CN108009355A - A kind of darkroom spheric array Compact Range dead zone characteristic spectrum analysis method - Google Patents
A kind of darkroom spheric array Compact Range dead zone characteristic spectrum analysis method Download PDFInfo
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- CN108009355A CN108009355A CN201711247327.9A CN201711247327A CN108009355A CN 108009355 A CN108009355 A CN 108009355A CN 201711247327 A CN201711247327 A CN 201711247327A CN 108009355 A CN108009355 A CN 108009355A
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Abstract
The invention discloses a kind of darkroom spheric array Compact Range dead zone characteristic spectrum analysis method, including, according to frequency range and Compact Range size, design feed antenna, reflecting surface and spheric array model;The model of design is imported into Electromagnetic Modeling software, extracts the electric field distribution of dead zone quarry sampling point;It is distributed according to the electric field of dead zone quarry sampling point, calculates dead zone rink corner Spectral structure;According to the spectrum analysis diffraction field distribution of dead zone rink corner.The present invention can directly generate dead zone field data due to Electromagnetic Modeling software, it is not necessary to consider the field distribution of bore face and free space network receptance function, can analyze influence of the spheric array to Compact Range.
Description
Technical field
The present invention relates to a kind of darkroom spheric array Compact Range dead zone characteristic spectrum analysis method, belong to Compact Range design field.
Background technology
In reflecting surface Compact Range (Compact Range:It is interior in a limited space to simulate far-field radiation, scattering strip in microwave dark room
The electromagnetic field that part obtains) in design process, in order to obtain stable dead zone (dead zone:In microwave dark room, mesh to be analyzed
It is necessary to have the characteristics of electric field phase, amplitude stabilization for position where marking) it is distributed, it is necessary to reflector shape and exposure field point
Cloth optimizes, still, since there are a variety of diffraction field components, non-uniform standing wave point can be formed in space in dead zone
Cloth, in frequency shift, spatial domain field distribution changes correspondingly.When carrying out Compact Range optimization design, in order to investigate the quality of design,
Conventional method is integrated, work to compare the change that dead zone obtains standing wave peak value or root mean square on multiple frequency points in full frequency band
Work amount is larger.And due to this one kind index only reflect a variety of diffraction field components and deposit resultant field change, do not set up with
The direct relation of certain a kind of diffraction field, therefore be inconvenient to analyze the mechanism of diffraction field generation.
At present, it can be used for analyzing the diffraction field feature of Compact Range according to the bore near field angular-spectrum analysis method of convolution method,
Since bore near field or far field can be expressed as the convolution of bore occasion spatial network respective function, it is near bore can be exported
Space (is considered as wave filter, is put at space any point by the angular spectrum in field and far field for aperture field angular spectrum and network receptance function
Put a shock pulse, then receive obtained electric field space is more any other, shock pulse and reception obtain electric field it
Between function, be exactly network receptance function) product of angular spectrum, so as to calculate the angular spectrum in bore near field and far field.Wherein, root first
Aperture field angular spectrum is obtained according to Aperture field distribution, its angular spectrum asked further according to free space network receptance function, finally by aperture field
Angular spectrum is multiplied with free space network receptance function angular spectrum, obtains final result.
But the feed of the generation aperture field of this method, it is ripple antenna or square horn antenna in Practical Project, by
The influence undesirable to its directional diagram, bore face (bore face:The bore section of reflector antenna) distribution of obtained electric field with
Ideal distribution differs farther out, especially when occurring spheric array (spheric array in Compact Range:One metal for being disposed with mutiple antennas
Sphere, for the plane wave of the simulation generation any direction in microwave dark room) when large-scale diffraction field produces the situation of structure.Cause
This, the aperture field provided according to ideal mathematics model differs farther out with actual distribution.
Secondly, when producing structure when large-scale diffraction field there are spheric array in Compact Range, can not try to achieve one has had
The spatial network receptance function of standby mathematic(al) representation, therefore conventional method can not provide the characteristic angle of spatial network receptance function
Spectrum.Therefore, the method that dead zone characteristic angle Spectral structure is tried to achieve by convolution method is infeasible.
The content of the invention
In order to solve the above technical problem, the present invention provides a kind of darkroom spheric array Compact Range dead zone characteristic spectrum analysis side
Method.
In order to achieve the above object, the technical solution adopted in the present invention is:
A kind of darkroom spheric array Compact Range dead zone characteristic spectrum analysis method, including,
According to frequency range and Compact Range size, design feed antenna, reflecting surface and spheric array model;
The model of design is imported into Electromagnetic Modeling software, extracts the electric field distribution of dead zone quarry sampling point;
It is distributed according to the electric field of dead zone quarry sampling point, calculates dead zone rink corner Spectral structure;
According to the spectrum analysis diffraction field distribution of dead zone rink corner.
According to frequency range and Compact Range size, design feed antenna, reflecting surface and spheric array model in CAD software.
Model is imported into FEKO, excitation types are set, extracts the electric field distribution of dead zone quarry sampling point.
The excitation types of setting are waveguide excitation, and sampled point is smaller than 1/3 operation wavelength.
FEKO exports .out files, and the electric field distribution of dead zone quarry sampling point is extracted from this document.
Dead zone rink corner Spectral structure is calculated using FFT and IFFT, formula is,
Wherein, M and N is respectively dead zone field in the quantity of x and y directions sampled point, kxFor the x durection components of wave number, kyFor ripple
Several y durection components, g are dead zone electric field component, G be dead zone rink corner spectral component, FFT and IFFT for Fast Fourier Transform with
Inverse transformation, p and q are the element numbers of Two-dimensional FFT, and Δ x, Δ y are the spacing of sampled point in the x and y direction, x0、y0It is in dead zone
The heart is with respect to origin.
kxAnd kyRelation with angular spectrum incidence angle is,
kx=k0sin(θ)cos(φ)
ky=k0sin(θ)sin(φ)
Wherein, k0For the wave number in free space, θ, φ are the angle component of spherical coordinate system.
The beneficial effect that the present invention is reached:1st, the present invention due to Electromagnetic Modeling software (using Computational electromagnetics algorithm into
The software of row Electromagnetic Simulation) dead zone field data can be directly generated, it is not necessary to consider the field distribution of bore face and free space network
Receptance function;2nd, the present invention can analyze influence of the spheric array to Compact Range;3rd, the present invention accelerates angular spectrum using fast Flourier
Analysis.
Brief description of the drawings
Fig. 1 is the flow chart of the present invention;
Fig. 2 is feed antenna schematic diagram;
Fig. 3 is spheric array Compact Range front view;
Fig. 4 is spheric array Compact Range side view;
Fig. 5 is spheric array Compact Range top view;
Fig. 6 is angular spectrum schematic diagram.
Embodiment
The invention will be further described below in conjunction with the accompanying drawings.Following embodiments are only used for clearly illustrating the present invention
Technical solution, and be not intended to limit the protection scope of the present invention and limit the scope of the invention.
As shown in Figure 1, a kind of darkroom spheric array Compact Range dead zone characteristic spectrum analysis method, comprises the following steps:
Step 1, in CAD software, according to frequency range and Compact Range size, design feed antenna, reflecting surface and spheric array mould
Type, as shown in Figure 2-5, wherein spheric array shows to simplify, and is replaced using ideal spherical face.
Step 2, the model of design is imported into Electromagnetic Modeling software, excitation types is set, extract dead zone quarry sampling point
Electric field is distributed.
The excitation types of setting are waveguide excitation, and sampled point is smaller than 1/3 operation wavelength, and existing Electromagnetic Modeling is soft
Part has CST, HFSS, FEKO etc., can be used, and here using FEKO, FEKO export .out files, are read using programming software
Enter the .out files that FEKO is generated, the electric field distribution of dead zone quarry sampling point is extracted from this document.
Step 3, it is distributed according to the electric field of dead zone quarry sampling point, calculates dead zone rink corner Spectral structure.
In order to accelerate angular-spectrum analysis, dead zone rink corner Spectral structure is calculated used here as FFT and IFFT, specific formula is as follows:
Wherein, M and N is respectively dead zone field in the quantity of x and y directions sampled point, kxFor the x durection components of wave number, kyFor ripple
Several y durection components, g for dead zone electric field component (g (x, y), g (M, 1:N the g implications in) are dead zone electric field component), G
For dead zone rink corner spectral component, FFT and IFFT are Fast Fourier Transform and inverse transformation, p and the element numbers that q is Two-dimensional FFT, Δ
X, Δ y is the spacing of sampled point in the x and y direction, x0、y0It is dead zone center with respect to origin.
Step 4, according to the spectrum analysis diffraction field distribution of dead zone rink corner.
kxAnd kyRelation with angular spectrum incidence angle is,
kx=k0sin(θ)cos(φ)
ky=k0sin(θ)sin(φ)
Wherein, k0For the wave number in free space, θ, φ are the angle component of spherical coordinate system., can be with after wave number is obtained
The electric field component on different directions is obtained according to formulas Extraction.The dead zone rink corner spectrum of reflecting surface is only installed and reflecting surface is installed at the same time
It is as shown in Figure 6 with the dead zone rink corner spectrum of spheric array, it is seen then that, can be in dead zone after mounting spherical battle array under 10GHz working frequencies
The diffraction field component of 70 degree to 90 degree arrival bearings is produced, while by the secondary reflection of reflecting surface, arrival bearing can be spent -30
New diffraction field component is produced, its amplitude is respectively less than 10dB.
The above method can be straight due to Electromagnetic Modeling software (software that Electromagnetic Simulation is carried out using Computational electromagnetics algorithm)
Deliver a child into dead zone field data, it is not necessary to consider the field distribution of bore face and free space network receptance function, spheric array can be analyzed
Influence to Compact Range.
The above is only the preferred embodiment of the present invention, it is noted that for the ordinary skill people of the art
For member, without departing from the technical principles of the invention, some improvement and deformation can also be made, these are improved and deformation
Also it should be regarded as protection scope of the present invention.
Claims (7)
- A kind of 1. darkroom spheric array Compact Range dead zone characteristic spectrum analysis method, it is characterised in that:Including,According to frequency range and Compact Range size, design feed antenna, reflecting surface and spheric array model;The model of design is imported into Electromagnetic Modeling software, extracts the electric field distribution of dead zone quarry sampling point;It is distributed according to the electric field of dead zone quarry sampling point, calculates dead zone rink corner Spectral structure;According to the spectrum analysis diffraction field distribution of dead zone rink corner.
- A kind of 2. darkroom spheric array Compact Range dead zone characteristic spectrum analysis method according to claim 1, it is characterised in that: According to frequency range and Compact Range size, design feed antenna, reflecting surface and spheric array model in CAD software.
- A kind of 3. darkroom spheric array Compact Range dead zone characteristic spectrum analysis method according to claim 1, it is characterised in that:Will Model imports FEKO, sets excitation types, extracts the electric field distribution of dead zone quarry sampling point.
- A kind of 4. darkroom spheric array Compact Range dead zone characteristic spectrum analysis method according to claim 3, it is characterised in that:If The excitation types put are waveguide excitation, and sampled point is smaller than 1/3 operation wavelength.
- A kind of 5. darkroom spheric array Compact Range dead zone characteristic spectrum analysis method according to claim 3, it is characterised in that: FEKO exports .out files, and the electric field distribution of dead zone quarry sampling point is extracted from this document.
- A kind of 6. darkroom spheric array Compact Range dead zone characteristic spectrum analysis method according to claim 1, it is characterised in that:Make Dead zone rink corner Spectral structure is calculated with FFT and IFFT, formula is,<mfenced open = "" close = ""> <mtable> <mtr> <mtd> <mrow> <mi>G</mi> <mrow> <mo>(</mo> <mrow> <mi>p</mi> <mo>,</mo> <mi>q</mi> </mrow> <mo>)</mo> </mrow> <mo>=</mo> <msubsup> <mo>&Integral;</mo> <mrow> <mo>-</mo> <mi>&infin;</mi> </mrow> <mi>&infin;</mi> </msubsup> <msubsup> <mo>&Integral;</mo> <mrow> <mo>-</mo> <mi>&infin;</mi> </mrow> <mi>&infin;</mi> </msubsup> <mi>g</mi> <mrow> <mo>(</mo> <mrow> <mi>x</mi> <mo>,</mo> <mi>y</mi> </mrow> <mo>)</mo> </mrow> <msup> <mi>e</mi> <mrow> <mi>j</mi> <mrow> <mo>(</mo> <mrow> <msub> <mi>k</mi> <mi>x</mi> </msub> <mrow> <mo>(</mo> <mi>p</mi> <mo>)</mo> </mrow> <mi>x</mi> <mo>+</mo> <msub> <mi>k</mi> <mi>y</mi> </msub> <mrow> <mo>(</mo> <mi>q</mi> <mo>)</mo> </mrow> <mi>y</mi> </mrow> <mo>)</mo> </mrow> 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<mi>F</mi> <mi>F</mi> <mi>T</mi> <mrow> <mo>&lsqb;</mo> <mrow> <mi>g</mi> <mrow> <mo>(</mo> <mrow> <mn>2</mn> <mo>,</mo> <mn>1</mn> <mo>:</mo> <mi>N</mi> </mrow> <mo>)</mo> </mrow> </mrow> <mo>&rsqb;</mo> </mrow> <mrow> <mo>(</mo> <mi>q</mi> <mo>)</mo> </mrow> </mrow> </mtd> </mtr> <mtr> <mtd> <mn>...</mn> </mtd> </mtr> <mtr> <mtd> <mrow> <mi>I</mi> <mi>F</mi> <mi>F</mi> <mi>T</mi> <mrow> <mo>&lsqb;</mo> <mrow> <mi>g</mi> <mrow> <mo>(</mo> <mrow> <mi>M</mi> <mo>,</mo> <mn>1</mn> <mo>:</mo> <mi>N</mi> </mrow> <mo>)</mo> </mrow> </mrow> <mo>&rsqb;</mo> </mrow> <mrow> <mo>(</mo> <mi>q</mi> <mo>)</mo> </mrow> </mrow> </mtd> </mtr> </mtable> </mfenced> <mo>}</mo> </mrow> <mrow> <mo>(</mo> <mi>p</mi> <mo>)</mo> </mrow> </mrow> </mtd> <mtd> <mrow> <msub> <mi>k</mi> <mi>x</mi> </msub> <mrow> <mo>(</mo> <mi>p</mi> <mo>)</mo> </mrow> <mo>=</mo> <mo>-</mo> <mfrac> <mrow> <mn>2</mn> <mi>&pi;</mi> <mrow> <mo>(</mo> <mrow> <mi>p</mi> <mo>-</mo> <mn>1</mn> </mrow> <mo>)</mo> </mrow> </mrow> <mrow> <mi>M</mi> <mi>&Delta;</mi> <mi>x</mi> </mrow> </mfrac> <mo>&le;</mo> <mn>0</mn> </mrow> </mtd> <mtd> <mrow> <msub> <mi>k</mi> <mi>y</mi> </msub> <mrow> <mo>(</mo> <mi>q</mi> <mo>)</mo> </mrow> <mo>=</mo> <mfrac> <mrow> <mn>2</mn> <mi>&pi;</mi> <mrow> <mo>(</mo> <mrow> <mi>q</mi> <mo>-</mo> <mn>1</mn> </mrow> <mo>)</mo> </mrow> </mrow> <mrow> <mi>N</mi> <mi>&Delta;</mi> <mi>y</mi> </mrow> </mfrac> <mo>&GreaterEqual;</mo> <mn>0</mn> </mrow> </mtd> </mtr> <mtr> <mtd> <mrow> <mi>F</mi> <mi>F</mi> <mi>T</mi> <mrow> <mo>{</mo> <mfenced open = "[" close = "]"> <mtable> <mtr> <mtd> <mrow> <mi>F</mi> <mi>F</mi> <mi>T</mi> <mrow> <mo>&lsqb;</mo> <mrow> <mi>g</mi> <mrow> <mo>(</mo> <mrow> <mn>1</mn> <mo>,</mo> <mn>1</mn> <mo>:</mo> <mi>N</mi> </mrow> <mo>)</mo> </mrow> </mrow> <mo>&rsqb;</mo> </mrow> <mrow> <mo>(</mo> <mi>q</mi> <mo>)</mo> </mrow> </mrow> </mtd> </mtr> <mtr> <mtd> <mrow> <mi>F</mi> <mi>F</mi> <mi>T</mi> <mrow> <mo>&lsqb;</mo> <mrow> <mi>g</mi> <mrow> <mo>(</mo> <mrow> <mn>2</mn> <mo>,</mo> <mn>1</mn> <mo>:</mo> <mi>N</mi> </mrow> <mo>)</mo> </mrow> </mrow> <mo>&rsqb;</mo> </mrow> <mrow> <mo>(</mo> <mi>q</mi> <mo>)</mo> </mrow> </mrow> </mtd> </mtr> <mtr> <mtd> <mn>...</mn> </mtd> </mtr> <mtr> <mtd> <mrow> <mi>F</mi> <mi>F</mi> <mi>T</mi> <mrow> <mo>&lsqb;</mo> <mrow> <mi>g</mi> <mrow> <mo>(</mo> <mrow> <mi>M</mi> <mo>,</mo> <mn>1</mn> <mo>:</mo> <mi>N</mi> </mrow> <mo>)</mo> </mrow> </mrow> <mo>&rsqb;</mo> </mrow> <mrow> <mo>(</mo> <mi>q</mi> <mo>)</mo> </mrow> </mrow> </mtd> </mtr> </mtable> </mfenced> <mo>}</mo> </mrow> <mrow> <mo>(</mo> <mi>p</mi> <mo>)</mo> </mrow> </mrow> </mtd> <mtd> <mrow> <msub> <mi>k</mi> <mi>x</mi> </msub> <mrow> <mo>(</mo> <mi>p</mi> <mo>)</mo> </mrow> <mo>=</mo> <mo>-</mo> <mfrac> <mrow> <mn>2</mn> <mi>&pi;</mi> <mrow> <mo>(</mo> <mrow> <mi>p</mi> <mo>-</mo> <mn>1</mn> </mrow> <mo>)</mo> </mrow> </mrow> <mrow> <mi>M</mi> <mi>&Delta;</mi> <mi>x</mi> </mrow> </mfrac> <mo>&le;</mo> <mn>0</mn> </mrow> </mtd> <mtd> <mrow> <msub> <mi>k</mi> <mi>y</mi> </msub> <mrow> <mo>(</mo> <mi>q</mi> <mo>)</mo> </mrow> <mo>=</mo> <mo>-</mo> <mfrac> <mrow> <mn>2</mn> <mi>&pi;</mi> <mrow> <mo>(</mo> <mrow> <mi>q</mi> <mo>-</mo> <mn>1</mn> </mrow> <mo>)</mo> </mrow> </mrow> <mrow> <mi>N</mi> <mi>&Delta;</mi> <mi>y</mi> </mrow> </mfrac> <mo>&le;</mo> <mn>0</mn> </mrow> </mtd> </mtr> </mtable> </mfenced> </mtd> </mtr> </mtable> </mfenced>Wherein, M and N is respectively dead zone field in the quantity of x and y directions sampled point, kxFor the x durection components of wave number, kyFor wave number Y durection components, g are dead zone electric field component, and G is dead zone rink corner spectral component, and FFT and IFFT are Fast Fourier Transform and inversion Change, p and q are the element numbers of Two-dimensional FFT, and Δ x, Δ y are the spacing of sampled point in the x and y direction, x0、y0It is dead zone center phase To origin.
- A kind of 7. darkroom spheric array Compact Range dead zone characteristic spectrum analysis method according to claim 6, it is characterised in that:kx And kyRelation with angular spectrum incidence angle is,kx=k0sin(θ)cos(φ)ky=k0sin(θ)sin(φ)Wherein, k0For the wave number in free space, θ, φ are the angle component of spherical coordinate system.
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