[go: up one dir, main page]

TWI779895B - Antenna testing method and system thereof - Google Patents

Antenna testing method and system thereof Download PDF

Info

Publication number
TWI779895B
TWI779895B TW110139159A TW110139159A TWI779895B TW I779895 B TWI779895 B TW I779895B TW 110139159 A TW110139159 A TW 110139159A TW 110139159 A TW110139159 A TW 110139159A TW I779895 B TWI779895 B TW I779895B
Authority
TW
Taiwan
Prior art keywords
gain
dimensional coordinate
parameters
under test
device under
Prior art date
Application number
TW110139159A
Other languages
Chinese (zh)
Other versions
TW202318008A (en
Inventor
王文彥
江正雄
Original Assignee
微星科技股份有限公司
大陸商微盟電子(昆山)有限公司
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by 微星科技股份有限公司, 大陸商微盟電子(昆山)有限公司 filed Critical 微星科技股份有限公司
Priority to TW110139159A priority Critical patent/TWI779895B/en
Priority to CN202111452000.1A priority patent/CN116008675A/en
Application granted granted Critical
Publication of TWI779895B publication Critical patent/TWI779895B/en
Publication of TW202318008A publication Critical patent/TW202318008A/en

Links

Images

Landscapes

  • Burglar Alarm Systems (AREA)
  • Testing Electric Properties And Detecting Electric Faults (AREA)
  • Variable-Direction Aerials And Aerial Arrays (AREA)

Abstract

An antenna testing method includes establishing, based on a two-dimensional coordinate system, a position parameter of at least one noise element in a to-be-tested device; measuring a radiation signal from the to-be tested device to generate a three-dimensional gain information, wherein the three-dimensional gain information includes a plurality of three-dimensional coordinate parameters; converting the three-dimensional coordinate parameters into a plurality of two-dimensional coordinate parameters and a plurality of gain parameters under the two-dimensional coordinate system, wherein the two-dimensional coordinate parameters correspond to the gain parameters respectively; generating a gain variation diagram according to the two-dimensional coordinate parameters and the gain parameters; matching the position parameter with the gain variation diagram to obtain a noise interference level respectively corresponding to at least one noise element; and determining, according to the noise interference level, whether the to-be-tested device is a radiation-defective device or not.

Description

天線測試方法及其系統Antenna testing method and system thereof

本發明是關於一種天線技術,尤其是一種天線測試方法及其系統。The present invention relates to an antenna technology, in particular to an antenna testing method and system thereof.

現在的生活中已有許多無線之通訊設備,且此些設備一般設置有天線以實現無線通訊的功能。然而,天線的輻射訊號容易受到雜訊的影響而造成無線通訊效能下降。因此,在產品出廠或維修時,廠商會利用一些測試儀器來對無線通訊設備(即待測裝置)的天線的輻射訊號進行測試及調整,以避免天線的輻射訊號受雜訊影響。然而,由於待測裝置可能具有多種可能對輻射訊號產生影響的元件,致使在進行天線的輻射訊號測試時,無法判斷出雜訊源的位置及無法從根本上消除雜訊源。再者,某些測試儀器(例如頻譜分析儀)也可能增加測試成本。There are many wireless communication devices in today's life, and these devices are generally provided with antennas to realize the function of wireless communication. However, the radiated signal of the antenna is easily affected by noise, which will cause the degradation of wireless communication performance. Therefore, when the product leaves the factory or is repaired, the manufacturer will use some test instruments to test and adjust the radiation signal of the antenna of the wireless communication device (ie, the device under test), so as to prevent the radiation signal of the antenna from being affected by noise. However, since the device under test may have various components that may affect the radiation signal, it is impossible to determine the location of the noise source and fundamentally eliminate the noise source when testing the radiation signal of the antenna. Furthermore, certain test instruments (such as spectrum analyzers) may also increase the cost of testing.

鑑於上述,本發明提供一種天線測試方法及其系統。依據一些實施例,本發明可以分析出雜訊源於待測裝置的位置及雜訊源對於天線的輻射訊號之干擾程度。依據一些實施例,透過簡易的測試設備即可實現天線測試,從而降低測試成本。In view of the above, the present invention provides an antenna testing method and system thereof. According to some embodiments, the present invention can analyze the location where the noise originates from the device under test and the interference degree of the noise source to the radiated signal of the antenna. According to some embodiments, the antenna test can be realized through simple test equipment, thereby reducing the test cost.

依據一些實施例,天線測試方法包含基於一二維座標系統,建立一待測裝置中至少一雜訊元件之一位置參數;量測來自待測裝置之輻射訊號,以產生一三維增益資訊,其中三維增益資訊包含複數三維座標參數;轉換該些三維座標參數為在二維座標系統下之複數二維座標參數及複數增益參數,且該些二維座標參數分別與該些增益參數相對應;根據該些二維座標參數及該些增益參數,產生一增益變化圖;匹配位置參數於增益變化圖,以獲得分別對應於至少一雜訊元件之一雜訊干擾程度;及根據雜訊干擾程度,判斷待測裝置是否為一輻射不良裝置。According to some embodiments, the antenna testing method includes establishing a position parameter of at least one noise element in a device under test based on a two-dimensional coordinate system; measuring a radiation signal from the device under test to generate a three-dimensional gain information, wherein The 3D gain information includes complex 3D coordinate parameters; converting these 3D coordinate parameters into complex 2D coordinate parameters and complex gain parameters under a 2D coordinate system, and these 2D coordinate parameters correspond to the gain parameters respectively; According to these two-dimensional coordinate parameters and these gain parameters, generate a gain variation diagram; match the position parameters in the gain variation diagram to obtain noise interference levels respectively corresponding to at least one noise element; and according to the noise interference degree , to determine whether the device under test is a poor radiation device.

依據一些實施例,天線測試系統包含一天線測試室、一網路分析儀及一計算裝置。天線測試室用以容置一待測裝置並接收待測裝置發出的一輻射訊號。網路分析儀耦接天線測試室。網路分析儀用以量測輻射訊號,並產生一分析資訊。計算裝置耦接網路分析儀。計算裝置用以基於一二維座標系統,建立待測裝置中至少一雜訊元件之一位置參數;依據分析資訊產生一三維增益資訊,其中三維增益資訊包含複數三維座標參數;轉換該些三維座標參數為在二維座標系統下之複數二維座標參數及複數增益參數,且該些二維座標參數分別對應該些增益參數;根據該些二維座標參數及該些增益參數,產生一增益變化圖;匹配位置參數於增益變化圖,以獲得分別對應於至少一雜訊元件之一雜訊干擾程度;及根據雜訊干擾程度,判斷待測裝置是否為一輻射不良裝置。According to some embodiments, an antenna testing system includes an antenna testing chamber, a network analyzer, and a computing device. The antenna testing room is used for accommodating a device under test and receiving a radiation signal from the device under test. A network analyzer is coupled to the antenna test chamber. The network analyzer is used to measure the radiation signal and generate analysis information. The computing device is coupled to the network analyzer. The calculation device is used to establish a position parameter of at least one noise component in the device under test based on a two-dimensional coordinate system; generate a three-dimensional gain information according to the analysis information, wherein the three-dimensional gain information includes complex three-dimensional coordinate parameters; convert the three-dimensional coordinates The parameters are complex two-dimensional coordinate parameters and complex gain parameters under the two-dimensional coordinate system, and the two-dimensional coordinate parameters correspond to the gain parameters respectively; according to the two-dimensional coordinate parameters and the gain parameters, a gain Variation diagram; matching the position parameter with the gain variation diagram to obtain noise interference levels respectively corresponding to at least one noise component; and judging whether the device under test is a poor radiation device according to the noise interference level.

綜上所述,依據一些實施例,藉由將待測元件之雜訊元件之位置參數匹配關聯待測裝置之輻射訊號的增益變化圖,即可從增益變化圖獲得雜訊源的位置及雜訊源對於輻射訊號之干擾程度。依據一些實施例,由於增益變化圖可以是視覺化的圖形,因此使用者可以快速判斷出雜訊源的位置及干擾程度。依據一些實施例,由於簡易的測試設備即可實現天線測試,因此可以降低測試成本。例如,可以僅需被動天線測試儀器(例如天線測試室及網路分析儀)來量測輻射訊號,並以計算裝置來獲得增益變化圖及雜訊干擾程度,從而減少天線測試儀器的成本。To sum up, according to some embodiments, by matching the position parameter of the noise element of the DUT with the gain variation diagram of the radiation signal associated with the DUT, the position of the noise source and the noise source can be obtained from the gain variation diagram. The interference degree of the signal source to the radiated signal. According to some embodiments, since the gain change graph can be a visualized graph, the user can quickly determine the location of the noise source and the degree of interference. According to some embodiments, since antenna testing can be implemented with simple testing equipment, the testing cost can be reduced. For example, only passive antenna test instruments (such as antenna test chambers and network analyzers) can be used to measure radiation signals, and the calculation device can be used to obtain gain variation diagrams and noise interference levels, thereby reducing the cost of antenna test instruments.

參照圖1,係為本發明依據一些實施例之天線測試系統10之架構示意圖。天線測試系統10包含天線測試室12、網路分析儀(Network analyzer)14及計算裝置16。網路分析儀14耦接天線測試室12。計算裝置16耦接網路分析儀14。天線測試室12用以容置一待測裝置20並接收待測裝置20發出的一輻射訊號。例如,天線測試室12包含一本體121及一量測天線123。本體121用以容置待測裝置20。量測天線123用以接收來自待測裝置20的輻射訊號,並將輻射訊號傳輸至網路分析儀14。在一些實施例中,天線測試室12包含吸波元件125。吸波元件125用以吸收天線測試室12內的電磁波,以消除輻射訊號反射疊加的混波效應,從而模擬開闊場域。量測天線123可以為號角天線(Horn antenna)。天線測試室12可以為電波暗室(Electromagnetic anechoic chamber)。待測裝置20可以為具有用以發出輻射訊號的天線之裝置,例如筆記型電腦、電視盒等。網路分析儀14用以量測輻射訊號,並產生一分析資訊,以供計算裝置16進行運算。計算裝置16可以為電腦、微處理機、嵌入式系統等運算裝置。Referring to FIG. 1 , it is a schematic structural diagram of an antenna testing system 10 according to some embodiments of the present invention. The antenna testing system 10 includes an antenna testing room 12 , a network analyzer 14 and a computing device 16 . The network analyzer 14 is coupled to the antenna testing room 12 . The computing device 16 is coupled to the network analyzer 14 . The antenna testing room 12 is used for accommodating a device under test 20 and receiving a radiation signal from the device under test 20 . For example, the antenna test room 12 includes a body 121 and a measurement antenna 123 . The body 121 is used for accommodating the device under test 20 . The measurement antenna 123 is used for receiving the radiation signal from the device under test 20 and transmitting the radiation signal to the network analyzer 14 . In some embodiments, antenna test chamber 12 includes absorbing element 125 . The wave-absorbing element 125 is used to absorb electromagnetic waves in the antenna testing room 12 to eliminate the mixing effect of radiation signal reflection and superimposition, thereby simulating an open field. The measurement antenna 123 may be a horn antenna (Horn antenna). The antenna test chamber 12 may be an electromagnetic anechoic chamber. The device under test 20 may be a device having an antenna for emitting radiation signals, such as a notebook computer, a TV box, and the like. The network analyzer 14 is used for measuring radiation signals and generating analysis information for the computing device 16 to perform calculations. The computing device 16 may be computing devices such as computers, microprocessors, and embedded systems.

參照圖2,係為本發明依據一些實施例之天線測試方法之流程示意圖。天線測試方法適於由計算裝置16執行。首先,計算裝置16基於一二維座標系統,建立待測裝置20中至少一雜訊元件之一位置參數(步驟S201)。雜訊元件可以為待測裝置20中的高頻元件,例如中央處理器、圖形處理器、記憶體等。其中,高頻是指量測天線123之可量測的頻寬範圍,例如高頻為500MHz(百萬赫茲)~26.5GHz(吉赫茲)。二維座標系統可以為單位向量下的球座標系統,且位置參數可以以(θ,φ)來表示。Referring to FIG. 2 , it is a schematic flowchart of an antenna testing method according to some embodiments of the present invention. The antenna testing method is suitable for execution by the computing device 16 . First, the computing device 16 establishes a position parameter of at least one noise component in the device under test 20 based on a two-dimensional coordinate system (step S201 ). The noise components may be high-frequency components in the device under test 20 , such as a central processing unit, a graphics processing unit, a memory, and the like. Wherein, the high frequency refers to the measurable bandwidth range of the measurement antenna 123 , for example, the high frequency ranges from 500 MHz (megahertz) to 26.5 GHz (gigahertz). The two-dimensional coordinate system can be a spherical coordinate system under the unit vector, and the position parameter can be represented by (θ, φ).

以待測裝置20為筆記型電腦為例進行說明。如圖1所示,天線測試室12包含一待測支架127。待測支架127供設置待測裝置20(如筆記型電腦)。筆記型電腦之鍵盤、輸出入埠、電路板及雜訊元件是設置在待測支架127於第一維度X與第二維度Y所形成的第一切面上。筆記型電腦之顯示螢幕是設置在待測支架127於第三維度Z與第一維度X所形成的第二切面上。第一維度X與第二維度Y之間的夾角被定義為二維座標系統中的φ角,第三維度Z與第一維度X之間(或是第三維度Z與第二維度Y之間)的夾角被定義為二維座標系統中的θ角。計算裝置16依據雜訊元件在二維座標系統中的位置,建立雜訊元件的位置參數。The device under test 20 is a notebook computer as an example for illustration. As shown in FIG. 1 , the antenna test room 12 includes a test frame 127 . The test bracket 127 is used for setting the test device 20 (such as a notebook computer). The keyboard, input/output port, circuit board and noise components of the notebook computer are arranged on the first cut plane formed by the first dimension X and the second dimension Y of the bracket 127 to be tested. The display screen of the notebook computer is arranged on the second cut plane formed by the third dimension Z and the first dimension X of the bracket 127 to be tested. The angle between the first dimension X and the second dimension Y is defined as the φ angle in the two-dimensional coordinate system, between the third dimension Z and the first dimension X (or between the third dimension Z and the second dimension Y ) is defined as the angle θ in the two-dimensional coordinate system. The computing device 16 establishes position parameters of the noise element according to the position of the noise element in the two-dimensional coordinate system.

參照圖3及圖4。圖3係為本發明依據一些實施例之待測裝置20之雜訊元件於第一切面上的位置之示意圖。圖4係為本發明依據一些實施例之待測裝置20之雜訊元件於第三切面上的位置之示意圖。其中,第三切面是由第三維度Z與第二維度Y形成。圖3及圖4之待測裝置20是以筆記型電腦為示例,且雜訊元件是以中央處理器31、圖形處理器33及記憶體35A~35B為示例。從圖3及圖4可見,計算裝置16依據中央處理器31、圖形處理器33及記憶體35A~35B在二維座標系統中的位置,而獲得中央處理器31、圖形處理器33及記憶體35A~35B之φ角分別為15∘(度)、145∘、45∘、及80∘,並獲得中央處理器31、圖形處理器33及記憶體35A~35B之θ角皆為105∘,以建立出中央處理器31、圖形處理器33及記憶體35A~35B之位置參數。Refer to FIG. 3 and FIG. 4 . FIG. 3 is a schematic diagram showing the position of the noise element of the device under test 20 on the first cut plane according to some embodiments of the present invention. FIG. 4 is a schematic diagram of the position of the noise element of the device under test 20 on the third cut plane according to some embodiments of the present invention. Wherein, the third cut plane is formed by the third dimension Z and the second dimension Y. The device under test 20 in FIG. 3 and FIG. 4 is an example of a notebook computer, and the noise components are an example of a CPU 31 , a graphics processor 33 and memories 35A-35B. It can be seen from Fig. 3 and Fig. 4 that the computing device 16 obtains the central processing unit 31, the graphics processing unit 33 and the memory according to the positions of the central processing unit 31, the graphics processing unit 33 and the memories 35A~35B in the two-dimensional coordinate system. The φ angles of 35A~35B are 15∘ (degrees), 145∘, 45∘, and 80∘ respectively, and the θ angles of the central processing unit 31, graphics processing unit 33, and memory 35A~35B are all 105∘, so that The location parameters of the CPU 31, the graphics processor 33 and the memories 35A-35B are established.

復參照圖2,計算裝置16透過網路分析儀14量測來自待測裝置20之輻射訊號,以產生三維增益資訊(步驟S203)。具體來說,計算裝置16依據網路分析儀14的分析資訊而產生三維增益資訊。其中,三維增益資訊包含複數三維座標參數。三維座標參數為直角座標系統下的座標參數,且可以以

Figure 02_image001
來表示。在一些實施例中,如圖1所示,待測支架127包含一旋轉軸1271及一旋轉盤1273。旋轉軸1271用以使待測裝置20在第一切面上沿著第一旋轉方向RD1轉動。旋轉盤1273用以使待測裝置20在第二切面上沿著第二旋轉方向RD2轉動。其中,旋轉軸1271及旋轉盤1273的轉動角度可以是由計算裝置16控制。透過轉動待測裝置20,以使計算裝置16透過網路分析儀14所量測到的輻射訊號可以為一三維天線場型。 Referring again to FIG. 2 , the computing device 16 measures the radiation signal from the device under test 20 through the network analyzer 14 to generate three-dimensional gain information (step S203 ). Specifically, the computing device 16 generates three-dimensional gain information according to the analysis information of the network analyzer 14 . Wherein, the 3D gain information includes complex 3D coordinate parameters. The three-dimensional coordinate parameters are coordinate parameters under the Cartesian coordinate system, and can be
Figure 02_image001
To represent. In some embodiments, as shown in FIG. 1 , the test frame 127 includes a rotating shaft 1271 and a rotating disk 1273 . The rotation shaft 1271 is used to rotate the device under test 20 along the first rotation direction RD1 on the first sectional plane. The rotating disc 1273 is used to rotate the device under test 20 along the second rotating direction RD2 on the second sectional plane. Wherein, the rotation angles of the rotating shaft 1271 and the rotating disk 1273 may be controlled by the computing device 16 . By rotating the device under test 20, the radiation signal measured by the computing device 16 through the network analyzer 14 can be a three-dimensional antenna pattern.

接著,計算裝置16轉換該些三維座標參數為在二維座標系統下之複數二維座標參數及複數增益參數(步驟S205)。其中,該些二維座標參數分別與該些增益參數相對應。之後,計算裝置16根據該些二維座標參數及該些增益參數,產生一增益變化圖(步驟S207)。增益變化圖可以是以視覺可辨識的方式來呈現增益的變化,例如增益較高的位置顏色較深,增益較低的位置顏色較淺。在一些實施例中,增益參數可以為天線增益,即比較天線的基底場型與全向性場型而獲得的絕對增益。在一些實施例中,建立位置參數及轉換三維座標參數時是使用同一二維座標系統。舉例來說,計算裝置16依據式1~式3將三維座標參數轉換為二維座標參數及增益參數,其中二維座標參數可以以(θ,φ)表示,增益參數以γ表示,且三維座標參數可以如同前述以

Figure 02_image001
表示。 Next, the computing device 16 converts the three-dimensional coordinate parameters into complex two-dimensional coordinate parameters and complex gain parameters under the two-dimensional coordinate system (step S205 ). Wherein, the two-dimensional coordinate parameters correspond to the gain parameters respectively. Afterwards, the computing device 16 generates a gain variation map according to the two-dimensional coordinate parameters and the gain parameters (step S207 ). The gain variation graph may present the variation of the gain in a visually identifiable manner, for example, a position with a higher gain has a darker color, and a position with a lower gain has a lighter color. In some embodiments, the gain parameter may be antenna gain, that is, the absolute gain obtained by comparing the antenna's ground pattern and omnidirectional pattern. In some embodiments, the same two-dimensional coordinate system is used for establishing the position parameter and converting the three-dimensional coordinate parameter. For example, the computing device 16 converts the three-dimensional coordinate parameters into two-dimensional coordinate parameters and gain parameters according to formulas 1 to 3, wherein the two-dimensional coordinate parameters can be represented by (θ, φ), the gain parameters can be represented by γ, and the three-dimensional coordinate parameters parameters can be as described above
Figure 02_image001
express.

Figure 02_image003
……………………………………(式1)
Figure 02_image003
……………………………………(Formula 1)

Figure 02_image005
……(式2)
Figure 02_image005
... (Formula 2)

Figure 02_image007
………(式3)
Figure 02_image007
……… (Formula 3)

在產生出增益變化圖之後,計算裝置16匹配位置參數於增益變化圖,以獲得分別對應於至少一雜訊元件之一雜訊干擾程度(步驟S209)。由於增益變化圖是依據二維座標參數及增益參數而產生,且二維座標參數及位置參數是基於同一二維座標系統而產生,因此計算裝置16可以依據位置參數之θ角及φ角,而將位置參數匹配於增益變化圖,並將位置參數於增益變化圖之匹配位置中的增益參數作為雜訊干擾程度。例如,當匹配位置中的增益參數較大(或是以顏色較深來呈現)時,表示雜訊干擾程度較大;反之則表示雜訊干擾程度較小。如此,使用者即可快速地得知雜訊元件之雜訊干擾程度之大小,並可判斷出雜訊的來源,以從根本上消除雜訊。After the gain variation map is generated, the calculation device 16 matches the position parameters with the gain variation map to obtain noise interference levels respectively corresponding to at least one noise element (step S209 ). Since the gain change graph is generated based on the two-dimensional coordinate parameters and the gain parameters, and the two-dimensional coordinate parameters and the position parameters are generated based on the same two-dimensional coordinate system, the calculation device 16 can be based on the θ angle and the φ angle of the position parameters, The position parameter is matched to the gain variation diagram, and the gain parameter in the matching position of the position parameter in the gain variation diagram is used as the noise interference degree. For example, when the gain parameter in the matching position is larger (or presented in a darker color), it means that the degree of noise interference is greater; otherwise, it means that the degree of noise interference is smaller. In this way, the user can quickly know the degree of noise interference of the noise element, and can determine the source of the noise, so as to eliminate the noise fundamentally.

參照圖5,係為本發明依據一些實施例之增益變化圖之示意圖。從圖5可見,增益變化圖是以θ角及φ角來作為座標軸,以供位置參數匹配。增益參數是以數值或是顏色深淺來表示大小,且雜訊元件(如中央處理器51、圖形處理器52、記憶體53、通用序列匯流排(USB)54、固態硬碟55)之位置參數於增益變化圖之匹配位置中的增益參數是較大的或是較深的(即雜訊干擾程度是較大的或是較深的),因而可將此些雜訊元件視為雜訊源。也就是說,使用者透過增益變化圖及雜訊干擾程度即可判斷出雜訊源的位置及大小。Referring to FIG. 5 , it is a schematic diagram of a gain variation diagram according to some embodiments of the present invention. It can be seen from FIG. 5 that the gain change graph uses the angle θ and angle φ as coordinate axes for matching position parameters. Gain parameters are represented by numerical values or color shades, and the position parameters of noise components (such as central processing unit 51, graphics processing unit 52, memory 53, universal serial bus (USB) 54, solid state hard disk 55) The gain parameter in the matching position of the gain variation diagram is larger or deeper (that is, the degree of noise interference is larger or deeper), so these noise components can be regarded as noise sources . That is to say, the user can judge the position and size of the noise source through the gain change graph and the degree of noise interference.

復參照圖2,在獲得雜訊干擾程度後,計算裝置16根據雜訊干擾程度,判斷待測裝置20是否為一輻射不良裝置(步驟S211)。在一些實施例中,當雜訊干擾程度不大於一雜訊閾值時,計算裝置16判斷待測裝置20為輻射良品裝置。當雜訊干擾程度大於雜訊閾值時,計算裝置16判斷待測裝置20為輻射不良裝置,並通知使用者(例如以顏色提示、閃爍提示、震動提示、鈴聲提示等方式通知使用者),以使使用者針對雜訊源進行改善。雜訊閾值可以預先儲存或是被輸入於計算裝置16中。Referring again to FIG. 2 , after obtaining the degree of noise interference, the computing device 16 determines whether the device under test 20 is a poor radiation device according to the degree of noise interference (step S211 ). In some embodiments, when the degree of noise interference is not greater than a noise threshold, the computing device 16 determines that the device under test 20 is a radiation-qualified device. When the degree of noise interference is greater than the noise threshold, the computing device 16 determines that the device under test 20 is a poor radiation device, and notifies the user (for example, notifying the user by color prompts, flashing prompts, vibration prompts, ringtone prompts, etc.), and Allow users to improve the noise source. The noise threshold may be pre-stored or entered into the computing device 16 .

在一些實施例中,由於雜訊干擾程度是透過計算裝置16運算而得,因此可以降低受人為變因的影響,以提高分析之穩定性。在一些實施例中,透過簡單的測試設備(如天線測試室12與網路分析儀14),可以減少能量耗損,致使分析所得的雜訊干擾程度與待測裝置20實際使用時所受到的雜訊干擾程度可以是實質一致的。在一些實施例中,由於天線測試方法的流程步驟相對簡易,因此可以減少分析出雜訊干擾程度所需的時間。In some embodiments, since the degree of noise interference is calculated by the computing device 16 , it can reduce the influence of human variables to improve the stability of the analysis. In some embodiments, through simple test equipment (such as the antenna test room 12 and the network analyzer 14), energy consumption can be reduced, so that the degree of noise interference obtained from the analysis is the same as the noise received by the device under test 20 when it is actually used. The degree of signal interference may be substantially consistent. In some embodiments, since the steps of the antenna testing method are relatively simple, the time required for analyzing the degree of noise interference can be reduced.

參照圖6,係為本發明依據一些實施例之天線測試方法的流程示意圖。在一些實施例中,在產生出增益變化圖之前或是之後,計算裝置16取得待測裝置20之影像檔(步驟S601)。例如,計算裝置16可以自其外部或是內部的儲存設備來取得待測裝置20之影像檔。影像檔可以是待測裝置20之機構圖檔或是照片。接著,計算裝置16基於二維座標系統,將增益變化圖結合影像檔(步驟S603)。如此,可以使增益變化圖進一步呈現待測裝置20之元件分布。在本實施例中,建立位置參數、轉換三維座標參數及結合影像檔時是使用同一二維座標系統。舉例來說,計算裝置16對影像檔進行影像辨識,以識別出計算裝置16的每一元件(例如雜訊元件),並依據每一元件在二維座標系統中的位置,而將每一元件在影像檔中的影像淡化後,疊加至增益變化圖中對應的位置。如此,使用者透過處理後的增益變化圖,即可在得知增益大小的同時,得知待測裝置20對應的元件分布。Referring to FIG. 6 , it is a schematic flowchart of an antenna testing method according to some embodiments of the present invention. In some embodiments, the computing device 16 obtains the image file of the device under test 20 before or after generating the gain variation map (step S601 ). For example, the computing device 16 can obtain the image file of the device under test 20 from its external or internal storage device. The image file may be a structural image file or a photo of the device under test 20 . Next, the computing device 16 combines the gain change map with the image file based on the two-dimensional coordinate system (step S603 ). In this way, the gain variation graph can further present the component distribution of the device under test 20 . In this embodiment, the same two-dimensional coordinate system is used when establishing position parameters, converting three-dimensional coordinate parameters and combining image files. For example, the computing device 16 performs image recognition on the image file to identify each component of the computing device 16 (such as a noise component), and according to the position of each component in the two-dimensional coordinate system, each component After the image in the image file is faded, it will be superimposed on the corresponding position in the gain change graph. In this way, the user can know the distribution of components corresponding to the device under test 20 while knowing the magnitude of the gain through the processed gain variation map.

參照圖7,係為本發明依據一些實施例之天線測試方法的流程示意圖。在一些實施例中,在產生出增益變化圖之前,計算裝置16將該些增益參數區分為複數不同的增益階級(步驟S701)。例如,如表1所示,每一不同的增益階級分別對應多個不同的增益參數。接著,計算裝置16是根據該些二維座標參數及該些增益階級,產生增益變化圖(步驟S703)。合併參照圖5,可見藉由以二維座標參數及增益階級60來產生增益變化圖,可以簡化增益變化圖上所呈現的訊息。例如,簡化增益變化圖上所呈現的增益數值而以增益階級60替代呈現。Referring to FIG. 7 , it is a schematic flowchart of an antenna testing method according to some embodiments of the present invention. In some embodiments, before generating the gain change map, the computing device 16 divides the gain parameters into a plurality of different gain levels (step S701 ). For example, as shown in Table 1, each different gain level corresponds to a plurality of different gain parameters. Next, the computing device 16 generates a gain variation map according to the two-dimensional coordinate parameters and the gain levels (step S703 ). Referring to FIG. 5 together, it can be seen that by using the two-dimensional coordinate parameters and the gain level 60 to generate the gain variation diagram, the information presented on the gain variation diagram can be simplified. For example, the gain values presented on the gain variation graph are simplified and presented with gain levels 60 instead.

[表1]係為本發明依據一些實施例之部分的增益階級60與增益參數之對照表。 增益階級 增益參數 5 dBi 5~3 dBi 3 dBi 3~1 dBi 1 dBi 1~-1 dBi -1 dBi -1~-3 dBi -3 dBi -3~-5 dBi -5 dBi -5~-7 dBi -7 dBi -7~-9 dBi [Table 1] is a comparison table of gain stages 60 and gain parameters according to some embodiments of the present invention. Gain class Gain parameter 5 dBi 5~3dBi 3 dBi 3~1dBi 1 dBi 1~-1 dBi -1 dBi -1~-3 dBi -3 dBi -3~-5dBi -5 dBi -5~-7dBi -7 dBi -7~-9 dBi

在一些實施例中,在區分出增益階級60之前,計算裝置16可以根據一臨界上限值及一臨界下限值,刪除超出臨界上限值及臨界下限值之增益參數,並保留在臨界上限值及臨界下限值內之增益參數。之後,計算裝置16是根據被保留的增益參數來區分出不同的增益階級60(步驟S701)。如此,即可簡化增益參數的數據量,以減輕計算裝置16的運算負擔。在一些實施例中,臨界上限值及臨界下限值可以被預先儲存於計算裝置16或是被輸入於計算裝置16。In some embodiments, before distinguishing the gain level 60, the computing device 16 may delete gain parameters that exceed the upper critical limit and the lower critical limit according to an upper critical limit and a lower critical limit, and keep them at the critical upper limit. Gain parameters within the upper limit and critical lower limit. Afterwards, the computing device 16 distinguishes different gain levels 60 according to the retained gain parameters (step S701 ). In this way, the amount of data of the gain parameters can be simplified to reduce the calculation burden of the calculation device 16 . In some embodiments, the upper critical limit and the lower critical limit may be pre-stored or input into the computing device 16 .

在一些實施例中,如圖5所示,計算裝置16是根據一等值線函數來對該些二維座標參數及該些增益階級60進行運算處理,以產生由該些增益階級60形成之一等值線圖,並將等值線圖作為增益變化圖。如此,即可使增益變化圖以連續分布且逐漸變化的方式呈現,並使使用者可以快速地獲得雜訊源的位置及大小。In some embodiments, as shown in FIG. 5 , the calculation device 16 performs calculation processing on the two-dimensional coordinate parameters and the gain levels 60 according to a contour function, so as to generate a result formed by the gain levels 60 A contour map, and use the contour map as a gain change map. In this way, the gain change diagram can be presented in a continuous distribution and gradually changing manner, and the user can quickly obtain the position and size of the noise source.

綜上所述,依據一些實施例,藉由將待測元件之雜訊元件之位置參數匹配關聯待測裝置之輻射訊號的增益變化圖,即可從增益變化圖獲得雜訊源的位置及雜訊源對於輻射訊號之干擾程度。依據一些實施例,由於增益變化圖可以是視覺化的圖形,因此使用者可以快速判斷出雜訊源的位置及干擾程度。依據一些實施例,由於簡易的測試設備即可實現天線測試,因此可以降低測試成本。例如,可以僅需被動天線測試儀器(例如天線測試室及網路分析儀)來量測輻射訊號,並以計算裝置來獲得增益變化圖及雜訊干擾程度,從而減少天線測試儀器的成本。To sum up, according to some embodiments, by matching the position parameter of the noise element of the DUT with the gain variation diagram of the radiation signal associated with the DUT, the position of the noise source and the noise source can be obtained from the gain variation diagram. The interference degree of the signal source to the radiated signal. According to some embodiments, since the gain change graph can be a visualized graph, the user can quickly determine the location of the noise source and the degree of interference. According to some embodiments, since antenna testing can be implemented with simple testing equipment, the testing cost can be reduced. For example, only passive antenna test instruments (such as antenna test chambers and network analyzers) can be used to measure radiation signals, and the calculation device can be used to obtain gain variation diagrams and noise interference levels, thereby reducing the cost of antenna test instruments.

10:天線測試系統 12:天線測試室 121:本體 123:量測天線 125:吸波元件 127:待測支架 1271:旋轉軸 1273:旋轉盤 14:網路分析儀 16:計算裝置 20:待測裝置 31、51:中央處理器 33、52:圖形處理器 35A、35B、53:記憶體 54:通用序列匯流排 55:固態硬碟 60:增益階級 RD1:第一旋轉方向 RD2:第二旋轉方向 X:第一維度 Y:第二維度 Z:第三維度 S201~S211、S601~S603、S701~S703:步驟 θ:角度 φ:角度 10: Antenna test system 12:Antenna test room 121: Ontology 123: Measuring Antenna 125: absorbing element 127: Stent to be tested 1271:Rotary axis 1273: rotating disk 14: Network Analyzer 16: Computing device 20: Device under test 31, 51: CPU 33, 52: graphics processor 35A, 35B, 53: memory 54:Universal serial bus 55: SSD 60: Buff class RD1: First direction of rotation RD2: Second direction of rotation X: first dimension Y: second dimension Z: the third dimension S201~S211, S601~S603, S701~S703: steps θ: angle φ: angle

[圖1]係為本發明依據一些實施例之天線測試系統之架構示意圖。 [圖2]係為本發明依據一些實施例之天線測試方法之流程示意圖。 [圖3]係為本發明依據一些實施例之待測裝置之雜訊元件於第一切面上的位置之示意圖。 [圖4]係為本發明依據一些實施例之待測裝置之雜訊元件於第三切面上的位置之示意圖。 [圖5]係為本發明依據一些實施例之增益變化圖之示意圖。 [圖6]係為本發明依據一些實施例之天線測試方法的流程示意圖。 [圖7]係為本發明依據一些實施例之天線測試方法的流程示意圖。 [ FIG. 1 ] is a schematic structural diagram of an antenna test system according to some embodiments of the present invention. [ FIG. 2 ] is a schematic flowchart of an antenna testing method according to some embodiments of the present invention. [ FIG. 3 ] is a schematic diagram of the position of the noise element of the device under test according to some embodiments of the present invention on the first cut plane. [ FIG. 4 ] is a schematic diagram of the position of the noise element of the device under test according to some embodiments of the present invention on the third cut plane. [ FIG. 5 ] is a schematic diagram of a gain variation diagram according to some embodiments of the present invention. [ FIG. 6 ] is a schematic flowchart of an antenna testing method according to some embodiments of the present invention. [ FIG. 7 ] is a schematic flowchart of an antenna testing method according to some embodiments of the present invention.

S201~S211:步驟 S201~S211: steps

Claims (10)

一種天線測試方法,包含:基於一二維座標系統及依據一待測裝置中至少一雜訊元件在該二維座標系統中的位置,建立該待測裝置中該至少一雜訊元件之一位置參數;量測來自該待測裝置之一輻射訊號,以產生一三維增益資訊,其中該三維增益資訊包含複數三維座標參數;轉換該些三維座標參數為在該二維座標系統下之複數二維座標參數及複數增益參數,且該些二維座標參數分別與該些增益參數相對應;根據該些二維座標參數及該些增益參數,產生一增益變化圖;匹配該位置參數於該增益變化圖,以獲得分別對應於該至少一雜訊元件之一雜訊干擾程度;及根據該雜訊干擾程度,判斷該待測裝置是否為一輻射不良裝置。 An antenna testing method, comprising: based on a two-dimensional coordinate system and according to the position of at least one noise element in a device under test in the two-dimensional coordinate system, establishing a position of the at least one noise element in the device under test Parameters; measuring a radiation signal from the device under test to generate a three-dimensional gain information, wherein the three-dimensional gain information includes complex three-dimensional coordinate parameters; transforming the three-dimensional coordinate parameters into a complex number two under the two-dimensional coordinate system One-dimensional coordinate parameters and complex gain parameters, and these two-dimensional coordinate parameters are respectively corresponding to these gain parameters; according to these two-dimensional coordinate parameters and these gain parameters, a gain change map is generated; matching the position parameter to the gain changing the graph to obtain a noise interference degree respectively corresponding to the at least one noise element; and judging whether the device under test is a poor radiation device according to the noise interference degree. 如請求項1所述之天線測試方法,更包含:將該些增益參數區分為複數不同的增益階級;及產生該增益變化圖的步驟是,根據該些二維座標參數及該些增益階級,產生該增益變化圖。 The antenna testing method as described in Claim 1, further comprising: dividing these gain parameters into multiple different gain levels; and the step of generating the gain change diagram is, according to the two-dimensional coordinate parameters and the gain levels, The gain variation map is generated. 如請求項2所述之天線測試方法,其中,根據該些二維座標參數及該些增益階級,產生該增益變化圖的步驟是,進一步根據一等值線函數,以將由該些增益階級形成之一等值線圖作為該增益變化圖。 The antenna testing method as described in claim 2, wherein, according to the two-dimensional coordinate parameters and the gain levels, the step of generating the gain change map is to further use a contour function to form the gain levels One of the contour maps is used as the gain variation map. 如請求項1所述之天線測試方法,其中,當該雜訊干擾程度大於一雜訊閾值時,判斷該待測裝置為該輻射不良裝置。 The antenna testing method according to claim 1, wherein when the noise interference degree is greater than a noise threshold, it is determined that the device under test is the poor radiation device. 如請求項1所述之天線測試方法,更包含: 取得該待測裝置之一影像檔;及基於該二維座標系統,將該增益變化圖結合該影像檔,以使該增益變化圖進一步呈現該待測裝置之元件分布。 The antenna testing method as described in claim 1 further includes: Obtaining an image file of the device under test; and combining the gain change map with the image file based on the two-dimensional coordinate system, so that the gain change map further presents the component distribution of the device under test. 一種天線測試系統,包含:一天線測試室,用以容置一待測裝置並接收該待測裝置發出的一輻射訊號;一網路分析儀,耦接該天線測試室,用以量測該輻射訊號,並產生一分析資訊;及一計算裝置,耦接該網路分析儀,用以基於一二維座標系統及依據該待測裝置中至少一雜訊元件在該二維座標系統中的位置,建立該待測裝置中該至少一雜訊元件之一位置參數;依據該分析資訊產生一三維增益資訊,其中該三維增益資訊包含複數三維座標參數;轉換該些三維座標參數為在該二維座標系統下之複數二維座標參數及複數增益參數,且該些二維座標參數分別對應該些增益參數;根據該些二維座標參數及該些增益參數,產生一增益變化圖;匹配該位置參數於該增益變化圖,以獲得分別對應於該至少一雜訊元件之一雜訊干擾程度;及根據該雜訊干擾程度,判斷該待測裝置是否為一輻射不良裝置。 An antenna test system, comprising: an antenna test room for accommodating a device under test and receiving a radiation signal from the device under test; a network analyzer coupled to the antenna test room for measuring the Radiation signal, and generate an analysis information; and a computing device, coupled to the network analyzer, to be based on a two-dimensional coordinate system and according to the at least one noise component in the device under test in the two-dimensional coordinate system position, establishing a position parameter of the at least one noise element in the device under test; generating a three-dimensional gain information according to the analysis information, wherein the three-dimensional gain information includes complex three-dimensional coordinate parameters; transforming the three-dimensional coordinate parameters into the two Complex two-dimensional coordinate parameters and complex gain parameters under the three-dimensional coordinate system, and these two-dimensional coordinate parameters correspond to these gain parameters respectively; according to these two-dimensional coordinate parameters and these gain parameters, a gain change map is generated; matching The position parameter is used in the gain change diagram to obtain noise interference levels respectively corresponding to the at least one noise element; and according to the noise interference levels, it is judged whether the device under test is a poor radiation device. 如請求項6所述之天線測試系統,其中,該計算裝置將該些增益參數區分為複數不同的增益階級,並根據該些二維座標參數及該些增益階級,產生該增益變化圖。 The antenna test system as described in Claim 6, wherein the calculating device divides the gain parameters into multiple gain levels, and generates the gain change diagram according to the two-dimensional coordinate parameters and the gain levels. 如請求項7所述之天線測試系統,其中,該計算裝置根據該些二維座標參數、該些增益階級及一等值線函數,產生由該些增益階級形成之一等值線圖,以作為該增益變化圖。 The antenna test system as described in Claim 7, wherein the calculation device generates a contour map formed by the gain stages according to the two-dimensional coordinate parameters, the gain stages and a contour function, so as to as the gain variation graph. 如請求項6所述之天線測試系統,其中,當該雜訊干擾程度大於一雜訊閾值時,該計算裝置判斷該待測裝置為該輻射不良裝置。 The antenna testing system according to claim 6, wherein when the noise interference degree is greater than a noise threshold, the computing device determines that the device under test is the poor radiation device. 如請求項6所述之天線測試系統,其中,該計算裝置取得該待測裝置之一影像檔,並基於該二維座標系統,將該增益變化圖結合該影像檔,以使該增益變化圖進一步呈現該待測裝置之元件分布。 The antenna test system as described in claim 6, wherein the computing device obtains an image file of the device under test, and combines the gain change map with the image file based on the two-dimensional coordinate system, so that the gain change map The component distribution of the device under test is further presented.
TW110139159A 2021-10-21 2021-10-21 Antenna testing method and system thereof TWI779895B (en)

Priority Applications (2)

Application Number Priority Date Filing Date Title
TW110139159A TWI779895B (en) 2021-10-21 2021-10-21 Antenna testing method and system thereof
CN202111452000.1A CN116008675A (en) 2021-10-21 2021-12-01 Antenna testing method and system thereof

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
TW110139159A TWI779895B (en) 2021-10-21 2021-10-21 Antenna testing method and system thereof

Publications (2)

Publication Number Publication Date
TWI779895B true TWI779895B (en) 2022-10-01
TW202318008A TW202318008A (en) 2023-05-01

Family

ID=85475807

Family Applications (1)

Application Number Title Priority Date Filing Date
TW110139159A TWI779895B (en) 2021-10-21 2021-10-21 Antenna testing method and system thereof

Country Status (2)

Country Link
CN (1) CN116008675A (en)
TW (1) TWI779895B (en)

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101088016A (en) * 2004-10-25 2007-12-12 高通股份有限公司 Systems, methods and apparatus for determining a radiated performance of a wireless device
US20110133982A1 (en) * 2007-12-31 2011-06-09 Elta Systems Ltd. System and Method for Calibration of Phased Array Antenna Having Integral Calibration Network in Presence of an Interfering Body
CN102967771A (en) * 2011-09-01 2013-03-13 太阳诱电株式会社 An electromagnetic interference source determiner, an electromagnetic determining method, and an information storage medium
CN111208463A (en) * 2020-01-15 2020-05-29 湖南卫导信息科技有限公司 Link insertion loss rapid calibration method for darkroom starry test system
US11131701B1 (en) * 2019-07-03 2021-09-28 The United States Of America, As Represented By The Secretary Of The Navy Multi-probe anechoic chamber for beam performance testing of an active electronically steered array antenna

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP3775999B2 (en) * 2001-04-23 2006-05-17 富士通テン株式会社 Noise visualization system and display method thereof
FR3001550B1 (en) * 2013-01-31 2015-02-06 Eutelsat Sa DATA COLLECTION DEVICE AND METHOD FOR LOCATING AN INTERFERENCE SOURCE
TWI667842B (en) * 2016-04-15 2019-08-01 和碩聯合科技股份有限公司 Antenna system and control method
CN107679304B (en) * 2017-09-22 2021-05-11 北京神州泰岳软件股份有限公司 Method and device for calculating gain of three-dimensional antenna
CN111601332A (en) * 2019-02-21 2020-08-28 大唐移动通信设备有限公司 Method and device for determining position of interference source

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101088016A (en) * 2004-10-25 2007-12-12 高通股份有限公司 Systems, methods and apparatus for determining a radiated performance of a wireless device
US20110133982A1 (en) * 2007-12-31 2011-06-09 Elta Systems Ltd. System and Method for Calibration of Phased Array Antenna Having Integral Calibration Network in Presence of an Interfering Body
CN102967771A (en) * 2011-09-01 2013-03-13 太阳诱电株式会社 An electromagnetic interference source determiner, an electromagnetic determining method, and an information storage medium
US11131701B1 (en) * 2019-07-03 2021-09-28 The United States Of America, As Represented By The Secretary Of The Navy Multi-probe anechoic chamber for beam performance testing of an active electronically steered array antenna
CN111208463A (en) * 2020-01-15 2020-05-29 湖南卫导信息科技有限公司 Link insertion loss rapid calibration method for darkroom starry test system

Also Published As

Publication number Publication date
CN116008675A (en) 2023-04-25
TW202318008A (en) 2023-05-01

Similar Documents

Publication Publication Date Title
US9699678B2 (en) Plane wave generation within a small volume of space for evaluation of wireless devices
US10116398B2 (en) System for testing efficacy of electromagnetic shielding and method
CN108923863B (en) Equipment Equivalent Isotropic Radiated Power Measurement Method, Apparatus, Equipment and Medium
CN110542798A (en) Method and system for testing antenna arrays using midfield antenna patterns
CN104730503B (en) Determine methods and compensation method of the high resolution SAR reference target RCS on calibration influence
CN106526562A (en) Antenna directional pattern-based method for correcting RCS of calculation target
JP7016303B2 (en) Radiation power estimation method
US11656260B2 (en) Electromagnetic wave measurement point calculation program and radiation interference wave measurement device
Gregson et al. Examination of the effect of common CATR quiet zone specifications on antenna pattern measurement uncertainties
CN107228797B (en) Shock location method and device
US12176961B2 (en) System and method for determining corrected total radiated power (TRP) or corrected total isotropic sensitivity (TIS) of offset antenna under test
TWI779895B (en) Antenna testing method and system thereof
TWI846058B (en) Method and system for aligning test environments
US11012163B1 (en) Apparatus and methods for fast and accurate near-field measurement
CN112114293A (en) Device and method for testing performance of millimeter wave radar under multipath condition
Jankowski-Mihułowicz et al. Numerical model of directional radiation pattern based on primary antenna parameters
Monebhurrun et al. Development of IEEE P2816: Recommended practice for computational electromagnetics applied to modeling and simulation of antennas
CN219225073U (en) Accuracy verification system of target RCS
US12422468B2 (en) Method of testing multi-panel user equipment with spherical coverage
US12339395B2 (en) Object detection apparatus, object detection method, and non-transitory computer readable medium
Chiu et al. Robust and fast near-field antenna measurement technique
Stockman et al. Efficient full-wave modeling of electromagnetic interference in the presence of multiple non-collocated noise sources
CN120547606A (en) Unified RCS modeling method for multiple perception targets based on communication and perception integration
Jung et al. Analysis of reflection and scattering characteristics at the 60GHz frequency
Molares et al. The influence of positional uncertainty in free-field microphone calibration

Legal Events

Date Code Title Description
GD4A Issue of patent certificate for granted invention patent