CN112287516B - Method and system for calculating electromagnetic scattering field of vortex beam in Debye dispersive plasma sphere - Google Patents

Method and system for calculating electromagnetic scattering field of vortex beam in Debye dispersive plasma sphere Download PDF

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CN112287516B
CN112287516B CN202011004255.7A CN202011004255A CN112287516B CN 112287516 B CN112287516 B CN 112287516B CN 202011004255 A CN202011004255 A CN 202011004255A CN 112287516 B CN112287516 B CN 112287516B
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刘松华
孙明浩
郭立新
朱从宽
史晨鸽
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Abstract

本发明属于涡旋电磁波散射场仿真计算领域,公开了一种Debye色散等离子体球的涡旋波束电磁散射场计算方法及系统,本发明实现过程:(1)利用复源点方法,得到高阶厄米‑高斯波束矢势的球矢量波函数展开式;(2)拉盖尔‑高斯涡旋波束的球矢量波函数展开式;(3)色散等离子体球的Mie散射系数;(4)拉盖尔‑高斯涡旋波束内场和散射场的球矢量波函数展开式;(5)结合边界条件和Mie散射系数可得散射场展开系数;(6)通过散射场展开系数和散射相函数得到远场雷达散射截面;(7)改变涡旋波频率,重复(1)~(6)可分析等离子体球的色散效应。本发明通过对涡旋波束电磁散射场的广义洛伦兹Mie解析求解,得到色散等离子体球的散射截面,弥补了行业空白。

Figure 202011004255

The invention belongs to the field of vortex electromagnetic wave scattering field simulation calculation, and discloses a method and system for calculating a vortex beam electromagnetic scattering field of a Debye dispersion plasma sphere. Spherical vector wave function expansion of Hermit-Gaussian beam vector potential; (2) Spherical vector wave function expansion of Laguerre-Gaussian vortex beam; (3) Mie scattering coefficient of dispersive plasma sphere; (4) Laguerre-Gaussian vortex beam expansion Spherical vector wave function expansions of Gal-Gaussian vortex beam inner and scattered fields; (5) Combining boundary conditions and Mie scattering coefficients to obtain scattering field expansion coefficients; (6) Obtaining scattering field expansion coefficients and scattering phase functions Far-field radar scattering cross section; (7) Change the frequency of the vortex wave and repeat (1) to (6) to analyze the dispersion effect of the plasma sphere. The invention obtains the scattering cross section of the dispersive plasma sphere through the analytical solution of the generalized Lorentz Mie of the electromagnetic scattering field of the vortex beam, which fills the gap in the industry.

Figure 202011004255

Description

Debye色散等离子体球的涡旋波束电磁散射场计算方法及 系统Method and system for calculating electromagnetic scattering field of vortex beam in Debye dispersive plasma sphere

技术领域technical field

本发明属于涡旋电磁波检测技术领域,尤其涉及一种Debye色散等离子体球 的涡旋波束电磁散射场计算方法及系统。The invention belongs to the technical field of vortex electromagnetic wave detection, and in particular relates to a method and system for calculating a vortex beam electromagnetic scattering field of a Debye dispersion plasma sphere.

背景技术Background technique

临近空间高超声速飞行器再入过程中会与周围大气剧烈摩擦,导致飞行器周围温度上升,压力增大。在高温高压下,不同的空气组分之间会发生复杂的化学 反应,出现电离现象,进而在飞行器周围形成由自由电子、各种离子和中性粒 子组成的等离子体绕流。目标表面存在的等离子体严重影响了雷达对飞行目标 的预警、探测以及监测站与飞行器之间的通信质量,甚至导致通信上的“黑障” 现象,目标表面等离子体的存在严重制约了临近空间飞行器的发展。此外,等 离子体广泛存在于空间电离层、微波实验室等环境当中,也广泛应用于环境目 标的隐身技术,所以研究等离子体目标的电磁散射特性具有重要意义。During the re-entry of a hypersonic vehicle in near space, it will rub violently with the surrounding atmosphere, causing the temperature and pressure around the vehicle to rise. Under high temperature and high pressure, complex chemical reactions will occur between different air components, and ionization will occur, and then a plasma flow composed of free electrons, various ions and neutral particles will be formed around the aircraft. Plasma on the surface of the target seriously affects the radar's early warning and detection of flying targets, as well as the quality of communication between the monitoring station and the aircraft, and even leads to the "black barrier" phenomenon in communication. The existence of plasma on the target surface seriously restricts the near space. The development of aircraft. In addition, plasma widely exists in space ionosphere, microwave laboratory and other environments, and is also widely used in stealth technology of environmental targets, so it is of great significance to study the electromagnetic scattering characteristics of plasma targets.

以往对等离子体目标电磁散射特性的研究大多基于平面波入射,入射波类型为涡旋电磁波的报道还较少。涡旋波束的研究最早起源于光学领域,并且目前主 要的研究仍集中于光学领域。涡旋电磁波即为携带有轨道角动量的电磁波,由于 其相位波前呈螺旋状分布,相比于传统电磁波有着更高维度的信息调制自由度, 在无线通信、目标探测及成像等领域具有很大的应用潜力。在涡旋电磁波的照 射下,雷达波束在不同目标处形成具有差异性分布的辐射场激励,目标散射特 性与传统平面波照射下的目标特性有较大的不同。不同轨道角动量本征态之间 相互正交,并且理论上可以张成一个无穷维的希尔伯特空间。每一个轨道角动 量本征态都用一个特定的整数来表示,即拓扑荷数,其他任意一个状态均可以 表示为本征态的线性叠加。这一性质表明,具有不同模式数的涡旋电磁波在物 理上可以分离,为其在无线通信,雷达探测等领域的应用奠定了物理和数学基 础。此外,传统平面电磁波只存在一个强度峰值且波前分布平滑,不存在角向 相位的变化。涡旋电磁波由于携带有轨道角动量,使其与传统电磁波存在着明 显的差异。首先,涡旋电磁波的波束强度分布为特殊的空心环状分布,其传输 轴上存在强度为零的相位奇点。其次,涡旋电磁波携带有一种新的空间自由度 —轨道角动量,使其在大容量通信以及高性能雷达探测等领域具有巨大的应用 前景。The previous studies on the electromagnetic scattering characteristics of plasma targets are mostly based on the incident plane wave, and there are few reports that the incident wave type is vortex electromagnetic wave. The study of vortex beams originated in the field of optics, and the main research is still in the field of optics. Vortex electromagnetic waves are electromagnetic waves that carry orbital angular momentum. Compared with traditional electromagnetic waves, they have a higher degree of freedom of information modulation due to their helical phase wavefront distribution. great application potential. Under the irradiation of vortex electromagnetic waves, the radar beam forms radiation field excitations with different distributions at different targets, and the target scattering characteristics are quite different from those under the traditional plane wave irradiation. The eigenstates of different orbital angular momentum are orthogonal to each other, and can theoretically be expanded into an infinite-dimensional Hilbert space. Each orbital angular momentum eigenstate is represented by a specific integer, namely the topological charge, and any other state can be represented as a linear superposition of eigenstates. This property shows that vortex electromagnetic waves with different mode numbers can be physically separated, which lays a physical and mathematical foundation for their applications in wireless communication, radar detection and other fields. In addition, the traditional plane electromagnetic wave has only one intensity peak and the wavefront distribution is smooth, and there is no angular phase change. Vortex electromagnetic waves are significantly different from traditional electromagnetic waves because they carry orbital angular momentum. First, the beam intensity distribution of the vortex electromagnetic wave is a special hollow annular distribution, and there is a phase singularity with zero intensity on its transmission axis. Secondly, the vortex electromagnetic wave carries a new space degree of freedom—orbital angular momentum, which makes it have great application prospects in the fields of large-capacity communication and high-performance radar detection.

涡旋电磁波照射等离子体目标散射特性的研究有望解决高超声速飞行器目 标雷达探测困难的问题,并为隐身飞行器的反隐身研究提供了新的选择。前人 研究了涡旋电磁波束对等离子体球的散射特性,然而并未考虑等离子体球本身 的色散特性。本发明基于Debye色散模型,提供了一种计算色散等离子体球雷 达散射截面的方法,弥补了行业空白。The research on the scattering characteristics of plasma targets irradiated by vortex electromagnetic waves is expected to solve the difficult problem of radar detection of hypersonic aircraft targets, and provide a new option for the anti-stealth research of stealth aircraft. Previous studies have studied the scattering characteristics of vortex electromagnetic beams to plasma spheres, but the dispersion characteristics of plasma spheres themselves have not been considered. Based on the Debye dispersion model, the invention provides a method for calculating the scattering cross section of the dispersion plasma sphere radar, which fills the gap in the industry.

发明内容SUMMARY OF THE INVENTION

针对现有技术存在的问题,本发明提供了一种Debye色散等离子体球的涡 旋波束电磁散射场计算方法及系统。Aiming at the problems existing in the prior art, the present invention provides a method and system for calculating the electromagnetic scattering field of the vortex beam of the Debye dispersion plasma sphere.

本发明是这样实现的,一种Debye色散等离子体球的涡旋波束电磁散射场 计算方法,所述涡旋波束电磁散射场计算方法包括:The present invention is realized like this, a kind of vortex beam electromagnetic scattered field calculation method of Debye dispersion plasma sphere, described vortex beam electromagnetic scattered field calculation method comprises:

步骤一,利用复源点方法,采用复源点多极子叠加的方法描述高阶波束, 得到高阶厄米-高斯波束矢势的球矢量波函数展开式;Step 1, using the complex source point method and the complex source point multipole superposition method to describe the high-order beam, and obtaining the spherical vector wave function expansion of the high-order Hermitian-Gaussian beam vector potential;

步骤二,通过拉盖尔-高斯波束与厄米-高斯波束模之间的数学关系,得到拉 盖尔-高斯涡旋波束的标量波函数展开,将其代入携带有轨道角动量的拉盖尔- 高斯涡旋波束的矢势表达式,进而可得到拉盖尔-高斯涡旋波束的球矢量波函数 展开式;Step 2, through the mathematical relationship between the Laguerre-Gaussian beam and the Hermitian-Gaussian beam mode, the scalar wave function expansion of the Laguerre-Gaussian vortex beam is obtained, and it is substituted into the Laguerre carrying the orbital angular momentum. - The vector potential expression of the Gaussian vortex beam, and then the spherical vector wave function expansion of the Laguerre-Gaussian vortex beam can be obtained;

步骤三,结合Debye色散模型下介电参数表达式、折射率与介电参数关系 式以及Mie理论,可以得到色散等离子体球的Mie散射系数;Step 3, in conjunction with the dielectric parameter expression, the relationship between the refractive index and the dielectric parameter and the Mie theory under the Debye dispersion model, the Mie scattering coefficient of the dispersive plasma sphere can be obtained;

步骤四,通过拉盖尔-高斯涡旋波束矢势的球矢量波函数展开式进一步处理 可得到电磁场入射表达式,根据同样方法也可以获得拉盖尔-高斯涡旋波束内场 和散射场的球矢量波函数展开式;In step 4, the electromagnetic field incident expression can be obtained by further processing the spherical vector wave function expansion of the Laguerre-Gaussian vortex beam vector potential. Ball vector wave function expansion;

步骤五,在介质球表面根据电场磁场满足连续性边界条件原理,结合步骤 三所得色散等离子体球的Mie散射系数,并将入射场、内场和散射场的球矢量 波函数展开式代入边界条件,就可以得到拉盖尔-高斯涡旋波束入射下的散射场 展开系数;Step 5: On the surface of the dielectric sphere, according to the principle that the electric field and magnetic field satisfy the continuity boundary condition, combine the Mie scattering coefficient of the dispersive plasma sphere obtained in step 3, and substitute the spherical vector wave function expansions of the incident field, inner field and scattering field into the boundary conditions , the expansion coefficient of the scattered field under the incidence of the Laguerre-Gaussian vortex beam can be obtained;

步骤六,通过散射场展开系数和散射相函数得到远场雷达散射截面;Step 6: Obtain the far-field radar scattering cross section through the scattering field expansion coefficient and the scattering phase function;

步骤七,改变拉盖尔-高斯涡旋波束的频率,重复步骤一~步骤六,可得不同 频率下色散等离子体球的电磁散射场,进而可以分析不同频率雷达波束照射下 等离子体球色散效应对涡旋波束电磁散射特性的影响。Step 7: Change the frequency of the Laguerre-Gaussian vortex beam, and repeat steps 1 to 6 to obtain the electromagnetic scattering field of the dispersive plasma sphere at different frequencies, and then analyze the dispersion effect of the plasma sphere under the irradiation of radar beams of different frequencies. Effects on electromagnetic scattering properties of vortex beams.

进一步,所述利用复源点方法,采用复源点多极子叠加的方法描述高阶波 束,得到高阶厄米-高斯波束矢势的球矢量波函数展开式包括:利用复源点方法, 采用复源点多极子叠加的方法描述高阶波束,得到高阶厄米-高斯波束矢势的球 矢量波函数的展开式为:Further, using the complex source point method to describe the high-order beam by using the complex source point multipole superposition method to obtain the spherical vector wave function expansion of the high-order Hermitian-Gaussian beam vector potential includes: using the complex source point method, The high-order beam is described by the method of complex source point multipole superposition, and the expansion of the spherical vector wave function of the high-order Hermitian-Gaussian beam vector potential is obtained as:

Figure RE-GDA0002806778480000031
Figure RE-GDA0002806778480000031

式中下标u,v分别表示厄米-高斯波束沿x、y方向变化的模阶数;

Figure BDA0002695357810000032
为第一类球矢量波函数,系数α(1)(u,v,n,m)、β(1)(u,v,n,m)表示HG波束的球矢量 波函数展开系数,其数学表达式为:where the subscripts u and v represent the modulo order of the Hermitian-Gaussian beam along the x and y directions, respectively;
Figure BDA0002695357810000032
is the first type of spherical vector wave function, the coefficients α (1) (u,v,n,m), β (1) (u,v,n,m) represent the expansion coefficient of the spherical vector wave function of the HG beam, and its mathematical The expression is:

Figure RE-GDA0002806778480000033
Figure RE-GDA0002806778480000033

Figure BDA0002695357810000034
Figure BDA0002695357810000034

其中

Figure BDA0002695357810000035
满足以下迭代关系:in
Figure BDA0002695357810000035
The following iterative relations are satisfied:

Figure BDA0002695357810000041
Figure BDA0002695357810000041

Figure BDA0002695357810000042
Figure BDA0002695357810000042

当u=v=0时,高阶厄米-高斯波束退化成高斯基模,

Figure BDA0002695357810000043
表达式如下:When u=v=0, the high-order Hermitian-Gaussian beam degenerates into a Gaussian fundamental mode,
Figure BDA0002695357810000043
The expression is as follows:

Figure BDA0002695357810000044
Figure BDA0002695357810000044

其中参数具体为:

Figure BDA0002695357810000045
cosθ0=(z0+ib)/r0
Figure BDA0002695357810000046
The parameters are specifically:
Figure BDA0002695357810000045
cosθ 0 =(z 0 +ib)/r 0 ,
Figure BDA0002695357810000046

进一步,所述通过拉盖尔-高斯波束与厄米-高斯波束模之间的数学关系,可 以得到拉盖尔-高斯涡旋波束的标量波函数展开,将其代入携带有轨道角动量的 拉盖尔-高斯涡旋波束的矢势表达式,进而可得到拉盖尔-高斯涡旋波束的球矢量 波函数展开式包括:Further, through the mathematical relationship between the Laguerre-Gaussian beam and the Hermitian-Gaussian beam mode, the scalar wave function expansion of the Laguerre-Gaussian vortex beam can be obtained, and it is substituted into the Laguerre-Gaussian vortex beam carrying the orbital angular momentum. The vector potential expression of the Gale-Gaussian vortex beam, and then the spherical vector wave function expansion of the Laguerre-Gaussian vortex beam can be obtained, including:

(1)拉盖尔-高斯涡旋波束为傍轴波动方程在圆柱坐标系下的近似解,傍轴 波动方程在圆柱坐标系

Figure BDA0002695357810000047
下的表达式写作:(1) The Laguerre-Gaussian vortex beam is an approximate solution of the paraxial wave equation in the cylindrical coordinate system, and the paraxial wave equation in the cylindrical coordinate system
Figure BDA0002695357810000047
The following expression is written:

Figure BDA0002695357810000048
Figure BDA0002695357810000048

设方程的解为:Let the solution of the equation be:

Figure BDA0002695357810000049
Figure BDA0002695357810000049

其中w(z)表示波束在z处的波束宽度,p(z)表示复相移,与波束的传输相关, q(z)是复波束的参数,被用于描述波束的强度随着与传输轴距离的高斯变化, 相位波前曲率在近轴为球面;具体表达式为

Figure BDA00026953578100000410
p(z)=iln(q0+z), q(z)=q0+z,
Figure BDA00026953578100000411
表示共焦参数,
Figure BDA00026953578100000412
为方位角,
Figure BDA00026953578100000413
where w(z) is the beam width at z, p(z) is the complex phase shift, which is related to the transmission of the beam, and q(z) is the parameter of the complex beam, which is used to describe the intensity of the beam with the transmission The Gaussian variation of the axial distance, the phase wavefront curvature is spherical at the paraxial; the specific expression is
Figure BDA00026953578100000410
p(z)=iln(q 0 +z), q(z)=q 0 +z,
Figure BDA00026953578100000411
is the confocal parameter,
Figure BDA00026953578100000412
is the azimuth,
Figure BDA00026953578100000413

(2)将方程的解代入傍轴波动方程,利用分离变量法:(2) Substitute the solution of the equation into the paraxial wave equation, and use the separation of variables method:

g=M(ζ)Z(z);g=M(ζ)Z(z);

其中

Figure BDA0002695357810000051
得到如下方程组:in
Figure BDA0002695357810000051
The following equations are obtained:

Figure BDA0002695357810000052
Figure BDA0002695357810000052

Figure BDA0002695357810000053
Figure BDA0002695357810000053

其中

Figure BDA0002695357810000054
为伴随拉盖尔多项式,表示为:in
Figure BDA0002695357810000054
is the adjoint Laguerre polynomial, expressed as:

Figure BDA0002695357810000055
Figure BDA0002695357810000055

(3)将

Figure BDA0002695357810000056
和Z(z)的表达式代入到M(ζ)和g的表达式中并且与ψ进行对 比,得到拉盖尔-高斯涡旋波束具体表达式:(3) will
Figure BDA0002695357810000056
The expressions of and Z(z) are substituted into the expressions of M(ζ) and g and compared with ψ to obtain the specific expression of the Laguerre-Gaussian vortex beam:

Figure BDA0002695357810000057
Figure BDA0002695357810000057

式中p,l分别表示拉盖尔-高斯涡旋波束的径向模阶数和拓扑荷数;where p and l represent the radial mode order and topological charge of the Laguerre-Gaussian vortex beam, respectively;

(4)对拉盖尔-高斯涡旋波束具体表达式进行归一化,得到:(4) Normalize the specific expression of Laguerre-Gaussian vortex beam to get:

Figure BDA0002695357810000058
Figure BDA0002695357810000058

当p=l=0时,拉盖尔-高斯涡旋波束就会退化到高斯波束入射情况,当束腰 半径w0→∞时,就会由高斯波束退化至平面波;When p=l=0, the Laguerre-Gaussian vortex beam will degenerate to the incident Gaussian beam, and when the beam waist radius w 0 →∞, it will degenerate from the Gaussian beam to the plane wave;

(5)携带有轨道角动量的拉盖尔-高斯涡旋波束的矢势表述为:(5) The vector potential of a Laguerre-Gaussian vortex beam carrying orbital angular momentum is expressed as:

Figure BDA0002695357810000059
Figure BDA0002695357810000059

其中:in:

Figure BDA0002695357810000061
Figure BDA0002695357810000061

式中

Figure BDA0002695357810000062
分别对应角度依赖关系中的
Figure BDA0002695357810000063
δ0l为狄拉克函数,根据拉盖 尔-高斯波束与厄米-高斯波束模之间的数学关系式,得到拉盖尔-高斯涡旋波束 的标量波函数展开,具体如下:in the formula
Figure BDA0002695357810000062
Corresponding to the angle dependencies in the
Figure BDA0002695357810000063
δ 0l is the Dirac function. According to the mathematical relationship between the Laguerre-Gaussian beam and the Hermitian-Gaussian beam mode, the scalar wave function expansion of the Laguerre-Gaussian vortex beam is obtained, as follows:

Figure BDA0002695357810000064
Figure BDA0002695357810000064

Figure BDA0002695357810000065
Figure BDA0002695357810000065

(6)将

Figure BDA0002695357810000066
Figure BDA0002695357810000067
的具体表达式代入到拉盖尔-高斯涡旋波束 矢势表达式当中,得到拉盖尔-高斯涡旋波束的球矢量波函数的展开系数 χ(1)(p,l,n,m)和κ(1)(p,l,n,m)的表达式如下:(6) will
Figure BDA0002695357810000066
and
Figure BDA0002695357810000067
Substitute the specific expression into the Laguerre-Gaussian vortex beam vector potential expression to obtain the expansion coefficient χ (1) (p,l,n,m) of the spherical vector wave function of the Laguerre-Gaussian vortex beam. and κ (1) (p,l,n,m) are expressed as:

Figure BDA0002695357810000068
Figure BDA0002695357810000068

Figure BDA0002695357810000071
Figure BDA0002695357810000071

那么拉盖尔-高斯涡旋波束矢势的球矢量波函数展开为:Then the spherical vector wave function of the Laguerre-Gaussian vortex beam vector potential expands as:

Figure RE-GDA0002806778480000072
Figure RE-GDA0002806778480000072

进一步,所述结合Debye色散模型下介电参数表达式、折射率与介电参数 关系式以及Mie理论,可以得到色散等离子体球的Mie散射系数;Further, the Mie scattering coefficient of the dispersive plasma sphere can be obtained in combination with the dielectric parameter expression, the refractive index and the dielectric parameter relational formula and the Mie theory under the Debye dispersion model;

(1)记an,bn为Mie理论中的散射系数,其具体表达式写作:(1) Denote a n , b n is the scattering coefficient in Mie theory, and its specific expression is written as:

Figure BDA0002695357810000073
Figure BDA0002695357810000073

其中

Figure BDA0002695357810000074
in
Figure BDA0002695357810000074

(2)基于Debye色散模型,色散等离子体球的介电参数表达式为:(2) Based on the Debye dispersion model, the dielectric parameter expression of the dispersive plasma sphere is:

Figure BDA0002695357810000075
μr=1。
Figure BDA0002695357810000075
μ r =1.

进一步,所述通过拉盖尔-高斯涡旋波束矢势的球矢量波函数展开式进一步 处理可得到电磁场入射表达式,根据同样方法也可以获得拉盖尔-高斯涡旋波束 内场和散射场的球矢量波函数展开式包括:Further, the electromagnetic field incident expression can be obtained by further processing the spherical vector wave function expansion of the Laguerre-Gaussian vortex beam vector potential, and the Laguerre-Gaussian vortex beam inner field and scattering field can also be obtained according to the same method. The spherical vector wave function expansion of includes:

(1)拉盖尔-高斯涡旋波束矢势的球矢量波函数开展式为:(1) The expansion of the spherical vector wave function of the Laguerre-Gaussian vortex beam vector potential is:

Figure RE-GDA0002806778480000076
Figure RE-GDA0002806778480000076

将上式代入:Substitute the above formula into:

Figure RE-GDA0002806778480000081
Figure RE-GDA0002806778480000081

得到传播方向为+z轴方向,电矢量为x方向极化的电磁场入射表达式:The electromagnetic field incident expression with the propagation direction as the +z-axis direction and the electric vector as the polarization in the x-direction is obtained:

Figure BDA0002695357810000082
Figure BDA0002695357810000082

(2)同理获得拉盖尔-高斯涡旋波束内场和散射场的球矢量波函数展开式。(2) In the same way, the spherical vector wave function expansions of the inner and scattered fields of the Laguerre-Gaussian vortex beam are obtained.

进一步,所述在介质球表面根据电场磁场满足连续性边界条件原理,结合 步骤(3)所得色散等离子体球的Mie散射系数,并将入射场、内场和散射场的 球矢量波函数展开式代入边界条件,就可以得到拉盖尔-高斯涡旋波束入射下的 散射场展开系数包括:Further, according to the principle that the electric field and the magnetic field satisfy the continuity boundary condition on the surface of the dielectric sphere, combined with the Mie scattering coefficient of the dispersive plasma sphere obtained in step (3), the spherical vector wave functions of the incident field, the inner field and the scattered field are expanded to the formula By substituting the boundary conditions, the expansion coefficients of the scattered field under the incidence of the Laguerre-Gaussian vortex beam can be obtained, including:

散射场展开系数为:The scattering field expansion coefficient is:

Figure BDA0002695357810000083
Figure BDA0002695357810000083

其中in

Figure BDA0002695357810000084
Figure BDA0002695357810000084

式中an,bn为Mie理论中的散射系数; where an and bn are the scattering coefficients in the Mie theory;

通过散射场展开系数和散射相函数得到远场雷达散射截面包括:The far-field radar scattering cross section obtained by the scattered field expansion coefficient and the scattered phase function includes:

远场雷达散射截面表达式如下所示:The far-field radar cross section expression is as follows:

Figure BDA0002695357810000085
Figure BDA0002695357810000085

式中

Figure BDA0002695357810000086
Figure BDA0002695357810000087
表示散射场的分量,具体表达式如下:in the formula
Figure BDA0002695357810000086
and
Figure BDA0002695357810000087
represents the component of the scattered field, and the specific expression is as follows:

Figure BDA0002695357810000091
Figure BDA0002695357810000091

其中散射相函数

Figure BDA0002695357810000092
Figure BDA0002695357810000093
具体为:where the scattering phase function
Figure BDA0002695357810000092
and
Figure BDA0002695357810000093
Specifically:

Figure BDA0002695357810000094
Figure BDA0002695357810000094

Figure BDA0002695357810000095
Figure BDA0002695357810000095

Figure BDA0002695357810000096
Figure BDA0002695357810000096

Figure BDA0002695357810000097
为连带勒让德多项式,有:
Figure BDA0002695357810000097
For the associated Legendre polynomial, we have:

Figure BDA0002695357810000098
Figure BDA0002695357810000098

其中:in:

Figure BDA0002695357810000099
Figure BDA0002695357810000099

本发明的另一目的在于提供一种实施所述涡旋波束电磁散射场计算方法的 涡旋波束电磁散射场计算系统,所述涡旋波束电磁散射场计算系统包括:Another object of the present invention is to provide a vortex beam electromagnetic scattered field calculation system for implementing the vortex beam electromagnetic scattered field calculation method, and the vortex beam electromagnetic scattered field calculation system includes:

高阶厄米-高斯波束矢势的球矢量波函数展开式获取模块,用于利用复源点 方法,采用复源点多极子叠加的方法描述高阶波束,得到高阶厄米-高斯波束矢 势的球矢量波函数展开式;The spherical vector wave function expansion acquisition module of the high-order Hermitian-Gaussian beam vector potential is used to describe high-order beams by using the complex source point method and the method of complex source point multipole superposition to obtain high-order Hermitian-Gaussian beams The spherical vector wave function expansion of the vector potential;

拉盖尔-高斯涡旋波束的球矢量波函数展开式获取模块,用于通过拉盖尔- 高斯波束与厄米-高斯波束模之间的数学关系,可以得到拉盖尔-高斯涡旋波束的 标量波函数展开,将其代入携带有轨道角动量的拉盖尔-高斯涡旋波束的矢势表 达式,进而可得到拉盖尔-高斯涡旋波束的球矢量波函数展开式;The spherical vector wave function expansion acquisition module of the Laguerre-Gaussian vortex beam, which is used to obtain the Laguerre-Gaussian vortex beam through the mathematical relationship between the Laguerre-Gaussian beam and the Hermitian-Gaussian beam mode The scalar wave function expansion of , and substitute it into the vector potential expression of the Laguerre-Gaussian vortex beam carrying the orbital angular momentum, and then the spherical vector wave function expansion of the Laguerre-Gaussian vortex beam can be obtained;

Mie散射系数获取模块,用于结合Debye色散模型下介电参数表达式、折 射率与介电参数关系式以及Mie理论,可以得到色散等离子体球的Mie散射系 数;The Mie scattering coefficient acquisition module is used to obtain the Mie scattering coefficient of the dispersive plasma sphere by combining the expressions of dielectric parameters under the Debye dispersion model, the relationship between the refractive index and the dielectric parameters, and the Mie theory;

拉盖尔-高斯涡旋波束内场和散射场的球矢量波函数展开式模块,用于通过 拉盖尔-高斯涡旋波束矢势的球矢量波函数展开式进一步处理可得到电磁场入射 表达式,根据同样方法也可以获得拉盖尔-高斯涡旋波束内场和散射场的球矢量 波函数展开式;Spherical vector wave function expansion module of Laguerre-Gaussian vortex beam internal and scattered fields, which can be used to obtain electromagnetic field incidence expressions by further processing the spherical vector wave function expansion of Laguerre-Gaussian vortex beam vector potential , the spherical vector wave function expansions of the Laguerre-Gaussian vortex beam inner field and scattered field can also be obtained according to the same method;

散射场展开系数获取模块,用于在介质球表面根据电场磁场满足连续性边 界条件原理,结合所得色散等离子体球的Mie散射系数,并将入射场、内场和 散射场的球矢量波函数展开式代入边界条件,就可以得到拉盖尔-高斯涡旋波束 入射下的散射场展开系数;Scattering field expansion coefficient acquisition module, which is used to expand the spherical vector wave functions of the incident field, internal field and scattered field by combining the Mie scattering coefficient of the obtained dispersive plasma sphere according to the principle that the electric and magnetic fields satisfy the continuity boundary condition on the surface of the dielectric sphere. By substituting the boundary conditions into the formula, the expansion coefficient of the scattered field under the incidence of the Laguerre-Gaussian vortex beam can be obtained;

远场雷达散射截面获取模块,用于通过散射场展开系数和散射相函数可以 得到远场雷达散射截面。The far-field radar cross section acquisition module is used to obtain the far-field radar cross section through the scattered field expansion coefficient and the scattered phase function.

涡旋波束电磁散射特性的影响分析模块,用于改变拉盖尔-高斯涡旋波束的 频率,得不同频率下色散等离子体球的电磁散射场,进而可以分析不同频率雷 达波束照射下等离子体球色散效应对涡旋波束电磁散射特性的影响。The influence analysis module of electromagnetic scattering characteristics of vortex beams is used to change the frequency of Laguerre-Gaussian vortex beams to obtain the electromagnetic scattering fields of dispersive plasma spheres at different frequencies, and then analyze the plasma spheres irradiated by radar beams of different frequencies. Influence of dispersion effects on electromagnetic scattering properties of vortex beams.

本发明的另一目的在于提供一种临近空间高超声速飞行器通信方法,所述 临近空间高超声速飞行器通信方法使用所述的涡旋波束电磁散射场计算方法。Another object of the present invention is to provide a near-space hypersonic vehicle communication method, which uses the vortex beam electromagnetic scattering field calculation method.

结合上述的所有技术方案,本发明所具备的优点及积极效果为:本发明通 过对涡旋波束电磁散射场的广义洛伦兹Mie解析求解,可得到色散等离子体球 的雷达散射截面,以往只计算了非色散等离子体球的散射特性,弥补行业空白, 有望解决高超声速飞行器目标雷达探测困难的问题,并为隐身飞行器的反隐身 研究提供了新的选择。Combined with all the above technical solutions, the advantages and positive effects of the present invention are as follows: the present invention can obtain the radar scattering cross section of the dispersive plasma sphere by solving the generalized Lorentz Mie analytical solution of the electromagnetic scattering field of the vortex beam. The scattering properties of non-dispersive plasma spheres are calculated, which fills the gap in the industry, is expected to solve the difficult problem of radar detection of hypersonic aircraft targets, and provides a new option for the anti-stealth research of stealth aircraft.

本发明利用涡旋电磁波独特的相位波前结构,特殊的强度分布等特点来计 算Debye色散等离子体球的雷达散射截面,提出了一种计算Debye色散等离子 体球的涡旋波束电磁散射场的方法,研究涡旋电磁波束照射下的Debye色散等 离子球的散射特性,有望解决高超声速飞行器目标雷达探测困难的问题,并为 隐身飞行器的反隐身研究提供了新的选择。The invention utilizes the unique phase wave front structure and special intensity distribution of the vortex electromagnetic wave to calculate the radar scattering cross section of the Debye dispersion plasma sphere, and proposes a method for calculating the vortex beam electromagnetic scattering field of the Debye dispersion plasma sphere , to study the scattering characteristics of Debye dispersive plasma spheres under the irradiation of vortex electromagnetic beams, which is expected to solve the difficult problem of radar detection of hypersonic aircraft targets, and provides a new option for anti-stealth research of stealth aircraft.

附图说明Description of drawings

为了更清楚地说明本申请实施例的技术方案,下面将对本申请实施例中所 需要使用的附图做简单的介绍,显而易见地,下面所描述的附图仅仅是本申请 的一些实施例,对于本领域普通技术人员来讲,在不付出创造性劳动的前提下 还可以根据这些附图获得其他的附图。In order to explain the technical solutions of the embodiments of the present application more clearly, the following will briefly introduce the drawings that need to be used in the embodiments of the present application. Obviously, the drawings described below are only some embodiments of the present application. For those of ordinary skill in the art, other drawings can also be obtained from these drawings without creative effort.

图1是本发明实施例提供的涡旋波束电磁散射场计算方法流程图。FIG. 1 is a flowchart of a method for calculating a vortex beam electromagnetic scattering field provided by an embodiment of the present invention.

图2是本发明实施例提供的涡旋波束电磁散射场计算系统的结构示意图;2 is a schematic structural diagram of a vortex beam electromagnetic scattered field calculation system provided by an embodiment of the present invention;

图2中:1、高阶厄米-高斯波束矢势的球矢量波函数展开式获取模块;2、 拉盖尔-高斯涡旋波束的球矢量波函数展开式获取模块;3、Mie散射系数获取模 块;4、拉盖尔-高斯涡旋波束内场和散射场的球矢量波函数展开式模块;5、散 射场展开系数获取模块;6、远场雷达散射截面获取模块;7、涡旋波束电磁散 射特性的影响分析模块。In Figure 2: 1. The acquisition module of the spherical vector wave function expansion of the high-order Hermitian-Gaussian beam vector potential; 2. The acquisition module of the spherical vector wave function expansion of the Laguerre-Gaussian vortex beam; 3. The Mie scattering coefficient Acquisition module; 4. Spherical vector wave function expansion module of Laguerre-Gaussian vortex beam inner field and scattered field; 5. Scattered field expansion coefficient acquisition module; 6. Far-field radar cross section acquisition module; 7. Vortex A module for analyzing the effects of beam electromagnetic scattering properties.

图3是拉盖尔-高斯涡旋波束照射Debye色散等离子体球的几何示意图。Figure 3 is a geometric schematic diagram of the Laguerre-Gaussian vortex beam irradiating the Debye dispersive plasma sphere.

图4是本发明实施例提供的广义洛伦兹Mie理论计算拉盖尔-高斯涡旋波束 照射下的Debye色散等离子体球散射截面框图。Fig. 4 is a block diagram of the Debye dispersion plasma sphere scattering cross section under the Laguerre-Gaussian vortex beam irradiation provided by the generalized Lorentz Mie theory calculation provided by the embodiment of the present invention.

图5是本发明实施例提供的不同等离子体碰撞频率对LG00涡旋波束入射 下等离子体碰撞频率对色散等离子体球散射截面的影响。Fig. 5 is the influence of the plasma collision frequency on the scattering cross section of the dispersive plasma sphere under the incidence of the LG00 vortex beam provided by the embodiment of the present invention.

图6是本发明实施例提供的不同等离子体碰撞频率对LG01涡旋波束入射色 散等离子体球散射截面的影响示意图。Fig. 6 is a schematic diagram showing the influence of different plasma collision frequencies on the scattering cross section of the LG01 vortex beam incident dispersive plasma sphere according to an embodiment of the present invention.

图7是本发明实施例提供的不同等离子体碰撞频率对LG02涡旋波束入射色 散等离子体球散射截面的影响示意图。Fig. 7 is a schematic diagram showing the influence of different plasma collision frequencies on the scattering cross section of the incident dispersive plasma sphere of the LG02 vortex beam provided by the embodiment of the present invention.

具体实施方式Detailed ways

为了使本发明的目的、技术方案及优点更加清楚明白,以下结合实施例, 对本发明进行进一步详细说明。应当理解,此处所描述的具体实施例仅仅用以 解释本发明,并不用于限定本发明。In order to make the objectives, technical solutions and advantages of the present invention clearer, the present invention will be further described in detail below with reference to the embodiments. It should be understood that the specific embodiments described herein are only used to explain the present invention, but not to limit the present invention.

针对现有技术存在的问题,本发明提供了一种Debye色散等离子体球的涡 旋波束电磁散射场计算方法及系统,下面结合附图对本发明作详细的描述。In view of the existing problems in the prior art, the present invention provides a method and system for calculating the electromagnetic scattering field of a vortex beam of a Debye dispersion plasma sphere. The present invention is described in detail below with reference to the accompanying drawings.

如图1所示,本发明提供的涡旋波束电磁散射场计算方法包括以下步骤:As shown in FIG. 1 , the method for calculating the vortex beam electromagnetic scattering field provided by the present invention includes the following steps:

S101:利用复源点方法,采用复源点多极子叠加的方法描述高阶波束,得 到高阶厄米-高斯波束矢势的球矢量波函数展开式;S101: Using the complex source point method and using the complex source point multipole superposition method to describe the high-order beam, obtain the spherical vector wave function expansion of the high-order Hermitian-Gaussian beam vector potential;

S102:通过拉盖尔-高斯波束与厄米-高斯波束模之间的数学关系,可以得到 拉盖尔-高斯涡旋波束的标量波函数展开,将其代入携带有轨道角动量的拉盖尔- 高斯涡旋波束的矢势表达式,进而可得到拉盖尔-高斯涡旋波束的球矢量波函数 展开式;S102: Through the mathematical relationship between the Laguerre-Gaussian beam and the Hermitian-Gaussian beam mode, the scalar wave function expansion of the Laguerre-Gaussian vortex beam can be obtained, and it is substituted into the Laguerre carrying the orbital angular momentum - The vector potential expression of the Gaussian vortex beam, and then the spherical vector wave function expansion of the Laguerre-Gaussian vortex beam can be obtained;

S103:结合Debye色散模型下介电参数表达式、折射率与介电参数关系式 以及Mie理论,可以得到色散等离子体球的Mie散射系数;S103: The Mie scattering coefficient of the dispersive plasma sphere can be obtained by combining the expressions of dielectric parameters under the Debye dispersion model, the relationship between refractive index and dielectric parameters, and the Mie theory;

S104:通过拉盖尔-高斯涡旋波束矢势的球矢量波函数展开式进一步处理可 得到电磁场入射表达式,根据同样方法也可以获得拉盖尔-高斯涡旋波束内场和 散射场的球矢量波函数展开式;S104: The electromagnetic field incident expression can be obtained by further processing the spherical vector wave function expansion of the Laguerre-Gaussian vortex beam vector potential. According to the same method, the spherical inner field and scattering field of the Laguerre-Gaussian vortex beam can also be obtained. Vector wave function expansion;

S105:在介质球表面根据电场磁场满足连续性边界条件原理,结合步骤S103 所得色散等离子体球的Mie散射系数,并将入射场、内场和散射场的球矢量波 函数展开式代入边界条件,就可以得到拉盖尔-高斯涡旋波束入射下的散射场展 开系数;S105: According to the principle that the electric field and the magnetic field satisfy the continuity boundary condition on the surface of the dielectric sphere, combine the Mie scattering coefficient of the dispersive plasma sphere obtained in step S103, and substitute the spherical vector wave function expansions of the incident field, the inner field and the scattering field into the boundary conditions, Then the expansion coefficient of the scattered field under the incidence of the Laguerre-Gaussian vortex beam can be obtained;

S106:通过散射场展开系数和散射相函数可以得到远场雷达散射截面。S106: The far-field radar scattering cross section can be obtained by the scattering field expansion coefficient and the scattering phase function.

S107:改变拉盖尔-高斯涡旋波束的频率,重复步骤S101~步骤S106,可得 不同频率下色散等离子体球的电磁散射场,进而可以分析不同频率雷达波束照 射下等离子体球色散效应对涡旋波束电磁散射特性的影响。S107: Change the frequency of the Laguerre-Gaussian vortex beam, and repeat steps S101 to S106 to obtain the electromagnetic scattering field of the dispersive plasma sphere at different frequencies, and then analyze the effect of the plasma sphere on the dispersion effect of the plasma sphere under the irradiation of radar beams of different frequencies. Influence of electromagnetic scattering properties of vortex beams.

本发明提供的涡旋波束电磁散射场计算方法业内的普通技术人员还可以采 用其他的步骤实施,图1的本发明提供的涡旋波束电磁散射场计算方法仅仅是 一个具体实施例而已。Those skilled in the art of the vortex beam electromagnetic scattered field calculation method provided by the present invention can also use other steps to implement, and the vortex beam electromagnetic scattered field calculation method provided by the present invention in FIG. 1 is only a specific embodiment.

如图2所示,本发明提供的涡旋波束电磁散射场计算系统包括:As shown in Figure 2, the vortex beam electromagnetic scattered field calculation system provided by the present invention includes:

高阶厄米-高斯波束矢势的球矢量波函数展开式获取模块1,用于利用复源 点方法,采用复源点多极子叠加的方法描述高阶波束,得到高阶厄米-高斯波束 矢势的球矢量波函数展开式;The spherical vector wave function expansion acquisition module 1 of the high-order Hermitian-Gaussian beam vector potential is used to describe the high-order beam by using the complex source point method and the complex source point multipole superposition method to obtain the high-order Hermitian-Gaussian beam. The spherical vector wave function expansion of the beam vector potential;

拉盖尔-高斯涡旋波束的球矢量波函数展开式获取模块2,用于通过拉盖尔- 高斯波束与厄米-高斯波束模之间的数学关系,可以得到拉盖尔-高斯涡旋波束的 标量波函数展开,将其代入携带有轨道角动量的拉盖尔-高斯涡旋波束的矢势表 达式,进而可得到拉盖尔-高斯涡旋波束的球矢量波函数展开式;The spherical vector wave function expansion acquisition module 2 of the Laguerre-Gaussian vortex beam is used to obtain the Laguerre-Gaussian vortex through the mathematical relationship between the Laguerre-Gaussian beam and the Hermitian-Gaussian beam mode Expand the scalar wave function of the beam, and substitute it into the vector potential expression of the Laguerre-Gaussian vortex beam carrying the orbital angular momentum, and then the spherical vector wave function expansion of the Laguerre-Gaussian vortex beam can be obtained;

Mie散射系数获取模块3,用于结合Debye色散模型下介电参数表达式、折 射率与介电参数关系式以及Mie理论,可以得到色散等离子体球的Mie散射系 数;The Mie scattering coefficient acquisition module 3 is used to obtain the Mie scattering coefficient of the dispersive plasma sphere by combining the dielectric parameter expression, the relationship between the refractive index and the dielectric parameter and the Mie theory under the Debye dispersion model;

拉盖尔-高斯涡旋波束内场和散射场的球矢量波函数展开式模块4,用于通 过拉盖尔-高斯涡旋波束矢势的球矢量波函数展开式进一步处理可得到电磁场入 射表达式,根据同样方法也可以获得拉盖尔-高斯涡旋波束内场和散射场的球矢 量波函数展开式;The spherical vector wave function expansion module 4 of the Laguerre-Gaussian vortex beam internal and scattered fields is used to further process the spherical vector wave function expansion of the Laguerre-Gaussian vortex beam vector potential to obtain the electromagnetic field incident expression According to the same method, the spherical vector wave function expansions of the inner and scattered fields of the Laguerre-Gaussian vortex beam can also be obtained;

散射场展开系数获取模块5,用于在介质球表面根据电场磁场满足连续性边 界条件原理,结合所得色散等离子体球的Mie散射系数,并将入射场、内场和 散射场的球矢量波函数展开式代入边界条件,就可以得到拉盖尔-高斯涡旋波束 入射下的散射场展开系数;Scattering field expansion coefficient acquisition module 5 is used to combine the Mie scattering coefficient of the obtained dispersive plasma sphere on the surface of the dielectric sphere according to the principle that the electric field and magnetic field satisfy the continuity boundary condition, and calculate the spherical vector wave function of the incident field, inner field and scattered field. By substituting the expansion into the boundary conditions, the expansion coefficient of the scattered field under the incidence of the Laguerre-Gaussian vortex beam can be obtained;

远场雷达散射截面获取模块6,用于通过散射场展开系数和散射相函数可以 得到远场雷达散射截面。The far-field radar scattering cross section acquisition module 6 is used to obtain the far-field radar scattering cross section through the scattering field expansion coefficient and the scattering phase function.

涡旋波束电磁散射特性的影响分析模块7,用于改变拉盖尔-高斯涡旋波束 的频率,得不同频率下色散等离子体球的电磁散射场,进而可以分析不同频率 雷达波束照射下等离子体球色散效应对涡旋波束电磁散射特性的影响。The influence analysis module 7 of the electromagnetic scattering characteristics of the vortex beam is used to change the frequency of the Laguerre-Gaussian vortex beam to obtain the electromagnetic scattering field of the dispersive plasma sphere at different frequencies, and then analyze the plasma irradiated by the radar beam of different frequencies. Influence of spherical dispersion effect on electromagnetic scattering properties of vortex beams.

下面结合附图对本发明的技术方案作进一步的描述。The technical solutions of the present invention will be further described below with reference to the accompanying drawings.

如图4所示,本发明的涡旋波束电磁散射场计算具体实现步骤如下:As shown in Figure 4, the specific implementation steps of the vortex beam electromagnetic scattering field calculation of the present invention are as follows:

步骤1:利用复源点方法,采用复源点多极子叠加的方法描述高阶波束,得 到高阶厄米-高斯波束矢势的球矢量波函数展开式。Step 1: Using the complex source point method, the high-order beam is described by the method of complex source point multipole superposition, and the spherical vector wave function expansion of the high-order Hermitian-Gaussian beam vector potential is obtained.

(1.1)复源点方法是基于格林函数的一种等效快速算法,所以在积分类方 法中,都可以引入复源点方法。(1.1) The complex source point method is an equivalent fast algorithm based on Green's function, so the complex source point method can be introduced into the integral method.

(1.2)利用复源点方法,即采用复源点多极子叠加的方法来描述高阶波束, 可以得到高阶厄米-高斯波束矢势的球矢量波函数的展开式为:(1.2) Using the complex source point method, that is, using the complex source point multipole superposition method to describe the high-order beam, the expansion of the spherical vector wave function of the high-order Hermitian-Gaussian beam vector potential can be obtained as:

Figure RE-GDA0002806778480000141
Figure RE-GDA0002806778480000141

式中下标u,v分别表示厄米-高斯波束沿x、y方向变化的模阶数;

Figure BDA0002695357810000142
为第一类球矢量波函数,系数α(1)(u,v,n,m)、β(1)(u,v,n,m)表示HG波束的球矢量 波函数展开系数,其数学表达式为:where the subscripts u and v represent the modulo order of the Hermitian-Gaussian beam along the x and y directions, respectively;
Figure BDA0002695357810000142
is the first type of spherical vector wave function, the coefficients α (1) (u,v,n,m), β (1) (u,v,n,m) represent the expansion coefficient of the spherical vector wave function of the HG beam, and its mathematical The expression is:

Figure RE-GDA0002806778480000143
Figure RE-GDA0002806778480000143

Figure BDA0002695357810000144
Figure BDA0002695357810000144

其中

Figure BDA0002695357810000145
满足以下迭代关系:in
Figure BDA0002695357810000145
The following iterative relations are satisfied:

Figure BDA0002695357810000146
Figure BDA0002695357810000146

Figure BDA0002695357810000147
Figure BDA0002695357810000147

当u=v=0时,高阶厄米-高斯波束退化成高斯基模,

Figure BDA0002695357810000148
表达式如下:When u=v=0, the high-order Hermitian-Gaussian beam degenerates into a Gaussian fundamental mode,
Figure BDA0002695357810000148
The expression is as follows:

Figure RE-GDA0002806778480000151
Figure RE-GDA0002806778480000151

其中参数具体为:

Figure BDA0002695357810000152
cosθ0=(z0+ib)/r0
Figure BDA0002695357810000153
The parameters are specifically:
Figure BDA0002695357810000152
cosθ 0 =(z 0 +ib)/r 0 ,
Figure BDA0002695357810000153

步骤2:通过拉盖尔-高斯波束与厄米-高斯波束模之间的数学关系,可以得 到拉盖尔-高斯涡旋波束的标量波函数展开,将其代入携带有轨道角动量的拉盖 尔-高斯涡旋波束的矢势表达式,进而可得到拉盖尔-高斯涡旋波束的球矢量波函 数展开式;Step 2: Through the mathematical relationship between the Laguerre-Gaussian beam and the Hermitian-Gaussian beam mode, the scalar wave function expansion of the Laguerre-Gaussian vortex beam can be obtained and substituted into the Laguerre carrying the orbital angular momentum The vector potential expression of the Laguerre-Gaussian vortex beam, and then the spherical vector wave function expansion of the Laguerre-Gaussian vortex beam can be obtained;

(2.1)拉盖尔-高斯涡旋波束为傍轴波动方程在圆柱坐标系下的近似解。傍 轴波动方程在圆柱坐标系

Figure BDA0002695357810000154
下的表达式可以写作:(2.1) The Laguerre-Gaussian vortex beam is an approximate solution of the paraxial wave equation in the cylindrical coordinate system. Paraxial Wave Equation in Cylindrical Coordinate System
Figure BDA0002695357810000154
The following expression can be written as:

Figure BDA0002695357810000155
Figure BDA0002695357810000155

设方程的解为:Let the solution of the equation be:

Figure BDA0002695357810000156
Figure BDA0002695357810000156

其中w(z)表示波束在z处的波束宽度,p(z)表示复相移,与波束的传输相关, q(z)是复波束的参数,被用于描述波束的强度随着与传输轴距离的高斯变化, 相位波前曲率在近轴为球面。其具体表达式为

Figure BDA0002695357810000157
p(z)=iln(q0+z),q(z)=q0+z,
Figure BDA0002695357810000158
表示共焦参数,
Figure BDA0002695357810000159
为方位角,
Figure BDA00026953578100001510
where w(z) is the beam width at z, p(z) is the complex phase shift, which is related to the transmission of the beam, and q(z) is the parameter of the complex beam, which is used to describe the intensity of the beam with the transmission Gaussian variation of the axial distance, the phase wavefront curvature is spherical in the paraxial direction. Its specific expression is
Figure BDA0002695357810000157
p(z)=iln(q 0 +z), q(z)=q 0 +z,
Figure BDA0002695357810000158
is the confocal parameter,
Figure BDA0002695357810000159
is the azimuth,
Figure BDA00026953578100001510

(2.2)将方程的解代入傍轴波动方程,利用分离变量法,假设:(2.2) Substitute the solution of the equation into the paraxial wave equation and use the separation of variables method, assuming:

g=M(ζ)Z(z);g=M(ζ)Z(z);

其中

Figure BDA00026953578100001511
可以得到如下方程组:in
Figure BDA00026953578100001511
The following equations can be obtained:

Figure BDA00026953578100001512
Figure BDA00026953578100001512

Figure BDA0002695357810000161
Figure BDA0002695357810000161

其中

Figure BDA0002695357810000162
为伴随拉盖尔多项式,可以表示为:in
Figure BDA0002695357810000162
is the adjoint Laguerre polynomial, which can be expressed as:

Figure BDA0002695357810000163
Figure BDA0002695357810000163

(2.3)将

Figure BDA0002695357810000164
和Z(z)的表达式代入到M(ζ)和g的表达式中并且与ψ进行 对比,可以得到拉盖尔-高斯涡旋波束具体表达式:(2.3) will
Figure BDA0002695357810000164
The expressions of and Z(z) are substituted into the expressions of M(ζ) and g and compared with ψ, the specific expression of the Laguerre-Gaussian vortex beam can be obtained:

Figure BDA0002695357810000165
Figure BDA0002695357810000165

式中p,l分别表示拉盖尔-高斯涡旋波束的径向模阶数和拓扑荷数where p and l represent the radial mode order and topological charge of the Laguerre-Gaussian vortex beam, respectively

(2.4)对拉盖尔-高斯涡旋波束具体表达式进行归一化,可以得到:(2.4) Normalize the specific expression of Laguerre-Gaussian vortex beam, we can get:

Figure BDA0002695357810000166
Figure BDA0002695357810000166

当p=l=0时,拉盖尔-高斯涡旋波束就会退化到高斯波束入射情况,当束腰 半径w0→∞时,就会由高斯波束退化至平面波。When p=l=0, the Laguerre-Gaussian vortex beam will degenerate to the incident Gaussian beam, and when the beam waist radius w 0 →∞, it will degenerate from the Gaussian beam to the plane wave.

(2.5)携带有轨道角动量的拉盖尔-高斯涡旋波束的矢势可以表述为:(2.5) The vector potential of a Laguerre-Gaussian vortex beam carrying orbital angular momentum can be expressed as:

Figure BDA0002695357810000167
Figure BDA0002695357810000167

其中:in:

Figure BDA0002695357810000168
Figure BDA0002695357810000168

式中

Figure BDA0002695357810000169
分别对应角度依赖关系中的
Figure BDA00026953578100001610
δ0l为狄拉克函数。根据拉盖 尔-高斯波束与厄米-高斯波束模之间的数学关系式,可以得到拉盖尔-高斯涡旋 波束的标量波函数展开,具体如下:in the formula
Figure BDA0002695357810000169
Corresponding to the angle dependencies in the
Figure BDA00026953578100001610
δ 0l is the Dirac function. According to the mathematical relationship between the Laguerre-Gaussian beam and the Hermitian-Gaussian beam mode, the scalar wave function expansion of the Laguerre-Gaussian vortex beam can be obtained, as follows:

Figure BDA0002695357810000171
Figure BDA0002695357810000171

Figure BDA0002695357810000172
Figure BDA0002695357810000172

(2.6)将

Figure BDA0002695357810000173
Figure BDA0002695357810000174
的具体表达式代入到拉盖尔-高斯涡旋波束 矢势表达式当中,可以得到拉盖尔-高斯涡旋波束的球矢量波函数的展开系数 χ(1)(p,l,n,m)和κ(1)(p,l,n,m)的表达式如下:(2.6) will
Figure BDA0002695357810000173
and
Figure BDA0002695357810000174
Substitute the specific expression into the Laguerre-Gaussian vortex beam vector potential expression to obtain the expansion coefficient χ (1) (p,l,n,m) of the spherical vector wave function of the Laguerre-Gaussian vortex beam. ) and κ (1) (p,l,n,m) are expressed as follows:

Figure BDA0002695357810000175
Figure BDA0002695357810000175

Figure BDA0002695357810000176
Figure BDA0002695357810000176

那么拉盖尔-高斯涡旋波束矢势的球矢量波函数可以展开为:Then the spherical vector wave function of the Laguerre-Gaussian vortex beam vector potential can be expanded as:

Figure RE-GDA0002806778480000177
Figure RE-GDA0002806778480000177

步骤3:结合Debye色散模型下介电参数表达式、折射率与介电参数关系式 以及Mie理论,可以得到色散等离子体球的Mie散射系数;Step 3: The Mie scattering coefficient of the dispersive plasma sphere can be obtained by combining the expressions of dielectric parameters under the Debye dispersion model, the relationship between the refractive index and the dielectric parameters, and the Mie theory;

(3.1)记an,bn为Mie理论中的散射系数,其具体表达式可以写作:(3.1) Denote a n , b n is the scattering coefficient in Mie theory, and its specific expression can be written as:

Figure BDA0002695357810000181
Figure BDA0002695357810000181

其中

Figure BDA0002695357810000182
in
Figure BDA0002695357810000182

(3.2)因为目标为均匀且各向同性的Debye色散等离子体球,考虑等离子 体频率色散性对涡旋波束等离子体球电磁散射的影响,单层不同参数等离子体 包覆层的

Figure BDA0002695357810000183
μr=1。(3.2) Since the target is a uniform and isotropic Debye dispersion plasma sphere, considering the effect of the plasma frequency dispersion on the electromagnetic scattering of the vortex beam plasma sphere, the single-layer plasma cladding with different parameters
Figure BDA0002695357810000183
μ r =1.

步骤4:通过拉盖尔-高斯涡旋波束矢势的球矢量波函数展开式进一步处理 可得到电磁场入射表达式,根据同样方法也可以获得拉盖尔-高斯涡旋波束内场 和散射场的球矢量波函数展开式;Step 4: The electromagnetic field incident expression can be obtained by further processing the spherical vector wave function expansion of the Laguerre-Gaussian vortex beam vector potential. Ball vector wave function expansion;

(4.1)拉盖尔-高斯涡旋波束矢势的球矢量波函数开展式为:(4.1) The spherical vector wave function expansion of the Laguerre-Gaussian vortex beam vector potential is:

Figure RE-GDA0002806778480000184
Figure RE-GDA0002806778480000184

将上式代入:Substitute the above formula into:

Figure RE-GDA0002806778480000185
Figure RE-GDA0002806778480000185

就可以得到传播方向为+z轴方向,电矢量为x方向极化的电磁场入射表达 式:Then we can obtain the electromagnetic field incident expression with the propagation direction as the +z-axis direction and the electric vector as the polarization in the x-direction:

Figure BDA0002695357810000186
Figure BDA0002695357810000186

(4.2)同理可获得拉盖尔-高斯涡旋波束内场和散射场的球矢量波函数展开 式。(4.2) Similarly, the spherical vector wave function expansions of the Laguerre-Gaussian vortex beam inner field and scattered field can be obtained.

步骤5:在介质球表面根据电场磁场满足连续性边界条件原理,结合步骤 (3)所得色散等离子体球的Mie散射系数,并将入射场、内场和散射场的球矢 量波函数展开式代入边界条件,就可以得到拉盖尔-高斯涡旋波束入射下的散射 场展开系数;Step 5: On the surface of the dielectric sphere, according to the principle that the electric field and magnetic field satisfy the continuity boundary condition, combine the Mie scattering coefficient of the dispersive plasma sphere obtained in step (3), and substitute the spherical vector wave function expansions of the incident field, inner field and scattered field into Boundary conditions, the expansion coefficient of the scattered field under the incidence of the Laguerre-Gaussian vortex beam can be obtained;

散射场展开系数为:The scattering field expansion coefficient is:

Figure BDA0002695357810000191
Figure BDA0002695357810000191

其中in

Figure BDA0002695357810000192
Figure BDA0002695357810000192

式中an,bn为Mie理论中的散射系数。 where an and bn are the scattering coefficients in the Mie theory.

步骤6:通过散射场展开系数和散射相函数可以得到远场雷达散射截面;Step 6: The far-field radar scattering cross section can be obtained by the scattering field expansion coefficient and the scattering phase function;

远场雷达散射截面表达式如下所示:The far-field radar cross section expression is as follows:

Figure BDA0002695357810000193
Figure BDA0002695357810000193

上式中

Figure BDA0002695357810000194
Figure BDA0002695357810000195
表示散射场的分量,具体表达式如下:In the above formula
Figure BDA0002695357810000194
and
Figure BDA0002695357810000195
represents the component of the scattered field, and the specific expression is as follows:

Figure BDA0002695357810000196
Figure BDA0002695357810000196

其中散射相函数

Figure BDA0002695357810000197
Figure BDA0002695357810000198
具体为:where the scattering phase function
Figure BDA0002695357810000197
and
Figure BDA0002695357810000198
Specifically:

Figure BDA0002695357810000199
Figure BDA0002695357810000199

Figure BDA00026953578100001910
Figure BDA00026953578100001910

Figure BDA0002695357810000201
Figure BDA0002695357810000201

Figure BDA0002695357810000202
为连带勒让德多项式,有:
Figure BDA0002695357810000202
For the associated Legendre polynomial, we have:

Figure BDA0002695357810000203
Figure BDA0002695357810000203

其中:in:

Figure BDA0002695357810000204
Figure BDA0002695357810000204

步骤7:改变拉盖尔-高斯涡旋波束的频率,重复步骤(1)~(6),可得不 同频率下色散等离子体球的电磁散射场,进而可以分析不同频率雷达波束照射 下等离子体球色散效应对涡旋波束电磁散射特性的影响。Step 7: Change the frequency of the Laguerre-Gaussian vortex beam, and repeat steps (1) to (6) to obtain the electromagnetic scattering field of the dispersive plasma sphere at different frequencies, and then analyze the plasma irradiated by radar beams of different frequencies. Influence of spherical dispersion effect on electromagnetic scattering properties of vortex beams.

下面结合仿真对本发明的技术效果作详细的描述。The technical effects of the present invention will be described in detail below in conjunction with simulation.

(1)试验仿真条件(1) Test simulation conditions

相关计算参数选择如下:色散等离子体球半径a=0.05m,等离子体频率 ωp=10GHz,束腰半径为一个波长,碰撞频率分别ν=10GHz,ν=20GHz,ν=50GHz, 入射涡旋电磁波频率分别为f=4GHz和f=10GHz,径向模阶数p=0,角量子数 分别为l=0,l=1,l=2。The relevant calculation parameters are selected as follows: the radius of the dispersive plasma sphere a=0.05m, the plasma frequency ωp =10GHz, the beam waist radius is one wavelength, the collision frequencies are ν=10GHz, ν=20GHz, ν=50GHz, the incident vortex electromagnetic wave is The frequencies are f=4GHz and f=10GHz, the radial mode order p=0, and the angular quantum numbers are l=0, l=1, and l=2, respectively.

(2)试验仿真结果分析(2) Analysis of test simulation results

图5分别计算了涡旋电磁波(LG00)频率为4GHz和10GHz时,不同碰撞 频率下色散等离子体球的电磁散射场。由计算结果可以看出,随着碰撞频率的 增加,色散等离子体球的散射场逐渐减小。这是因为碰撞越频繁,等离子体球 对电磁波的吸收越大,导致散射强度降低。此外,随着涡旋电磁波频率的增加, 色散等离子体球的散射场主瓣宽度变窄,旁瓣宽度增加。Figure 5 calculates the electromagnetic scattering fields of the dispersive plasma spheres at different collision frequencies when the frequency of the vortex electromagnetic wave (LG00) is 4 GHz and 10 GHz, respectively. It can be seen from the calculation results that with the increase of the collision frequency, the scattered field of the dispersive plasma sphere gradually decreases. This is because the more frequent the collision, the greater the absorption of electromagnetic waves by the plasma sphere, resulting in a decrease in the scattering intensity. In addition, as the frequency of the vortex electromagnetic wave increases, the width of the main lobe of the scattered field of the dispersive plasma sphere narrows, and the width of the side lobe increases.

图6分别计算了涡旋电磁波(LG01)频率为4GHz和10GHz时,不同碰撞 频率下色散等离子体球的电磁散射场。散射场强度随碰撞频率的变化规律与图3 类似,即碰撞频率越大,散射场强度越小。此外,随着涡旋电磁波频率的增加, 色散等离子体球散射场的旁瓣强度减小。Figure 6 calculates the electromagnetic scattering fields of the dispersive plasma spheres at different collision frequencies when the frequency of the vortex electromagnetic wave (LG01) is 4 GHz and 10 GHz, respectively. The variation law of scattering field intensity with collision frequency is similar to Fig. 3, that is, the larger the collision frequency, the smaller the scattering field intensity. In addition, as the frequency of the vortex electromagnetic wave increases, the side lobe intensity of the scattered field of the dispersive plasma sphere decreases.

图7分别计算了涡旋电磁波(LG02)频率为4GHz和10GHz时,不同碰撞 频率下色散等离子体球的电磁散射场。散射场强度随碰撞频率的变化规律与图3 类似,即碰撞频率越大,散射场强度越小。此外,随着涡旋电磁波频率的增加, 色散等离子体球散射场的主瓣峰值减小,且旁瓣宽度也减小。Figure 7 calculates the electromagnetic scattering fields of the dispersive plasma spheres at different collision frequencies when the frequency of the vortex electromagnetic wave (LG02) is 4 GHz and 10 GHz, respectively. The variation law of scattering field intensity with collision frequency is similar to Fig. 3, that is, the larger the collision frequency, the smaller the scattering field intensity. In addition, as the frequency of the vortex electromagnetic wave increases, the peak value of the main lobe of the scattered field of the dispersive plasma sphere decreases, and the width of the side lobe also decreases.

应当注意,本发明的实施方式可以通过硬件、软件或者软件和硬件的结合 来实现。硬件部分可以利用专用逻辑来实现;软件部分可以存储在存储器中, 由适当的指令执行系统,例如微处理器或者专用设计硬件来执行。本领域的普 通技术人员可以理解上述的设备和方法可以使用计算机可执行指令和/或包含在 处理器控制代码中来实现,例如在诸如磁盘、CD或DVD-ROM的载体介质、诸 如只读存储器(固件)的可编程的存储器或者诸如光学或电子信号载体的数据载 体上提供了这样的代码。本发明的设备及其模块可以由诸如超大规模集成电路 或门阵列、诸如逻辑芯片、晶体管等的半导体、或者诸如现场可编程门阵列、 可编程逻辑设备等的可编程硬件设备的硬件电路实现,也可以用由各种类型的 处理器执行的软件实现,也可以由上述硬件电路和软件的结合例如固件来实现。It should be noted that embodiments of the present invention may be implemented by hardware, software, or a combination of software and hardware. The hardware portion may be implemented using special purpose logic; the software portion may be stored in memory and executed by a suitable instruction execution system, such as a microprocessor or specially designed hardware. Those of ordinary skill in the art will appreciate that the apparatus and methods described above may be implemented using computer-executable instructions and/or embodied in processor control code, for example on a carrier medium such as a disk, CD or DVD-ROM, such as a read-only memory Such code is provided on a programmable memory (firmware) or a data carrier such as an optical or electronic signal carrier. The device of the present invention and its modules can be implemented by hardware circuits such as very large scale integrated circuits or gate arrays, semiconductors such as logic chips, transistors, etc., or programmable hardware devices such as field programmable gate arrays, programmable logic devices, etc., It can also be implemented by software executed by various types of processors, or by a combination of the above-mentioned hardware circuits and software, such as firmware.

以上所述,仅为本发明的具体实施方式,但本发明的保护范围并不局限于 此,任何熟悉本技术领域的技术人员在本发明揭露的技术范围内,凡在本发明 的精神和原则之内所作的任何修改、等同替换和改进等,都应涵盖在本发明的 保护范围之内。The above are only specific embodiments of the present invention, but the protection scope of the present invention is not limited to this. Any person skilled in the art is within the technical scope disclosed by the present invention, and all within the spirit and principle of the present invention Any modifications, equivalent replacements and improvements made within the scope of the present invention should be included within the protection scope of the present invention.

Claims (8)

1. A vortex beam electromagnetic scattering field calculation method of a Debye dispersive plasma sphere is characterized by comprising the following steps:
describing a high-order wave beam by using a multi-source point method and a multi-pole superposition method to obtain a spherical vector wave function expansion of a high-order Hermite-Gaussian wave beam vector potential;
step two, through the mathematical relation between the Laguerre-Gaussian beam and the Hermite-Gaussian beam model, the scalar wave function expansion of the Laguerre-Gaussian vortex beam is obtained, and the scalar wave function expansion is substituted into the vector potential expression of the Laguerre-Gaussian vortex beam carrying the orbital angular momentum, so that the spherical vector wave function expansion of the Laguerre-Gaussian vortex beam can be obtained;
combining a dielectric parameter expression under a Debye dispersion model, a refractive index-dielectric parameter relational expression and a Mie theory to obtain a Mie scattering coefficient of the dispersion plasma sphere;
step four, further processing the Laguerre-Gaussian vortex beam vector potential spherical vector wave function expansion to obtain an electromagnetic field incident expression, and obtaining the Laguerre-Gaussian vortex beam internal field and scattering field spherical vector wave function expansion according to the same method;
step five, combining the Mie scattering coefficient of the dispersion plasma sphere obtained in the step three on the surface of the medium sphere according to the principle that the electric field and the magnetic field meet the continuous boundary condition, and substituting the spherical vector wave function expansion of the incident field, the internal field and the scattering field into the boundary condition to obtain the scattering field expansion coefficient under the incidence of the Laguerre-Gaussian vortex beam;
step six, obtaining a far-field radar scattering cross section through a scattering field expansion coefficient and a scattering phase function;
and step seven, changing the frequency of the Laguerre-Gaussian vortex beam, repeating the step one to the step six, obtaining the electromagnetic scattering field of the dispersion plasma ball under different frequencies, and further analyzing the influence of the dispersion effect of the plasma ball under the irradiation of radar beams with different frequencies on the electromagnetic scattering characteristic of the vortex beam.
2. The method for computing an electromagnetic scattered field of a vortex beam according to claim 1, wherein the describing the high-order beam by a multi-source point method and a multi-pole superposition method by using a multi-source point, and obtaining a spherical vector wave function expansion of the vector potential of the high-order Hermi-Gaussian beam comprises the following steps: describing a high-order wave beam by using a complex source point method and a complex source point multipole superposition method, and obtaining an expansion formula of a spherical vector wave function of the vector potential of the high-order Hermite-Gaussian wave beam as follows:
Figure RE-FDA0002806778470000021
subscripts u and v in the formula respectively represent the mode orders of Hermitian-Gaussian beams changing along the x direction and the y direction;
Figure RE-FDA0002806778470000022
for the first spherical vector wave function, coefficient α (1) (u,v,n,m)、β (1) (u, v, n, m) represents a spherical vector wave function expansion coefficient of the HG beam, and its mathematical expression is:
Figure RE-FDA0002806778470000023
Figure RE-FDA0002806778470000024
wherein
Figure RE-FDA0002806778470000025
The following iterative relationship is satisfied:
Figure RE-FDA0002806778470000026
Figure RE-FDA0002806778470000027
when u-v-0, the higher order hermi-gaussian beam degenerates into the gaussian fundamental mode,
Figure RE-FDA0002806778470000028
the expression is as follows:
Figure RE-FDA0002806778470000029
the parameters are specifically as follows:
Figure RE-FDA00028067784700000210
cosθ 0 =(z 0 +ib)/r 0
Figure RE-FDA00028067784700000211
3. the method of calculating an electromagnetic scattered field of a vortex beam of claim 1, wherein the step of obtaining a scalar wavefunction expansion of a Laguerre-Gaussian vortex beam by a mathematical relationship between the Laguerre-Gaussian beam and the Hermite-Gaussian beam mode, and substituting the scalar wavefunction expansion into a vector expression of the Laguerre-Gaussian vortex beam carrying orbital angular momentum, thereby obtaining a spherical vector wavefunction expansion of the Laguerre-Gaussian vortex beam comprises:
(1) the Laguerre-Gaussian vortex beam is an approximate solution of paraxial wave equation in a cylindrical coordinate system
Figure FDA0002695357800000031
The following expression is written:
Figure FDA0002695357800000032
let the solution of the equation be:
Figure FDA0002695357800000033
where w (z) denotes the beam width of the beam at z, p (z) denotes the complex phase shift associated with the transmission of the beam, q (z) is a parameter of the complex beam used to describe the gaussian variation of the intensity of the beam with distance from the transmission axis, the curvature of the phase wavefront being spherical at the proximal axis; the specific expression is
Figure FDA0002695357800000034
p(z)=iln(q 0 +z),q(z)=q 0 +z,
Figure FDA0002695357800000035
Which represents the confocal parameters of the image to be scanned,
Figure FDA0002695357800000036
in order to be the azimuth angle,
Figure FDA0002695357800000037
(2) substituting the solution of the equation into a paraxial wave equation, and utilizing a separation variable method:
g=M(ζ)Z(z);
wherein
Figure FDA0002695357800000038
The following system of equations is obtained:
Figure FDA00026953578000000313
Figure FDA0002695357800000039
wherein
Figure FDA00026953578000000312
Is a concomitant laguerre polynomial expressed as:
Figure FDA00026953578000000310
(3) will be provided with
Figure FDA00026953578000000314
And the expression of Z (z) is substituted into the expressions of M (ζ) and g and compared with ψ, resulting in a Laguerre-Gaussian vortex beam specific expression:
Figure FDA00026953578000000311
in the formula, p and l respectively represent the radial module order and the topological charge number of the Laguerre-Gaussian vortex beam;
(4) normalizing the specific expression of the Laguerre-Gaussian vortex beam to obtain:
Figure FDA0002695357800000041
when p is 0, the Laguerre-Gaussian vortex beam is degraded to the incident situation of the Gaussian beam, and when the beam waist radius w is equal to 0 Will degenerate from a gaussian beam to a plane wave → ∞;
(5) the rise of a laguerre-gaussian vortex beam carrying orbital angular momentum is expressed as:
Figure FDA0002695357800000042
wherein:
Figure FDA0002695357800000043
in the formula
Figure FDA0002695357800000044
Respectively corresponding to angle dependence
Figure FDA0002695357800000045
δ 0l Obtaining a scalar wave function expansion of the Laguerre-Gaussian vortex beam according to a mathematical relation between the Laguerre-Gaussian beam and the Hermite beam mode as a Dirac function, wherein the scalar wave function expansion comprises the following specific steps:
Figure FDA0002695357800000046
Figure FDA0002695357800000047
(6) will be provided with
Figure FDA0002695357800000048
And
Figure FDA0002695357800000049
the specific expression is substituted into the vector potential expression of the Laguerre-Gaussian vortex beam to obtain the expansion coefficient chi of the spherical vector wave function of the Laguerre-Gaussian vortex beam (1) (p, l, n, m) and κ (1) The expression of (p, l, n, m) is as follows:
Figure FDA0002695357800000051
Figure FDA0002695357800000052
then the spherical vector wave function of the vector potential of the laguerre-gaussian vortex beam is expanded as:
Figure FDA0002695357800000053
4. the method for calculating the vortex beam electromagnetic scattering field according to claim 1, wherein the Mie scattering coefficient of the dispersive plasma sphere can be obtained by combining a dielectric parameter expression under a Debye dispersion model, a refractive index-dielectric parameter relational expression and a Mie theory;
(1) note a n ,b n The scattering coefficient in Mie theory is expressed by the following specific expression:
Figure FDA0002695357800000054
wherein
Figure FDA0002695357800000055
(2) Based on a Debye dispersion model, the dielectric parameter expression of the dispersion plasma sphere is as follows:
Figure FDA0002695357800000056
μ r =1。
5. the method of claim 1, wherein the further processing by spherical vector wave function expansion of the vector potential of the Laguerre-Gaussian vortex beam to obtain an electromagnetic field incident expression with a propagation direction of + z and an electric vector of x-direction polarization, and obtaining spherical vector wave function expansion of the inner field and the scattered field of the Laguerre-Gaussian vortex beam according to the same method comprises:
(1) the spherical vector wave function development formula of the vector potential of the Laguerre-Gaussian vortex beam is as follows:
Figure FDA0002695357800000061
substituting the above formula into:
Figure FDA0002695357800000062
obtaining an electromagnetic field incidence expression with the propagation direction being + z-axis direction and the electric vector being x-direction polarization:
Figure FDA0002695357800000063
(2) and obtaining spherical vector wave function expansion of the Laguerre-Gaussian vortex beam internal field and the scattering field in the same way.
6. The method for calculating an electromagnetic scattered field of a vortex beam according to claim 1, wherein the scattered field expansion coefficient under the incidence of a Laguerre-Gaussian vortex beam can be obtained by combining the Mie scattering coefficient of the dispersive plasma sphere obtained in step (3) on the surface of the medium sphere according to the principle that the electric field and the magnetic field satisfy the continuity boundary condition and substituting the spherical vector wave function expansion of the incident field, the internal field and the scattered field into the boundary condition:
the scatter field expansion coefficient is:
Figure FDA0002695357800000064
wherein
Figure FDA0002695357800000065
In the formula a n ,b n Is the scattering coefficient in the Mie theory;
obtaining a far-field radar scattering cross section through a scattering field expansion coefficient and a scattering phase function comprises the following steps:
the far-field radar scattering cross-section expression is as follows:
Figure FDA0002695357800000071
in the formula
Figure FDA0002695357800000072
And
Figure FDA0002695357800000073
representing the components of the scattered field, the specific expression is as follows:
Figure FDA0002695357800000074
in which the scattering phase function
Figure FDA0002695357800000075
And
Figure FDA0002695357800000076
the method comprises the following specific steps:
Figure FDA0002695357800000077
Figure FDA0002695357800000078
Figure FDA0002695357800000079
Figure FDA00026953578000000710
is a conjunctive legendre polynomial, having:
Figure FDA00026953578000000711
wherein:
Figure FDA00026953578000000712
7. a vortex beam electromagnetic scattered field calculation system for implementing the vortex beam electromagnetic scattered field calculation method according to any one of claims 1 to 6, wherein the vortex beam electromagnetic scattered field calculation system comprises:
the device comprises a spherical vector wave function expansion acquisition module of the vector potential of the high-order hermitian-Gaussian beam, a vector wave function expansion acquisition module and a vector wave function expansion module, wherein the spherical vector wave function expansion acquisition module is used for describing the high-order beam by using a complex source point method and a complex source point multipole superposition method to obtain the vector wave function expansion of the high-order hermitian-Gaussian beam vector potential;
the acquisition module is used for obtaining the scalar wave function expansion of the Laguerre-Gaussian vortex wave beam through the mathematical relationship between the Laguerre-Gaussian wave beam and the Hermite-Gaussian wave beam module, substituting the scalar wave function expansion into the vector expression of the Laguerre-Gaussian vortex wave beam carrying the orbital angular momentum, and further obtaining the spherical vector wave function expansion of the Laguerre-Gaussian vortex wave beam;
the Mie scattering coefficient acquisition module is used for combining a dielectric parameter expression under a Debye dispersion model, a refractive index and dielectric parameter relation and a Mie theory to obtain the Mie scattering coefficient of the dispersion plasma sphere;
the Laguerre-Gaussian vortex beam inner field and scattering field spherical vector wave function expansion module is used for further processing through the Laguerre-Gaussian vortex beam vector potential spherical vector wave function expansion to obtain an electromagnetic field incident expression, and the Laguerre-Gaussian vortex beam inner field and scattering field spherical vector wave function expansion can also be obtained according to the same method;
the scattered field expansion coefficient acquisition module is used for combining the Mie scattering coefficient of the obtained dispersion plasma sphere on the surface of the medium sphere according to the principle that the electric field and the magnetic field meet the continuous boundary condition, and substituting the spherical vector wave function expansion of the incident field, the internal field and the scattered field into the boundary condition to obtain the scattered field expansion coefficient under the incidence of the Laguerre-Gaussian vortex beam;
the far-field radar cross section acquisition module is used for obtaining a far-field radar cross section through a scattered field expansion coefficient and a scattered phase function;
and the influence analysis module of the vortex beam electromagnetic scattering characteristic is used for changing the frequency of the Laguerre-Gaussian vortex beam to obtain the electromagnetic scattering field of the dispersion plasma ball under different frequencies, and further analyzing the influence of the plasma ball dispersion effect under the irradiation of radar beams with different frequencies on the vortex beam electromagnetic scattering characteristic.
8. A near space hypersonic aircraft communication method is characterized in that the method for calculating the vortex beam electromagnetic scattering field is used as claimed in any one of claims 1 to 6.
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