radius beta of a beta sphere (a hypersphere with an origin as a sphere center and a reliability index beta as a radius) (1)
Step three: generating sample points subject to truncation importance distribution by using screening method
Figure BDA0002427843410000021
Step four: calculating failure probability estimates
Figure BDA0002427843410000022
Step five: calculating variance
Figure BDA0002427843410000023
And coefficient of variation
Figure BDA0002427843410000024
Step six: updating the checking point and the radius of the beta sphere;
step seven: judgment of
Figure BDA0002427843410000025
(epsilon is a preset precision requirement) or not; if the precision is insufficient, l = l +1, and the step three is carried out until the precision requirement is met.
Wherein in step one, the step of converting the original random variable into a random variable Y in a standard normal space = (Y) 1 ,Y 2 ,...,Y n ) ", it does the following:
Figure BDA0002427843410000026
in the formula (I), the compound is shown in the specification,
Figure BDA0002427843410000027
is the mean value of the random variable and,
Figure BDA0002427843410000028
is the standard deviation of the random variable;
wherein the "extreme state function" in step one is converted to g (Y) "by:
will be provided with
Figure BDA0002427843410000029
And substituting the original limit state function to obtain the converted limit state function.
Wherein "determining the checking point y" described in the second step *(1) And beta sphere radius beta (1) ", it does the following:
determination of checking points by order moment method
Figure BDA00024278434100000210
Calculating the radius of the beta sphere in a standard normal space
Figure BDA00024278434100000211
A smaller beta value can also be preset, and the average value point is taken as the initial checking point.
Wherein the generation of sample points subject to truncation of the significance distribution by means of the screening method described in step three
Figure BDA00024278434100000212
", it does the following:
firstly, taking checking points
Figure BDA00024278434100000213
For sampling the gravity center, important sampling is performed to obtain a group of random numbers
Figure BDA00024278434100000214
And screening the obtained sample points, if the sample points can simultaneously meet the following requirements:
Figure BDA00024278434100000215
and
Figure BDA00024278434100000216
the sample points are described as being subject to the truncation importance distribution and are recorded as
Figure BDA00024278434100000217
Wherein the failure probability estimate is calculated as described in step four
Figure BDA0002427843410000031
", which is done as follows:
Figure BDA0002427843410000032
wherein M = M (1) +M (2) +...+M (s) The total number of samples; s is the number of iterations; n is a radical of hydrogen (l) For each iteration to fall within the region omega 2 The number of sample points (division of area range is shown in fig. 2); i (·) is an illustrative function; f (-) is a probability density function; h is a total of (l) (. Cndot.) represents the significant sample density function in the l-th iteration.
Note: falls into the region omega 1 And Ω 3 The sample(s) can be judged to be within the safe domain without being substituted into the solution of the extreme state function g (Y).
Wherein "calculating the variance" described in step five
Figure BDA0002427843410000033
And coefficient of variation
Figure BDA0002427843410000034
", which is done as follows:
Figure BDA0002427843410000035
wherein M = M (1) +M (2) +...+M (s) The total number of samples; s is the number of iterations; n is a radical of hydrogen (l) For each iteration to fall within the region omega 2 The number of sample points (division of area range is shown in fig. 2); i (-) is an illustrative function; f (-) is a probability density function; h is (l) (. Cndot.) represents the significant sample density function in the l-th iteration; n = N (1) +N (2) +...+N (s) To fall into the region Ω 2 The total number of sample points;
Figure BDA0002427843410000036
is an estimated value of the failure probability;
Figure BDA0002427843410000037
in the formula (I), the compound is shown in the specification,
Figure BDA0002427843410000038
is the variance;
Figure BDA0002427843410000039
is an estimate of the probability of failure.
Wherein, the method for updating the checking point and the beta sphere radius in the step six is as follows:
if any sample point falls into the failure domain, recording the sample point corresponding to the maximum probability density value in the failure domain
Figure BDA00024278434100000310
Figure BDA00024278434100000311
Comparative inequality
Figure BDA00024278434100000312
Gamma is generally 1.02, if yes, the sample point corresponding to the minimum limit state value in the safety domain is recorded
Figure BDA00024278434100000313
Figure BDA00024278434100000314
β (l+1) =β **(l) (ii) a If not, y *(l+1) =y *(l) ,β (l+1) =β (l)
If no sample point falls into the failure domain, recording the sample point corresponding to the minimum limit state value in the safety domain
Figure BDA00024278434100000315
Figure BDA00024278434100000316
β (l+1) =β **(l)
The schematic diagram of the checking points and the update of the beta sphere radius is shown in figure 3.
The invention has the beneficial effects that:
(1) The method of the invention adopts the mode of beta sphere and section double truncation in single iteration to reduce the important sampling area, reduce the calling times of the extreme state function, and has small calculated amount and high sampling efficiency.
(2) The method can give a smaller beta value in advance in the first iteration and continuously adjust according to the sample point in the subsequent iteration, thereby solving the problem that the traditional truncation important sampling method can not be independently used under the condition of unknown check points (or reliability indexes).
(3) The method of the invention continuously adjusts the checking points in each iteration, thereby being capable of rapidly approaching to the vicinity of the real design checking points, being more accurate compared with the traditional truncation important sampling method which adopts a moment method and other positioning checking points, thereby increasing the occurrence probability of sample points which have great contribution to failure probability in effective sampling and accelerating the convergence speed of failure probability calculation.
(4) The method of the invention continuously adjusts the radius of the beta sphere in each iteration, thereby being capable of rapidly approaching to the real beta value and leading the accuracy of the calculation result to be higher.
(5) The method of the invention is scientific, has good manufacturability and has wide popularization and application value.
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FIG. 1 is a flow chart of the method of the present invention.
Fig. 2, a schematic diagram of region range division.
Fig. 3, schematic diagram of the verification points and the radius update of the beta sphere.
Fig. 4 is a model diagram of the mechanics of the tie rod of example 1.
Figure 5, example 2 cantilever beam structure with concentrated force schematic.
Fig. 6, example 3 schematic view of an internally pressurized cylindrical container.
Detailed Description
Example 1: a symmetric hollow circular tube pull rod is shown in figure 4 by a mechanical model diagram, and the ultimate equation of state is
Figure BDA0002427843410000041
Wherein R is the strength of the pull rod, Q is the load on the pull rod, d 1 Is the outer diameter of the cross section, d 0 The inner diameters of the sections are in normal distribution, and the parameters are shown in Table 1.
Table 1 example 1 random variable parameters
Figure BDA0002427843410000042
Figure BDA0002427843410000051
The invention discloses a high-efficiency failure probability calculation method based on self-adaptive double-truncation important sampling, which is shown in figure 1 and comprises the following steps:
the method comprises the following steps: in this example, there are four random variables, and the distribution type and parameters are given.
Normalizing the original random variable standard:
Figure BDA0002427843410000052
the extreme state equation after standard normalization is
Figure BDA0002427843410000053
Step two: the iteration number l =1, and the checking point y is preset in the example *(1) = (0,0,0,0), beta sphere radius beta (1) =1
Step three: generating sample points that are subject to a truncated importance distribution
The sample points that resulted in a distribution that obeyed truncation of the significance are shown in table 2, programmed with MATLAB software.
Table 2 example 1 first iteration sample points
Figure BDA0002427843410000054
Step four: calculating failure probability estimates
Figure BDA0002427843410000055
Ω 2 The division of the area range is schematically shown in figure 2;
step five: calculating variance
Figure BDA0002427843410000056
And coefficient of variation
Figure BDA0002427843410000057
Figure BDA0002427843410000058
Figure BDA0002427843410000059
Step six: updating the checking points and the radius of the beta sphere
y *(2) =(-1.7323,1.9311,-0.9873,0.3970)
β (2) =2.8040
The checking point and beta sphere radius updating process is schematically shown in FIG. 3;
step seven: first iteration without judgment
Figure BDA0002427843410000061
(in this example, ε =10 -3 ) And directly entering second iteration, wherein l =2, and turning to the third step until the precision requirement is met.
The convergence condition is reached through 3 iterations in this example, and the result of the iterative calculation of the probability of failure is shown in table 3.
Table 3 example 1 iterative calculation of failure probability
Figure BDA0002427843410000062
Table 4 shows the comparison of the method of the present invention with other methods, and the calculated failure probability is compared with the above method, and the result of 1000000 times of sampling by the monte carlo method is used as an accurate solution, and the relative error is calculated.
Table 4 comparison of calculation results of each method in example 1
Method Probability of failure Number of samples Relative error (%)
Monte Carlo method 0.004761 1000000 ——
Beta sphere truncation important sampling method 0.004645 3000 2.4365
The method of the invention 0.004798 3000 0.7771
As can be seen from table 4, compared with the beta sphere truncation important sampling method, the method provided by the present invention can be independently used under the condition of unknown check points (or reliability indexes), has a wider application range, and has a more accurate calculation result under the same sampling times, which indicates that the method of the present invention can effectively solve the problem of failure probability calculation, and has a higher advantage in practical engineering application.
Example 2: a cantilever beam with concentrated force is shown in figure 5 in its configuration and loaded condition. The elastic modulus E, the section moment of inertia I and the applied load force P are independent normal random variables, and the parameters are shown in a table 5; length L =5m is constant.
Table 5 example 2 random variable parameters
Figure BDA0002427843410000063
Figure BDA0002427843410000071
And (3) establishing a limit state equation by considering the maximum deformation of the cantilever beam:
g=EI-78.125P=0
the invention relates to a high-efficiency failure probability calculation method based on self-adaptive double-truncation important samples, which is shown in figure 1 and comprises the following steps:
the method comprises the following steps: in this example, there are three random variables, the distribution type and parameters are given.
Normalizing the original random variable standard:
Figure BDA0002427843410000072
the extreme state equation after standard normalization is (5Y) 1 +20)(Y 2 +10)-7.8125(2.5Y 3 +8)=0
Step two: the iteration number l =1, and the checking point y is preset in the example *(1) = 0, beta sphere radius beta (1) =1
Step three: generating sample points that are subject to a truncated importance distribution
The sample points that resulted in a distribution that obeyed truncation of the significance are shown in table 6, programmed with MATLAB software.
Table 6 example 2 first iteration sample points
Figure BDA0002427843410000073
Step four: calculating failure probability estimates
Figure BDA0002427843410000074
Ω 2 The division of the area range is schematically shown in figure 2;
step five: calculating variance
Figure BDA0002427843410000075
And coefficient of variation
Figure BDA0002427843410000076
Figure BDA0002427843410000077
Figure BDA0002427843410000078
Step six: updating the checking points and the radius of the beta sphere
y *(2) =(-2.1304,-0.9784,1.0031)
β (2) =2.5499
The checking point and beta sphere radius updating process is schematically shown in FIG. 3;
step seven: first iteration need not judge
Figure BDA0002427843410000081
(in this example,. Epsilon = 10) -3 ) And directly entering second iteration, wherein l =2, and turning to the third step until the precision requirement is met.
The convergence condition is reached through 2 iterations in this example, and the result of the iterative calculation of the probability of failure is shown in table 7.
Table 7 example 2 iterative calculation of failure probability
Figure BDA0002427843410000082
Table 8 shows the comparison of the method of the present invention with other methods, and the calculated failure probability is compared with the calculation results of the above method, and the relative error is calculated using the result of 1000000 times of sampling by the monte carlo method as an accurate solution.
Table 8 comparison of the calculation results of the methods of example 2
Method Probability of failure (10-3) Number of samples Relative error (%)
Monte Carlo method 5.9630 1000000 ——
Beta sphere truncation important sampling method 6.0517 2000 1.4875
The method of the invention 5.9540 2000 0.1509
As can be seen from table 8, compared with the beta sphere truncation important sampling method, the method provided by the present invention can be independently used under the condition of unknown check points (or reliability indexes), has a wider application range, and has a more accurate calculation result at the same sampling times, which indicates that the method of the present invention can effectively solve the problem of failure probability calculation, and has a higher advantage in practical engineering application.
Example 3: a cylindrical container with internal pressure is shown in FIG. 6, and 15MnV is used as the material. Inner diameter D, inner pressure P, wall thickness t and yield strength σ s Is independent of normalThe random variables, parameters are shown in Table 9.
Table 9 example 3 random variable parameters
Figure BDA0002427843410000083
Figure BDA0002427843410000091
For conventional internally-pressurized cylindrical thin-walled containers, subjected to two-way, i.e. axial, stresses
Figure BDA0002427843410000092
Stress in circumferential direction
Figure BDA0002427843410000093
Radial stress S r 0. According to the first strength theory (maximum principal stress theory), the ultimate state equation of the internal pressure cylinder can be obtained as follows:
g=σ s -S eq =0
in the formula, S eq For equivalent stress, in this example
Figure BDA0002427843410000094
The invention discloses a high-efficiency failure probability calculation method based on self-adaptive double-truncation important sampling, which is shown in figure 1 and comprises the following steps:
the method comprises the following steps: in this example, there are four random variables, and the distribution type and parameters are given.
Normalizing the original random variable standard:
Figure BDA0002427843410000095
the extreme state equation after standard normalization is
Figure BDA0002427843410000096
Step two: the iteration number l =1, and the checking point y is preset in the example *(1) = (0,0,0,0), beta sphere radius beta (1) =1
Step three: generating sample points that are subject to a truncated importance distribution
The sample points that resulted in a obedient truncation of the significance distributions are shown in table 10, programmed with MATLAB software.
Table 10 example 3 first iteration sample points
Figure BDA0002427843410000097
Step four: calculating failure probability estimates
Figure BDA0002427843410000098
Ω 2 The division of the area range is schematically shown in figure 2;
step five: calculating variance
Figure BDA0002427843410000101
And coefficient of variation
Figure BDA0002427843410000102
Figure BDA0002427843410000103
Figure BDA0002427843410000104
Step six: updating checking point and beta sphere radius
y *(2) =(-2.3146,1.5738,1.1962,-0.7278)
β (2) =3.1297
The checking point and beta sphere radius updating process is schematically shown in FIG. 3;
step seven: first iteration need not judge
Figure BDA0002427843410000105
(in this example,. Epsilon = 10) -4 ) And directly entering second iteration, wherein l =2, and turning to the third step until the precision requirement is met.
The convergence condition is achieved through 3 iterations in this example, and the calculation result of the iteration of the failure probability is shown in table 11.
Table 11 example 3 iterative calculation of failure probability
Figure BDA0002427843410000106
Table 12 shows the comparison of the method of the present invention with other methods, and the calculated failure probability is compared with the above method, and the result of 1000000 times of sampling by the monte carlo method is used as an accurate solution, and the relative error is calculated.
Table 12 comparison of calculation results of example 3 methods
Method Probability of failure (10) -4 ) Number of samples Relative error (%)
Monte Carlo method 4.8000 1000000 ——
Beta sphere truncation important sampling method 4.5763 4500 4.6604
The method of the invention 4.8165 4500 0.3438
It can be seen from table 12 that, compared with the beta sphere truncation important sampling method, the method provided by the present invention can be independently used under the condition of unknown check point (or reliability index), the application range is wider, and the calculation result is more accurate under the same sampling times, which shows that the method of the present invention can effectively solve the problem of failure probability calculation, and has higher advantages in practical engineering application.

Claims (24)

1. A high-efficiency failure probability calculation method based on self-adaptive double-truncation important sampling aims at a hollow circular tube pull rod with a symmetrical structure and has a limit state equation of
Figure FDA0003938157250000011
Wherein R is the strength of the pull rod, Q is the load on the pull rod, d 1 Is the outer diameter of the cross section, d 0 The inner diameters of the sections are in normal distribution, and the parameters are shown in table 1;
TABLE 1
Variables of Mean value Standard deviation of R(MPa) 400 11 Q(N) 170000 2600 d 1 (mm) 35 0.175 d 0 (mm) 25 0.125
The method is characterized by comprising the following steps:
the method comprises the following steps: four random variables are provided, and distribution types and parameters are given;
normalizing the original random variable standard:
Figure FDA0003938157250000012
the extreme state equation after standard normalization is
Figure FDA0003938157250000013
Step two: the iteration number l =1 and a preset check point y *(1) = (0,0,0,0), beta sphere radius beta (1) =1;
Step three: generating sample points which are subject to truncation of the important distribution;
programming by using MATLAB software to obtain sample points which obey truncation important distribution, wherein the sample points are shown in a table 2;
TABLE 2
Figure FDA0003938157250000014
Figure FDA0003938157250000021
Step four: calculating a failure probability estimation value;
Figure FDA0003938157250000022
step five: calculating variance
Figure FDA0003938157250000023
And coefficient of variation
Figure FDA0003938157250000024
Figure FDA0003938157250000025
Figure FDA0003938157250000026
Step six: updating the checking point and the radius of the beta sphere;
y *(2) =(-1.7323,1.9311,-0.9873,0.3970)
β (2) =2.8040
step seven: first iteration need not judge
Figure FDA0003938157250000027
Directly entering second iteration, wherein l =2, and turning to the third step until the precision requirement is met;
the convergence condition is reached through 3 iterations, and the result of the iterative calculation of the failure probability is shown in table 3;
TABLE 3
Figure FDA0003938157250000028
2. The method for calculating the high-efficiency failure probability based on the adaptive double-truncation important sampling as claimed in claim 1, wherein the method comprises the following steps: in the first step of the method,
Figure FDA0003938157250000029
in the formula (I), the compound is shown in the specification,
Figure FDA00039381572500000210
is the average of the random variables and is,
Figure FDA00039381572500000211
is the standard deviation of the random variable.
3. The method for calculating the high-efficiency failure probability based on the adaptive double truncated important samples as claimed in claim 1, characterized in that: in step one, the
Figure FDA00039381572500000212
And substituting the original limit state function to obtain the converted limit state function.
4. The method for calculating the high-efficiency failure probability based on the adaptive double-truncation important sampling as claimed in claim 1, wherein the method comprises the following steps: in step two, a checking point y is determined *(1) And beta sphere radius beta (1) ", do the following:
determination of checking points by order moment method
Figure FDA0003938157250000031
Calculated in standard normal spaceRadius of interrue beta sphere
Figure FDA0003938157250000032
5. The method for calculating the high-efficiency failure probability based on the adaptive double-truncation important sampling as claimed in claim 1, wherein the method comprises the following steps: in step three, the procedure is as follows:
first, taking the checking points
Figure FDA0003938157250000033
For sampling the center of gravity, important sampling is performed to obtain a group of random numbers
Figure FDA0003938157250000034
And screening the obtained sample points, if the sample points can simultaneously meet the following requirements:
Figure FDA0003938157250000035
and
Figure FDA0003938157250000036
then the sample points are described as being subject to truncation importance distribution, and is recorded as
Figure FDA0003938157250000037
6. The method for calculating the high-efficiency failure probability based on the adaptive double truncated important samples as claimed in claim 1, characterized in that: in step four, the procedure is as follows:
Figure FDA0003938157250000038
wherein M = M (1) +M (2) +...+M (s) Total number of samples; s is the number of iterations; n is a radical of hydrogen (l) For each iteration to fall within the region omega 2 The number of sample points; i (·) is an illustrative function; f (·)) Is a probability density function; h is a total of (l) (. Cndot.) represents the significant sampling density function in the l-th iteration.
7. The method for calculating the high-efficiency failure probability based on the adaptive double-truncation important sampling as claimed in claim 1, wherein the method comprises the following steps: in step five, the variance is calculated
Figure FDA0003938157250000039
And coefficient of variation
Figure FDA00039381572500000310
", do the following:
Figure FDA00039381572500000311
wherein M = M (1) +M (2) +...+M (s) Total number of samples; s is the number of iterations; n is a radical of (l) For each iteration to fall within the region omega 2 The number of sample points; i (-) is an illustrative function; f (-) is a probability density function; h is a total of (l) (. H) represents the significant sampling density function in the l-th iteration; n = N (1) +N (2) +...+N (s) To fall into the region omega 2 The total number of sample points;
Figure FDA00039381572500000312
is an estimated value of the failure probability;
Figure FDA00039381572500000313
in the formula (I), the compound is shown in the specification,
Figure FDA00039381572500000314
is the variance;
Figure FDA00039381572500000315
is an estimated failure probability.
8. The method for calculating the high-efficiency failure probability based on the adaptive double-truncation important sampling as claimed in claim 1, wherein the method comprises the following steps: in step six, updating the checking point and the beta sphere radius as follows:
if any sample point falls into the failure domain, recording the sample point corresponding to the maximum probability density value in the failure domain
Figure FDA0003938157250000041
Figure FDA0003938157250000042
Comparison inequality beta *(l) >γβ (l) And if the minimum limit state value is satisfied, recording a sample point corresponding to the minimum limit state value in the safety domain
Figure FDA0003938157250000043
Figure FDA0003938157250000044
β (l+1) =β **(l) (ii) a If not, y *(l+1) =y *(l) ,β (l+1) =β (l)
If no sample point falls into the failure domain, recording the sample point corresponding to the minimum limit state value in the safety domain
Figure FDA0003938157250000045
Figure FDA0003938157250000046
β (l+1) =β **(l)
9. A high-efficiency failure probability calculation method based on self-adaptive double-truncation important sampling aims at a cantilever beam with a concentrated force; the elastic modulus E, the section moment of inertia I and the applied load force P are independent normal random variables, and the parameters are shown in a table 4; length L =5m is constant;
TABLE 4
Variables of Mean value Standard deviation of E(kN/m 2 ) 2×10 7 0.5×10 7 I(m 4 ) 10 -4 0.1×10 -4 P(kN) 8 2.5
And (3) establishing a limit state equation by considering the maximum deformation of the cantilever beam:
g=EI-78.125P=0
the method is characterized by comprising the following steps:
the method comprises the following steps: three random variables are provided, and distribution types and parameters are given;
normalizing the original random variable standard:
Figure FDA0003938157250000047
the extreme state equation after standard normalization is (5Y) 1 +20)(Y 2 +10)-7.8125(2.5Y 3 +8)=0
Step two: the iteration number l =1 and a preset check point y *(1) = (0,0,0), beta sphere radius beta (1) =1;
Step three: generating sample points which are subject to truncation of the important distribution;
using MATLAB software to program, obtaining sample points which obey truncation important distribution as shown in Table 5;
TABLE 5
Figure FDA0003938157250000048
Figure FDA0003938157250000051
Step four: calculating a failure probability estimation value;
Figure FDA0003938157250000052
step five: calculating variance
Figure FDA0003938157250000053
And coefficient of variation
Figure FDA0003938157250000054
Figure FDA0003938157250000055
Figure FDA0003938157250000056
Step six: updating the checking point and the radius of the beta sphere;
y *(2) =(-2.1304,-0.9784,1.0031)
β (2) =2.5499
step seven: first iteration without judgment
Figure FDA0003938157250000057
Directly entering second iteration, wherein l =2, and turning to the third step until the precision requirement is met;
the convergence condition is achieved through 2 iterations, and the failure probability iterative computation result is shown in table 6;
TABLE 6
Figure FDA0003938157250000058
10. The method for calculating the high efficiency failure probability based on the adaptive double truncated important samples according to claim 9, is characterized in that: in the first step, the first step is carried out,
Figure FDA0003938157250000059
in the formula (I), the compound is shown in the specification,
Figure FDA00039381572500000510
is the average of the random variables and is,
Figure FDA00039381572500000511
is the standard deviation of the random variable.
11. The method for calculating the high efficiency failure probability based on the adaptive double truncated important samples according to claim 9, characterized in that: in step one, the
Figure FDA00039381572500000512
And substituting the original limit state function to obtain the converted limit state function.
12. A radical as claimed in claim 9The high-efficiency failure probability calculation method for the self-adaptive double-truncation important sampling is characterized by comprising the following steps of: in step two, a checking point y is determined *(1) And beta sphere radius beta (1) ", do the following:
determination of checking points by order moment method
Figure FDA0003938157250000061
Calculating the radius of the beta sphere in a standard normal space
Figure FDA0003938157250000062
13. The method for calculating the high efficiency failure probability based on the adaptive double truncated important samples according to claim 9, characterized in that: in step three, the procedure is as follows:
firstly, taking checking points
Figure FDA0003938157250000063
For sampling the gravity center, important sampling is performed to obtain a group of random numbers
Figure FDA0003938157250000064
And screening the obtained sample points, if the sample points can meet the following requirements:
Figure FDA0003938157250000065
and
Figure FDA0003938157250000066
then the sample points are described as being subject to truncation importance distribution, and is recorded as
Figure FDA0003938157250000067
14. The method for calculating the high efficiency failure probability based on the adaptive double truncated important samples according to claim 9, characterized in that: in step four, the procedure is as follows:
Figure FDA0003938157250000068
wherein M = M (1) +M (2) +...+M (s) The total number of samples; s is the number of iterations; n is a radical of hydrogen (l) For each iteration to fall within the region omega 2 The number of sample points; i (-) is an illustrative function; f (-) is a probability density function; h is a total of (l) (. Cndot.) represents the significant sample density function in the l-th iteration.
15. The method for calculating the high efficiency failure probability based on the adaptive double truncated important samples according to claim 9, characterized in that: in step five, the variance is calculated
Figure FDA0003938157250000069
And coefficient of variation
Figure FDA00039381572500000610
", do the following:
Figure FDA00039381572500000611
wherein M = M (1) +M (2) +...+M (s) The total number of samples; s is the number of iterations; n is a radical of (l) For each iteration to fall within the region omega 2 The number of sample points; i (-) is an illustrative function; f (-) is a probability density function; h is a total of (l) (. Cndot.) represents the significant sample density function in the l-th iteration; n = N (1) +N (2) +...+N (s) To fall into the region Ω 2 The total number of sample points;
Figure FDA00039381572500000612
is an estimated value of the failure probability;
Figure FDA00039381572500000613
in the formula (I), the compound is shown in the specification,
Figure FDA0003938157250000071
is the variance;
Figure FDA0003938157250000072
is an estimated failure probability.
16. The method for calculating the high efficiency failure probability based on the adaptive double truncated important samples according to claim 9, is characterized in that: in step six, the checking point and the beta sphere radius are updated as follows:
if any sample point falls into the failure domain, recording the sample point corresponding to the maximum probability density value in the failure domain
Figure FDA0003938157250000073
Figure FDA0003938157250000074
Comparison of inequality beta *(l) >γβ (l) And if the minimum limit state value is satisfied, recording a sample point corresponding to the minimum limit state value in the safety domain
Figure FDA0003938157250000075
Figure FDA0003938157250000076
β (l+1) =β **(l) (ii) a If not, y *(l+1) =y *(l) ,β (l+1) =β (l)
If no sample point falls into the failure domain, recording the sample point corresponding to the minimum limit state value in the safety domain
Figure FDA0003938157250000077
Figure FDA0003938157250000078
β (l+1) =β **(l)
17. A high-efficiency failure probability calculation method based on self-adaptive double-truncation important sampling is characterized in that for a certain internal-pressure cylindrical container, 15MnV is used as a material; inner diameter D, inner pressure P, wall thickness t and yield strength σ s Is an independent normal random variable, and the parameters are shown in a table 7;
TABLE 7
Variables of Mean value Standard deviation of σ s (MPa) 392 31.4 P(MPa) 20 2.4 D(mm) 460 7.0 t(mm) 19 0.8
The cylindrical, thin-walled, internally-pressurized container being subjected to bidirectional, i.e. axial, stresses
Figure FDA0003938157250000079
Stress in circumferential direction
Figure FDA00039381572500000710
Radial stress S r ≈0;
The ultimate equation of state for the internal pressure cylinder is obtained according to the first intensity theory as:
g=σ s -S eq =0
in the formula, S eq In order to be an equivalent stress,
Figure FDA00039381572500000711
the method is characterized by comprising the following steps:
the method comprises the following steps: four random variables are provided, and distribution types and parameters are given;
normalizing the original random variable standard:
Figure FDA00039381572500000712
the extreme state equation after standard normalization is
Figure FDA0003938157250000081
Step two: the iteration number l =1 and a preset checking point y *(1) = (0,0,0,0), beta sphere radius beta (1) =1;
Step three: generating sample points which obey the truncated important distribution;
using MATLAB software to program, the sample points that obey the truncated significant distribution are obtained as shown in Table 8;
TABLE 8
Figure FDA0003938157250000082
Step four: calculating a failure probability estimation value;
Figure FDA0003938157250000083
step five: calculating variance
Figure FDA0003938157250000084
And coefficient of variation
Figure FDA0003938157250000085
Figure FDA0003938157250000086
Figure FDA0003938157250000087
Step six: updating the checking point and the radius of the beta sphere;
y *(2) =(-2.3146,1.5738,1.1962,-0.7278)
β (2) =3.1297
step seven: first iteration need not judge
Figure FDA0003938157250000088
Directly entering second iteration, wherein l =2, and turning to the third step until the precision requirement is met;
the convergence condition is achieved through 3 iterations, and the failure probability iterative computation result is shown in table 9;
TABLE 9
Figure FDA0003938157250000089
Figure FDA0003938157250000091
18. The method of claim 17 for efficient failure probability computation based on adaptive double truncated key samples, wherein: in the first step, the first step is carried out,
Figure FDA0003938157250000092
in the formula (I), the compound is shown in the specification,
Figure FDA0003938157250000093
is the mean value of the random variable and,
Figure FDA0003938157250000094
is the standard deviation of the random variable.
19. The method of claim 17, wherein the method comprises the following steps: in step one, the
Figure FDA0003938157250000095
And substituting the original limit state function to obtain the converted limit state function.
20. The method of claim 17 for efficient failure probability computation based on adaptive double truncated key samples, wherein: in step two, a checking point y is determined *(1) And beta sphere radius beta (1) ", do the following:
determination of checking points by order moment method
Figure FDA0003938157250000096
Calculating the radius of the beta sphere in a standard normal space
Figure FDA0003938157250000097
21. The method of claim 17, wherein the method comprises the following steps: in step three, the method is as follows:
firstly, taking checking points
Figure FDA0003938157250000098
For sampling the center of gravity, important sampling is performed to obtain a group of random numbers
Figure FDA0003938157250000099
And screening the obtained sample points, if the sample points can meet the following requirements:
Figure FDA00039381572500000910
and
Figure FDA00039381572500000911
then the sample points are described as being subject to truncation importance distribution, and is recorded as
Figure FDA00039381572500000912
22. The method of claim 17 for efficient failure probability computation based on adaptive double truncated key samples, wherein: in step four, the procedure is as follows:
Figure FDA00039381572500000913
wherein M = M (1) +M (2) +...+M (s) Total number of samples; s is the number of iterations; n is a radical of (l) For each iteration to fall within the region omega 2 The number of sample points; i (·) is an illustrative function; f (-) is a probability density function; h is a total of (l) (. Cndot.) represents the significant sampling density function in the l-th iteration.
23. An efficient failure based on adaptive double truncated significant sampling as claimed in claim 17The probability calculation method is characterized in that: in step five, the variance is calculated
Figure FDA00039381572500000914
And coefficient of variation
Figure FDA00039381572500000915
", do the following:
Figure FDA0003938157250000101
wherein M = M (1) +M (2) +...+M (s) The total number of samples; s is the number of iterations; n is a radical of hydrogen (l) For each iteration to fall within the region omega 2 The number of sample points; i (·) is an illustrative function; f (-) is a probability density function; h is (l) (. H) represents the significant sampling density function in the l-th iteration; n = N (1) +N (2) +...+N (s) To fall into the region Ω 2 The total number of sample points;
Figure FDA0003938157250000102
is an estimated value of the failure probability;
Figure FDA0003938157250000103
in the formula (I), the compound is shown in the specification,
Figure FDA0003938157250000104
is the variance;
Figure FDA0003938157250000105
is an estimated failure probability.
24. The method of claim 17, wherein the method comprises the following steps: in step six, updating the checking point and the beta sphere radius as follows:
if any sample point falls into the failure domain, recording the sample point corresponding to the maximum probability density value in the failure domain
Figure FDA0003938157250000106
Figure FDA0003938157250000107
Comparison of inequality beta *(l) >γβ (l) And if the minimum limit state value is satisfied, recording a sample point corresponding to the minimum limit state value in the safety domain
Figure FDA0003938157250000108
Figure FDA0003938157250000109
β (l+1) =β **(l) (ii) a If not, y *(l+1) =y *(l) ,β (l+1) =β (l)
If no sample point falls into the failure domain, recording the sample point corresponding to the minimum limit state value in the safety domain
Figure FDA00039381572500001010
Figure FDA00039381572500001011
β (l+1) =β **(l)
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* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102663176A (en) * 2012-03-28 2012-09-12 北京航空航天大学 Active reliability analyzing and evaluating method for highly-reliable mechanical products
CN110532513A (en) * 2019-07-11 2019-12-03 肇庆学院 Vehicle rollover prediction algorithm based on radius importance sampling failure probability method
CN110533796A (en) * 2019-07-11 2019-12-03 肇庆学院 Vehicle rollover prediction algorithm based on truncation importance sampling failure probability method

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102663176A (en) * 2012-03-28 2012-09-12 北京航空航天大学 Active reliability analyzing and evaluating method for highly-reliable mechanical products
CN110532513A (en) * 2019-07-11 2019-12-03 肇庆学院 Vehicle rollover prediction algorithm based on radius importance sampling failure probability method
CN110533796A (en) * 2019-07-11 2019-12-03 肇庆学院 Vehicle rollover prediction algorithm based on truncation importance sampling failure probability method

Non-Patent Citations (2)

* Cited by examiner, † Cited by third party
Title
A new structural reliability analysis method in presence of mixed uncertainty variables;Lingfei YOU等;《Chinese Journal of Aeronautics》;20200211;全文 *
Neural Networks Combined with Importance Sampling Techniques for Reliability Evaluation of Explosive Initiating Device;GONG Qi等;《Chinese Journal of Aeronautics》;20121231;全文 *

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