CN114545331A - Method for Reconstructing Sound Field Directly Radiated by Sound Source in Semi-Open Space - Google Patents

Method for Reconstructing Sound Field Directly Radiated by Sound Source in Semi-Open Space Download PDF

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CN114545331A
CN114545331A CN202210145733.9A CN202210145733A CN114545331A CN 114545331 A CN114545331 A CN 114545331A CN 202210145733 A CN202210145733 A CN 202210145733A CN 114545331 A CN114545331 A CN 114545331A
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CN114545331B (en
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周达仁
卢奂采
程相乐
汝泽宇
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Zhejiang University of Technology ZJUT
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    • G01SRADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
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Abstract

A method for reconstructing a sound source direct radiation sound field in a semi-open space, which is a method for reconstructing the sound source direct radiation sound field in the semi-open space containing a plane reflection boundary, comprises the following steps: 1. establishing a mathematical model for expressing the total sound pressure field of the direct radiation and the boundary reflected sound contribution of the sound source by linear superposition of a semispherical wave basis function; 2. arranging a holographic measuring surface at the near field of a sound source to perform sound pressure holographic measurement; 3. taking the holographic measured values of part of the measuring points as input, reconstructing the sound pressure values of the other measuring points, and determining the optimal basis function expansion term number by taking the sound pressure reconstruction error as the minimum; 4. and solving the spherical wave basis function coefficient of the semispace under the condition of the optimal expansion term number, acquiring the spherical wave basis function coefficient of the free space for expressing the sound source direct radiation sound field, and realizing the reconstruction of the sound source direct radiation sound field. The invention provides a mathematical basis for measurement and evaluation of large-size structure sound source radiation, and can realize sound field imaging and identification and positioning of the structure sound source in a semi-open space.

Description

半开放空间中重构声源直接辐射声场的方法Method for Reconstructing Sound Field Directly Radiated by Sound Source in Semi-Open Space

技术领域:Technical field:

本发明涉及在含有平面反射边界的半开放空间中,利用传感器阵列测量由声源直接辐射与平面边界反射叠加的总声学量分布,获得声源的直接辐射声学量分布的方法。属于声源识别定位、声场成像、近场声全息、声波分离以及噪声控制技术领域。The invention relates to a method for obtaining the direct radiated acoustic quantity distribution of the sound source by measuring the total acoustic quantity distribution superimposed by the direct radiation of the sound source and the reflection from the planar boundary by using a sensor array in a semi-open space containing a plane reflection boundary. It belongs to the technical fields of sound source identification and positioning, sound field imaging, near-field sound holography, sound wave separation and noise control.

背景技术:Background technique:

声源辐射声学量的测量和评估一般需要在全消声或半消声标准环境中进行。对于大尺寸、复杂装备而言,通常没有这样的理想声学测量环境。例如,大型舰船的声辐射测试通常只能于存在反射边界的船坞或码头中进行。在这种情况下,受到边界反射污染的声学测量值既不能如实反映声源在测点处的辐射量级,也不能结合建立在自由空间中的近场声全息方法,来重构声源在三维空间中的外辐射声学量分布。The measurement and evaluation of the acoustic quantity radiated by a sound source generally needs to be carried out in a fully anechoic or semi-anechoic standard environment. For large-scale, complex equipment, there is often no such ideal acoustic measurement environment. For example, acoustic radiation testing of large ships can usually only be performed in docks or piers with reflective boundaries. In this case, the acoustic measurements polluted by boundary reflection can neither faithfully reflect the radiation level of the sound source at the measuring point, nor can it be combined with the near-field acoustic holography method established in free space to reconstruct the sound source at the measuring point. External radiated acoustic volume distribution in three-dimensional space.

基于傅里叶声学法的半空间声场重构方法仅适用于全息测量面为规则的几何形状(平面、柱面或者球面)的情形。基于逆边界元法和等效源法的半空间声场重构方法需要针对声源表面设置大量离散节点和等效源点,由此而引出巨大测点数目和求逆计算量的需求。The half-space sound field reconstruction method based on the Fourier acoustic method is only suitable for the case where the holographic measurement surface is a regular geometric shape (plane, cylinder or sphere). The half-space sound field reconstruction method based on the inverse boundary element method and the equivalent source method needs to set a large number of discrete nodes and equivalent source points on the surface of the sound source, which leads to the requirement of a huge number of measuring points and the amount of inversion calculation.

发明内容:Invention content:

本发明要克服现有技术的上述缺点,提供一种半开放空间中重构声源直接辐射声场的方法。The present invention aims to overcome the above shortcomings of the prior art, and provides a method for reconstructing the direct radiation sound field of a sound source in a semi-open space.

本发明可以在含有反射边界的半开放空间中,实现声源直接辐射声场的重构。The invention can realize the reconstruction of the sound field directly radiated by the sound source in the semi-open space containing the reflection boundary.

本发明将声源直接辐射与平面边界反射声贡献的总声压场表述为一组半空间球面波基函数的线性叠加;在声源近场布置声压全息测量面,测得一组半空间总声压值,将其与半空间球面波基函数的线性叠加相匹配;通过求伪逆求解半空间球面波基函数系数;利用一组自由空间球面波基函数与求得的基函数系数重构声源在全息测量面或者任意场点处的直接辐射声压值,实现声场的重构。The invention expresses the total sound pressure field contributed by the direct radiation of the sound source and the reflected sound from the plane boundary as the linear superposition of a set of half-space spherical wave base functions; The total sound pressure value is matched with the linear superposition of the half-space spherical wave basis function; the half-space spherical wave basis function coefficients are solved by calculating the pseudo-inverse; a set of free-space spherical wave basis functions and the obtained basis function coefficients are repeated. The direct radiation sound pressure value of the sound source on the holographic measurement surface or any field point is constructed to realize the reconstruction of the sound field.

半开放空间的平面边界为局部反应(Locally Reaction)边界,其边界声阻抗率是与声波入射角和入射声波波前无关的常量,且为已知量。The plane boundary of the semi-open space is the Locally Reaction boundary, and its boundary acoustic impedance is a constant irrelevant to the incident angle of the acoustic wave and the incident acoustic wave front, and is a known quantity.

构造半空间球面波基函数的基础,是利用最速下降法(Steepest DescentMethod)求解非齐次Helmholtz方程和边界条件得到的多极子声源在半开放空间中激励的声压场的解析解。The basis of constructing the half-space spherical wave basis function is the analytical solution of the sound pressure field excited by the multipole sound source in the half-open space, which is obtained by solving the inhomogeneous Helmholtz equation and boundary conditions by the Steepest Descent Method.

解析解的表达式中包含三个叠加项,分别表述多极子直接辐射声、关于边界的镜像多极子辐射声和边界声。The expression of the analytical solution contains three superposition terms, which represent the direct radiation of the multipole, the mirrored multipole radiation about the boundary, and the boundary sound.

表述总声压场的一组半空间球面波基函数与表述声源直接辐射声压场的一组自由空间球面波基函数共用同一组基函数系数。A set of half-space spherical wave basis functions that express the total sound pressure field and a set of free-space spherical wave basis functions that express the sound pressure field directly radiated by the sound source share the same set of basis function coefficients.

本发明适用于具有任意几何形状的声源,声压全息测量面可以是不规则的单层测量面。The present invention is suitable for sound sources with arbitrary geometric shapes, and the sound pressure holographic measurement surface can be an irregular single-layer measurement surface.

本发明的半开放空间中重构声源直接辐射声场的方法,包含以下内容:The method for reconstructing the direct radiation sound field of a sound source in a semi-open space of the present invention includes the following contents:

1.建立以半空间球面波基函数的线性叠加表述声源直接辐射与边界反射声贡献的总声压场的数学模型;1. Establish a mathematical model that expresses the total sound pressure field contributed by the direct radiation of the sound source and the boundary reflection sound by the linear superposition of the half-space spherical wave basis functions;

以声源几何中心O1在边界上的投影O为原点建立全局坐标系,O1的全局坐标记为xO1=(0,0,hs),hs为O1到边界的距离;O1关于边界的镜像点记为O2。通过对全局坐标系平移,以O1和O2分别为原点建立局部坐标系,场点x在两局部坐标系中的坐标分别记为x1≡(r111)和x2≡(r222),三者之间满足如下关系:A global coordinate system is established with the projection O of the sound source geometric center O 1 on the boundary as the origin. The global coordinate of O 1 is marked as x O1 =(0,0,h s ), and h s is the distance from O 1 to the boundary; O 1 The mirror point about the boundary is denoted as O 2 . By translating the global coordinate system, a local coordinate system is established with O 1 and O 2 as the origins, respectively, and the coordinates of the field point x in the two local coordinate systems are denoted as x 1 ≡(r 1 , θ 1 , φ 1 ) and x 2 ≡(r 2 , θ 2 , φ 2 ), the following relationship is satisfied between the three:

x1=x-hsez,x2=x+hsez (1)x 1 =xh s e z , x 2 =x+h s e z (1)

其中,ez为z-向单位向量。where ez is the z -direction unit vector.

对于稳态声场,场点x处的半空间总声压phalf(x;ω)可以表述为有限项半空间球面波基函数的线性叠加:For a steady-state sound field, the half-space total sound pressure p half (x; ω) at field point x can be expressed as a linear superposition of finite-term half-space spherical wave basis functions:

Figure BDA0003508829930000021
Figure BDA0003508829930000021

其中,ω为声波角频率;ψjhalf(x;ω)为半空间球面波基函数;cj(ω)为基函数展开项系数;j为展开项序数,J为展开项项数。半空间球面波基函数ψjhalf(x;ω)的表达式为:Among them, ω is the angular frequency of the acoustic wave; ψ jhalf (x; ω) is the half-space spherical wave basis function; c j (ω) is the coefficient of the expansion term of the basis function; j is the ordinal number of the expansion term, and J is the number of the expansion term. The expression of the half-space spherical wave basis function ψ jhalf (x; ω) is:

ψjhalf(x;ω)=ψj(x|x-hsez;ω)+ψj(x|x+hsez;ω)+ξj(x|x+hsez;ω) (3)ψ jhalf (x; ω)=ψ j (x|xh s e z ; ω)+ψ j (x|x+h s e z ; ω)+ξ j (x|x+h s e z ;ω) (3)

其中,ψj(x|x-hsez;ω)和ψj(x|x+hsez;ω)分别为表述声源及其镜像虚源直接辐射声的第j项自由空间球面波基函数。在球面坐标系中,ψj的表达式为:Among them, ψ j (x|xh s e z ; ω) and ψ j (x|x+h s e z ; ω) are the j-th free-space spherical waves representing the direct radiation sound of the sound source and its mirror image virtual source, respectively basis function. In the spherical coordinate system, the expression of ψ j is:

Figure BDA0003508829930000031
Figure BDA0003508829930000031

其中,

Figure BDA0003508829930000032
为第一类球汉克尔函数,k=ω/c为声波波数,c为声速;
Figure BDA0003508829930000033
为球谐函数。在式(2)~式(4)中,整数n,l和j满足关系式j=n2+n+l+1,其中,-n≤l≤n,0≤n≤N,N为n的截断值。在计算式(3)时,其右边的前两项分别代入局部坐标x1和x2进行计算。ξj(x|x+hsez;ω)表述边界声,其表达式为:in,
Figure BDA0003508829930000032
is the first kind of spherical Hankel function, k=ω/c is the wave number of the sound wave, and c is the speed of sound;
Figure BDA0003508829930000033
is a spherical harmonic function. In equations (2) to (4), the integers n, l and j satisfy the relational expression j=n 2 +n+l+1, where -n≤l≤n, 0≤n≤N, and N is n cutoff value. When calculating formula (3), the first two items on the right side are respectively substituted into the local coordinates x 1 and x 2 for calculation. ξ j (x|x+h s e z ; ω) represents the boundary sound, and its expression is:

Figure BDA0003508829930000034
Figure BDA0003508829930000034

其中,in,

Figure BDA0003508829930000035
Figure BDA0003508829930000035

Figure BDA0003508829930000036
Figure BDA0003508829930000036

以及as well as

Figure BDA0003508829930000037
Figure BDA0003508829930000037

在式(5)~式(8)中,Rp2;ω)、F(w)和w分别为声压反射系数、边界损失因子和数值间距;局部坐标r1和r2分别为声源几何中心和镜像虚源几何中心到场点的距离;θ2为声波入射角,为场点和虚源几何中心的连线与z-轴正方向的夹角;

Figure BDA0003508829930000038
复角μp为:In equations (5) to (8), R p2 ; ω), F(w) and w are the sound pressure reflection coefficient, boundary loss factor and numerical spacing, respectively; the local coordinates r 1 and r 2 are respectively The distance from the geometric center of the sound source and the geometric center of the image virtual source to the field point; θ 2 is the incident angle of the sound wave, which is the angle between the line connecting the field point and the virtual source geometric center and the positive direction of the z-axis;
Figure BDA0003508829930000038
The complex angle μ p is:

Figure BDA0003508829930000039
Figure BDA0003508829930000039

其中,β为归一化的边界声导纳,where β is the normalized boundary acoustic admittance,

Figure BDA0003508829930000041
Figure BDA0003508829930000041

其中,Z为边界声阻抗率,Z0为归一化的边界声阻抗率,ρ0为流体介质密度。本方法的实施假定声阻抗率Z0为已知量,Z0可以根据声阻抗的原位测量方法获取。Among them, Z is the boundary acoustic impedance ratio, Z 0 is the normalized boundary acoustic impedance ratio, and ρ 0 is the density of the fluid medium. The implementation of this method assumes that the acoustic impedance rate Z 0 is a known quantity, and Z 0 can be obtained according to the in-situ measurement method of acoustic impedance.

2.在声源近场布置全息测量面进行声压全息测量;在声源近场布置一组声压传感器,形成声压全息测量面,测量声源直接辐射声与边界反射声共同贡献的总声压分布,其中,根据声源所在流体介质的不同,本方法采用的声压传感器可以是传声器、水听器或其它类型的传感器。2. Arrange a holographic measurement surface in the near field of the sound source for sound pressure holographic measurement; arrange a group of sound pressure sensors in the near field of the sound source to form a sound pressure holographic measurement surface, and measure the total contribution of the direct radiation sound of the sound source and the boundary reflection sound. Sound pressure distribution, wherein, according to the difference of the fluid medium where the sound source is located, the sound pressure sensor used in this method may be a microphone, a hydrophone or other types of sensors.

3.以部分测点的全息测量值作为输入,重构其余测点的声压值,以声压重构误差为最小为原则确定最优基函数展开项数;将全息测量面上的测点坐标记为

Figure BDA0003508829930000042
M为声压测点数目。按照隔点取点的方式,将声压测点分为两组。第一组测点坐标记为
Figure BDA0003508829930000043
Figure BDA0003508829930000044
第二组测点坐标记为
Figure BDA0003508829930000045
Figure BDA0003508829930000046
其中,
Figure BDA0003508829930000047
Figure BDA0003508829930000048
分别表示向上取整和向下取整。3. Using the holographic measurement values of some measuring points as input, reconstruct the sound pressure values of the remaining measuring points, and determine the optimal basis function expansion terms based on the principle of the sound pressure reconstruction error being the smallest; Coordinates are marked as
Figure BDA0003508829930000042
M is the number of sound pressure measurement points. The sound pressure measurement points are divided into two groups according to the method of taking points at intervals. The first group of measuring point coordinates is marked as
Figure BDA0003508829930000043
Figure BDA0003508829930000044
The second group of measuring point coordinates is marked as
Figure BDA0003508829930000045
Figure BDA0003508829930000046
in,
Figure BDA0003508829930000047
and
Figure BDA0003508829930000048
Represent round up and round down, respectively.

设定基函数展开项数J可能取值的上限为Jmax,即1≤J≤Jmax。对于该范围内的任意J,根据式(2),全息测量面的第一组测点采集的声压值可以表示为如下矩阵形式:The upper limit of the possible value of the basis function expansion term J is set to be J max , that is, 1≤J≤J max . For any J within this range, according to formula (2), the sound pressure values collected by the first group of measuring points on the holographic measurement surface can be expressed as the following matrix form:

Figure BDA0003508829930000049
Figure BDA0003508829930000049

其中,

Figure BDA00035088299300000410
为半空间总声压测量值组成的列向量:in,
Figure BDA00035088299300000410
Column vector of half-space total sound pressure measurements:

Figure BDA00035088299300000411
Figure BDA00035088299300000411

其中,上标T为向量转置。{C(ω)}J×1为半空间球面波基函数系数组成的列向量:Among them, the superscript T is the vector transpose. {C(ω)} J×1 is the column vector composed of the half-space spherical wave basis function coefficients:

Figure BDA00035088299300000412
Figure BDA00035088299300000412

Figure BDA0003508829930000051
为半空间球面波基函数在各测点的展开项组成的矩阵:
Figure BDA0003508829930000051
is the matrix composed of the expansion terms of the half-space spherical wave basis function at each measuring point:

Figure BDA0003508829930000052
Figure BDA0003508829930000052

对式(11)求解,可得系数列向量:Solving equation (11), the coefficient column vector can be obtained:

Figure BDA0003508829930000053
Figure BDA0003508829930000053

其中,上标

Figure BDA0003508829930000054
表示对矩阵求伪逆,Among them, the superscript
Figure BDA0003508829930000054
represents the pseudo-inverse of the matrix,

Figure BDA0003508829930000055
Figure BDA0003508829930000055

其中,上标H为矩阵的共轭转置。where the superscript H is the conjugate transpose of the matrix.

当系数列向量{C(ω)}J×1确定之后,可以进一步重构第二组测点的声压:After the coefficient column vector {C(ω)} J×1 is determined, the sound pressure of the second group of measuring points can be further reconstructed:

Figure BDA0003508829930000056
Figure BDA0003508829930000056

并计算第二组测点的声压重构值与测量值之间的相对误差:And calculate the relative error between the sound pressure reconstruction value and the measured value of the second set of measuring points:

Figure BDA0003508829930000057
Figure BDA0003508829930000057

其中,||·||2为向量的2-范数。where ||·|| 2 is the 2-norm of the vector.

从1~Jmax遍历所有的J,利用式(11)~式(18),计算相对误差ε,将ε最小值对应的展开项数确定为最优展开项数JoptTraverse all J from 1 to J max , use equations (11) to (18) to calculate the relative error ε, and determine the number of expansion terms corresponding to the minimum value of ε as the optimal number of expansion terms J opt .

4.在最优展开项数条件下求解半空间球面波基函数系数,获取表述声源直接辐射声场的自由空间球面波基函数系数,实现声源直接辐射声场的重构;设定基函数展开项数为Jopt,根据式(2),全息测量面采集的声压值可以表示为如下矩阵形式:4. Solve the half-space spherical wave basis function coefficients under the condition of the optimal expansion term, obtain the free-space spherical wave basis function coefficients representing the sound field directly radiated by the sound source, and realize the reconstruction of the sound field directly radiated by the sound source; set the basis function expansion The number of terms is J opt . According to equation (2), the sound pressure value collected by the holographic measurement surface can be expressed in the following matrix form:

Figure BDA0003508829930000061
Figure BDA0003508829930000061

对式(19)求伪逆以求解系数列向量

Figure BDA0003508829930000062
Pseudo-inverse equation (19) to solve for the column vector of coefficients
Figure BDA0003508829930000062

Figure BDA0003508829930000063
Figure BDA0003508829930000063

从而,可得声压重构面上声源直接辐射声压的重构值:Therefore, the reconstructed value of the sound pressure directly radiated by the sound source on the sound pressure reconstruction surface can be obtained:

Figure BDA0003508829930000064
Figure BDA0003508829930000064

其中,

Figure BDA0003508829930000065
为声压重构点坐标,s=1,2,…,S,S为重构点数目;in,
Figure BDA0003508829930000065
is the sound pressure reconstruction point coordinates, s=1,2,...,S, S is the number of reconstruction points;

Figure BDA0003508829930000066
为自由空间球面波基函数在重构点
Figure BDA0003508829930000067
的展开项组成的矩阵:
Figure BDA0003508829930000066
for the free-space spherical wave basis function at the reconstruction point
Figure BDA0003508829930000067
A matrix of expanded terms of :

Figure BDA0003508829930000068
Figure BDA0003508829930000068

本发明在基于自由空间球面波基函数叠加表述声源辐射声场的数学模型基础上,以边界声阻抗作为参量,构造满足Helmholtz方程和边界条件的半空间球面波基函数,建立基于半空间球面波基函数叠加表述半空间总声场的数学模型。对含有平面边界的半开放空间中具有任意几何形状的结构声源的声场进行全息测量,通过逆向求解基函数系数,获取声源直接辐射声场的基函数系数,实现声源直接辐射声场的重构。The invention constructs a half-space spherical wave basis function satisfying the Helmholtz equation and boundary conditions on the basis of a mathematical model expressing the sound source radiated sound field based on the superposition of the free-space spherical wave basis functions, and establishes a half-space spherical wave based on the boundary acoustic impedance as a parameter. Basis function superposition expresses a mathematical model of the total sound field in the half-space. Holographic measurement of the sound field of a structural sound source with any geometric shape in a semi-open space with a planar boundary, and by inversely solving the basis function coefficients, the basis function coefficients of the sound source's direct radiation sound field are obtained, and the reconstruction of the sound source's direct radiation sound field is realized. .

本发明的有益效果:Beneficial effects of the present invention:

1.本发明提出的基于半空间球面波基函数叠加的数学模型,可以表述含有限阻抗边界的半开放空间声场,对于在不具备理想声学测量条件的情况下,实施结构声源,特别是大尺寸结构声源辐射的测量和评估,提供了数学基础。1. The mathematical model based on the superposition of the semi-space spherical wave basis functions proposed by the present invention can express the semi-open space sound field with finite impedance boundary. Measurement and evaluation of radiation from dimensionally structured sound sources, providing a mathematical basis.

2.以阵列测量的半空间总声压分布,代入声场的数学模型进行求解,可以实现近场声全息方法能够实现的目的,即能够实现半开放空间中声场成像和结构声源的识别和定位。2. Substitute the total sound pressure distribution in the half space measured by the array into the mathematical model of the sound field to solve, which can achieve the goal that the near-field acoustic holography method can achieve, that is, it can realize the identification and localization of sound field imaging and structural sound sources in the semi-open space .

3.本发明适用于具有任意几何形状的结构声源,声压全息测量面可以是不规则的单层全息测量面。3. The present invention is applicable to structured sound sources with arbitrary geometric shapes, and the sound pressure holographic measurement surface can be an irregular single-layer holographic measurement surface.

附图说明:Description of drawings:

图1是声源和平面边界构成的半开放空间声场示意图;Figure 1 is a schematic diagram of a semi-open space sound field composed of a sound source and a plane boundary;

图2是声源及其镜像虚源的几何中心、场点和平面边界之间的几何关系;Figure 2 is the geometric relationship between the geometric center, field point and plane boundary of the sound source and its mirror image virtual source;

图3是选取最优展开项数时测点分组示意图;Fig. 3 is a schematic diagram of measuring point grouping when selecting the optimal number of expansion items;

图4是脉动球声源、平面边界和水听器阵列组成的仿真声场示意图;Figure 4 is a schematic diagram of a simulated sound field composed of a pulsating ball sound source, a plane boundary and a hydrophone array;

图5是阵列上水听器的分布和编号规则示意图;Figure 5 is a schematic diagram of the distribution and numbering rules of the hydrophones on the array;

图6是半空间总声压值、声源直接辐射声压重构值和声源直接辐射声压真实值在全息测点上的分布曲线。Figure 6 is the distribution curve of the total sound pressure value in the half space, the reconstructed value of the sound pressure directly radiated by the sound source and the real value of the sound pressure directly radiated by the sound source on the holographic measuring point.

具体实施方式Detailed ways

下面结合附图具体说明本发明的实施方式。Embodiments of the present invention will be described in detail below with reference to the accompanying drawings.

本发明的半开放空间中重构声源直接辐射声场的方法的实施按以下步骤进行:The implementation of the method for reconstructing the direct radiation sound field of a sound source in a semi-open space of the present invention is carried out according to the following steps:

步骤1,建立基于半空间球面波基函数叠加的声场数学模型。Step 1, establish a sound field mathematical model based on the superposition of the half-space spherical wave basis functions.

如图1和图2所示,以声源几何中心O1在边界上的投影O为原点建立全局坐标系,O1的全局坐标记为

Figure BDA0003508829930000071
hs为O1到边界的距离;O1关于边界的镜像点记为O2。通过对全局坐标系平移,以O1和O2分别为原点建立局部坐标系,场点x在两局部坐标系中的坐标分别记为x1≡(r111)和x2≡(r222),三者之间满足如下关系:As shown in Figure 1 and Figure 2, a global coordinate system is established with the projection O of the sound source geometric center O 1 on the boundary as the origin, and the global coordinate of O 1 is marked as
Figure BDA0003508829930000071
h s is the distance from O 1 to the boundary; the mirror point of O 1 about the boundary is denoted as O 2 . By translating the global coordinate system, a local coordinate system is established with O 1 and O 2 as the origins, respectively, and the coordinates of the field point x in the two local coordinate systems are denoted as x 1 ≡(r 1 , θ 1 , φ 1 ) and x 2 ≡(r 2 , θ 2 , φ 2 ), the following relationship is satisfied between the three:

x1=x-hsez,x2=x+hsez (1)x 1 =xh s e z , x 2 =x+h s e z (1)

其中,ez为z-向单位向量。where ez is the z -direction unit vector.

对于稳态声场,场点x处的半空间总声压phalf(x;ω)可以表述为有限项半空间球面波基函数的线性叠加:For a steady-state sound field, the half-space total sound pressure p half (x; ω) at field point x can be expressed as a linear superposition of finite-term half-space spherical wave basis functions:

Figure BDA0003508829930000081
Figure BDA0003508829930000081

其中,ω为声波角频率;ψjhalf(x;ω)为半空间球面波基函数;cj(ω)为基函数展开项系数;j为展开项序数,J为展开项项数。半空间球面波基函数ψjhalf(x;ω)的表达式为:Among them, ω is the angular frequency of the acoustic wave; ψ jhalf (x; ω) is the half-space spherical wave basis function; c j (ω) is the coefficient of the expansion term of the basis function; j is the ordinal number of the expansion term, and J is the number of the expansion term. The expression of the half-space spherical wave basis function ψ jhalf (x; ω) is:

ψjhalf(x;ω)=ψj(x|x-hsez;ω)+ψj(x|x+hsez;ω)+ξj(x|x+hsez;ω) (3)ψ jhalf (x; ω)=ψ j (x|xh s e z ; ω)+ψ j (x|x+h s e z ; ω)+ξ j (x|x+h s e z ;ω) (3)

其中,ψj(x|x-hsez;ω)和ψj(x|x+hsez;ω)分别为表述声源及其镜像虚源直接辐射声的第j项自由空间球面波基函数。在球面坐标系中,ψj的表达式为:Among them, ψ j (x|xh s e z ; ω) and ψ j (x|x+h s e z ; ω) are the j-th free-space spherical waves representing the direct radiation sound of the sound source and its mirror image virtual source, respectively basis function. In the spherical coordinate system, the expression of ψ j is:

Figure BDA0003508829930000082
Figure BDA0003508829930000082

其中,

Figure BDA0003508829930000083
为第一类球汉克尔函数,k=ω/c为声波波数,c为声速;
Figure BDA0003508829930000084
为球谐函数。在式(2)~式(4)中,整数n,l和j满足关系式j=n2+n+l+1,其中,-n≤l≤n,0≤n≤N,N为n的截断值。在计算式(3)时,其右边的前两项分别代入局部坐标x1和x2进行计算。ξj(x|x+hsez;ω)表述边界声,其表达式为:in,
Figure BDA0003508829930000083
is the first kind of spherical Hankel function, k=ω/c is the wave number of the sound wave, and c is the speed of sound;
Figure BDA0003508829930000084
is a spherical harmonic function. In equations (2) to (4), the integers n, l and j satisfy the relational expression j=n 2 +n+l+1, where -n≤l≤n, 0≤n≤N, and N is n cutoff value. When calculating formula (3), the first two items on the right side are respectively substituted into the local coordinates x 1 and x 2 for calculation. ξ j (x|x+h s e z ; ω) represents the boundary sound, and its expression is:

Figure BDA0003508829930000085
Figure BDA0003508829930000085

其中,in,

Figure BDA0003508829930000086
Figure BDA0003508829930000086

Figure BDA0003508829930000087
Figure BDA0003508829930000087

以及as well as

Figure BDA0003508829930000088
Figure BDA0003508829930000088

在式(5)~式(8)中,Rp2;ω)、F(w)和w分别为声压反射系数、边界损失因子和数值间距;局部坐标r1和r2分别为声源几何中心和镜像虚源几何中心到场点的距离;θ2为声波入射角,为场点和虚源几何中心的连线与z-轴正方向的夹角,如图2所示;

Figure BDA0003508829930000091
复角μp为:In equations (5) to (8), R p2 ; ω), F(w) and w are the sound pressure reflection coefficient, boundary loss factor and numerical spacing, respectively; the local coordinates r 1 and r 2 are respectively The distance from the geometric center of the sound source and the geometric center of the mirror virtual source to the field point; θ 2 is the incident angle of the sound wave, which is the angle between the line connecting the field point and the virtual source geometric center and the positive direction of the z-axis, as shown in Figure 2;
Figure BDA0003508829930000091
The complex angle μ p is:

Figure BDA0003508829930000092
Figure BDA0003508829930000092

其中,β为归一化的边界声导纳,where β is the normalized boundary acoustic admittance,

Figure BDA0003508829930000093
Figure BDA0003508829930000093

其中,Z为边界声阻抗率,Z0为归一化的边界声阻抗率,ρ0为流体介质密度。本方法的实施假定声阻抗率Z0为已知量,Z0可以根据声阻抗的原位测量方法获取。Among them, Z is the boundary acoustic impedance ratio, Z 0 is the normalized boundary acoustic impedance ratio, and ρ 0 is the density of the fluid medium. The implementation of this method assumes that the acoustic impedance rate Z 0 is a known quantity, and Z 0 can be obtained according to the in-situ measurement method of acoustic impedance.

步骤2,获取全息测量值。Step 2, obtaining holographic measurement values.

如图1所示,在声源近场布置一组声压传感器,形成声压全息测量面,测量声源直接辐射声与边界反射声共同贡献的总声压分布,其中,根据声源所在流体介质的不同,本方法采用的声压传感器可以是传声器、水听器或其它类型的传感器。As shown in Figure 1, a group of sound pressure sensors are arranged in the near field of the sound source to form a sound pressure holographic measurement surface, and the total sound pressure distribution contributed by the direct radiation sound of the sound source and the boundary reflected sound is measured. Depending on the medium, the sound pressure sensor used in this method may be a microphone, a hydrophone or other types of sensors.

步骤3,选取半空间球面波基函数的最优展开项数。Step 3, select the optimal expansion term of the half-space spherical wave basis function.

将全息测量面上的测点坐标记为

Figure BDA0003508829930000094
M为声压测点数目。按照隔点取点的方式,将声压测点分为两组。第一组测点坐标记为
Figure BDA0003508829930000095
Figure BDA0003508829930000096
Figure BDA0003508829930000097
第二组测点坐标记为
Figure BDA0003508829930000098
Figure BDA0003508829930000099
其中,
Figure BDA00035088299300000910
Figure BDA00035088299300000911
分别表示向上取整和向下取整。以6行6列均匀分布的声压测点组成的平面阵列为例,对测点进行分组,其示意图如图3所示。Mark the coordinates of the measuring point on the holographic measuring surface as
Figure BDA0003508829930000094
M is the number of sound pressure measurement points. The sound pressure measurement points are divided into two groups according to the method of taking points at intervals. The first group of measuring point coordinates is marked as
Figure BDA0003508829930000095
Figure BDA0003508829930000096
Figure BDA0003508829930000097
The second group of measuring point coordinates is marked as
Figure BDA0003508829930000098
Figure BDA0003508829930000099
in,
Figure BDA00035088299300000910
and
Figure BDA00035088299300000911
Represent round up and round down, respectively. Taking a plane array composed of sound pressure measurement points with 6 rows and 6 columns evenly distributed as an example, the measurement points are grouped, and the schematic diagram is shown in Figure 3.

设定基函数展开项数J可能取值的上限为Jmax,即1≤J≤Jmax。对于该范围内的任意J,根据式(2),全息测量面的第一组测点采集的声压值可以表示为如下矩阵形式:The upper limit of the possible value of the basis function expansion term J is set to be J max , that is, 1≤J≤J max . For any J within this range, according to formula (2), the sound pressure values collected by the first group of measuring points on the holographic measurement surface can be expressed as the following matrix form:

Figure BDA0003508829930000101
Figure BDA0003508829930000101

其中,

Figure BDA0003508829930000102
为半空间总声压测量值组成的列向量:in,
Figure BDA0003508829930000102
Column vector of half-space total sound pressure measurements:

Figure BDA0003508829930000103
Figure BDA0003508829930000103

其中,上标T为向量转置。{C(ω)}J×1为半空间球面波基函数系数组成的列向量:Among them, the superscript T is the vector transpose. {C(ω)} J×1 is the column vector composed of the half-space spherical wave basis function coefficients:

Figure BDA0003508829930000104
Figure BDA0003508829930000104

Figure BDA0003508829930000105
为半空间球面波基函数在各测点的展开项组成的矩阵:
Figure BDA0003508829930000105
is the matrix composed of the expansion terms of the half-space spherical wave basis function at each measuring point:

Figure BDA0003508829930000106
Figure BDA0003508829930000106

对式(11)求解,可得系数列向量:Solving equation (11), the coefficient column vector can be obtained:

Figure BDA0003508829930000107
Figure BDA0003508829930000107

其中,上标

Figure BDA0003508829930000108
表示对矩阵求伪逆,Among them, the superscript
Figure BDA0003508829930000108
represents the pseudo-inverse of the matrix,

Figure BDA0003508829930000109
Figure BDA0003508829930000109

其中,上标H为矩阵的共轭转置。where the superscript H is the conjugate transpose of the matrix.

当系数列向量{C(ω)}J×1确定之后,可以进一步重构第二组测点的声压:After the coefficient column vector {C(ω)} J×1 is determined, the sound pressure of the second group of measuring points can be further reconstructed:

Figure BDA00035088299300001010
Figure BDA00035088299300001010

并计算第二组测点的声压重构值与测量值之间的相对误差:And calculate the relative error between the sound pressure reconstruction value and the measured value of the second set of measuring points:

Figure BDA00035088299300001011
Figure BDA00035088299300001011

其中,||·||2为向量的2-范数。where ||·|| 2 is the 2-norm of the vector.

从1~Jmax遍历所有的J,利用式(11)~式(18),计算相对误差ε,将ε最小值对应的展开项数确定为最优展开项数JoptTraverse all J from 1 to J max , use equations (11) to (18) to calculate the relative error ε, and determine the number of expansion terms corresponding to the minimum value of ε as the optimal number of expansion terms J opt .

步骤4,重构声源的直接辐射声场。Step 4, reconstruct the direct radiation sound field of the sound source.

设定基函数展开项数为Jopt,根据式(2),全息测量面采集的声压值可以表示为如下矩阵形式:Set the number of expansion terms of the basis function as J opt , according to formula (2), the sound pressure value collected by the holographic measurement surface can be expressed as the following matrix form:

Figure BDA0003508829930000111
Figure BDA0003508829930000111

对式(19)求伪逆以求解系数列向量

Figure BDA0003508829930000112
Pseudo-inverse equation (19) to solve for the column vector of coefficients
Figure BDA0003508829930000112

Figure BDA0003508829930000113
Figure BDA0003508829930000113

从而,可得声压重构面上声源直接辐射声压的重构值:Therefore, the reconstructed value of the sound pressure directly radiated by the sound source on the sound pressure reconstruction surface can be obtained:

Figure BDA0003508829930000114
Figure BDA0003508829930000114

其中,

Figure BDA0003508829930000115
为声压重构点坐标,s=1,2,…,S,S为重构点数目;
Figure BDA0003508829930000116
为自由空间球面波基函数在重构点
Figure BDA0003508829930000117
的展开项组成的矩阵:in,
Figure BDA0003508829930000115
is the sound pressure reconstruction point coordinates, s=1,2,...,S, S is the number of reconstruction points;
Figure BDA0003508829930000116
for the free-space spherical wave basis function at the reconstruction point
Figure BDA0003508829930000117
A matrix of expanded terms of :

Figure BDA0003508829930000118
Figure BDA0003508829930000118

实施例:脉动球声源和平面边界的布置如图4所示,其中,边界位于z=0平面,声阻抗率Z0=2+3i;脉动球的半径a=0.05m,其几何中心O1的坐标

Figure BDA0003508829930000121
表面质点径向振动速度V0=0.01m/s,频率f=3000Hz;使用平面水听器阵列进行声压全息测量,阵列面与x-轴垂直,其几何中心与球心O1的连线垂直于阵列面,距离球心ds=0.15m;阵列孔径0.15m×0.15m,由6×6个测点组成,相邻测点间距为0.03m。为了便于描述和分析计算结果,对36个测点依次编号,如图5所示,其中,第1号测点坐标为(0.150m,-0.075m,0.375m),第36号测点坐标为(0.150m,0.075m,0.225m)。水介质密度为ρ0=1000kg/m3,声速为c=1500m/s。模拟水听器测量误差的影响,对测量值附加信噪比为30dB的高斯白噪声。Example: The arrangement of the pulsating sphere sound source and the plane boundary is shown in Figure 4, where the boundary is located on the z=0 plane, the acoustic impedance rate Z 0 =2+3i; the radius of the pulsating sphere a=0.05m, its geometric center O 1 's coordinates
Figure BDA0003508829930000121
Surface particle radial vibration velocity V 0 =0.01m/s, frequency f = 3000Hz; sound pressure holographic measurement using a planar hydrophone array, the array surface is perpendicular to the x-axis, and the line connecting its geometric center and the center of the sphere O 1 Vertical to the array surface, the distance from the center of the sphere is d s =0.15m; the array aperture is 0.15m×0.15m, consisting of 6×6 measuring points, and the distance between adjacent measuring points is 0.03m. In order to facilitate the description and analysis of the calculation results, the 36 measuring points are numbered in sequence, as shown in Figure 5, where the coordinates of the No. 1 measuring point are (0.150m, -0.075m, 0.375m), and the coordinates of the No. 36 measuring point are (0.150m, 0.075m, 0.225m). The density of the water medium is ρ 0 =1000kg/m 3 , and the speed of sound is c=1500m/s. The influence of the measurement error of the hydrophone is simulated, and the Gaussian white noise with a signal-to-noise ratio of 30dB is added to the measurement value.

图6所示为各测点处的无量纲声压幅值|p/ρ0cV0|的分布,包括半空间总声压值、声源直接辐射声压的重构值和声源直接辐射声压的真实值。观察图6发现,声源直接辐射声压的重构值与真实值能够很好地吻合。结果表明,本发明能够实现半开放空间中声源直接辐射声场的重构。Figure 6 shows the distribution of the dimensionless sound pressure amplitude |p/ρ 0 cV 0 | at each measuring point, including the half-space total sound pressure value, the reconstructed value of the sound pressure directly radiated by the sound source, and the direct sound source radiation True value of sound pressure. Observing Figure 6, it is found that the reconstructed value of the sound pressure directly radiated by the sound source is in good agreement with the real value. The results show that the invention can realize the reconstruction of the sound field directly radiated by the sound source in the semi-open space.

本说明书实施例所述的内容仅仅是对发明构思的实现形式的案例之一。本发明的保护范围包含但不限于实施例所陈述的具体形式和参数,也包含本领域技术人员根据本发明构思所能够想到的同等技术手段。The content described in the embodiments of this specification is only one example of the implementation form of the inventive concept. The protection scope of the present invention includes, but is not limited to, the specific forms and parameters stated in the embodiments, and also includes equivalent technical means that can be conceived by those skilled in the art according to the inventive concept.

Claims (2)

1.半开放空间中重构声源直接辐射声场的方法,其特征在于:包含如下步骤:1. the method for reconstructing the direct radiation sound field of a sound source in a semi-open space, is characterized in that: comprise the following steps: S1.建立以半空间球面波基函数的线性叠加表述声源直接辐射与边界反射声贡献的总声压场的数学模型;以声源几何中心O1在边界上的投影O为原点建立全局坐标系,O1的全局坐标记为
Figure FDA0003508829920000015
hs为O1到边界的距离;O1关于边界的镜像点记为O2;通过对全局坐标系平移,以O1和O2分别为原点建立局部坐标系,场点x在两局部坐标系中的坐标分别记为x1≡(r111)和x2≡(r222),三者之间满足如下关系:
S1. Establish a mathematical model that expresses the total sound pressure field contributed by the direct radiation of the sound source and the sound reflected by the boundary by the linear superposition of the half-space spherical wave basis functions; establish the global coordinate with the projection O of the geometric center O 1 of the sound source on the boundary as the origin system, the global coordinates of O 1 are marked as
Figure FDA0003508829920000015
h s is the distance from O 1 to the boundary; the mirror point of O 1 about the boundary is denoted as O 2 ; by translating the global coordinate system, a local coordinate system is established with O 1 and O 2 as the origin respectively, and the field point x is at the two local coordinates The coordinates in the system are respectively denoted as x 1 ≡(r 1 , θ 1 , φ 1 ) and x 2 ≡(r 2 , θ 2 , φ 2 ), and the following relations are satisfied between the three:
x1=x-hsez,x2=x+hsez (1)x 1 =xh s e z , x 2 =x+h s e z (1) 其中,ez为z-向单位向量;Among them, e z is the z-direction unit vector; 对于稳态声场,场点x处的半空间总声压phalf(x;ω)可以表述为有限项半空间球面波基函数的线性叠加:For a steady-state sound field, the half-space total sound pressure p half (x; ω) at field point x can be expressed as a linear superposition of finite-term half-space spherical wave basis functions:
Figure FDA0003508829920000011
Figure FDA0003508829920000011
其中,ω为声波角频率;ψjhalf(x;ω)为半空间球面波基函数;cj(ω)为基函数展开项系数;j为展开项序数,J为展开项项数;半空间球面波基函数ψjhalf(x;ω)的表达式为:Among them, ω is the angular frequency of the sound wave; ψ jhalf (x; ω) is the half-space spherical wave basis function; c j (ω) is the basis function expansion term coefficient; j is the expansion term ordinal number, J is the expansion term number; The expression of the spherical wave basis function ψ jhalf (x; ω) is: ψjhalf(x;ω)=ψj(x|x-hsez;ω)+ψj(x|x+hsez;ω)+ξj(x|x+hsez;ω) (3)ψ jhalf (x; ω)=ψ j (x|xh s e z ; ω)+ψ j (x|x+h s e z ; ω)+ξ j (x|x+h s e z ;ω) (3) 其中,ψj(x|x-hsez;ω)和ψj(x|x+hsez;ω)分别为表述声源及其镜像虚源直接辐射声的第j项自由空间球面波基函数;在球面坐标系中,ψj的表达式为:Among them, ψ j (x|xh s e z ; ω) and ψ j (x|x+h s e z ; ω) are the j-th free-space spherical waves representing the direct radiation sound of the sound source and its mirror image virtual source, respectively Basis function; in spherical coordinate system, the expression of ψ j is:
Figure FDA0003508829920000012
Figure FDA0003508829920000012
其中,
Figure FDA0003508829920000013
为第一类球汉克尔函数,k=ω/c为声波波数,c为声速;
Figure FDA0003508829920000014
为球谐函数;在式(2)~式(4)中,整数n,l和j满足关系式j=n2+n+l+1,其中,-n≤l≤n,0≤n≤N,N为n的截断值;在计算式(3)时,其右边的前两项分别代入局部坐标x1和x2进行计算;ξj(x|x+hsez;ω)表述边界声,其表达式为:
in,
Figure FDA0003508829920000013
is the first kind of spherical Hankel function, k=ω/c is the wave number of the sound wave, and c is the speed of sound;
Figure FDA0003508829920000014
is a spherical harmonic function; in equations (2) to (4), the integers n, l and j satisfy the relational expression j=n 2 +n+l+1, where -n≤l≤n, 0≤n≤ N, N is the truncation value of n; when calculating formula (3), the first two items on the right side are respectively substituted into the local coordinates x 1 and x 2 for calculation; ξ j (x|x+h s e z ; ω) expression Boundary sound, its expression is:
Figure FDA0003508829920000021
Figure FDA0003508829920000021
其中,in,
Figure FDA0003508829920000022
Figure FDA0003508829920000022
Figure FDA0003508829920000023
Figure FDA0003508829920000023
以及as well as
Figure FDA0003508829920000024
Figure FDA0003508829920000024
在式(5)~式(8)中,Rp2;ω)、F(w)和w分别为声压反射系数、边界损失因子(BoundaryLoss Factor)和数值间距(Numerical Distance);局部坐标r1和r2分别为声源几何中心和镜像虚源几何中心到场点的距离;θ2为声波入射角,为场点和虚源几何中心的连线与z-轴正方向的夹角;
Figure FDA0003508829920000025
复角μp为:
In equations (5) to (8), R p2 ; ω), F(w) and w are the sound pressure reflection coefficient, the boundary loss factor (Boundary Loss Factor) and the numerical distance (Numerical Distance), respectively; The coordinates r 1 and r 2 are the distances from the geometric center of the sound source and the geometric center of the image virtual source to the field point, respectively; θ 2 is the incident angle of the sound wave, which is the angle between the line connecting the field point and the virtual source geometric center and the positive direction of the z-axis ;
Figure FDA0003508829920000025
The complex angle μ p is:
Figure FDA0003508829920000026
Figure FDA0003508829920000026
其中,β为归一化的边界声导纳,where β is the normalized boundary acoustic admittance,
Figure FDA0003508829920000027
Figure FDA0003508829920000027
其中,Z为边界声阻抗率,Z0为归一化的边界声阻抗率,ρ0为流体介质密度;本方法的实施假定声阻抗率Z0为已知量,Z0可以根据声阻抗的原位测量方法获取;Among them, Z is the boundary acoustic impedance ratio, Z 0 is the normalized boundary acoustic impedance ratio, and ρ 0 is the density of the fluid medium; the implementation of this method assumes that the acoustic impedance ratio Z 0 is a known quantity, and Z 0 can be based on the acoustic impedance. In situ measurement method acquisition; S2.在声源近场布置全息测量面进行声压全息测量;S2. Arrange the holographic measurement surface in the near field of the sound source for sound pressure holographic measurement; 在声源近场布置一组声压传感器,形成声压全息测量面,测量声源直接辐射声与边界反射声共同贡献的总声压分布;Arrange a group of sound pressure sensors in the near field of the sound source to form a sound pressure holographic measurement surface, and measure the total sound pressure distribution contributed by the direct radiation sound of the sound source and the boundary reflection sound; S3.以部分测点的全息测量值作为输入,重构其余测点的声压值,以声压重构误差为最小为原则确定最优基函数展开项数;S3. Take the holographic measurement values of some measuring points as input, reconstruct the sound pressure values of the remaining measuring points, and determine the optimal number of expansion terms of the basis function based on the principle of the sound pressure reconstruction error being the smallest; 将全息测量面上的测点坐标记为
Figure FDA0003508829920000031
M为声压测点数目;按照隔点取点的方式,将声压测点分为两组;第一组测点坐标记为
Figure FDA0003508829920000032
Figure FDA0003508829920000033
第二组测点坐标记为
Figure FDA0003508829920000034
Figure FDA0003508829920000035
其中,
Figure FDA0003508829920000036
Figure FDA0003508829920000037
分别表示向上取整和向下取整;
Mark the coordinates of the measuring point on the holographic measuring surface as
Figure FDA0003508829920000031
M is the number of sound pressure measurement points; the sound pressure measurement points are divided into two groups according to the method of taking points at intervals; the coordinates of the first group of measurement points are marked as
Figure FDA0003508829920000032
Figure FDA0003508829920000033
The second set of measuring point coordinates are marked as
Figure FDA0003508829920000034
Figure FDA0003508829920000035
in,
Figure FDA0003508829920000036
and
Figure FDA0003508829920000037
Represent round up and round down respectively;
设定基函数展开项数J可能取值的上限为Jmax,即1≤J≤Jmax;对于该范围内的任意J,根据式(2),全息测量面的第一组测点采集的声压值可以表示为如下矩阵形式:Set the upper limit of the possible value of the basis function expansion term J to J max , that is, 1≤J≤J max ; for any J within this range, according to formula (2), the first set of measuring points on the holographic measurement surface The sound pressure value can be expressed in the following matrix form:
Figure FDA0003508829920000038
Figure FDA0003508829920000038
其中,
Figure FDA0003508829920000039
为半空间总声压测量值组成的列向量:
in,
Figure FDA0003508829920000039
Column vector of half-space total sound pressure measurements:
Figure FDA00035088299200000310
Figure FDA00035088299200000310
其中,上标T为向量转置;{C(ω)}J×1为半空间球面波基函数系数组成的列向量:Among them, the superscript T is the vector transpose; {C(ω)} J×1 is the column vector composed of the half-space spherical wave basis function coefficients:
Figure FDA00035088299200000311
Figure FDA00035088299200000311
Figure FDA00035088299200000312
为半空间球面波基函数在各测点的展开项组成的矩阵:
Figure FDA00035088299200000312
is the matrix composed of the expansion terms of the half-space spherical wave basis function at each measuring point:
Figure FDA00035088299200000313
Figure FDA00035088299200000313
对式(11)求解,可得系数列向量:Solving equation (11), the coefficient column vector can be obtained:
Figure FDA00035088299200000314
Figure FDA00035088299200000314
其中,上标
Figure FDA0003508829920000041
表示对矩阵求伪逆,
Among them, the superscript
Figure FDA0003508829920000041
represents the pseudo-inverse of the matrix,
Figure FDA0003508829920000042
Figure FDA0003508829920000042
其中,上标H为矩阵的共轭转置;Among them, the superscript H is the conjugate transpose of the matrix; 当系数列向量{C(ω)}J×1确定之后,可以进一步重构第二组测点的声压:After the coefficient column vector {C(ω)} J×1 is determined, the sound pressure of the second group of measuring points can be further reconstructed:
Figure FDA0003508829920000043
Figure FDA0003508829920000043
并计算第二组测点的声压重构值与测量值之间的相对误差:And calculate the relative error between the sound pressure reconstruction value and the measured value of the second set of measuring points:
Figure FDA0003508829920000044
Figure FDA0003508829920000044
其中,||·||2为向量的2-范数;Among them, ||·|| 2 is the 2-norm of the vector; 从1~Jmax遍历所有的J,利用式(11)~式(18),计算相对误差ε,将ε最小值对应的展开项数确定为最优展开项数JoptTraverse all J from 1 to J max , use equations (11) to (18) to calculate the relative error ε, and determine the number of expansion terms corresponding to the minimum value of ε as the optimal number of expansion terms J opt ; S4.在最优展开项数条件下求解半空间球面波基函数系数,获取表述声源直接辐射声场的自由空间球面波基函数系数,实现声源直接辐射声场的重构;S4. Solve the half-space spherical wave basis function coefficients under the condition of the optimal expansion term, obtain the free-space spherical wave basis function coefficients representing the sound field directly radiated by the sound source, and realize the reconstruction of the sound field directly radiated by the sound source; 设定基函数展开项数为Jopt,根据式(2),全息测量面采集的声压值可以表示为如下矩阵形式:The number of expansion terms of the basis function is set as J opt , according to formula (2), the sound pressure value collected by the holographic measurement surface can be expressed as the following matrix form:
Figure FDA0003508829920000045
Figure FDA0003508829920000045
对式(19)求伪逆以求解系数列向量
Figure FDA0003508829920000046
Pseudo-inverse equation (19) to solve for the column vector of coefficients
Figure FDA0003508829920000046
Figure FDA0003508829920000047
Figure FDA0003508829920000047
从而,可得声压重构面上声源直接辐射声压的重构值:Therefore, the reconstructed value of the sound pressure directly radiated by the sound source on the sound pressure reconstruction surface can be obtained:
Figure FDA0003508829920000048
Figure FDA0003508829920000048
其中,
Figure FDA0003508829920000049
为声压重构点坐标,s=1,2,…,S,S为重构点数目;
Figure FDA00035088299200000410
为自由空间球面波基函数在重构点
Figure FDA00035088299200000411
的展开项组成的矩阵:
in,
Figure FDA0003508829920000049
is the sound pressure reconstruction point coordinates, s=1,2,...,S, S is the number of reconstruction points;
Figure FDA00035088299200000410
for the free-space spherical wave basis function at the reconstruction point
Figure FDA00035088299200000411
A matrix of expanded terms of :
Figure FDA0003508829920000051
Figure FDA0003508829920000051
2.如权利要求1所述的半开放空间中重构声源直接辐射声场的方法,其特征在于:步骤S2所述的声压传感器,根据声源所在流体介质的不同,采用传声器、水听器或其它类型的传感器。2. The method for reconstructing the direct radiation sound field of a sound source in a semi-open space as claimed in claim 1, wherein the sound pressure sensor in step S2 adopts a microphone, a hydrophone according to the difference of the fluid medium where the sound source is located. device or other type of sensor.
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