TWI698649B - Antenna measurment system for mimo ota - Google Patents

Antenna measurment system for mimo ota Download PDF

Info

Publication number
TWI698649B
TWI698649B TW108132966A TW108132966A TWI698649B TW I698649 B TWI698649 B TW I698649B TW 108132966 A TW108132966 A TW 108132966A TW 108132966 A TW108132966 A TW 108132966A TW I698649 B TWI698649 B TW I698649B
Authority
TW
Taiwan
Prior art keywords
corner
bottom corner
rotating base
anechoic chamber
field antenna
Prior art date
Application number
TW108132966A
Other languages
Chinese (zh)
Other versions
TW202111338A (en
Inventor
何松林
盧增錦
張耀元
邱宗文
宋芳燕
洪淑芬
Original Assignee
川升股份有限公司
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 川升股份有限公司 filed Critical 川升股份有限公司
Priority to TW108132966A priority Critical patent/TWI698649B/en
Application granted granted Critical
Publication of TWI698649B publication Critical patent/TWI698649B/en
Publication of TW202111338A publication Critical patent/TW202111338A/en

Links

Images

Landscapes

  • Aerials With Secondary Devices (AREA)

Abstract

An antenna measurement system for MIMO OTA includes an anechoic chamber, a rotating base and a plurality of CATR units. The rotating base is used to place a DUT. The DUT includes a plurality of antennas to be tested. A signal source in each of the CATR units is configured to emit a first RF signal toward the corresponding concave mirror, the concave mirror reflecting the first RF signal into a second RF signal, wherein each of the second RF signals is a uniform plane wave and each second RF signal is transmitted toward a platform of the rotating base, and the concave mirrors of any two CATR units are not disposed face to face.

Description

用於多輸入多輸出空中傳輸的天線量測系統 Antenna measurement system for multi-input multi-output air transmission

本發明是關於一種量測系統,特別是一種應用於多重路徑環境下的多輸入多輸出空中傳輸量測系統。 The invention relates to a measurement system, in particular to a multi-input multi-output air transmission measurement system applied in a multi-path environment.

參閱圖1,是美國專利申請號US 2012/0282863 A1(以下簡稱已知技術1)公開的一種天線測試系統的局部示意圖,此種已知技術是將一待測裝置17放置在電波暗室1中,並利用6個測試天線等間距地環繞該待測裝置17,以量測該待測裝置17的天線特性。 1 is a partial schematic diagram of an antenna testing system disclosed in US Patent Application No. US 2012/0282863 A1 (hereinafter referred to as known technology 1). This known technology is to place a device under test 17 in an anechoic chamber 1 , And use 6 test antennas to surround the device under test 17 at equal intervals to measure the antenna characteristics of the device under test 17.

這種已知技術1的缺點在於:(1)、測試天線11與測試天線12彼此相對,所以量測該待測裝置17的接收特性時,相對的兩測試天線11、12所發射出的電磁波就會彼此碰撞干擾造成量測誤差,同理,相對的兩測試天線13、14,以及相對的兩測試天線15、16也會有同樣的問題。(2)、習知1若是採用遠場量測技術,則該等測試天線11、12、13、14、15、16中的任一者距離該待測裝置17的距離r就必須遠大於2D2/λ,以使得從每一個測試天線11、12、13、14、15、16到達該待測裝置17的電磁波是近似均勻平面波。純理論計算時,參數D就是待測天線171的最大幾何直徑,λ是量測時該待測天線171的工作波長,然而在實務應用上,若是該待測裝置17是手機、平板,或是筆記型電腦,則該待測天線171是連接待測裝置17內部的電 路板(圖未示出),以將此電路板作為參考接地面,這會使得整體待測裝置17都參與輻射,而不僅只是該待測天線171而已,因此,為了修正理論與實務的偏差,參數D應修正為待測裝置17的最大幾何直徑,在進入5G毫米波的通訊時代,智慧型手機的尺寸所對應的參數D幾乎不變,但是毫米波的波長λ小至毫米等級,經計算2D2/λ就會變得非常大,因此用於5G通訊量測時的電波暗室1的空間就要遠大於4G通訊量測時的要求,這會嚴重增加建置的場地需求並提高建置費用。(3)、若是要解決前述第(2)項的問題,則類似如圖1的已知技術就得採用近場量測技術以取代遠場量測技術,但近場量測技術在過去被動式天線量測就得將到達該待測裝置17處的非均勻平面波的相位經過複雜的計算,才能轉換達到近似遠場的量測效果,不但無法避免地引入轉換計算誤差,還會因計算時間降低量測效率,但更難克服的問題就是近場量測只適用於被動式量測(待測裝置17關機並將待測天線171以傳導線外接儀器量測),無法對該待測裝置17進行主動式量測(就是將待測裝置17開機進入實際通訊模式量測),原因在於近場量測必須知道量測時電磁波的相位,再利用數值計算的方式將近場量的數據轉換成遠場,但是該待測裝置17於主動式量測時的電磁波都是經過通訊調變後的訊號,因此難以回推計算未調變前的電磁波相位,且越複雜的計算過程引入的誤差和運算時間需求也越大,因此已知技術也沒有辦法解決5G毫米波主動式量測時電波暗室1的空間需求問題。 The disadvantages of this known technology 1 are: (1) The test antenna 11 and the test antenna 12 are opposite to each other, so when measuring the receiving characteristics of the device under test 17, the electromagnetic waves emitted by the two opposite test antennas 11, 12 are It will collide and interfere with each other and cause measurement errors. Similarly, the two opposite test antennas 13, 14 and the opposite two test antennas 15, 16 will have the same problem. (2). Convention 1 If far-field measurement technology is used, the distance r between any one of the test antennas 11, 12, 13, 14, 15, 16 and the device under test 17 must be much greater than 2D 2 /λ, so that the electromagnetic waves arriving at the device under test 17 from each test antenna 11, 12, 13, 14, 15, 16 are approximately uniform plane waves. In a purely theoretical calculation, the parameter D is the maximum geometric diameter of the antenna 171 under test, and λ is the working wavelength of the antenna 171 under test during measurement. However, in practical applications, if the device under test 17 is a mobile phone, a tablet, or For notebook computers, the antenna under test 171 is connected to a circuit board (not shown in the figure) inside the device under test 17 to use this circuit board as a reference ground plane, which will make the entire device under test 17 participate in radiation, not just It is only the antenna 171 under test. Therefore, in order to correct the deviation between theory and practice, the parameter D should be corrected to the maximum geometric diameter of the device under test 17. In the era of 5G millimeter wave communication, the size of the smartphone corresponds to the parameter D is almost unchanged, but the wavelength λ of millimeter waves is as small as millimeters, and 2D 2 /λ will become very large after calculation. Therefore, the space of the anechoic chamber 1 used for 5G communication measurement is much larger than the 4G communication volume. Time measurement requirements, which will seriously increase the site requirements for construction and increase construction costs. (3). If the problem in item (2) above is to be solved, the known technology similar to Figure 1 has to use near-field measurement technology to replace far-field measurement technology, but near-field measurement technology has been passive in the past For antenna measurement, the phase of the non-uniform plane wave arriving at the device under test 17 must undergo complex calculations to convert to approximate far-field measurement results. Not only does it unavoidably introduce conversion calculation errors, but also reduces the calculation time. Measurement efficiency, but the more difficult problem to overcome is that the near field measurement is only suitable for passive measurement (the device under test 17 is turned off and the antenna 171 under test is measured with a conductive wire connected to an external instrument), and the device under test 17 cannot be measured. Active measurement (that is, the device under test 17 is turned on to enter the actual communication mode for measurement). The reason is that the near-field measurement must know the phase of the electromagnetic wave during the measurement, and then use numerical calculation to convert the near-field data into the far-field However, the electromagnetic waves of the device under test 17 during active measurement are all signals after communication modulation, so it is difficult to calculate the phase of the electromagnetic waves before the unmodulation, and the more complicated the calculation process introduces errors and calculation time The demand is also greater, and therefore, the known technology cannot solve the problem of the space requirement of the anechoic chamber 1 during the 5G millimeter wave active measurement.

為了解決前述已知技術的問題,本發明提出一種相較遠場量測節省電波暗室的空間,無須近場轉遠場的繁複 計算,同時適用主、被動式量測,以及還能避免多個測試天線彼此電磁干擾的測試系統。 In order to solve the aforementioned problems of the known technology, the present invention proposes a method that saves the space of the anechoic chamber compared to the far-field measurement, and does not require the complexities of converting the near field to the far field. Calculation, applicable to both active and passive measurement, as well as a test system that can avoid electromagnetic interference between multiple test antennas.

本發明用於多輸入多輸出空中傳輸的天線量測系統包括一電波暗室、一旋轉基座及多數個縮距場天線單元。 The antenna measurement system used for multi-input multi-output air transmission of the present invention includes an electric wave anechoic chamber, a rotating base and a plurality of short-distance field antenna units.

該旋轉基座設置於該電波暗室中,該旋轉基座包括一平台面,該平台面用以放置一待測裝置,該待測裝置包括多數個待測天線。 The rotating base is arranged in the anechoic chamber, and the rotating base includes a platform surface for placing a device to be tested, and the device to be tested includes a plurality of antennas to be tested.

每一個縮距場天線單元包括一訊號饋源,一凹面鏡,一用以固定該訊號饋源與該凹面鏡的連接臂,每一個縮距場天線單元中的該訊號饋源用以朝向對應的該凹面鏡發射一第一射頻訊號,該凹面鏡面向該旋轉基座的平台面設置,用以將該第一射頻訊號反射成為朝向該旋轉基座的平台面的一第二射頻訊號,其中,每一第二射頻訊號是均勻平面波,且任兩個縮距場天線單元的凹面鏡不面對面地設置。 Each narrow field antenna unit includes a signal feed, a concave mirror, and a connecting arm for fixing the signal feed and the concave mirror. The signal feed in each narrow field antenna unit is used to face the corresponding The concave mirror emits a first radio frequency signal, and the concave mirror is arranged facing the platform surface of the rotating base to reflect the first radio frequency signal into a second radio frequency signal facing the platform surface of the rotating base, wherein each The two radio frequency signals are uniform plane waves, and the concave mirrors of any two narrow-field antenna units are not arranged face to face.

較佳地,該電波暗室呈一立方體,並包括一第一頂角、一第二頂角、一第三頂角、一第四頂角、一第一底角、一第二底角、一第三底角、一第四底角。該第一頂角、該旋轉基座的平台面及該第三底角三者依序沿著一直線排列;該第二頂角、該旋轉基座的平台面及該第四底角三者依序沿著一直線排列;該第三頂角、該旋轉基座的平台面及該第一底角三者依序沿著一直線排列;該第四頂角、該旋轉基座的平台面及該第二底角三者依序沿著一直線排列。其中,該等縮 距場天線單元的數量是兩個,分別位於第一頂角及第二底角。 Preferably, the anechoic chamber is in the shape of a cube and includes a first top corner, a second top corner, a third top corner, a fourth top corner, a first bottom corner, a second bottom corner, and a The third bottom corner, a fourth bottom corner. The first top angle, the platform surface of the rotating base, and the third bottom angle are sequentially arranged along a straight line; the second top angle, the platform surface of the rotating base, and the fourth bottom angle are arranged according to The sequence is arranged along a straight line; the third vertex, the platform surface of the rotating base, and the first bottom angle are sequentially arranged along a straight line; the fourth vertex angle, the platform surface of the rotating base, and the The three bottom corners are arranged in sequence along a straight line. Among them, the contraction The number of distance field antenna elements is two, which are located at the first top corner and the second bottom corner respectively.

較佳地,該電波暗室呈一立方體,並包括一第一頂角、一第二頂角、一第三頂角、一第四頂角、一第一底角、一第二底角、一第三底角、一第四底角。該第一頂角、該旋轉基座的平台面及該第三底角三者依序沿著一直線排列;該第二頂角、該旋轉基座的平台面及該第四底角三者依序沿著一直線排列;該第三頂角、該旋轉基座的平台面及該第一底角三者依序沿著一直線排列;該第四頂角、該旋轉基座的平台面及該第二底角三者依序沿著一直線排列。其中,該等縮距場天線單元的數量是三個,分別位於第一頂角、第二底角,以及第三底角與第四頂角的連線中間。 Preferably, the anechoic chamber is in the shape of a cube and includes a first top corner, a second top corner, a third top corner, a fourth top corner, a first bottom corner, a second bottom corner, and a The third bottom corner, a fourth bottom corner. The first top angle, the platform surface of the rotating base, and the third bottom angle are sequentially arranged along a straight line; the second top angle, the platform surface of the rotating base, and the fourth bottom angle are arranged according to The sequence is arranged along a straight line; the third vertex, the platform surface of the rotating base, and the first bottom angle are sequentially arranged along a straight line; the fourth vertex angle, the platform surface of the rotating base, and the The three bottom corners are arranged in sequence along a straight line. Wherein, the number of the reduced-distance field antenna units is three, which are respectively located at the first top corner, the second bottom corner, and the middle of the line connecting the third bottom corner and the fourth top corner.

較佳地,該電波暗室呈一立方體,並包括一第一頂角、一第二頂角、一第三頂角、一第四頂角、一第一底角、一第二底角、一第三底角、一第四底角。該第一頂角、該旋轉基座的平台面及該第三底角三者依序沿著一直線排列;該第二頂角、該旋轉基座的平台面及該第四底角三者依序沿著一直線排列;該第三頂角、該旋轉基座的平台面及該第一底角三者依序沿著一直線排列;該第四頂角、該旋轉基座的平台面及該第二底角三者依序沿著一直線排列,其中,該等縮距場天線單元的數量是四個,分別位於第一頂角、第二底角、第三頂角及第四底角。 Preferably, the anechoic chamber is in the shape of a cube and includes a first top corner, a second top corner, a third top corner, a fourth top corner, a first bottom corner, a second bottom corner, and a The third bottom corner, a fourth bottom corner. The first top angle, the platform surface of the rotating base, and the third bottom angle are sequentially arranged along a straight line; the second top angle, the platform surface of the rotating base, and the fourth bottom angle are arranged according to The sequence is arranged along a straight line; the third vertex, the platform surface of the rotating base, and the first bottom angle are sequentially arranged along a straight line; the fourth vertex angle, the platform surface of the rotating base, and the The three of the two bottom corners are arranged in sequence along a straight line, wherein the number of the reduced-distance field antenna units is four, which are respectively located at the first top corner, the second bottom corner, the third top corner, and the fourth bottom corner.

較佳地,該電波暗室呈一立方體,並包括一第一 頂角、一第二頂角、一第三頂角、一第四頂角、一第一底角、一第二底角、一第三底角、一第四底角。該第一頂角、該旋轉基座的平台面及該第三底角三者依序沿著一直線排列;該第二頂角、該旋轉基座的平台面及該第四底角三者依序沿著一直線排列;該第三頂角、該旋轉基座的平台面及該第一底角三者依序沿著一直線排列;該第四頂角、該旋轉基座的平台面及該第二底角三者依序沿著一直線排列。其中,該等縮距場天線單元的數量是六個,分別位於第一頂角、第二底角、第三頂角、第四底角、第二頂角與第二底角的連線中間,以及第三頂角與第三底角的連線中間。 Preferably, the anechoic chamber is a cube and includes a first Top corner, a second top corner, a third top corner, a fourth top corner, a first bottom corner, a second bottom corner, a third bottom corner, and a fourth bottom corner. The first top angle, the platform surface of the rotating base, and the third bottom angle are sequentially arranged along a straight line; the second top angle, the platform surface of the rotating base, and the fourth bottom angle are arranged according to The sequence is arranged along a straight line; the third vertex, the platform surface of the rotating base, and the first bottom angle are sequentially arranged along a straight line; the fourth vertex angle, the platform surface of the rotating base, and the The three bottom corners are arranged in sequence along a straight line. Among them, the number of the reduced-distance field antenna units is six, which are located in the middle of the line connecting the first top corner, the second bottom corner, the third top corner, the fourth bottom corner, the second top corner, and the second bottom corner. , And the middle of the line between the third top corner and the third bottom corner.

較佳地,該電波暗室還包括多數個螺絲孔,每一個縮距場天線單元的連接臂包括一第一臂部及一第二臂部,每一第一臂部固定於該電波暗室,每一連接臂的第二臂部與該凹面鏡相連接。 Preferably, the anechoic chamber further includes a plurality of screw holes, and the connecting arm of each shortened field antenna unit includes a first arm portion and a second arm portion, and each first arm portion is fixed to the anechoic chamber, each The second arm part of a connecting arm is connected with the concave mirror.

較佳地,該凹面鏡可以相對該連接臂的第二臂部轉動。 Preferably, the concave mirror can rotate relative to the second arm portion of the connecting arm.

較佳地,用於多輸入多輸出空中傳輸的天線量測系統更包括一第一支撐板,該第一支撐板為非導體、低介電常數(permittivity)、低介質損耗(dielectric loss)的材料,該第一支撐板固定於該電波暗室的一壁板,用來支撐對應的一個該縮距場天線單元的重量,且受該第一支撐板支撐的該縮距場天線單元是位於第三頂角與第三底角的連線中間的位 置。 Preferably, the antenna measurement system for multi-input multi-output air transmission further includes a first support plate, the first support plate is non-conductor, low permittivity (permittivity), low dielectric loss (dielectric loss) Material, the first supporting plate is fixed to a wall plate of the anechoic chamber to support the weight of a corresponding one of the short-distance field antenna units, and the short-distance field antenna unit supported by the first supporting plate is located in the first The position in the middle of the line between the three top corners and the third bottom corner Set.

較佳地,用於多輸入多輸出空中傳輸的天線量測系統,更包括一個也是非導體、低介電常數、低介質損耗的第二支撐板,該第二支撐板固定於該電波暗室的該壁板,用來支撐對應的另一個該縮距場天線單元的重量,且受該第二支撐板支撐的該縮距場天線單元是位於第二頂角與第二底角的連線中間的位置。 Preferably, the antenna measurement system for multi-input multi-output air transmission further includes a second support plate that is also non-conductor, low dielectric constant, and low dielectric loss, and the second support plate is fixed to the anechoic chamber. The wall plate is used to support the weight of another corresponding narrow-range field antenna unit, and the narrow-range field antenna unit supported by the second support plate is located in the middle of the line connecting the second top corner and the second bottom corner s position.

較佳地,用於多輸入多輸出空中傳輸的天線量測系統更包括呈T形狀或倒L形狀的一第一支撐柱及一第二支撐柱,該第一支撐板為非導體、低介電常數、低介質損耗的材料,該第一支撐柱固定於該電波暗室的一底板上,用來支撐對應的一個該縮距場天線單元的重量,且受該第一支撐柱支撐的該縮距場天線單元是位於第三頂角與第三底角的連線中間的位置,該第二支撐柱也是非導體、低介電常數、低介質損耗的材料,該第二支撐柱固定於該電波暗室的該底板上,用來支撐對應的另一個該縮距場天線單元的重量,且受該第二支撐柱支撐的該縮距場天線單元是位於第二頂角與第二底角的連線中間的位置。 Preferably, the antenna measurement system for multi-input multi-output air transmission further includes a first support column and a second support column in a T shape or an inverted L shape, and the first support plate is a non-conductor, low dielectric The first support column is fixed on a bottom plate of the electric wave anechoic chamber to support the weight of a corresponding one of the narrow-distance field antenna units, and is supported by the first support column. The distance field antenna unit is located in the middle of the line connecting the third top angle and the third bottom angle. The second support column is also a non-conductor, low dielectric constant, and low dielectric loss material. The second support column is fixed on the On the bottom plate of the anechoic chamber, it is used to support the weight of another corresponding narrowing field antenna unit, and the narrowing field antenna unit supported by the second supporting column is located at the second top corner and the second bottom corner The position in the middle of the connection.

本發明之效果在於:利用縮距場天線單元的凹面鏡將來自訊號饋源的非均勻平面波(第一射頻訊號)反射成均勻平面波(第二射頻訊號),就不受限如圖1習知技術參數r必須遠大於2D2/λ到達該待測裝置才是均勻平面波的限制,因 此改進了遠場量測電波暗室空間需求大或是近場量測計算複雜且不適合主動式量測的問題;此外,本發明亦考量該多數個縮距場天線單元在電波暗室中的空間配置,避免多輸入多輸出(MIMO)測試時任兩個縮距場天線單元反射出的第二射頻訊號相互碰撞干擾的問題。 The effect of the present invention is to use the concave mirror of the telescopic field antenna unit to reflect the non-uniform plane wave (the first radio frequency signal) from the signal feed into a uniform plane wave (the second radio frequency signal). The parameter r must be much larger than 2D 2 /λ to reach the device under test to reach the limit of the uniform plane wave. Therefore, the problem of large space requirement of the anechoic chamber for far-field measurement or complex calculation of near-field measurement and not suitable for active measurement is improved; In addition, the present invention also considers the spatial configuration of the plurality of short-distance field antenna units in the anechoic chamber, so as to avoid the collision and interference of the second radio frequency signals reflected by any two short-distance field antenna units during the multiple input multiple output (MIMO) test. problem.

1:電波暗室 1: anechoic chamber

11~16:測試天線 11~16: Test antenna

17:待測裝置 17: Device under test

171:待測天線 171: Antenna to be tested

2:電波暗室 2: anechoic chamber

200:壁板 200: siding

201:底板 201: Floor

21:第一頂角 21: The first vertex

22:第二頂角 22: second top corner

23:第三頂角 23: third vertex

24:第四頂角 24: fourth vertex

25:第一底角 25: first bottom corner

26:第二底角 26: second bottom corner

27:第三底角 27: Third bottom corner

28:第四底角 28: Fourth bottom corner

3:旋轉基座 3: Rotating base

31:平台面 31: platform surface

4:縮距場天線單元 4: Short-distance field antenna unit

41:訊號饋源 41: signal feed

42:凹面鏡 42: Concave mirror

43:連接臂 43: connecting arm

431:第一臂部 431: first arm

4311:螺絲 4311: screw

4312:固定金屬片 4312: fixed metal sheet

432:第二臂部 432: second arm

5:待測裝置 5: Device to be tested

51:待測天線 51: Antenna to be tested

111:第一射頻訊號 111: The first RF signal

112:第二射頻訊號 112: Second RF signal

291、293:位置 291, 293: Location

20:螺絲孔 20: Screw hole

61:第一支撐板 61: The first support plate

61:第二支撐板 61: second support plate

71:第一支撐柱 71: The first support column

72:第二支撐柱 72: second support column

第1圖是習知技術的局部示意圖。 Figure 1 is a partial schematic diagram of the conventional technology.

第2圖是本發明第一較佳實施例的示意圖。 Figure 2 is a schematic diagram of the first preferred embodiment of the present invention.

第3圖是一示意圖,說明第一較佳實施例的縮距場天線單元。 Figure 3 is a schematic diagram illustrating the reduced-range field antenna unit of the first preferred embodiment.

第4圖是本發明第二較佳實施例的示意圖。 Figure 4 is a schematic diagram of the second preferred embodiment of the present invention.

第5圖是本發明第三較佳實施例的示意圖。 Figure 5 is a schematic diagram of the third preferred embodiment of the present invention.

第6圖是本發明第四較佳實施例的示意圖。 Figure 6 is a schematic diagram of a fourth preferred embodiment of the present invention.

第7圖是一示意圖,說明任一較佳實施例的縮距場天線單元與電波暗室的一種固定方式。 Fig. 7 is a schematic diagram illustrating a method of fixing the distance field antenna unit and the anechoic chamber of any preferred embodiment.

第8圖是一示意圖,說明任一較佳實施例的縮距場天線單元與電波暗室的另一種固定方式。 Fig. 8 is a schematic diagram illustrating another method of fixing the distance field antenna unit and the anechoic chamber of any preferred embodiment.

第9圖是一示意圖,說明第一較佳實施例更包括一第一支撐板。 Figure 9 is a schematic diagram illustrating that the first preferred embodiment further includes a first support plate.

第10圖是一示意圖,說明第一較佳實施例更包括一第二支撐板。 Figure 10 is a schematic diagram illustrating that the first preferred embodiment further includes a second supporting plate.

第11圖是一示意圖,說明以T形狀第一支撐柱取代第一支撐板的實施方式。 Fig. 11 is a schematic diagram illustrating an embodiment in which a T-shaped first support column replaces the first support plate.

第12圖是一示意圖,說明以T形狀第二支撐柱取代第二支撐板的實施方式。 Figure 12 is a schematic diagram illustrating an embodiment in which a T-shaped second support column is used instead of the second support plate.

第13圖是一示意圖,說明以L形狀第一支撐柱取代第一支撐板的實施方式。 Figure 13 is a schematic diagram illustrating an embodiment in which an L-shaped first support column is used instead of the first support plate.

第14圖是一示意圖,說明以L形狀第二支撐柱取代第二支撐板的實施方式。 Fig. 14 is a schematic diagram illustrating an embodiment in which the second support plate is replaced by an L-shaped second support column.

參閱圖2及圖3,本發明用於多輸入多輸出空中傳輸的天線量測系統包括一電波暗室2、一旋轉基座3及多數個縮距場天線單元4。 2 and 3, the antenna measurement system for multi-input multi-output air transmission of the present invention includes an anechoic chamber 2, a rotating base 3, and a plurality of narrow field antenna units 4.

該旋轉基座3設置於該電波暗室2中,該旋轉基座3包括一平台面31,該平台面31用以放置一待測裝置5,該待測裝置5包括多數個待測天線51。 The rotating base 3 is disposed in the anechoic chamber 2. The rotating base 3 includes a platform surface 31 for placing a device under test 5, and the device under test 5 includes a plurality of antennas 51 under test.

於第一較佳實施例,該電波暗室2呈一立方體,並包括一第一頂角21、一第二頂角22、一第三頂角23、一第四頂角24、一第一底角25、一第二底角26、一第三底角27、一第四底角28。該第一頂角21、該旋轉基座3的平台面31及該第三底角27三者依序沿著一直線排列;該第二頂角22、該旋轉基座3的平台面31及該第四底角28三者依序沿著一直線排列;該第三頂角23、該旋轉基座3的平台面31及該第一底角25三者依序沿著一直線排列;該第四頂角24、該旋轉基座3的平台面31及該第二底角26三者依序沿著一直線排列。 In the first preferred embodiment, the anechoic chamber 2 is in the shape of a cube, and includes a first apex 21, a second apex 22, a third apex 23, a fourth apex 24, and a first bottom. Corner 25, a second bottom corner 26, a third bottom corner 27, and a fourth bottom corner 28. The first vertex 21, the platform surface 31 of the rotating base 3, and the third bottom corner 27 are arranged in a straight line; the second vertex 22, the platform surface 31 of the rotating base 3, and the The three fourth bottom corners 28 are arranged in sequence along a straight line; the third top corner 23, the platform surface 31 of the rotating base 3, and the first bottom corner 25 are arranged in sequence along a straight line; The angle 24, the platform surface 31 of the rotating base 3, and the second bottom angle 26 are sequentially arranged along a straight line.

每一個縮距場天線單元4包括一訊號饋源41,一凹面鏡42,一用以固定該訊號饋源41與該凹面鏡42的連接臂43。每一個縮距場天線單元4中的該訊號饋源41用以朝向對應的該凹面鏡42發射一第一射頻訊號111,該凹面鏡42面向該旋轉基座3的平台面31設置,用以將該第一射頻訊號111反射成為朝向該旋轉基座3的平台面31的一第二射頻訊號112,其中,每一第二射頻訊號112是均勻平面波,且任兩個縮距場天線單元4的凹面鏡42不面對面地設置。 Each narrow field antenna unit 4 includes a signal feed 41, a concave mirror 42, and a connecting arm 43 for fixing the signal feed 41 and the concave mirror 42. The signal feed 41 in each narrow field antenna unit 4 is used to transmit a first radio frequency signal 111 toward the corresponding concave mirror 42. The concave mirror 42 is arranged facing the platform surface 31 of the rotating base 3 for the The first radio frequency signal 111 is reflected as a second radio frequency signal 112 toward the platform surface 31 of the rotating base 3, wherein each second radio frequency signal 112 is a uniform plane wave, and the concave mirrors of any two narrow field antenna units 4 42 is not set face to face.

其中,該等縮距場天線單元4的數量是六個,分別位於第一頂角21、第二底角26、第三頂角23、第四底角28、第二頂角22與第二底角26的連線中間(位置293),以及第三頂角23與第三底角27的連線中間(位置291)。 Among them, the number of the shortened field antenna units 4 is six, which are located at the first apex angle 21, the second apex angle 26, the third apex angle 23, the fourth apex angle 28, the second apex angle 22, and the second apex angle. The middle of the line of the bottom corner 26 (position 293), and the middle of the line of the third top corner 23 and the third bottom corner 27 (position 291).

舉例說明,圖2中第一頂角21設置一個縮距場天線單元4,則第三底角27就不能設置縮距場天線單元4;第三頂角23設置一個縮距場天線單元4,則第二底角25就不能設置縮距場天線單元4;同理,位置291設置一個縮距場天線單元4,則位置292就不能設置縮距場天線單元4。如此,就能避免任兩個縮距場天線單元4的凹面鏡42面對面地設置產生兩個第二射頻訊號112相消的干擾問題。 For example, in FIG. 2, a short-range field antenna unit 4 is provided at the first apex 21, then the third bottom corner 27 cannot be provided with a short-distance field antenna unit 4; the third apex 23 is provided with a short-distance field antenna unit 4, Therefore, the short-distance field antenna unit 4 cannot be installed at the second bottom corner 25; in the same way, if a short-distance field antenna unit 4 is installed at the position 291, the short-distance field antenna unit 4 cannot be installed at the position 292. In this way, it is possible to avoid the problem of destructive interference of the two second radio frequency signals 112 when the concave mirrors 42 of any two narrow field antenna units 4 are arranged face to face.

參閱圖4,是本發明第二較佳實施例的一示意圖,第二較佳實施例與第一較佳實施例近似,差異在於:該等縮距場天線單元4的數量是四個,分別位於第一頂角21、第二底角26、第三頂角23及第四底角28。 Refer to FIG. 4, which is a schematic diagram of the second preferred embodiment of the present invention. The second preferred embodiment is similar to the first preferred embodiment, but the difference is that the number of the reduced field antenna units 4 is four, respectively Located at the first top corner 21, the second bottom corner 26, the third top corner 23 and the fourth bottom corner 28.

參閱圖5,是本發明第三較佳實施例的一示意圖,第三較佳實施例與第二較佳實施例近似,差異在於:該等縮距場天線單元4的數量是 三個,分別位於第一頂角21、第二底角26,以及第三底角27與第四頂角24的連線中間291。 Referring to FIG. 5, it is a schematic diagram of the third preferred embodiment of the present invention. The third preferred embodiment is similar to the second preferred embodiment, except that the number of the antenna units 4 of the shortened field is Three are located at the first top corner 21, the second bottom corner 26, and the middle 291 between the third bottom corner 27 and the fourth top corner 24, respectively.

參閱圖6,是本發明第四較佳實施例的一示意圖,第四較佳實施例與第三較佳實施例近似,差異在於:該等縮距場天線單元4的數量是兩個,分別位於第一頂角21及第二底角26。 Refer to FIG. 6, which is a schematic diagram of the fourth preferred embodiment of the present invention. The fourth preferred embodiment is similar to the third preferred embodiment, but the difference lies in that the number of the narrow field antenna units 4 is two, respectively Located at the first top corner 21 and the second bottom corner 26.

參閱圖7,前述的任一個較佳實施例的該電波暗室2還包括多數個螺絲孔20,每一個縮距場天線單元4的連接臂43包括一第一臂部431及一第二臂部432,每一第一臂部431以螺絲4311鎖接固定於該電波暗室2的壁板200上,每一連接臂43的第二臂部432與該凹面鏡42相連接,且該凹面鏡42可以相對該連接臂43的第二臂部432轉動,以調整該第二射頻訊號112的方向,該第二臂部432也可以相對該第一臂部431繞著Z方向軸轉動。 Referring to FIG. 7, the anechoic chamber 2 of any of the foregoing preferred embodiments further includes a plurality of screw holes 20, and the connecting arm 43 of each shortened field antenna unit 4 includes a first arm 431 and a second arm. 432. Each first arm portion 431 is fastened to the wall plate 200 of the anechoic chamber 2 with a screw 4311. The second arm portion 432 of each connecting arm 43 is connected to the concave mirror 42, and the concave mirror 42 can be opposite to each other. The second arm 432 of the connecting arm 43 rotates to adjust the direction of the second radio frequency signal 112, and the second arm 432 can also rotate about the Z-direction axis relative to the first arm 431.

參閱圖8,該縮距場天線單元4相較圖7的更包括一固定金屬片4312,該固定金屬片4312與該第一臂部431分別位於該電波暗室2的壁板200的兩側,兩個螺絲4311鎖接固定將該第一臂部431、該壁板200與該該固定金屬片4312三者鎖住固定。此外,在實際應用上不限於用螺絲4311鎖接,也可以用直接焊接的方式固定。 Referring to FIG. 8, the reduced-range field antenna unit 4 further includes a fixed metal sheet 4312 compared to that of FIG. 7. The fixed metal sheet 4312 and the first arm portion 431 are respectively located on both sides of the wall plate 200 of the anechoic chamber 2. Two screws 4311 lock and fix the first arm 431, the wall plate 200, and the fixing metal sheet 4312. In addition, the actual application is not limited to the use of screws 4311 for locking, but can also be fixed by direct welding.

參閱圖2及圖9,圖9示意該第一較佳實施例更包括一第一支撐板61,該第一支撐板61為非導體、低介電常數、低介質損耗的材料以降低對電磁波的干擾,該第一支撐板61固定於該電波暗室2的壁板200,用來支撐對應的一個該縮距場天線單元4的重量,且受該第一支撐板61支撐的該縮距場天線單元4是位於第三頂角23與第三底角27的連線中間的位置291。 2 and 9, FIG. 9 shows that the first preferred embodiment further includes a first support plate 61, the first support plate 61 is a non-conductor, low dielectric constant, low dielectric loss material to reduce the electromagnetic wave The first support plate 61 is fixed to the wall plate 200 of the anechoic chamber 2 to support the weight of the corresponding one of the retracted field antenna units 4, and the retracted field supported by the first support plate 61 The antenna unit 4 is located at a position 291 in the middle of the line connecting the third top corner 23 and the third bottom corner 27.

參閱圖2及圖10,圖10示意該第一較佳實施例更包括一個也 是非金屬導體、低介電常數、低介質損耗的第二支撐板62。該第二支撐板62固定於該電波暗室2的該壁板200,用來支撐對應的另一個該縮距場天線單元4的重量,且受該第二支撐板62支撐的該縮距場天線單元4是位於第二頂角22與第二底角26的連線中間的位置293。 2 and 10, FIG. 10 shows that the first preferred embodiment further includes a It is the second support plate 62 with non-metallic conductor, low dielectric constant and low dielectric loss. The second supporting plate 62 is fixed to the wall plate 200 of the anechoic chamber 2 to support the weight of the corresponding other short-range field antenna unit 4, and the short-range field antenna supported by the second support plate 62 The unit 4 is located at a position 293 in the middle of the line connecting the second top corner 22 and the second bottom corner 26.

參閱圖2、11、12,說明該第一支撐板61及該第二支撐板62(見圖9、10)也可以分別用一第一支撐柱71及一第二支撐柱72取代,該第一支撐柱71及該第二支撐柱72各呈T形狀、並設置固定在該電波暗室2的一底板201上的,且受該第一支撐柱71支撐的該縮距場天線單元4是位於第三頂角23與第三底角27的連線中間的位置291,受該第二支撐柱72支撐的該縮距場天線單元4是位於第二頂角22與第二底角26的連線中間的位置293。 Referring to Figures 2, 11, and 12, it is explained that the first support plate 61 and the second support plate 62 (see Figures 9 and 10) can also be replaced by a first support column 71 and a second support column 72, respectively. A supporting column 71 and the second supporting column 72 each have a T-shape, and are arranged and fixed on a bottom plate 201 of the anechoic chamber 2, and the retracted field antenna unit 4 supported by the first supporting column 71 is located At the position 291 in the middle of the line connecting the third top corner 23 and the third bottom corner 27, the reduced-distance field antenna unit 4 supported by the second supporting column 72 is located at the connection between the second top corner 22 and the second bottom corner 26 Position 293 in the middle of the line.

參閱圖2、13、14,該第一支撐柱71及該第二支撐柱72也可以置換成倒L形狀。 Referring to Figs. 2, 13, and 14, the first support column 71 and the second support column 72 can also be replaced with an inverted L shape.

本發明之效果在於:利用縮距場天線單元4的凹面鏡42將來自訊號饋源41的非均勻平面波(第一射頻訊號111)反射成均勻平面波(第二射頻訊號112),就不受限如圖1習知技術參數r必須遠大於2D2/λ到達該待測裝置5才是均勻平面波的限制,因此改進了遠場量測電波暗室2空間需求大或是近場量測計算複雜且不適合主動式量測的問題;此外,本發明亦考量該多數個縮距場天線單元4在電波暗室2中的空間配置,避免多輸入多輸出(MIMO)測試時任兩個縮距場天線單元4反射出的第二射頻訊號112相互碰撞干擾的問題。 The effect of the present invention is that the concave mirror 42 of the narrow field antenna unit 4 is used to reflect the non-uniform plane wave (the first radio frequency signal 111) from the signal feed 41 into a uniform plane wave (the second radio frequency signal 112). Figure 1 The conventional technical parameter r must be much larger than 2D 2 /λ to reach the device under test 5 to reach the limit of the uniform plane wave, so the far-field measurement anechoic chamber 2 has a large space requirement or the near-field measurement calculation is complicated and unsuitable The problem of active measurement; in addition, the present invention also considers the spatial configuration of the plurality of short-range field antenna units 4 in the anechoic chamber 2 to avoid reflections of any two short-range field antenna units 4 during multiple input multiple output (MIMO) testing. The second radio frequency signals 112 collide and interfere with each other.

2:電波暗室 2: anechoic chamber

21:第一頂角 21: The first vertex

22:第二頂角 22: second top corner

23:第三頂角 23: third vertex

24:第四頂角 24: fourth vertex

25:第一底角 25: first bottom corner

26:第二底角 26: second bottom corner

27:第三底角 27: Third bottom corner

28:第四底角 28: Fourth bottom corner

3:旋轉基座 3: Rotating base

31:平台面 31: platform surface

4:縮距場天線單元 4: Short-distance field antenna unit

5:待測裝置 5: Device to be tested

51:待測天線 51: Antenna to be tested

111:第一射頻訊號 111: The first RF signal

112:第二射頻訊號 112: Second RF signal

291、292、293、294:位置 291, 292, 293, 294: location

Claims (5)

一種用於多輸入多輸出空中傳輸的天線量測系統,包括:一電波暗室,該電波暗室呈一立方體,並包括一第一頂角、一第二頂角、一第三頂角、一第四頂角、一第一底角、一第二底角、一第三底角、一第四底角,該第一頂角、該旋轉基座的平台面及該第三底角三者依序沿著一直線排列,該第二頂角、該旋轉基座的平台面及該第四底角三者依序沿著一直線排列,該第三頂角、該旋轉基座的平台面及該第一底角三者依序沿著一直線排列,該第四頂角、該旋轉基座的平台面及該第二底角三者依序沿著一直線排列;一旋轉基座,設置於該電波暗室中,該旋轉基座包括一平台面,該平台面用以放置一待測裝置,該待測裝置包括多數個待測天線;六個縮距場天線單元,分別位於第一頂角、第二底角、第三頂角、第四底角、第二頂角與第二底角的連線中間,以及第三頂角與第三底角的連線中間,每一個縮距場天線單元包括一訊號饋源,一凹面鏡,一用以固定該訊號饋源與該凹面鏡的連接臂,每一個縮距場天線單元中的該訊號饋源用以朝向對應的該凹面鏡發射一第一射頻訊號,該凹面鏡面向該旋轉基座 的平台面設置,用以將該第一射頻訊號反射成為朝向該旋轉基座的平台面的一第二射頻訊號,其中,每一第二射頻訊號是均勻平面波,且任兩個縮距場天線單元的凹面鏡不面對面地設置;及一第一支撐板,該第一支撐板為非導體、低介電常數(permittivity)、低介質損耗(dielectric loss)的材料,該第一支撐板固定於該電波暗室的一壁板,用來支撐對應的一個該縮距場天線單元的重量,且受該第一支撐板支撐的該縮距場天線單元是位於第三頂角與第三底角的連線中間的位置。 An antenna measurement system for multi-input and multi-output air transmission includes: an anechoic chamber, which is in the form of a cube and includes a first apex angle, a second apex angle, a third apex angle, and a second apex angle. Four top corners, a first bottom corner, a second bottom corner, a third bottom corner, a fourth bottom corner, the first top corner, the platform surface of the rotating base, and the third bottom corner The order is arranged along a straight line, the second apex angle, the platform surface of the rotating base and the fourth bottom angle are arranged in sequence along a straight line, the third apex angle, the platform surface of the rotating base and the first A bottom corner is arranged in sequence along a straight line, the fourth top corner, the platform surface of the rotating base, and the second bottom corner are arranged in sequence along a straight line; a rotating base is arranged in the anechoic chamber Wherein, the rotating base includes a platform surface for placing a device to be tested, the device to be tested includes a plurality of antennas to be tested; The bottom corner, the third top corner, the fourth bottom corner, the middle of the line between the second top corner and the second bottom corner, and the middle of the line between the third top corner and the third bottom corner, each of the reduced-distance field antenna units includes A signal feed, a concave mirror, a connecting arm for fixing the signal feed and the concave mirror, the signal feed in each narrow field antenna unit is used to transmit a first radio frequency signal toward the corresponding concave mirror, The concave mirror faces the rotating base The platform surface is configured to reflect the first radio frequency signal into a second radio frequency signal toward the platform surface of the rotating base, wherein each second radio frequency signal is a uniform plane wave, and any two narrow field antennas The concave mirrors of the unit are not arranged face to face; and a first support plate, the first support plate is a non-conductor, low permittivity (permittivity), low dielectric loss (dielectric loss) material, the first support plate is fixed to the A wall plate of the anechoic chamber is used to support the weight of a corresponding one of the distance field antenna units, and the distance field antenna unit supported by the first support plate is located at the third top corner and the third bottom corner. The position in the middle of the line. 根據申請專利範圍第1項之用於多輸入多輸出空中傳輸的天線量測系統,其中該電波暗室還包括多數個螺絲孔,每一個縮距場天線單元的連接臂包括一第一臂部及一第二臂部,每一第一臂部固定於該電波暗室,每一連接臂的第二臂部與該凹面鏡相連接。 According to the first item of the scope of patent application, the antenna measurement system for multi-input multi-output air transmission, wherein the anechoic chamber also includes a plurality of screw holes, and the connecting arm of each shortened field antenna unit includes a first arm and A second arm part, each first arm part is fixed to the anechoic chamber, and the second arm part of each connecting arm is connected with the concave mirror. 根據申請專利範圍第2項之用於多輸入多輸出空中傳輸的天線量測系統,其中該凹面鏡可以相對該連接臂的第二臂部轉動。 According to the second item of the scope of patent application, the antenna measurement system for multiple input multiple output air transmission, wherein the concave mirror can rotate relative to the second arm of the connecting arm. 根據申請專利範圍第3項之用於多輸入多輸出空中傳輸的天線量測系統,更包括一個也是非導體、低介電常數、低介質損耗的第二支撐板,該第二支撐板固定於該電波暗室的該壁板,用來支撐對應的另一個該縮距場天線單元的重 量,且受該第二支撐板支撐的該縮距場天線單元是位於第二頂角與第二底角的連線中間的位置。 According to item 3 of the scope of patent application, the antenna measurement system for multi-input multi-output air transmission further includes a second support plate that is also non-conductor, low dielectric constant, and low dielectric loss. The second support plate is fixed on The wall plate of the anechoic chamber is used to support the corresponding weight of another antenna unit of the reduced distance field. The distance field antenna unit supported by the second support plate is located in the middle of the line connecting the second top corner and the second bottom corner. 根據申請專利範圍第1項之用於多輸入多輸出空中傳輸的天線量測系統,更包括呈T形狀或倒L形狀的一第一支撐柱及一第二支撐柱,該第一支撐板為非導體、低介電常數、低介質損耗的材料,該第一支撐柱固定於該電波暗室的一底板上,用來支撐對應的一個該縮距場天線單元的重量,且受該第一支撐柱支撐的該縮距場天線單元是位於第三頂角與第三底角的連線中間的位置,該第二支撐柱也是非導體、低介電常數、低介質損耗的材料,該第二支撐柱固定於該電波暗室的該底板上,用來支撐對應的另一個該縮距場天線單元的重量,且受該第二支撐柱支撐的該縮距場天線單元是位於第二頂角與第二底角的連線中間的位置。 According to item 1 of the scope of patent application, the antenna measurement system for multi-input multi-output air transmission further includes a first support column and a second support column in a T shape or an inverted L shape. The first support plate is Non-conductor, low-dielectric constant, low-dielectric loss material, the first support column is fixed on a bottom plate of the anechoic chamber, used to support the weight of a corresponding short-distance field antenna unit, and is supported by the first The narrow-distance field antenna unit supported by the column is located in the middle of the line connecting the third top corner and the third bottom corner. The second support column is also a non-conductor, low dielectric constant, and low dielectric loss material. The supporting column is fixed on the bottom plate of the anechoic chamber to support the weight of another corresponding narrow-range field antenna unit, and the narrow-range field antenna unit supported by the second supporting column is located at the second vertex angle and The position in the middle of the line at the second bottom corner.
TW108132966A 2019-09-10 2019-09-10 Antenna measurment system for mimo ota TWI698649B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
TW108132966A TWI698649B (en) 2019-09-10 2019-09-10 Antenna measurment system for mimo ota

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
TW108132966A TWI698649B (en) 2019-09-10 2019-09-10 Antenna measurment system for mimo ota

Publications (2)

Publication Number Publication Date
TWI698649B true TWI698649B (en) 2020-07-11
TW202111338A TW202111338A (en) 2021-03-16

Family

ID=72601853

Family Applications (1)

Application Number Title Priority Date Filing Date
TW108132966A TWI698649B (en) 2019-09-10 2019-09-10 Antenna measurment system for mimo ota

Country Status (1)

Country Link
TW (1) TWI698649B (en)

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5532704A (en) * 1993-06-15 1996-07-02 Siepel-Societe Industrielle D'etudes Et Protection Electroique Device for positioning antennas inside a measurment chamber of the anechoic or of the semi-anechoic type
EP1992961A2 (en) * 2007-05-11 2008-11-19 Rosemount Aerospace Inc. Scanning ladar with adjustable operational parameters
CN204741460U (en) * 2015-05-12 2015-11-04 彭嘉美 Wireless communication throughput testing arrangement
TWI635290B (en) * 2017-07-11 2018-09-11 川升股份有限公司 Antenna radiation pattern measurement system for multipath scenario application
CN208459486U (en) * 2018-05-30 2019-02-01 上海益麦电磁技术有限公司 A kind of Antenna testing system based on suction wave apparatus

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5532704A (en) * 1993-06-15 1996-07-02 Siepel-Societe Industrielle D'etudes Et Protection Electroique Device for positioning antennas inside a measurment chamber of the anechoic or of the semi-anechoic type
EP1992961A2 (en) * 2007-05-11 2008-11-19 Rosemount Aerospace Inc. Scanning ladar with adjustable operational parameters
CN204741460U (en) * 2015-05-12 2015-11-04 彭嘉美 Wireless communication throughput testing arrangement
TWI635290B (en) * 2017-07-11 2018-09-11 川升股份有限公司 Antenna radiation pattern measurement system for multipath scenario application
CN208459486U (en) * 2018-05-30 2019-02-01 上海益麦电磁技术有限公司 A kind of Antenna testing system based on suction wave apparatus

Also Published As

Publication number Publication date
TW202111338A (en) 2021-03-16

Similar Documents

Publication Publication Date Title
WO2020224044A1 (en) Antenna testing method and device, and storage medium
TWI635290B (en) Antenna radiation pattern measurement system for multipath scenario application
US20130141287A1 (en) Apparatus for Measuring a Radiation Pattern of an Active Antenna Arrangement
JP4438905B2 (en) Radiation efficiency measuring apparatus and radiation efficiency measuring method
US11933828B2 (en) Measurement method and device
US10156601B2 (en) Antenna measurement system and antenna measurement method
JP7329085B2 (en) High-speed OTA production line test platform
CN110007157B (en) Antenna measurement system and antenna measurement method
US10012683B2 (en) System for testing wireless terminal and method for controlling same
Boehm et al. Robotically controlled directivity and gain measurements of integrated antennas at 280 GHz
TWI540792B (en) A far-field calibration system of an antenna arrary system
TW202012945A (en) An automatic measurement system for antenna radiation pattern
CN109239472B (en) Antenna radiation pattern measuring system applied to multi-path environment
US20200264223A1 (en) Measurement system, measurement setup as well as method for performing measurements
CN115047256A (en) Array antenna multichannel parallel test device, test method and calibration method
CN210294411U (en) Terahertz compact field test system based on electric scanning antenna
TWI674416B (en) An automatic system for antenna measurement
TWI422838B (en) Multichannel absorberless near field measurement system
TWI698649B (en) Antenna measurment system for mimo ota
JP2010124360A (en) Phased-array antenna inspection system, phased-array antenna inspecting apparatus, phased-array antenna inspection method and phased-array antenna
TW202032140A (en) System for measuring electrical parameters
JP5760927B2 (en) Radio wave measuring apparatus and radio wave measuring method
JP2003315440A (en) Method and apparatus for measuring field in compact range
CN112557766A (en) Antenna measurement system for multiple-input multiple-output air transmission
KR20120071840A (en) Apparatus and method for testing antenna in wireless communication system