CN106202623A - Weapon station multi-state structural optimization method based on Kriging algorithm - Google Patents
Weapon station multi-state structural optimization method based on Kriging algorithm Download PDFInfo
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Abstract
The invention provides a kind of weapon station multi-state structural optimization method based on Kriging algorithm, comprise the steps: step one, given bracing frame elastic modelling quantity, cartridge box quality, the scope of buffer rigidity;Step 2, employing Latin hypercube EXPERIMENTAL DESIGN choose acquisition N group sample point;Step 3, the calculating vibration integrated parameter of gun muzzle;Step 4, associating N group sample point and the vibration integrated parameter of N number of gun muzzle constitute initial training sample point set;Step 5, use genetic algorithm carry out optimizing to kriging agent model, find out optimum point and greatest hope improves point;Step 6, based on dual kriging Model sequence iteration optimization algorithms structure parameter optimizing problem carried out optimizing until convergence.Step 7, the different firing angle structure optimization parameter of acquisition, and the optimum structure parameter of each firing angle is updated in the weapon station kinetic model of other operating mode, find the average structural parameters final structure parameters optimization the most optimizing amplitude maximum.
Description
Technical field
The invention belongs to weapon station technical field, tie particularly to a kind of weapon station multi-state based on Kriging algorithm
Structure optimization method.
Background technology
During Canon launching, the TRANSIENT HIGH TEMPERATURE of powder burning generation, pushed at high pressure bullet high-speed motion in thorax, cannon in addition
Effect of inertia, make cannon produce high vibration, cause gun muzzle point to change, have a strong impact on fire accuracy.Research cannon
The gun muzzle disturbance launched and Changing Pattern thereof, for evaluating and examine cannon performance, identifying that the cannon quality of production, raising cannon are penetrated
Hit precision and there is important theory significance.Make gun muzzle disturbance minimum by overhead weapon station structural parameters are optimized.
Summary of the invention
The present invention has designed and developed a kind of weapon station multi-state structural optimization method based on Kriging algorithm, by right
The optimization of structural parameters, it is thus achieved that optimize, under different firing angles, the parameter that amplitude is maximum, draws the structure ginseng that average optimization amplitude is maximum
Number final structure parameters optimization the most, solves the big problem affecting fire accuracy of gun muzzle disturbance amount.
The technical scheme that the present invention provides is:
A kind of weapon station multi-state structural optimization method based on Kriging algorithm, comprises the steps:
Step one, the scope E ∈ [E of given overhead weapon station bracing frame elastic modulus Ea,Eb], scope m of cartridge box quality m
∈[ma,mb], the scope K ∈ [K of buffer stiffness Ka,Kb];
Step 2, employing Latin hypercube EXPERIMENTAL DESIGN choose the value of E, m, K, obtain N group sample point (Ei,mi,Ki), i=
1,2,...,N;
Step 3, overhead weapon station bracing frame elastic modelling quantity, cartridge box quality, buffer rigidity are respectively set as Ei、mi、
Ki, overhead weapon station is carried out gun muzzle disturbance test, obtains height to linear velocity mean-square value Di(vz), level mean square to linear velocity
Value Di(vy), height to angular displacement mean-square value Di(θz) and level to angular displacement mean-square value Di(θy), calculate gun muzzle vibration integrated
Parameter Fi
Fi=w1D(vz)+w2D(θz)+w3D(vy)+w4D(θy)
Wherein, w1、w2、w3、w4For weight coefficient;
Step 4, associating N group sample point (Ei,mi,Ki) and vibration integrated parameter F of N number of gun muzzleiConstitute initial training sample
Point set, builds kriging agent model;
Step 5, use genetic algorithm carry out optimizing to kriging agent model, find out optimum point and greatest hope improves
Point;
Step 6, the optimum point obtained in step 5 and greatest hope are improved two variance smallest point of point as to be added
Sampled point, re-start kriging agent model optimizing, until optimum point restrain;The weapon station bracing frame bullet now obtained
Property modulus E0, cartridge box quality m0, buffer K0It is overhead weapon station structure optimization parameter;
Step 7, repeat the above steps three to step 5, obtain firing angle be respectively-5 °, 0 °, 15 °, 30 °, 45 °, 60 ° time
Overhead weapon station structure optimization parameter, and the optimum structure parameter of each firing angle is updated to the weapon station kinetic simulation of other operating mode
In type, find the average structural parameters final structure parameters optimization the most optimizing amplitude maximum.
Preferably, in step 3, w1=w3=1, w2=w4=10.
Preferably, in step 6, convergence criterion is:
Wherein,It is respectively kth generation, the optimal value of kth+1 generation kriging model.
Preferably, in step 2, Latin hypercube test is used to extract 35 groups of sample points.
Preferably, in step 5, Population in Genetic Algorithms quantity is 44, and crossover probability is 0.7, and mutation probability is 0.05, receives
Holding back threshold values is 0.001.
Preferably, the scope E ∈ [1.5,2.5] of bracing frame elastic modulus E.
Preferably, the scope m ∈ [50,130] of cartridge box quality m.
Preferably, the scope K ∈ [500,750] of buffer stiffness K.
The invention has the beneficial effects as follows: the invention provides a kind of weapon station multi-state structure based on Kriging algorithm
Optimization method, by designing the optimization of bracing frame elastic modelling quantity, cartridge box quality, buffer rigidity, makes gun muzzle disturbance amount minimum.
Accompanying drawing explanation
Fig. 1 is weapon station multi-state structural optimization method flow chart based on Kriging algorithm of the present invention.
Detailed description of the invention
The present invention is described in further detail below in conjunction with the accompanying drawings, to make those skilled in the art with reference to description literary composition
Word can be implemented according to this.
As it is shown in figure 1, the invention provides a kind of weapon station multi-state structural optimization method based on Kriging algorithm,
Comprise the following steps:
Step one: select bracing frame elastic modulus E, cartridge box quality m, buffer stiffness K these three structural parameters as excellent
The design variable of change problem, shown in the span chart 1 of these three parameter:
Table 1
Step 2: use Latin hypercube EXPERIMENTAL DESIGN to choose the value of E, m, K, obtain 35 groups of sample point (Ei,mi,Ki), i
=1,2 ..., 35.
Step 3, overhead weapon station bracing frame elastic modelling quantity, cartridge box quality, buffer rigidity are respectively set as Ei、mi、
Ki, overhead weapon station is carried out gun muzzle disturbance test, obtains height to linear velocity mean-square value Di(vz), level mean square to linear velocity
Value Di(vy), height to angular displacement mean-square value Di(θz) and level to angular displacement mean-square value Di(θy), calculate gun muzzle vibration integrated
Function
MinF=min (w1D(vz)+w2D(θz)+w3D(vy)+w4D(θy))
Wherein, w1、w2、w3、w4For weight coefficient, effect is that the dimension to Vibration Parameter is unified, and value is: w1=w3=
1, w2=w4=10.
Step 4: generate initial training sample space.By 35 groups of sample point (Ei,mi,Ki), i=1,2 ..., 35 together with big gun
The vibration integrated parameter of mouth generates initial training sample space, and part sample space is as shown in table 2
Table 2
Step 5: on the basis of initial training sample space, utilizes " DACE " Toolbox structure first in Matlab
For kriging model, regression function selects binary quadratic polynomial, and correlation function selects Gaussian function, and considers anisotropy
Effect, individually gives θ value to each design variable, and scope takes [0.1,20], and initial value is unified is set to 10.Select genetic algorithm
As optimized algorithm, arranging population quantity is 44, and crossover probability is 0.7, and mutation probability is 0.05, and convergence threshold values is 0.001.
Kriging agent model is substantially a kind of approximate model [139] based on theory of statistics, its effectiveness and accurately
Property is affected little by random error.Kriging agent model, when being predicted unknown point, needs by the most known sampling
The information of point, estimates unknown point by this information is weighted combination, and method of weighting is then according to minimizing estimated value error
Variance determine, it is therefore contemplated that kriging model is optimum linear unbiased estimate.
Kriging, as the approximate model of a kind of half parametric, is made up of linear regression part and nonparametric part:
In formula, F (β, x) for returning part, multinomial and regression coefficient β by a series of x together decide on:
In Interpolation Process, (β, x) provides overall situation approximation to F, and the polynomial form of x can be chosen as 0 rank, 1 rank or 2 rank.
Z (x) is nonparametric part, provides the approximation of partial deviations in Interpolation Process, has a following statistical property:
In formula, E is expectation, and Var is variance, and Cov is covariance, and R is correlation function, and θ is associated vector.
Assume that the sample point set comprising n design variable number known to a group is X=[x1,x2,…,xn]T, it is corresponding
Functional value be Y=[y1,y2,…,yn]T, then after using kriging to carry out interpolation, to any one unknown point response value
It is estimated as:
In formula, c is interpolation coefficient.The estimation difference of agent model is:
In formula, F=[f1,f2,…,fn]T, Z=[z1,z2,…,zn]T。
In order to ensure the unbiasedness of estimated result, need to make above-mentioned estimation difference is desired for 0:
I.e. have:
FTC-f (x)=0
Now, the mean square deviation of estimated value is:
In formula,
Kriging model needsMinimum, therefore coefficient c can minimize mean square deviation Optimized model by foundation and solves
Draw:
Introducing Lagrange multiplier obtains:
L (c, λ)=σ2(1+cTRc-2cTr)-λT(FTc-f(x))
Above formula about the gradient of c is:
Can obtain system equation in conjunction with constraints is:
Can derive further:
Above formula is substituted into:
The parameter estimation maximum likelihood function of logarithmic form is:
After θ initial value is given, by maximum likelihood function respectively to β and σ2Differentiate, and make it be equal to 0, then can obtain
Maximum-likelihood estimation to two parameters is:
Now, kriging is minimum dispersion linear unbiased estimator to the estimation of unknown point:
Step 6: according to above-mentioned initial condition, based on dual kriging Model sequence iteration optimization algorithms, weapon station is tied
Structure Parametric optimization problem carries out optimizing, and convergence criterion is:
In formula,It is respectively kth generation, the optimal value of kth+1 generation kriging model.
Result as shown in table 3, table 4, wherein x1、x2、x3The most corresponding bracing frame elastic modelling quantity, cartridge box quality and buffering
Device rigidity.
Table 3
Table 4
From characteristic point history, in the searching process of weapon station gun muzzle vibration optimization problem, optimal value is not one
Diminish taste, but fluctuate back and forth between-40 to 40, cause the kriging agent model that the reason of this phenomenon is to simulate
There is several close minimum points, when the pattern search of epicycle kriging to optimum point through add some points raising accuracy after, separately
One close minimum point highlights, and becomes the optimum point of next round kriging model, optimizing the most repeatedly, adds some points, and one
Until these several minimum points " are filled and led up ", globe optimum is retained.
Knowable to table 3, table 4, whole optimization process experienced by 26 renewals taking turns kriging model, altogether adds some points 26,
The global optimum of convergence is 1.965 eventually, has compared initial value, and objective function optimization amplitude is 24.7%, corresponding structure ginseng
Number optimal solution is: bracing frame elastic modelling quantity is 1.913GPa, cartridge box quality is 122.506kg, buffer rigidity 615.69N/mm.
Step 7, employing-5 °, 0 °, 15 °, 30 °, 45 °, 60 ° of these six kinds of firing angles test, and use dual kriging
It is solved by Model sequence iteration optimization algorithms respectively, and optimum results is as shown in table 5.
Table 5
As shown in Table 5, the optimal solution that under different firing angles, overhead weapon station structure parameter optimizing model is corresponding is different, and reason exists
Change in firing angle makes load direction of transfer change, and the power suffered by parts such as barrel, gudgeon, reel cage, bracket and moment have
Changed, so that weapon station integral power characteristic changes, ultimately resulted in the inconsistent of optimal solution.Indicated above, by
The optimal solution that single operating mode optimizing obtains, does not illustrate the optimality for other operating mode.
Therefore, for the feature of weapon station difference shooting operating mode correspondence Different structural parameters optimal solution, for showing that one group is fitted
With structural parameters widest in area, on the basis of each shooting operation optimization model optimizing result, by the optimum structure of each firing angle
Parameter is updated in the weapon station kinetic model of other operating mode;Contrast the optimization that all operating mode gun muzzles are vibrated by each structural parameters
Effect, selects the most averagely to optimize one group of maximum structural parameters of amplitude as multi-state optimal solution.Gun muzzle vibration before and after optimization
The contrast of comprehensive amount is as shown in table 6, and different optimal solutions are as shown in table 7 to the optimization amplitude of different firing angle kinetic models.
Table 6
Table 7
From result above, having compared the vibration integrated amount of gun muzzle of initial solution, different firing angle optimal solutions are to respective firing angle
Gun muzzle vibration degree of optimization of weapon station kinetic model differs, and wherein, seeks the weapon station kinetic model that firing angle is 60 °
The excellent optimal solution obtained is the highest to the degree of optimization of himself kinetic model, gun muzzle vibration suppressioning effect best, optimizes amplitude
Being 36.7%, remaining degree of optimization is followed successively by-5 ° of firing angles, 30 ° of firing angles, 0 ° of firing angle, 45 ° of firing angles and 15 ° of firing angles from high to low
The optimal solution that kinetic model is corresponding;For overall firing angle operating mode, different firing angle optimal solutions are to all operating mode weapon station kinetics
Gun muzzle vibration optimization amplitude of model differs, and even indivedual optimal solutions are vibrated also for gun muzzle of other firing angle kinetic model
Deterioration effect (being the situation of negative corresponding to amplitude of variation) can be played, wherein, seek the weapon station kinetic model that firing angle is 60 °
The excellent structural parameters optimal solution obtained, best to the global optimization effect of different operating mode weapon station kinetic model gun muzzle vibrations,
Average optimization amplitude is 16.2%, and remaining optimization amplitude is followed successively by-5 ° of firing angles, 30 ° of firing angles, 45 ° of firing angles, 0 ° of firing angle from high to low
And the optimal solution that 15 ° of firing angle kinetic models are corresponding.It is seen that, the structure that more the firing angle optimizing of edge, the more limit obtains
Parametric optimal solution, its suitability relaxes the good of firing angle than centre, and this illustrates to a certain extent by limiting condition optimizing
The optimum structure parameter obtained has to the compatibility relaxing operating mode.
To sum up, the weapon station kinetic model optimizing that firing angle is 60 ° the structural parameters optimal solution obtained is to all operating modes
Global optimization effect is ideal, the suitability best, the most also explanation overhead weapon station structural parameters are adjusted to
After this prioritization scheme, the adaptability to different operating modes is the strongest.
Although embodiment of the present invention are disclosed as above, but it is not restricted in description and embodiment listed
Using, it can be applied to various applicable the field of the invention completely, for those skilled in the art, and can be easily
Realizing other amendment, therefore under the general concept limited without departing substantially from claim and equivalency range, the present invention does not limit
In specific details with shown here as the legend with description.
Claims (8)
1. a weapon station multi-state structural optimization method based on Kriging algorithm, it is characterised in that comprise the steps:
Step one, the scope E ∈ [E of given overhead weapon station bracing frame elastic modulus Ea,Eb], the scope m ∈ of cartridge box quality m
[ma,mb], the scope K ∈ [K of buffer stiffness Ka,Kb];
Step 2, employing Latin hypercube EXPERIMENTAL DESIGN choose the value of E, m, K, obtain N group sample point (Ei,mi,Ki), i=1,
2,...,N;
Step 3, overhead weapon station bracing frame elastic modelling quantity, cartridge box quality, buffer rigidity are respectively set as Ei、mi、Ki, right
Overhead weapon station carries out gun muzzle disturbance test, obtains height to linear velocity mean-square value Di(vz), level is to linear velocity mean-square value Di
(vy), height to angular displacement mean-square value Di(θz) and level to angular displacement mean-square value Di(θy), calculate the vibration integrated parameter of gun muzzle
Fi
Fi=w1D(vz)+w2D(θz)+w3D(vy)+w4D(θy)
Wherein, w1、w2、w3、w4For weight coefficient;
Step 4, associating N group sample point (Ei,mi,Ki) and vibration integrated parameter F of N number of gun muzzleiConstitute initial training sample point set,
Build kriging agent model;
Step 5, use genetic algorithm carry out optimizing to kriging agent model, find out optimum point and greatest hope improves point;
Step 6, the optimum point obtained and greatest hope are improved two variance smallest point of point adopt as to be added in step 5
Sampling point, re-starts kriging agent model optimizing, until optimum point restrains;The weapon station bracing frame springform now obtained
Amount E0, cartridge box quality m0, buffer K0It is overhead weapon station structure optimization parameter;
Step 7, repeat the above steps three to step 5, obtain firing angle be respectively-5 °, 0 °, 15 °, 30 °, 45 °, 60 ° time overhead
Weapon station structure optimization parameter, and the optimum structure parameter of each firing angle being applied in weapon station, show that average optimization amplitude is
Big structural parameters final structure parameters optimization the most.
Weapon station multi-state structural optimization method based on Kriging algorithm the most according to claim 1, its feature exists
In, in step 3, w1=w3=1, w2=w4=10.
Weapon station multi-state structural optimization method based on Kriging algorithm the most according to claim 2, its feature exists
In, in step 6, convergence criterion is:
Wherein,It is respectively kth generation, the optimal value of kth+1 generation kriging model.
Weapon station multi-state structural optimization method based on Kriging algorithm the most according to claim 3, its feature exists
In, in step 2, use Latin hypercube test to extract 35 groups of sample points.
Weapon station multi-state structural optimization method based on Kriging algorithm the most according to claim 4, its feature exists
In, in step 5, Population in Genetic Algorithms quantity is 44, and crossover probability is 0.7, and mutation probability is 0.05, and convergence threshold values is 0.001.
Weapon station multi-state structural optimization method based on Kriging algorithm the most according to claim 5, its feature exists
In, the scope E ∈ [1.5,2.5] of bracing frame elastic modulus E.
Weapon station multi-state structural optimization method based on Kriging algorithm the most according to claim 5, its feature exists
In, the scope m ∈ [50,130] of cartridge box quality m.
Weapon station multi-state structural optimization method based on Kriging algorithm the most according to claim 5, its feature exists
In, the scope K ∈ [500,750] of buffer stiffness K.
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CN112733393A (en) * | 2020-11-27 | 2021-04-30 | 长春工业大学 | Method for optimizing performance of rivet-free riveting joint of metal heterogeneous plate |
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US20120024143A1 (en) * | 2010-07-27 | 2012-02-02 | Raytheon Company | Weapon Station and Associated Method |
CN102360403A (en) * | 2011-10-26 | 2012-02-22 | 中冶南方工程技术有限公司 | Method for optimally designing structure of sliding shaft sleeve based on Kriging model |
CN104750932A (en) * | 2015-04-01 | 2015-07-01 | 电子科技大学 | Structural reliability analysis method based on agent model under condition of hybrid uncertainty |
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US20120024143A1 (en) * | 2010-07-27 | 2012-02-02 | Raytheon Company | Weapon Station and Associated Method |
CN102360403A (en) * | 2011-10-26 | 2012-02-22 | 中冶南方工程技术有限公司 | Method for optimally designing structure of sliding shaft sleeve based on Kriging model |
CN104750932A (en) * | 2015-04-01 | 2015-07-01 | 电子科技大学 | Structural reliability analysis method based on agent model under condition of hybrid uncertainty |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
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CN112733393A (en) * | 2020-11-27 | 2021-04-30 | 长春工业大学 | Method for optimizing performance of rivet-free riveting joint of metal heterogeneous plate |
CN112733393B (en) * | 2020-11-27 | 2023-06-20 | 长春工业大学 | Method for optimizing performance of rivet-free riveting joint of metal heterogeneous plate |
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