JPH08122378A - Apparatus for measuring antenna - Google Patents
Apparatus for measuring antennaInfo
- Publication number
- JPH08122378A JPH08122378A JP25805894A JP25805894A JPH08122378A JP H08122378 A JPH08122378 A JP H08122378A JP 25805894 A JP25805894 A JP 25805894A JP 25805894 A JP25805894 A JP 25805894A JP H08122378 A JPH08122378 A JP H08122378A
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- JP
- Japan
- Prior art keywords
- antenna
- measurement
- measuring
- radiating elements
- excitation
- Prior art date
- Legal status (The legal status 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 status listed.)
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- Variable-Direction Aerials And Aerial Arrays (AREA)
Abstract
Description
【0001】[0001]
【産業上の利用分野】本発明は空中線測定装置に係り、
特にアレー空中線の近傍電界測定により放射素子個々の
相対励振条件を測定する空中線測定装置に関する。BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to an antenna measuring device,
More particularly, the present invention relates to an antenna measuring apparatus for measuring relative excitation conditions of individual radiating elements by measuring an electric field near an array antenna.
【0002】[0002]
【従来の技術】周知のように、アレー空中線は単独で使
用される場合と反射鏡と組み合わされて使用される場合
とがあるが、いずれの場合においても組み立てたアレー
空中線の放射特性には製造誤差やアレー空中線を構成す
る放射素子間の相互結合等に起因する設計値とのずれが
あるので、実際の使用における補正量の取得を目的とし
て放射素子個々の実際の励振条件を測定することが行わ
れる。2. Description of the Related Art As is well known, an array antenna may be used alone or in combination with a reflecting mirror. In either case, the radiation characteristics of the assembled array antenna are limited. Since there are deviations from the design values due to errors and mutual coupling between the radiating elements constituting the array antenna, it is necessary to measure the actual excitation conditions of each radiating element for the purpose of obtaining the correction amount in actual use. Done.
【0003】この測定は、アレー空中線の近傍界領域内
において行われるが、外来雑音を排除する観点から電波
無響室内に空中線測定装置を設定してアレー空中線の放
射開口面における各放射素子の放射電界を測定するとい
う形で行われるのが一般的である。[0003] This measurement is performed in the near-field region of the array antenna. From the viewpoint of eliminating extraneous noise, an antenna measurement device is set in a radio anechoic chamber and the radiation of each radiating element at the radiation aperture surface of the array antenna is set. It is generally done in the form of measuring an electric field.
【0004】上記の空中線測定装置は、近傍界測定用空
中線と、アレー空中線の各放射素子の励振条件を個々に
変化させ得る素子励振条件変更手段と、素子励振条件算
定手段とを基本的に備え、測定用空中線をアレー空中線
の各放射素子と予め定めた間隔をおいて、測定用空中線
を測定対象放射素子に正対する位置に設定し、測定対象
の放射素子を励振して電波の送信を行わせて測定用空中
線で放射電界を検出し、また測定対象の放射素子を励振
して測定用空中線が送信する電波の受信を行わせ、測定
対象放射素子の実際の励振振幅及び励振位相を算定す
る。The above-described antenna measuring apparatus basically includes an antenna for near-field measurement, element excitation condition changing means for individually changing the excitation conditions of each radiating element of the array antenna, and element excitation condition calculating means. The antenna for measurement is set at a position facing the radiating element to be measured at a predetermined interval from each radiating element of the array antenna, and the radiating element to be measured is excited to transmit radio waves. At the same time, the radiated electric field is detected by the antenna for measurement, and the radiating element to be measured is excited to receive the radio wave transmitted by the antenna for measurement, and the actual excitation amplitude and excitation phase of the radiating element to be measured are calculated. .
【0005】図11は従来の空中線測定装置における測
定用空中線と放射素子との位置関係の一例を示す。同図
に示すように、測定用空中線1とN個(Nは2以上の整
数)の放射素子9−1〜9−Nとは、それぞれ互いに予
め定めた間隔dをおいて正対する位置に設定されてい
る。また、放射素子9−1〜9−Nはそれぞれ同一方向
に向けて配置されている。FIG. 11 shows an example of the positional relationship between a measuring antenna and a radiating element in a conventional antenna measuring apparatus. As shown in the drawing, the measurement antenna 1 and N (N is an integer of 2 or more) radiating elements 9-1 to 9-N are set at positions facing each other with a predetermined interval d therebetween. Have been. Further, the radiating elements 9-1 to 9-N are respectively arranged in the same direction.
【0006】また、別の空中線測定装置では、測定用空
中線をアレー空中線の各放射素子と予め定めた間隔をお
いて測定用空中線を所定の放射素子に正対する位置に設
定し、測定用空中線が正対する放射素子及び当該放射素
子からM個(Mは1以上の整数)隔てた測定対象放射素
子を励振して電波の送信を行わせて測定用空中線で放射
電界を検出し、また、測定対象の放射素子を励振して測
定用空中線が送信する電波の受信を行わせ、測定対象放
射素子までの距離及び見込み角度を用いて補正し、測定
対象放射素子の実際の励振振幅及び励振位相を算定す
る。In another antenna measuring apparatus, the measuring antenna is set at a position facing the predetermined radiating element at a predetermined interval from each radiating element of the array antenna, and the measuring antenna is placed The radiating element facing and the radiating element to be measured separated from the radiating element by M (M is an integer of 1 or more) are excited to transmit radio waves, and the radiated electric field is detected by the antenna for measurement. Excitation of the radiating element to receive the radio wave transmitted by the antenna for measurement, correction using the distance and expected angle to the radiating element to be measured, and calculation of the actual excitation amplitude and excitation phase of the radiating element to be measured I do.
【0007】[0007]
【発明が解決しようとする課題】しかるに、上記の従来
の空中線測定装置では、放射素子の励振振幅と励振位相
を測定する場合、測定用空中線を測定対象放射素子に正
対する位置に設定し、正対している測定対象放射素子の
みの励振振幅と励振位相を測定するため、放射素子数と
同じ回数だけ測定用空中線の位置設定が必要となり、測
定に多大な時間を要した。However, in the above-mentioned conventional antenna measuring apparatus, when measuring the excitation amplitude and the excitation phase of the radiating element, the measuring antenna is set at a position directly facing the radiating element to be measured. In order to measure the excitation amplitude and the excitation phase of only the radiating element to be measured, it is necessary to set the position of the antenna for measurement by the same number of times as the number of radiating elements.
【0008】また、従来の別の空中線測定装置では、測
定用空中線が正対する放射素子からM個隔てた測定対象
放射素子を測定する場合には、測定対象放射素子までの
距離及び見込み角度を用いて補正しなければならず、補
正するための演算器、メモリ等が必要となり、測定装置
の構成が複雑になるという問題がある。In another conventional antenna measuring apparatus, when measuring a radiating element M away from a radiating element directly facing the measuring antenna, the distance and the expected angle to the radiating element to be measured are used. And a compensator, a memory, and the like for the correction are required, and the configuration of the measuring device is complicated.
【0009】本発明は以上の点に鑑みなされたもので、
測定用空中線の移動設定回数を減らし、アレー空中線を
構成する放射素子の励振振幅及び励振位相の測定時間の
短縮を可能にし、かつ、測定用空中線から測定対象放射
素子までの距離及び見込み角度を用いた測定結果の補正
を不要とした簡素な構成の空中線測定装置を提供するこ
とを目的とする。[0009] The present invention has been made in view of the above points,
Reduce the number of times the antenna for measurement is set to move, shorten the measurement time of the excitation amplitude and excitation phase of the radiating element constituting the array antenna, and use the distance and expected angle from the measuring antenna to the radiating element to be measured. It is an object of the present invention to provide an antenna measuring apparatus having a simple configuration that does not require correction of the measurement result.
【0010】[0010]
【課題を解決するための手段】本発明は上記の目的を達
成するため、縦方向及び横方向の間隔がそれぞれ等しく
なるように配列されたN個(ただし、Nは2以上の整
数)の放射素子から構成されたアレー空中線のN個の放
射素子の放射電界をそれぞれ測定する測定用空中線と、
N個の放射素子と予め定めた間隔を置いてN個の放射素
子のうち偶数個の放射素子に対する幾何学的距離がそれ
ぞれ等しい位置毎に測定用空中線を相対的に移動設定す
る位置制御手段と、N個の放射素子の励振条件を個々に
変化させる素子励振条件変更手段と、素子励振条件変更
手段による素子励振条件の変更前後のそれぞれについて
の測定用空中線の測定結果及び素子励振条件変更手段よ
りの励振条件とが少なくとも入力されて、測定用空中線
に対して幾何学的距離がそれぞれ所定値離れた一又は二
以上の放射素子のみの励振振幅と励振位相を算定する素
子励振算定手段とを有する構成としたものである。SUMMARY OF THE INVENTION In order to achieve the above-mentioned object, the present invention provides N (N is an integer of 2 or more) radiations arranged so that the vertical and horizontal intervals are equal. A measuring antenna for measuring the radiated electric field of each of the N radiating elements of the array antenna constituted by the elements,
Position control means for relatively moving and setting the measurement antenna for each of the N radiating elements and at a position having a predetermined distance from the N radiating elements and at the same geometric distance to the even number of radiating elements; , The element excitation condition changing means for individually changing the excitation conditions of the N radiating elements, and the measurement results of the measurement antenna before and after the element excitation conditions are changed by the element excitation condition changing means and the element excitation condition changing means. Element excitation calculation means for calculating the excitation amplitude and the excitation phase of only one or two or more radiating elements whose geometric distances are respectively separated from the measurement antenna by a predetermined value, at least when the excitation condition is inputted. It is configured.
【0011】ここで、本発明の前記位置制御手段は、ア
レー空中線のN個の放射素子のそれぞれに1対1対応で
正対する位置に順次に前記測定用空中線を移動設定する
か、アレー空中線のN個の放射素子のうち隣り合う2個
の放射素子の間の中心位置と1対1対応で正対する位置
に順次に前記測定用空中線を移動設定する。Here, the position control means of the present invention sequentially moves or sets the measurement antenna to a position that directly faces each of the N radiating elements of the array antenna in a one-to-one correspondence or sets the array antenna. Among the N radiating elements, the measurement antenna is sequentially moved and set to a position directly facing the center position between two adjacent radiating elements in a one-to-one correspondence.
【0012】[0012]
【作用】本発明では、測定用空中線をアレー空中線の各
放射素子と予め定めた間隔を置いて測定用空中線をアレ
ー空中線の各放射素子又は隣り合う放射素子間の中心位
置と1対1対応で正対する位置に移動設定させ、測定用
空中線から幾何学的に距離の等しい複数の放射素子を略
同時に測定するようにしたため、測定用空中線の移動設
定回数を従来よりも減らすことができる。In the present invention, the measurement antenna is spaced apart from each radiating element of the array antenna at a predetermined distance, and the measuring antenna is one-to-one corresponding to the center position between each radiating element of the array antenna or the adjacent radiating element. Since a plurality of radiating elements having geometrically equal distances from the measurement antenna are measured almost at the same time by moving the antenna to the position directly opposite thereto, the number of times the measurement antenna is moved can be reduced as compared with the related art.
【0013】また、本発明によれば、各放射素子の縦方
向及び横方向の放射素子間隔がそれぞれすべて等しい場
合、測定用空中線と測定対象放射素子までの距離及び見
込み角度が等しくなるため、測定した位相と振幅に対す
る補正を不要とすることができる。Further, according to the present invention, when the radiating element intervals in the vertical and horizontal directions of the radiating elements are all equal, the distance and the expected angle between the antenna for measurement and the radiating element to be measured become equal, so that It is not necessary to correct the phase and amplitude.
【0014】[0014]
【実施例】次に、本発明の実施例について説明する。図
1は本発明になる空中線測定装置の一実施例のブロック
図を示す。同図に示すように、本実施例は測定用空中線
1と、測定用受信機2と、素子励振条件変更手段5と、
測定用空中線位置制御手段6と、信号発生器7と、素子
励振条件算定手段8とを備える点は本出願人が先に提案
した特公平5−14230号公報と基本的に同様である
が、本実施例は測定用空中線位置制御手段6の動作に特
徴がある。また、素子励振条件変更手段5は、振幅/位
相制御器3及び可変減衰器/移相器4から構成されてい
る。Next, an embodiment of the present invention will be described. FIG. 1 is a block diagram showing an embodiment of an antenna measuring apparatus according to the present invention. As shown in the figure, in the present embodiment, a measuring antenna 1, a measuring receiver 2, an element excitation condition changing means 5,
The point that the measurement antenna position control means 6, the signal generator 7, and the element excitation condition calculation means 8 are provided is basically the same as that of Japanese Patent Publication No. 5-14230 previously proposed by the present applicant, This embodiment is characterized by the operation of the antenna position control means 6 for measurement. The element excitation condition changing means 5 is composed of an amplitude / phase controller 3 and a variable attenuator / phase shifter 4.
【0015】周知のように、アレー空中線は、基本的に
はN個の放射素子9−1〜9−Nがそれぞれ可変減衰器
/移相器4を個別に介して電力分配器10に接続された
構成である。ここでは、放射特性の測定のため、電力分
配器10には信号発生器7から測定用基準信号を給電
し、各放射素子9−1〜9−Nにそれぞれ対応して設け
られた可変減衰器/移相器4を振幅/位相制御器3がそ
れぞれ個別に制御する構成とされている。従って、振幅
/位相制御器3が制御した可変減衰器/移相器4に係る
放射素子9−iが、所定の振幅と位相で励振され、電波
放射を行う。As is well known, an array antenna basically has N radiating elements 9-1 to 9-N connected to a power distributor 10 via variable attenuators / phase shifters 4, respectively. Configuration. Here, in order to measure the radiation characteristics, the power divider 10 is supplied with a reference signal for measurement from the signal generator 7 and variable attenuators provided corresponding to the respective radiation elements 9-1 to 9-N. The amplitude / phase controller 3 controls the phase shifter 4 individually. Therefore, the radiating element 9-i of the variable attenuator / phase shifter 4 controlled by the amplitude / phase controller 3 is excited with a predetermined amplitude and phase, and emits radio waves.
【0016】アレー空中線には種々の形態があり、本発
明は任意の形態のアレー空中線に適用できる。しかし、
第1実施例では、原理的な説明の観点から放射素子9−
1〜9−Nは図1に示すように直線配列したものとす
る。There are various types of array antennas, and the present invention can be applied to any type of array antenna. But,
In the first embodiment, the radiating element 9-
1 to 9-N are linearly arranged as shown in FIG.
【0017】従って、測定用空中線1は、測定用空中線
位置制御手段6により、アレー空中線の各放射素子9−
1〜9−Nと予め定めた間隔を置いて1対1対応で正対
する位置に移動設定されるが、本実施例では各放射素子
9−1〜9−Nの配列位置から一定距離(例えば1m)
離間した位置に各放射素子9−1〜9−Nの配列方向に
平行して設定される測定用基準線101上を直線移動す
ることになる。Therefore, the measuring antenna 1 is controlled by the measuring antenna position control means 6 and each radiating element 9- of the array antenna is measured.
1 to 9-N are set to move to positions facing each other in a one-to-one correspondence with a predetermined interval, but in this embodiment, a fixed distance (for example, from the arrangement position of each of the radiating elements 9-1 to 9-N) 1m)
The linear movement is performed on the measurement reference line 101 set in parallel with the arrangement direction of the radiating elements 9-1 to 9-N at the separated positions.
【0018】この測定用基準線101をX軸とすると、
測定用空中線位置制御手段6は測定用空中線1を移動設
定する度にX軸上の位置情報を素子励振条件算定手段8
に与える。Assuming that the measurement reference line 101 is the X axis,
The measurement antenna position control means 6 reads the position information on the X-axis every time the measurement antenna 1 is moved and set.
Give to.
【0019】次に、本実施例の測定方法について説明す
る。測定方法には次の2通りがある。第1の方法は測定
用空中線1を移動しながら放射素子9−1〜9−Nに1
対1対応で正対させて、測定は測定用空中線1と放射素
子間との距離が幾何学的に等しい複数の放射素子につい
て行う方法である。Next, the measuring method of this embodiment will be described. There are the following two measurement methods. In the first method, the radiating elements 9-1 to 9-N are moved to 1 while moving the measuring antenna 1.
The measurement is performed on a plurality of radiating elements whose distances between the measuring antenna 1 and the radiating elements are geometrically equal.
【0020】すなわち、この第1の測定方法では、図2
に示すように、測定用空中線1を測定用基準線101上
を移動させて例えば放射素子9−iと正対させたときに
は、このとき測定用空中線1との距離が幾何学的に等し
い2つの放射素子9−(i−1)と9−(i+1)のそ
れぞれについて測定を順次に行う。That is, in the first measuring method, as shown in FIG.
As shown in the figure, when the measurement antenna 1 is moved on the measurement reference line 101 and is directly opposed to, for example, the radiating element 9-i, at this time, two distances from the measurement antenna 1 are geometrically equal. The measurement is sequentially performed for each of the radiating elements 9- (i-1) and 9- (i + 1).
【0021】勿論、この場合、測定用空中線1との距離
が幾何学的に等しい2つの放射素子は9−(i−2)及
び9−(i+2)など、放射素子9−(i−1)と9−
(i+1)のそれぞれのもっと外側にも存在するが、測
定用空中線1と放射素子の見込み角度が小さくなるた
め、測定用空中線1の単体放射パターンや放射素子のア
レーエレメントパターンが不安定となるパターンの外側
領域で測定することになる上、測定用空中線1と放射素
子の距離が離れるので、受信電力も低下することにな
り、測定精度が劣化してしまう。このため、なるべく内
側の測定用空中線に近い放射素子を測定する方がよい。Of course, in this case, the two radiating elements whose distance from the measurement antenna 1 are geometrically equal are radiating elements 9- (i-1) such as 9- (i-2) and 9- (i + 2). And 9-
Although it exists on the outer side of each of (i + 1), the single radiation pattern of the measurement antenna 1 and the array element pattern of the radiation element become unstable because the prospective angle between the measurement antenna 1 and the radiation element becomes small. In addition, since the measurement is performed in the outer region, the distance between the measurement antenna 1 and the radiating element increases, so that the received power also decreases and the measurement accuracy deteriorates. Therefore, it is better to measure the radiating element as close to the measuring antenna as possible inside.
【0022】放射素子数が4の倍数でないときには、こ
の第1の測定方法では放射素子9−(N−1)や9−N
が半端となって残ってしまうが、この場合は次のように
して測定する。すなわち、放射素子9−(N−1)を測
定する場合には、図3に示すように、測定用空中線1を
放射素子9−Nに正対させ、放射素子9−(N−1)の
みを測定する。同様に、放射素子9−Nを測定する場合
には、図4に示すように、測定用空中線1を仮想放射素
子9−(N+1)に正対させて放射素子9−Nのみを測
定する。When the number of radiating elements is not a multiple of four, the first measuring method uses the radiating elements 9- (N-1) and 9-N
Remains as an odd part. In this case, measurement is performed as follows. That is, when measuring the radiating element 9- (N-1), as shown in FIG. 3, the measurement antenna 1 is directly opposed to the radiating element 9-N, and only the radiating element 9- (N-1) is used. Is measured. Similarly, when measuring the radiating element 9-N, as shown in FIG. 4, the antenna 1 for measurement is made to face the virtual radiating element 9- (N + 1), and only the radiating element 9-N is measured.
【0023】次に、第2の方法は測定用空中線1を移動
しながら隣り合う2つの放射素子間の中心の位置に1対
1対応で正対させて、測定は測定用空中線1と放射素子
間との距離が幾何学的に等しい複数の放射素子について
行う方法である。Next, in the second method, the antenna 1 for measurement is directly opposed to the center position between two adjacent radiating elements while moving the antenna 1 for measurement. This is a method performed for a plurality of radiating elements having a geometrical distance from each other.
【0024】すなわち、この第2の測定方法では、図5
に示すように、測定用空中線1を測定用基準線101上
を移動させて例えば放射素子9−iと9−(i+1)と
の間の中心の位置に正対させたときには、このとき測定
用空中線1との距離が幾何学的に等しい2つの放射素子
9−iと9−(i+1)のそれぞれについて測定を順次
に行う。That is, in the second measuring method, FIG.
As shown in (2), when the measurement antenna 1 is moved on the measurement reference line 101 and is directly opposed to, for example, the center position between the radiating elements 9-i and 9- (i + 1), The measurement is sequentially performed for each of the two radiating elements 9-i and 9- (i + 1) whose geometric distances to the antenna 1 are geometrically equal.
【0025】勿論、この場合も、測定用空中線1との距
離が幾何学的に等しい2つの放射素子は9−(i−1)
及び9−(i+2)など、放射素子9−iと9−(i+
1)のそれぞれのもっと外側にも存在するが、前記した
理由により、なるべく内側の測定用空中線に近い放射素
子を測定する方がよい。Of course, also in this case, the two radiating elements whose distance from the measurement antenna 1 is geometrically equal are 9- (i-1).
And 9- (i + 2), such as radiating elements 9-i and 9- (i +
Although it is present on the outer side of each of 1), it is better to measure the radiating element as close as possible to the inner measuring antenna for the reason described above.
【0026】放射素子数が2の倍数でないときには、こ
の第2の測定方法では放射素子9−Nが半端となって残
ってしまうが、この場合の測定方法の一例について図6
と共に説明する。すなわち、放射素子9−Nを測定する
場合には、図6に示すように、測定用空中線1を放射素
子9−Nと仮想放射素子9−(N+1)との間の中心位
置に正対させて放射素子9−Nのみを測定する。When the number of radiating elements is not a multiple of two, the radiating element 9-N remains as an odd part in the second measuring method. An example of the measuring method in this case is shown in FIG.
Will be explained together. That is, when measuring the radiating element 9-N, as shown in FIG. 6, the measurement antenna 1 is directly opposed to the center position between the radiating element 9-N and the virtual radiating element 9- (N + 1). To measure only the radiating element 9-N.
【0027】次に、図1の実施例の動作について説明す
る。測定用空中線1は、測定用空中線位置制御手段6に
より測定用基準線101に沿って移動され、前述した2
通りの測定方法のうちいずれか定めた一の測定方法に従
い、放射素子9−1〜9−Nのうち1個の放射素子に正
対する位置又は隣り合う2個の放射素子の間の中心の位
置に測定用空中線1を設定する。このときの測定用空中
線1の設定位置をxで表す。Next, the operation of the embodiment shown in FIG. 1 will be described. The measurement antenna 1 is moved along the measurement reference line 101 by the measurement antenna position control means 6, and
According to one of the two measurement methods, one of the radiating elements 9-1 to 9-N faces directly one radiating element or the center position between two adjacent radiating elements. Set antenna 1 for measurement to. The set position of the measurement antenna 1 at this time is represented by x.
【0028】ここで、放射素子9−1〜9−Nのうちの
i番目の放射素子9−iの等価励振電流をIi、放射特
性(見込み角度の関数)をDiとし、位置xに設定され
ている測定用空中線1における放射素子9−iからの受
信電界をexiとすると、exiは次式で表される。Here, the equivalent excitation current of the i-th radiating element 9-i of the radiating elements 9-1 to 9-N is I i , the radiation characteristic (a function of the estimated angle) is D i , and the position x is set. Assuming that the received electric field from the radiating element 9-i in the set measurement antenna 1 is e xi , e xi is expressed by the following equation.
【0029】 exi=Di・Fxi・Ii (1) 上式において、Fxiは測定用空中線1と放射素子9−i
との間の相対的な位置関係等に関連する放射伝搬係数で
ある。E xi = D i · F xi · I i (1) In the above equation, F xi is the antenna 1 for measurement and the radiating element 9-i
It is a radiation propagation coefficient related to a relative positional relationship between and.
【0030】また、位置xに設定されている測定用空中
線1における全放射素子9−1〜9−Nからの放射によ
る受信電界をEx、放射素子9−iの等価励振電流をIi
からIi・δi(ただし、δiは放射素子9−iの励振条
件変更係数)に変更した場合における全放射素子9−1
〜9−Nからの放射による受信電界をExiとすると、次
式が成立することが知られている。Further, E x the received field caused by radiation from total radiation element 9-1 to 9-N in measuring antenna 1 which is set to the position x, the equivalent excitation current of the radiating element 9-i I i
From all the radiating elements 9-1 in the case of changing from I i · δ i (where δ i is the excitation condition changing coefficient of the radiating element 9-i).
When the received electric field by radiation from to 9-N and E xi, it is known that the following equation is established.
【0031】[0031]
【数1】 例えば、図5に示す位置に設定されているときの測定用
空中線1は(2)式の受信電界Ex及びExiを図1の測
定用受信機2に供給する。測定用受信機2は、信号発生
器7の出力測定用基準信号を基準として、入力受信電界
Ex及びExiの振幅値及び位相値を計測し、その計測結
果を素子励振条件算定手段8に供給する。[Equation 1] For example, measuring antenna 1 when set to the position shown in FIG. 5 (2) provides a received electric field E x and E xi to the measuring receiver 2 of FIG. 1 of Formula. Measuring receiver 2, based on the output measurement reference signal of the signal generator 7, to measure the amplitude values and phase values of the input reception electric field E x and E xi, the measurement result to the device the excitation condition calculating means 8 Supply.
【0032】また、(2)式の放射伝搬係数Fxi及び励
振条件変更係数δiは、それぞれ測定用空中線1の放射
特性と測定基準線101上の設定位置及び放射素子9−
iの等価励振電流変更条件等により予め設定されるパラ
メータであり、これらは測定用空中線位置制御手段6よ
り素子励振条件算定手段8に入力される。素子励振条件
算定手段8は、(2)式に基づいてDi・Iiを算出す
る。The radiation propagation coefficient F xi and the excitation condition change coefficient δ i in the equation (2) are the radiation characteristic of the measurement antenna 1, the set position on the measurement reference line 101, and the radiation element 9 −, respectively.
These parameters are set in advance according to the equivalent excitation current change condition of i, and are input from the measurement antenna position control means 6 to the element excitation condition calculation means 8. Element excitation condition calculating means 8 calculates the D i · I i based on the equation (2).
【0033】このように、測定用空中線1を測定用基準
線101上の所定位置xに設定し、放射素子9−iの等
価励振電流Iiを変更する前後のそれぞれについてアレ
ー空中線の近傍界としての放射電界を測定用空中線1に
より受信し、これらの受信電界Ex及びExiと、予め設
定される放射伝搬係数Fxi及び励振条件変更係数δiを
素子励振条件算定手段8に入力することにより、容易に
放射素子9−iと9−(i+1)のDi・Iiをそれぞれ
略同時に算出することができる。In this way, the measuring antenna 1 is set at a predetermined position x on the measuring reference line 101, and the near field of the array antenna is obtained before and after changing the equivalent excitation current I i of the radiating element 9-i. that of a radiation electric field received by the measuring antenna 1, and inputs and these reception electric field E x and E xi, a radiation propagation coefficient is set in advance F xi and excitation conditions change coefficient [delta] i in the element excitation condition calculating means 8 Thus, it is possible to easily calculate D i · I i of the radiating elements 9-i and 9- (i + 1) substantially simultaneously.
【0034】これは、図5の測定方法では、測定用空中
線1と放射素子9−iとの距離に幾何学的に等しいもう
1つの放射素子9−(i+1)についても放射素子9−
iのDi・Iiと同一であるからである。以下、上記と同
様の動作により、すべての放射素子9−1〜9−Nにつ
いて、基本的には2つの放射素子ずつDi・Iiをそれぞ
れ略同時に算出することができる。また、第1の測定方
法でも同様に測定できる。In the measuring method of FIG. 5, this is because the radiating element 9- (i + 1) is geometrically equal to the distance between the measuring antenna 1 and the radiating element 9-i.
This is because it is the same as Di · Ii of i . Hereinafter, the same operation as described above, for all of the radiating elements 9-1 to 9-N, basically it is possible to substantially simultaneously calculated respectively D i · I i by two radiating elements. Also, the measurement can be performed in the same manner by the first measurement method.
【0035】以上のように、本実施例によれば、放射素
子9−1〜9−Nのうち1個の放射素子に正対する位置
又は隣り合う2個の放射素子の間の中心の位置に測定用
空中線1を設定する度に、2個の放射素子を測定するこ
とを順次に繰り返すようにしたため、測定用空中線1の
移動設定回数を放射素子数の半分程度にできるため、放
射素子の励振振幅及び励振位相の測定時間を従来よりも
短縮できる。As described above, according to the present embodiment, at the position directly facing one of the radiating elements 9-1 to 9-N or at the center position between two adjacent radiating elements. Since the measurement of two radiating elements is sequentially repeated each time the measuring antenna 1 is set, the number of times of movement of the measuring antenna 1 can be reduced to about half of the number of radiating elements. The measurement time of the amplitude and the excitation phase can be shortened as compared with the related art.
【0036】また、一般的なアレー素子であれば、2個
の測定対象放射素子と測定用空中線1との間は本実施例
では常に等しくなるため、測定対象放射素子と測定用空
中線1の見込み角度も常に等しくなり、よって位相と振
幅の測定結果に対して補正する必要はなく、補正のため
の演算器やメモリなどの回路が不要であり、簡単な構成
とすることができる。Further, in the case of a general array element, since the two radiating elements to be measured and the antenna 1 for measurement are always equal in this embodiment, the radiating elements to be measured and the antenna 1 for measurement are expected. The angles are always the same, and therefore it is not necessary to correct the measurement results of the phase and the amplitude, and a circuit such as a computing unit or a memory for the correction is not required, and the configuration can be simplified.
【0037】以上は、放射素子を直線配列したアレー空
中線の例であるが、次に放射素子を平面配列したアレー
空中線について説明する。放射素子の配列方法として
は、一般に図7に示すような四角配列と、図8に示すよ
うな三角配列とが用いられる。図7及び図8のいずれも
アレー空中線を正面から見た場合の素子配列を示す。The above is an example of an array antenna in which radiating elements are linearly arranged. Next, an array antenna in which radiating elements are arranged in a plane will be described. As a method of arranging the radiating elements, a square array as shown in FIG. 7 and a triangular array as shown in FIG. 8 are generally used. 7 and 8 show the element arrangement when the array antenna is viewed from the front.
【0038】図7に示す四角配列では、一般的に縦方向
の放射素子19−(j,1)、19−(j,2)及び1
9−(j,3)(ただし、j=1,2,3)と横方向の
放射素子19−(1,j)、19−(2,j)及び19
−(3,j)とは、それぞれ間隔がすべて等しく配置さ
れている。このため、同一の縦方向及び横方向2個ずつ
の計4個の放射素子を「点」、放射素子間を「辺」と仮
定して、アレー空中線を正面から見ると、放射素子の配
列は長方形に見える。縦方向と横方向の両方の放射素子
間隔が等しい特殊な場合は、正四角配列となる。In the square array shown in FIG. 7, the radiating elements 19- (j, 1), 19- (j, 2) and 1
9- (j, 3) (where j = 1,2,3) and lateral radiating elements 19- (1, j), 19- (2, j) and 19
− (3, j) are arranged at equal intervals. For this reason, assuming that a total of four radiating elements, two each in the same vertical and horizontal directions, are “points” and the radiating elements are “sides”, and the array antenna is viewed from the front, the array of radiating elements is Looks rectangular. In a special case where the radiating element spacings in both the vertical and horizontal directions are equal, a regular square array is used.
【0039】図8に示す三角配列では、一般的に放射素
子29−(k,1)と29−(k,2)(ただし、k=
1,3)や29−(2,1)、29−(2,2)及び2
9−(2,3)は、縦方向及び横方向にそれぞれ間隔が
すべて等しく配置されている。このため、隣り合う3個
の放射素子を「点」、放射素子間を「辺」と仮定して、
アレー空中線を正面から見ると、放射素子の配列は二等
辺三角形に見える。In the triangular arrangement shown in FIG. 8, radiating elements 29- (k, 1) and 29- (k, 2) (where k =
1,3), 29- (2,1), 29- (2,2) and 2
9- (2, 3) are all equally spaced in the vertical and horizontal directions. For this reason, assuming that three adjacent radiating elements are “points” and the area between the radiating elements is “side”,
When the array antenna is viewed from the front, the array of radiating elements appears to be an isosceles triangle.
【0040】また、この三角配列では、縦方向と横方向
の素子間隔が次式を満足する特殊な場合は、正三角配列
となる。Further, in this triangular array, in a special case where the vertical and horizontal element intervals satisfy the following equation, an equilateral triangular array is used.
【0041】[0041]
【数2】 ここで、DEL:縦方向の放射素子間隔 DAZ:横方向の放射素子間隔 さて、図7の一般的な四角配列の場合、測定用空中線を
放射素子19−(2,2)に正対する位置に設定し、測
定は測定用空中線との距離が等しい放射素子19−
(1,1)、19−(1,3)、19−(3,1)及び
19−(3,3)の4個の素子について行う。[Equation 2] Here, D EL : spacing of radiating elements in the vertical direction D AZ : spacing of radiating elements in the horizontal direction In the case of the general square array shown in FIG. 7, the measurement antenna is directly opposed to the radiating element 19- (2, 2). Position, and the measurement is performed with the radiating element 19- having the same distance from the measurement antenna.
This is performed for four elements (1, 1), 19- (1, 3), 19- (3, 1), and 19- (3, 3).
【0042】また、特殊な四角配列である正四角配列の
場合、測定は一般的な四角配列の場合と同様に、放射素
子19−(1,1)、19−(1,3)、19−(3,
1)及び19−(3,3)の4個の素子について行う
か、もう一組の測定用空中線との距離が等しい放射素子
19−(1,2)、19−(2,1)、19−(2,
3)及び19−(3,2)の4個の素子について行う
か、いずれか一方を選択することができる。In the case of the regular square array which is a special square array, the measurement is performed in the same manner as in the case of the general square array, and the radiating elements 19- (1, 1), 19- (1, 3), 19- (3,
1) and 19- (3,3), or the radiating elements 19- (1,2), 19- (2,1), 19 having the same distance from the other set of measurement antennas. − (2,
3) and 19- (3, 2) can be performed or any one of them can be selected.
【0043】更に、測定用空中線を放射素子19−
(1,1)、19−(1,2)、19−(2,1)及び
19−(2,2)の4個の素子の図7に示す中心位置2
0に正対して設定することにより、一般的な四角配列及
び正四角配列の場合でも測定用空中線と放射素子19−
(1,1)、19−(1,2)、19−(2,1)及び
19−(2,2)間の距離がすべて等しいので、放射素
子19−(1,1)、19−(1,2)、19−(2,
1)及び19−(2,2)の4個の素子について測定を
行うことができる。Further, the measurement antenna is connected to the radiating element 19-.
The center position 2 shown in FIG. 7 of the four elements (1, 1), 19- (1, 2), 19- (2, 1) and 19- (2, 2).
By setting the value directly to 0, the antenna for measurement and the radiating element 19- are used even in a general square array and a square array.
Since the distances between (1,1), 19- (1,2), 19- (2,1) and 19- (2,2) are all equal, the radiating elements 19- (1,1), 19- ( 1,2), 19- (2,
Measurements can be performed on four elements 1) and 19- (2,2).
【0044】次に、図8の一般的な三角配列の場合、測
定用空中線を放射素子29−(2,2)に正対する位置
に設定し、測定は測定用空中線との距離が等しい放射素
子29−(1,1)、29−(1,2)、29−(3,
1)及び29−(3,2)の4個について行う。また、
特殊な三角配列である正三角配列の場合、測定は測定用
空中線との距離が等しい放射素子29−(1,1)、2
9−(1,2)、29−(2,1)、29−(2,
3)、29−(3,1)及び29−(3,2)の6個に
ついて行う。Next, in the case of the general triangular arrangement shown in FIG. 8, the measurement antenna is set at a position directly facing the radiating element 29- (2, 2), and the measurement is performed with the radiating element having the same distance from the measurement antenna. 29- (1, 1), 29- (1, 2), 29- (3,
1) and 29- (3, 2). Also,
In the case of the equilateral triangular arrangement, which is a special triangular arrangement, the measurement is performed using the radiating elements 29- (1, 1), 2 having the same distance from the measurement antenna.
9- (1, 2), 29- (2, 1), 29- (2, 2)
3), 29- (3, 1) and 29- (3, 2) are performed.
【0045】また、放射素子を円柱状に配列した円柱状
アレー空中線や放射素子を円環状に配列した円環状アレ
ー空中線においても、縦方向及び横方向の放射素子間隔
がそれぞれ等しい場合は、上記の実施例と同様な方法で
測定することができる。In the case of a cylindrical array antenna in which radiating elements are arranged in a columnar shape and an annular array antenna in which radiating elements are arranged in an annular shape, when the vertical and horizontal radiating element intervals are equal to each other, It can be measured in the same manner as in the examples.
【0046】例えば、図10に示すような、複数の放射
素子が円柱状に三角配列された円柱状アレー空中線60
の場合について説明するに、測定用空中線1を円柱の軸
方向に平行な測定用基準線101に沿って移動し、例え
ば放射素子39−(2,2)に正対する位置に設定した
ものとする。For example, as shown in FIG. 10, a columnar array antenna 60 in which a plurality of radiating elements are arranged in a columnar triangular shape.
In the following description, it is assumed that the measuring antenna 1 is moved along the measuring reference line 101 parallel to the axial direction of the cylinder, and is set at a position directly facing the radiating element 39- (2, 2), for example. .
【0047】この場合の測定は、測定用空中線1との距
離が等しい放射素子39−(1,1)、39−(1,
2)、39−(3,1)、39−(3,2)の4個につ
いて行う。In the measurement in this case, the radiation elements 39- (1, 1) and 39- (1, 1) having the same distance from the measurement antenna 1 are used.
2), 39- (3, 1), and 39- (3, 2).
【0048】なお、アレー空中線は回転台上に載置して
回転させ測定する。具体的には、例えばアレー空中線が
平板状の場合には、測定用空中線1が移動する測定用基
準線101と放射素子9−1〜9−Nの配列方向とが平
行となるように調整する。また、アレー空中線が円柱状
の場合には、測定用空中線1をアレー空中線の回転軸の
方向に平行に移動させ、回転台を回転してアレー空中線
を回転させる。アレー空中線が環状の場合には、特定の
場所に移動設定し、そこに固定し、回転台を回転してア
レー空中線を回転させる。The array antenna is mounted on a turntable and rotated for measurement. Specifically, for example, when the array antenna is a flat plate, the measurement reference line 101 on which the measurement antenna 1 moves and the arrangement direction of the radiating elements 9-1 to 9-N are adjusted to be parallel. . When the array antenna is cylindrical, the measurement antenna 1 is moved in parallel to the direction of the rotation axis of the array antenna, and the turntable is rotated to rotate the array antenna. When the array antenna is circular, it is moved to a specific place, fixed there, and the turntable is rotated to rotate the array antenna.
【0049】図1はアレー空中線の各放射素子に電波を
送信させ、測定する場合の空中線測定装置であるが、周
知のようにアレー空中線には、アクティブアレー空中線
とパッシブアレー空中線があり、パッシブアレー空中線
では送信と受信が同一の系で構成されるのに対し、アク
ティブアレー空中線では送信と受信が異なる系で構成さ
れる。従って、パッシブアレー空中線では以上説明した
送信による測定での値を受信の場合にも適用できるが、
アクティブアレー空中線では送信の他に受信の場合も測
定する必要がある。FIG. 1 shows an antenna measuring device for transmitting and measuring radio waves to each radiating element of the array antenna. As is well known, the array antenna includes an active array antenna and a passive array antenna, and a passive array antenna. In the antenna, transmission and reception are configured by the same system, whereas in the active array antenna, transmission and reception are configured by different systems. Therefore, the passive array antenna can be applied to the case of receiving the value measured by the above-mentioned transmission,
In the active array antenna, it is necessary to measure not only transmission but also reception.
【0050】図9は本発明の空中線測定装置の他の実施
例のブロック図を示す。同図中、図1と同一構成部分に
は同一符号を付し、その説明を省略する。図9におい
て、信号発生器11は、測定用空中線1と測定用受信機
2のそれぞれに基準信号を供給する。これにより、測定
用空中線1は電波を送信し、放射素子9−1〜9−Nの
うち測定対象放射素子の受信電界の振幅・位相を対応す
る可変減衰器/移相器4で設定し、それを電力分配器1
0を介して測定用受信機2に供給する。FIG. 9 is a block diagram showing another embodiment of the antenna measuring apparatus according to the present invention. In the figure, the same components as those in FIG. 1 are designated by the same reference numerals, and their description will be omitted. In FIG. 9, a signal generator 11 supplies a reference signal to each of the measurement antenna 1 and the measurement receiver 2. As a result, the measurement antenna 1 transmits radio waves, and among the radiating elements 9-1 to 9-N, the amplitude and phase of the reception electric field of the radiating element to be measured are set by the corresponding variable attenuator / phase shifter 4, Power distributor 1
0 to the measuring receiver 2.
【0051】これにより、上述したのと同様の手順で受
信時の測定ができる。すなわち、各放射素子9−1〜9
−N毎に測定した振幅、位相角から当該放射素子のみの
励振振幅及び励振位相を前記実施例と同様にして測定で
きる。Thus, measurement at the time of reception can be performed in the same procedure as described above. That is, each of the radiating elements 9-1 to 9
From the amplitude and phase angle measured for each −N, the excitation amplitude and excitation phase of only the radiating element can be measured in the same manner as in the above embodiment.
【0052】なお、以上の実施例では測定用空中線1を
設定する度に、2個の放射素子を測定することを順次に
繰り返すようにしたが、本発明はこれに限定されるもの
ではなく、基本的には測定用空中線1を設定する毎に複
数の放射素子の測定を略同時に行うことができる。In the above embodiment, the measurement of two radiating elements is sequentially repeated every time the antenna 1 for measurement is set. However, the present invention is not limited to this. Basically, measurement of a plurality of radiating elements can be performed substantially simultaneously each time the antenna 1 for measurement is set.
【0053】[0053]
【発明の効果】以上説明したように、本発明によれば、
測定用空中線をアレー空中線の各放射素子と予め定めた
間隔を置いて測定用空中線をアレー空中線の各放射素子
又は隣り合う放射素子間の中心位置と1対1対応で正対
する位置に移動設定させ、測定用空中線から幾何学的に
距離の等しい複数の放射素子を略同時に測定することに
より、測定用空中線の移動設定回数を従来よりも減らす
ようにしたため、従来よりもアレー空中線を構成する放
射素子の測定時間を短縮することができる。As described above, according to the present invention,
The measurement antenna is moved and set at a predetermined distance from each radiating element of the array antenna, and the measurement antenna is moved to a position directly facing the center position between each radiating element of the array antenna or the adjacent radiating element in a one-to-one correspondence. By measuring a plurality of radiating elements having the same geometric distance from the measuring antenna substantially simultaneously, the number of times of setting the moving of the measuring antenna is reduced as compared with the conventional one, so that the radiating element constituting the array antenna more than before. Measurement time can be shortened.
【0054】また、本発明によれば、各放射素子の縦方
向及び横方向の放射素子間隔がそれぞれすべて等しい場
合、測定用空中線と測定対象放射素子までの距離及び見
込み角度が等しくなり、測定した位相と振幅に対して補
正する必要がないため、従来のような補正のための演算
器やメモリが不要であり、よってより簡単な構成とする
ことができる。Further, according to the present invention, when the radiating element intervals in the vertical and horizontal directions of each radiating element are all equal, the distance and the expected angle between the antenna for measurement and the radiating element to be measured become equal, and the measurement was performed. Since there is no need to correct the phase and the amplitude, an arithmetic unit and a memory for correction as in the related art are not required, and thus a simpler configuration can be achieved.
【図1】本発明の一実施例のブロック図である。FIG. 1 is a block diagram of one embodiment of the present invention.
【図2】図1における第1の測定方法を説明する測定用
空中線と放射素子との位置関係の一例を示す図である。FIG. 2 is a diagram illustrating an example of a positional relationship between a measurement antenna and a radiating element for explaining the first measurement method in FIG.
【図3】図1における第1の測定方法を説明する測定用
空中線と放射素子との位置関係の一例を示す図である。FIG. 3 is a diagram illustrating an example of a positional relationship between a measurement antenna and a radiating element for explaining a first measurement method in FIG. 1;
【図4】図1における第1の測定方法を説明する測定用
空中線と放射素子との位置関係の一例を示す図である。FIG. 4 is a diagram illustrating an example of a positional relationship between a measuring antenna and a radiating element for explaining the first measuring method in FIG. 1.
【図5】図1における第2の測定方法を説明する測定用
空中線と放射素子との位置関係の一例を示す図である。FIG. 5 is a diagram illustrating an example of a positional relationship between a measurement antenna and a radiating element for explaining a second measurement method in FIG. 1;
【図6】図1における第2の測定方法を説明する測定用
空中線と放射素子との位置関係の一例を示す図である。FIG. 6 is a diagram illustrating an example of a positional relationship between a measurement antenna and a radiating element for explaining a second measurement method in FIG. 1;
【図7】放射素子の四角配列の一例を示す図である。FIG. 7 is a diagram showing an example of a square array of radiating elements.
【図8】放射素子の三角配列の一例を示す図である。FIG. 8 is a diagram illustrating an example of a triangular arrangement of radiating elements.
【図9】本発明の他の実施例のブロック図である。FIG. 9 is a block diagram of another embodiment of the present invention.
【図10】円柱状アレー空中線と測定用空中線を斜め上
方から見た斜視図である。FIG. 10 is a perspective view of a columnar array antenna and a measurement antenna viewed from obliquely above.
【図11】従来装置の空中線設定位置の一例を示す図で
ある。FIG. 11 is a diagram showing an example of an antenna setting position of the conventional device.
1 測定用空中線 2 測定用受信機 3 振幅/位相制御器 4 可変減衰器/移相器 5 素子励振条件変更手段 6 測定用空中線位置制御手段 7、11 信号発生器 8 素子励振条件算定手段 9−1〜9−(N+2)、19−(1,1)〜19−
(3,3)、29−(1,1)〜29−(3,2)、3
9−(1,1)〜39−(3,2) 放射素子 10 電力分配器 60 円柱状アレー空中線 101 測定用基準線DESCRIPTION OF SYMBOLS 1 Measurement antenna 2 Measurement receiver 3 Amplitude / phase controller 4 Variable attenuator / phase shifter 5 Element excitation condition changing means 6 Measurement antenna position control means 7, 11 Signal generator 8 Element excitation condition calculation means 9- 1-9- (N + 2), 19- (1,1) -19-
(3,3), 29- (1,1) to 29- (3,2), 3
9- (1, 1) to 39- (3, 2) Radiating element 10 Power splitter 60 Columnar array antenna 101 Measurement reference line
Claims (3)
くなるように配列されたN個(ただし、Nは2以上の整
数)の放射素子から構成されたアレー空中線の該N個の
放射素子の放射電界をそれぞれ測定する測定用空中線
と、 前記N個の放射素子と予め定めた間隔を置いて該N個の
放射素子のうち偶数個の該放射素子に対する幾何学的距
離がそれぞれ等しい位置毎に該測定用空中線を相対的に
移動設定する位置制御手段と、 前記N個の放射素子の励振条件を個々に変化させる素子
励振条件変更手段と、 前記素子励振条件変更手段による素子励振条件の変更前
後のそれぞれについての前記測定用空中線の測定結果及
び前記素子励振条件変更手段よりの励振条件とが少なく
とも入力されて、前記測定用空中線に対して幾何学的距
離がそれぞれ所定値離れた一又は二以上の放射素子のみ
の励振振幅と励振位相を算定する素子励振算定手段とを
有することを特徴とする空中線測定装置。1. An array antenna composed of N (where N is an integer equal to or greater than 2) radiating elements arranged so that the vertical and horizontal intervals are equal to each other. A measuring antenna for measuring a radiated electric field, and at every position where the geometric distance to the even number of the N radiating elements is equal to the N radiating elements at predetermined intervals from the N radiating elements. Position control means for relatively moving and setting the measurement antenna; element excitation condition changing means for individually changing the excitation conditions of the N radiating elements; before and after the element excitation condition is changed by the element excitation condition changing means. At least the measurement result of the measurement antenna and the excitation condition from the element excitation condition changing means are input, and the geometric distances to the measurement antenna are respectively predetermined. An antenna measurement apparatus comprising: element excitation calculation means for calculating the excitation amplitude and the excitation phase of only one or two or more radiation elements apart from each other.
のN個の放射素子のそれぞれに1対1対応で正対する位
置に順次に前記測定用空中線を移動設定することを特徴
とする請求項1記載の空中線測定装置。2. The position control means sequentially moves and sets the measurement aerial line to a position that directly faces each of the N radiating elements of the array aerial line in a one-to-one correspondence. The antenna measuring device described.
のN個の放射素子のうち隣り合う2個の放射素子の間の
中心位置と1対1対応で正対する位置に順次に前記測定
用空中線を移動設定することを特徴とする請求項1記載
の空中線測定装置。3. The position control means sequentially arranges the measurement antennas at positions facing one another in a one-to-one correspondence with the center position between two adjacent radiation elements of the N radiation elements of the array antenna. The antenna measuring device according to claim 1, wherein the antenna is moved and set.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP25805894A JP2606159B2 (en) | 1994-10-24 | 1994-10-24 | Antenna measurement device |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP25805894A JP2606159B2 (en) | 1994-10-24 | 1994-10-24 | Antenna measurement device |
Publications (2)
Publication Number | Publication Date |
---|---|
JPH08122378A true JPH08122378A (en) | 1996-05-17 |
JP2606159B2 JP2606159B2 (en) | 1997-04-30 |
Family
ID=17314955
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---|---|---|---|
JP25805894A Expired - Lifetime JP2606159B2 (en) | 1994-10-24 | 1994-10-24 | Antenna measurement device |
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JP (1) | JP2606159B2 (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2001094499A (en) * | 1999-09-21 | 2001-04-06 | Sanyo Electric Co Ltd | Adaptive array base station |
CN106872801A (en) * | 2017-04-02 | 2017-06-20 | 深圳市通用测试***有限公司 | A kind of near field test system |
Families Citing this family (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US6960848B2 (en) | 2003-05-09 | 2005-11-01 | Nisca Corporation | Electromagnetic drive device and light quantity adjustment device using the same |
JP3975179B2 (en) | 2003-05-09 | 2007-09-12 | ニスカ株式会社 | Electromagnetic drive device and light amount adjustment device using the same |
CN108020729A (en) * | 2017-11-29 | 2018-05-11 | 南京捷希科技有限公司 | The active standing wave test system and test method of a kind of extensive antenna |
-
1994
- 1994-10-24 JP JP25805894A patent/JP2606159B2/en not_active Expired - Lifetime
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2001094499A (en) * | 1999-09-21 | 2001-04-06 | Sanyo Electric Co Ltd | Adaptive array base station |
CN106872801A (en) * | 2017-04-02 | 2017-06-20 | 深圳市通用测试***有限公司 | A kind of near field test system |
CN106872801B (en) * | 2017-04-02 | 2024-04-30 | 深圳市通用测试***有限公司 | Near field test system |
Also Published As
Publication number | Publication date |
---|---|
JP2606159B2 (en) | 1997-04-30 |
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