CN115542268A - Large-aperture phased array antenna block testing method and system - Google Patents
Large-aperture phased array antenna block testing method and system Download PDFInfo
- Publication number
- CN115542268A CN115542268A CN202210938154.XA CN202210938154A CN115542268A CN 115542268 A CN115542268 A CN 115542268A CN 202210938154 A CN202210938154 A CN 202210938154A CN 115542268 A CN115542268 A CN 115542268A
- Authority
- CN
- China
- Prior art keywords
- test
- antenna
- subarray
- sub
- tested
- 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.)
- Pending
Links
Images
Classifications
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01S—RADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
- G01S7/00—Details of systems according to groups G01S13/00, G01S15/00, G01S17/00
- G01S7/02—Details of systems according to groups G01S13/00, G01S15/00, G01S17/00 of systems according to group G01S13/00
- G01S7/40—Means for monitoring or calibrating
- G01S7/4004—Means for monitoring or calibrating of parts of a radar system
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01R—MEASURING ELECTRIC VARIABLES; MEASURING MAGNETIC VARIABLES
- G01R29/00—Arrangements for measuring or indicating electric quantities not covered by groups G01R19/00 - G01R27/00
- G01R29/08—Measuring electromagnetic field characteristics
- G01R29/10—Radiation diagrams of antennas
Landscapes
- Physics & Mathematics (AREA)
- Engineering & Computer Science (AREA)
- General Physics & Mathematics (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- Electromagnetism (AREA)
- Computer Networks & Wireless Communication (AREA)
- Radar Systems Or Details Thereof (AREA)
Abstract
本发明提出了一种大口径相控阵天线分块测试方法及测试系统。该方法通过将原有大型天线划分为若干个子阵,每次在暗室内完成子阵天线的测试,最终将分块测试的数据进行科学有效的数值合成计算,可完成整个大口径天线辐射方向图的合成。该方法解决了暗室有限空间与待测天线大口径需求的矛盾,极大提高了大型天线阵面测试的效率和精度。
The invention provides a large-diameter phased array antenna block test method and test system. This method divides the original large-scale antenna into several sub-arrays, completes the test of the sub-array antenna in the dark room each time, and finally performs scientific and effective numerical synthesis calculation on the data of the block test, and can complete the radiation pattern of the entire large-aperture antenna Synthesis. This method solves the contradiction between the limited space of the darkroom and the large-aperture requirements of the antenna to be tested, and greatly improves the efficiency and accuracy of large-scale antenna array testing.
Description
技术领域technical field
本发明属于天线测试技术领域,具体涉及一种大口径相控阵天线分块测试方法及测试系统。The invention belongs to the technical field of antenna testing, and in particular relates to a large-diameter phased array antenna block testing method and testing system.
背景技术Background technique
近年来,基于卫星平台的星载雷达系统正在飞速发展。借助卫星平台高机动性、广阔的覆盖范围、全天时全天候工作的特性,卫星雷达被广泛应用于全球测绘、空间通信、星地互连等领域。相控阵天线作为雷达系统的核心部件,其主要作用是将射频信号转换为电磁波向空间辐射并接收空间传来的电磁波。随着系统应用需求的不断升级,相控阵天线的口径不断增大,系统复杂度不断提升,除了对系统设计提出了更高的要求外,天线的测试难度也大大增加。由于对空间环境洁净度、温湿度的高要求,星载相控阵天线无法在室外完成方向图测试,而只能在具备航天测试条件的微波暗室中进行。而随着星载雷达应用频段的下探和天线口径的增大,方向图测试对暗室空间的需求越来越大。目前,国内航天微波暗室的有效测试口径远远不能满足大型相控阵天线方向图测试需求。按照天线口径扩建暗室,成本巨大,且测试稳定性无法获得保证,并不是一种好的解决办法。因此,大型相控阵天线分块测试系统的研发迫在眉睫。In recent years, spaceborne radar systems based on satellite platforms are developing rapidly. With the characteristics of high mobility, wide coverage and all-weather work of satellite platforms, satellite radars are widely used in global surveying and mapping, space communications, satellite-ground interconnection and other fields. As the core component of the radar system, the phased array antenna is mainly used to convert radio frequency signals into electromagnetic waves to radiate into space and receive electromagnetic waves from space. With the continuous upgrading of system application requirements, the aperture of phased array antennas continues to increase, and the complexity of the system continues to increase. In addition to putting forward higher requirements for system design, the difficulty of testing antennas has also greatly increased. Due to the high requirements on the cleanliness, temperature and humidity of the space environment, the spaceborne phased array antenna cannot complete the pattern test outdoors, but can only be carried out in a microwave anechoic chamber with aerospace test conditions. With the lowering of the application frequency band of spaceborne radar and the increase of the antenna aperture, the demand for the darkroom space of the pattern test is increasing. At present, the effective test aperture of the domestic aerospace microwave anechoic chamber is far from meeting the test requirements of large phased array antenna pattern. It is not a good solution to expand the darkroom according to the antenna caliber, the cost is huge, and the test stability cannot be guaranteed. Therefore, the research and development of large-scale phased array antenna block testing system is imminent.
发明内容Contents of the invention
本发明突破了现有近场测量方法对天线口径的限制,提出了一种大口径天线分块测试的方法。该方法通过将原有大型天线划分为若干个子阵,每次在暗室内完成子阵级天线的测试,最终将分块测试的数据进行科学有效的数值合成计算,可完成整个大口径天线辐射方向图的合成。该方法解决了暗室有限空间与待测天线大口径需求的矛盾,极大提高了大型天线阵面测试的效率和精度。The invention breaks through the limitation of the antenna caliber by the existing near-field measurement method, and proposes a block testing method for the large-diameter antenna. This method divides the original large-scale antenna into several sub-arrays, completes the test of the sub-array-level antenna in the dark room each time, and finally performs scientific and effective numerical synthesis calculation on the data of the block test, and can complete the radiation direction of the entire large-aperture antenna. Composition of graphs. This method solves the contradiction between the limited space of the darkroom and the large-aperture requirements of the antenna to be tested, and greatly improves the efficiency and accuracy of large-scale antenna array testing.
本发明提供一种大口径相控阵天线分块测试方法及测试系统,用以解决暗室测试空间无法满足大型天线测试需求的问题。The invention provides a large-diameter phased array antenna block test method and a test system, which are used to solve the problem that the darkroom test space cannot meet the test requirements of large-scale antennas.
本发明提供了一种大口径相控阵天线分块测试方法,该方法步骤如下:The invention provides a large-diameter phased array antenna block test method, the method steps are as follows:
步骤1、根据微波暗室有效测试范围,将大口径相控阵天线划分为适配暗室尺寸的若干个子阵,子阵数量设为n,天线子阵编号为i,i=1、2、…、n,每次测试一个子阵;Step 1. According to the effective test range of the microwave anechoic chamber, the large-aperture phased array antenna is divided into several sub-arrays suitable for the size of the anechoic chamber. The number of sub-arrays is set to n, and the number of antenna sub-arrays is i, i=1, 2, ..., n, each test a sub-array;
步骤2、将待测天线子阵i置于微波暗室内,完成位置标校Step 2. Place the antenna sub-array i to be tested in the microwave anechoic chamber and complete the position calibration
将待测子阵i置于微波暗室内,i=1、2、…、n,通过天线安装定位系统校准待测子阵与测试探头之间的相对位置,使子阵平面与探头测试平面平行且天线子阵平面度满足一定要求;记录探头测试起始位置与待测子阵间的相对位置关系,保证每个子阵测试的相位中心恒定;Place the subarray i to be tested in the microwave anechoic chamber, i=1, 2,...,n, calibrate the relative position between the subarray to be tested and the test probe through the antenna installation and positioning system, so that the plane of the subarray is parallel to the test plane of the probe And the flatness of the antenna sub-array meets certain requirements; record the relative positional relationship between the starting position of the probe test and the sub-array to be tested, and ensure that the phase center of each sub-array test is constant;
步骤3、在微波暗室内完成天线子阵i测试系统配置Step 3. Complete the antenna subarray i test system configuration in the microwave anechoic chamber
通过终端显控系统、测试伺服系统设置天线测试参数,包括:测试探头扫描范围,扫描步进,扫描速率;射频探测系统工作频率、采样速率、测试波位、天线收/发状态选择等。Set antenna test parameters through terminal display and control system and test servo system, including: test probe scanning range, scanning step, scanning rate; RF detection system operating frequency, sampling rate, test wave position, antenna receiving/transmitting state selection, etc.
步骤4、运行测试系统,完成待测子阵近场平面幅度和相位数据录取Step 4. Run the test system to complete the acquisition of near-field plane amplitude and phase data of the subarray to be tested
该步骤可通过测试伺服系统、射频探测系统配合完成。测试伺服系统控制测试探头移动至指定位置,射频探测系统在指定位置进行射频信号采样,获得相应位置的电场幅度和相位信息,并将信息存储在终端显控系统内;This step can be completed through the cooperation of the test servo system and the radio frequency detection system. The test servo system controls the test probe to move to the designated position, and the radio frequency detection system samples the radio frequency signal at the designated position, obtains the electric field amplitude and phase information of the corresponding position, and stores the information in the terminal display and control system;
步骤5、计算天线子阵远场方向图fi Step 5. Calculate the far-field pattern f i of the antenna subarray
根据近场幅度和相位数据,采用近远场变换方法,计算子阵的远场方向图fi,i=1、2、…、n;According to the near-field amplitude and phase data, adopt the near-far field transformation method to calculate the far-field pattern f i of the sub-array, i=1, 2, ..., n;
步骤6、重复测试步骤2~6,完成所有子阵的近场幅度相位数据录取及远场方向图计算;Step 6. Repeat test steps 2 to 6 to complete the acquisition of near-field amplitude and phase data and calculation of far-field pattern for all subarrays;
步骤7、将每个子阵的远场方向图fi根据子阵相对位置关系进行矢量合成,计算得全阵面远场方向图;Step 7. Carry out vector synthesis of the far-field pattern fi of each sub-array according to the relative positional relationship of the sub-arrays, and calculate the far-field pattern of the whole array;
该步骤将每个子阵的远场方向图fi看作单元方向图。根据子阵的排布和划分,可参照如下公式对每个子阵的相位中心进行修正,最终将所有子阵的远场方向图进行远场矢量合成得到最终远场辐射方向图F。This step regards the far-field pattern fi of each subarray as the unit pattern. According to the arrangement and division of sub-arrays, the phase center of each sub-array can be corrected by referring to the following formula, and finally the far-field radiation pattern F of all sub-arrays is synthesized by far-field vector to obtain the final far-field radiation pattern F.
式中:F为大口径相控阵天线的最终方向图;In the formula: F is the final pattern of the large aperture phased array antenna;
fi为每个子阵的远场方向图,i=1、2、…、n;f i is the far field pattern of each sub-array, i=1, 2,..., n;
k为波数,k=2π/λ,λ为波长;k is the wave number, k=2π/λ, and λ is the wavelength;
u=sin(θ)cos(φ);u=sin(θ)cos(φ);
v=sin(θ)sin(φ);v=sin(θ)sin(φ);
xi,yi为第i个子阵在大口径相控阵天线中的相对位置。x i , y i are the relative positions of the ith sub-array in the large aperture phased array antenna.
本发明提供一种大口径相控阵天线分块测试系统,包括:终端显控系统、测试伺服系统、射频探测系统、天线安装定位系统。The invention provides a large-diameter phased array antenna block test system, including: a terminal display and control system, a test servo system, a radio frequency detection system, and an antenna installation and positioning system.
终端显控系统,用于协调完成待测天线、测试伺服系统、射频探测系统之间的状态配置和协同工作,包括:待测天线状态配置、伺服控制、射频系统状态配置、测试数据采集、测试数据存储、测试过程显示和测试结果处理等功能。The terminal display and control system is used to coordinate and complete the state configuration and collaborative work among the antenna under test, test servo system, and radio frequency detection system, including: state configuration of the antenna under test, servo control, radio frequency system state configuration, test data collection, test Functions such as data storage, test process display and test result processing.
测试伺服系统,用于完成天线测试过程中测试设备的机械运动,测试伺服系统包括平面近场扫描架和控制终端。终端显控系统可将测试状态控制指令发送至测试伺服系统,测试伺服系统可根据指令控制平面近场扫描架运行状态完成天线测试。The test servo system is used to complete the mechanical movement of the test equipment during the antenna test process. The test servo system includes a planar near-field scanning frame and a control terminal. The terminal display and control system can send the test status control command to the test servo system, and the test servo system can control the operating status of the plane near-field scanning frame to complete the antenna test according to the command.
射频探测系统,用于完成测试天线数据的采集,射频探测系统包括:矢量网络分析仪、测试探头、测试互连电缆等。矢量网络分析仪通过测试互连电缆与测试探头和待测天线互连。通过终端显控系统可配置矢量网络分析仪的相关测试状态。The radio frequency detection system is used to complete the collection of test antenna data. The radio frequency detection system includes: vector network analyzer, test probe, test interconnection cable, etc. The vector network analyzer is interconnected with the test probes and the antenna under test through the test interconnection cable. The relevant test status of the vector network analyzer can be configured through the terminal display and control system.
天线安装定位系统,用于完成待测天线的安装固定和位置校准,天线安装定位系统包括待测天线安装设备和光学定位设备。每次天线子阵测试前,需安装在相同的位置,通过光学定位设备校准测试探头与待测天线之间的相对位置关系。The antenna installation and positioning system is used to complete the installation, fixing and position calibration of the antenna to be tested. The antenna installation and positioning system includes the antenna installation equipment to be tested and the optical positioning equipment. Before each antenna sub-array test, it needs to be installed in the same position, and the relative positional relationship between the test probe and the antenna under test should be calibrated by optical positioning equipment.
本发明的有益效果是:The beneficial effects of the present invention are:
本发明提供的测试方法和测试系统,可将大型天线拆分为若干个子阵,分块完成天线方向图测试。与传统测试方法相比,该方法可降低大口径天线测试对测试场地空间的要求,同时提高天线测试故障排除的效率,测试过程灵活,测试效率高,可有效解决大口径天线与暗室测试空间有限之间的矛盾。The test method and test system provided by the invention can split a large antenna into several sub-arrays, and complete the antenna pattern test in blocks. Compared with the traditional test method, this method can reduce the space requirements of the test site for large-aperture antenna testing, and at the same time improve the efficiency of antenna test troubleshooting. The test process is flexible and the test efficiency is high. the contradiction between.
附图说明Description of drawings
图1为大口径相控阵天线分块测试方法流程图;Fig. 1 is the block test method flow chart of large aperture phased array antenna;
图2为大口径相控阵天线分块测试系统组成原理图;Figure 2 is a schematic diagram of the large-aperture phased array antenna block test system;
图3为大口径相控阵天线子阵划分示意图。Fig. 3 is a schematic diagram of the sub-array division of the large-aperture phased array antenna.
具体实施方式detailed description
以下将结合具体实施例对本发明提供的技术方案进行详细说明,应理解下述具体实施方式仅用于说明本发明而不用于限制本发明的范围。The technical solutions provided by the present invention will be described in detail below in conjunction with specific examples. It should be understood that the following specific embodiments are only used to illustrate the present invention and are not intended to limit the scope of the present invention.
本发明为解决大口径相控阵天线测试难题,总体思路如下:通过将原有大型天线分块,每次在暗室内完成部分天线的测试,最终将分块测试的数据进行科学有效的数值合成计算,可完成整个大口径天线辐射方向图的合成。The present invention solves the problem of large-diameter phased array antenna testing. The general idea is as follows: by dividing the original large-scale antenna into blocks, the test of some antennas is completed in the dark room each time, and finally the data of the block test is scientifically and effectively synthesized. The calculation can complete the synthesis of the radiation pattern of the entire large-aperture antenna.
实施例一:Embodiment one:
请参考图1和图2,本发明提供一种大口径相控阵天线分块测试方法,应用于相控阵天线分块测试系统,包括:Please refer to Fig. 1 and Fig. 2, the present invention provides a large aperture phased array antenna block test method, which is applied to the phased array antenna block test system, including:
步骤1、根据微波暗室有效测试范围,将大口径相控阵天线划分为适配暗室尺寸的若干个子阵,子阵数量设为n,天线子阵编号为i,i=1、2、…、n,每次测试一个子阵;Step 1. According to the effective test range of the microwave anechoic chamber, the large-aperture phased array antenna is divided into several sub-arrays suitable for the size of the anechoic chamber. The number of sub-arrays is set to n, and the number of antenna sub-arrays is i, i=1, 2, ..., n, each test a sub-array;
划分子阵以微波暗室的两维有效扫描能力为基限,子阵的尺寸必须小于等于微波暗室的有效扫描范围。在满足微波暗室条件的情况下,子阵的数量不限;The sub-array is divided based on the two-dimensional effective scanning capability of the microwave anechoic chamber, and the size of the sub-array must be smaller than or equal to the effective scanning range of the microwave anechoic chamber. In the case of meeting the conditions of the microwave anechoic chamber, the number of sub-arrays is not limited;
由于微波暗室大小各不相同,因此所述微波暗室有效测试范围可根据实际情况进行确定。例如,某微波暗室的有效测试范围为方位向25米、距离向20米。相控阵天线口径为方位向50米,距离向40米。则相控阵天线可分为排布为2╳2的4个子阵,每个子阵的大小为方位向25米,距离向20米,每个子阵均可适配微波暗室的有效测试范围。特殊情况下,可根据相控阵天线的结构组成,将子阵尺寸划分的更小。总之,子阵划分原则为子阵尺寸适配微波暗室的有效测量范围。Since the microwave anechoic chambers vary in size, the effective test range of the microwave anechoic chamber can be determined according to the actual situation. For example, the effective test range of a microwave anechoic chamber is 25 meters in azimuth and 20 meters in distance. The aperture of the phased array antenna is 50 meters in azimuth and 40 meters in distance. Then the phased array antenna can be divided into 4 sub-arrays arranged as 2╳2. The size of each sub-array is 25 meters in azimuth and 20 meters in distance. Each sub-array can be adapted to the effective test range of the microwave anechoic chamber. In special cases, the size of the sub-array can be divided into smaller ones according to the structural composition of the phased array antenna. In short, the subarray division principle is that the size of the subarray adapts to the effective measurement range of the microwave anechoic chamber.
步骤2、将待测天线子阵i置于微波暗室内,完成位置标校Step 2. Place the antenna sub-array i to be tested in the microwave anechoic chamber and complete the position calibration
将待测子阵i置于微波暗室内,i=1、2、…、n,通过天线安装定位系统校准待测子阵与测试探头之间的相对位置,使子阵平面与探头测试平面平行且天线子阵平面度满足一定要求;记录探头测试起始位置与待测子阵间的相对位置关系,保证每个子阵测试的相位中心恒定;Place the subarray i to be tested in the microwave anechoic chamber, i=1, 2,...,n, calibrate the relative position between the subarray to be tested and the test probe through the antenna installation and positioning system, so that the plane of the subarray is parallel to the test plane of the probe And the flatness of the antenna sub-array meets certain requirements; record the relative positional relationship between the starting position of the probe test and the sub-array to be tested, and ensure that the phase center of each sub-array test is constant;
所述天线安装定位系统采用光学定位设备及测试伺服系统配合工作,光学定位设备通过测试伺服系统移动,在相控阵天线表面采样若干个点,记录每个采样点的三坐标。通过采样点的坐标数据拟合相控阵天线的平面度数据。平面度指标可根据各相控阵天线具体要求进行适配。若当前状态不满足要求,可通过调整相控阵天线角度进行修正。每个子阵测试时,探头测试起始位置与待测子阵间的相对位置关系必须保持一致,这是为了保证每个子阵测试的相位中心恒定,后期进行方向图合成时避免产生相位中心误差。The antenna installation and positioning system uses optical positioning equipment and a test servo system to work together. The optical positioning equipment moves through the test servo system to sample several points on the surface of the phased array antenna and record the three coordinates of each sampling point. The flatness data of the phased array antenna is fitted by the coordinate data of the sampling points. The flatness index can be adapted according to the specific requirements of each phased array antenna. If the current state does not meet the requirements, it can be corrected by adjusting the angle of the phased array antenna. During each sub-array test, the relative positional relationship between the probe test starting position and the sub-array to be tested must be consistent. This is to ensure that the phase center of each sub-array test is constant, and to avoid phase center errors during pattern synthesis later.
步骤3、在微波暗室内完成天线子阵i测试系统配置Step 3. Complete the antenna subarray i test system configuration in the microwave anechoic chamber
通过终端显控系统、测试伺服系统设置天线测试参数,包括:测试探头扫描范围、扫描步进、扫描速率,射频探测系统工作频率、采样速率、测试波位、天线收/发状态选择等。Set antenna test parameters through terminal display and control system and test servo system, including: test probe scanning range, scanning step, scanning rate, RF detection system operating frequency, sampling rate, test wave position, antenna receiving/transmitting state selection, etc.
所述天线测试参数可根据不同天线的测试要求进行设置。测试人员可根据天线近场测量基本要求,通过终端显控系统软件对测试探头扫描范围、扫描步进、扫描速率等参数进行设置。The antenna test parameters can be set according to the test requirements of different antennas. Testers can set parameters such as the scanning range, scanning step, and scanning rate of the test probe through the terminal display and control system software according to the basic requirements of antenna near-field measurement.
步骤4、运行测试系统,完成待测子阵i近场平面幅度和相位数据录取;Step 4. Run the test system to complete the acquisition of near-field plane amplitude and phase data of the subarray i to be tested;
步骤5、计算天线子阵远场方向图fi Step 5. Calculate the far-field pattern f i of the antenna subarray
根据近场平面幅度和相位数据,采用近远场变换方法,计算子阵的远场方向图fi,i=1、2、…、n;According to the near-field plane amplitude and phase data, the near-far field transformation method is used to calculate the far-field pattern f i of the sub-array, i=1, 2, ..., n;
该步骤将获得的近场信息根据等效原理,通过近远场变换程序转换为远场方向图。In this step, the obtained near-field information is converted into a far-field pattern through a near-far field transformation program according to the equivalent principle.
步骤6、重复测试步骤2~6,完成所有子阵的近场幅度相位数据录取及远场方向图计算;Step 6. Repeat test steps 2 to 6 to complete the acquisition of near-field amplitude and phase data and calculation of far-field pattern for all subarrays;
步骤7、将每个子阵的远场方向图fi根据子阵相对位置关系进行矢量合成,计算得全阵面远场方向图。Step 7: Carry out vector synthesis of the far-field pattern fi of each sub-array according to the relative positional relationship of the sub-arrays, and calculate the far-field pattern of the whole array.
该步骤将每个子阵的远场方向图fi看作单元方向图。根据子阵的排布和划分,可参照如下公式对每个子阵的相位中心进行修正,最终将所有子阵的远场方向图进行远场矢量合成得到最终远场辐射方向图F。This step regards the far-field pattern fi of each subarray as the unit pattern. According to the arrangement and division of sub-arrays, the phase center of each sub-array can be corrected by referring to the following formula, and finally the far-field radiation pattern F of all sub-arrays is synthesized by far-field vector to obtain the final far-field radiation pattern F.
式中:F为大口径相控阵天线的最终方向图;In the formula: F is the final pattern of the large aperture phased array antenna;
fi为每个子阵的远场方向图,i=1、2、…、n;f i is the far field pattern of each sub-array, i=1, 2,..., n;
k为波数,k=2π/λ,λ为波长;k is the wave number, k=2π/λ, and λ is the wavelength;
u=sin(θ)cos(φ);u=sin(θ)cos(φ);
v=sin(θ)sin(φ);v=sin(θ)sin(φ);
xi,yi为第i个子阵在大口径相控阵天线中的相对位置。x i , y i are the relative positions of the ith sub-array in the large aperture phased array antenna.
例如:相控阵天线口径为方位向50米,距离向40米,若相控阵天线可分为4个子阵,每个子阵的大小为方位向25米,距离向20米。则x1=-25米,y1=20米。具体示例如图3所示。For example: the caliber of the phased array antenna is 50 meters in the azimuth direction and 40 meters in the distance direction. If the phased array antenna can be divided into 4 sub-arrays, the size of each sub-array is 25 meters in the azimuth direction and 20 meters in the distance direction. Then x 1 =-25 meters, y 1 =20 meters. A specific example is shown in Figure 3.
实施例二:Embodiment two:
本发明提供一种大口径相控阵天线分块测试系统,可适用于分块测试方法,请参照图2,该系统包括:终端显控系统、测试伺服系统、射频探测系统、天线安装定位系统。The present invention provides a large-diameter phased array antenna block test system, which can be applied to the block test method, please refer to Figure 2, the system includes: terminal display and control system, test servo system, radio frequency detection system, antenna installation and positioning system .
终端显控系统软件采用Qt开发环境搭建,负责协调完成待测天线、测试伺服系统、射频探测系统之间的状态配置和协同工作,包括:待测天线状态配置、伺服控制、射频系统状态配置、测试数据采集、测试数据存储、测试过程显示和测试结果处理等功能。天线状态配置包括天线工作频率、收发工作状态选择、测试波位;伺服控制包括测试探头扫描范围,扫描步进,扫描速率;射频系统状态配置包括射频系统工作频率、采样速率。终端显控系统通过COM、LAN、GPIB等标准通讯接口与测试伺服系统、射频探测系统互连,实现时钟同步、数据传输、数据存储等功能。The terminal display and control system software is built using the Qt development environment, and is responsible for coordinating and completing the state configuration and collaborative work among the antenna to be tested, the test servo system, and the radio frequency detection system, including: state configuration of the antenna to be tested, servo control, state configuration of the radio frequency system, Functions such as test data collection, test data storage, test process display and test result processing. Antenna status configuration includes antenna operating frequency, transceiver operating status selection, and test wave position; servo control includes test probe scanning range, scanning step, and scanning rate; RF system status configuration includes RF system operating frequency and sampling rate. The terminal display and control system is interconnected with the test servo system and radio frequency detection system through COM, LAN, GPIB and other standard communication interfaces to realize clock synchronization, data transmission, data storage and other functions.
测试伺服系统负责完成天线测试过程中测试设备的机械运动,包括平面近场扫描架和控制终端。平面近场扫描架包括待测天线安装平台、测试探头安装支架、探头运动导轨。待测天线安装平台和测试探头安装支架均预留了落空,可针对不同型号待测天线和探头进行适配安装。探头运动导轨具备水平和垂直两维运动能力,可根据用户需求,选择连续运动模式或步进走停模式。探头运动精度可实现0.01mm。控制终端软件采用VC++编写。可通过软件界面,对探头的运动轨迹进行设定,包括探头移动路径、移动速度、移动模式等等。The test servo system is responsible for completing the mechanical movement of the test equipment during the antenna test process, including the planar near-field scanning frame and the control terminal. The planar near-field scanning frame includes an antenna installation platform to be tested, a test probe installation bracket, and a probe movement guide rail. The installation platform of the antenna to be tested and the installation bracket of the test probe are reserved for the installation of different types of antennas and probes to be tested. The probe motion guide rail has horizontal and vertical two-dimensional motion capabilities, and can choose continuous motion mode or step stop mode according to user needs. Probe movement accuracy can be achieved 0.01mm. The control terminal software is written in VC++. The trajectory of the probe can be set through the software interface, including the probe moving path, moving speed, moving mode, etc.
射频探测系统负责完成测试天线数据的采集,包括:矢量网络分析仪、测试探头、测试互连电缆等。矢量网络分析仪和测试互连电缆接口为SMA。矢量网络分析仪1端口通过测试互连电缆与测试探头连接,2端口通过测试互连电缆与待测天线连接。为了适配不同型号天线的接口,测试互连电缆可采用专用转接器对SMA接头进行变换。通过终端显控系统,可对矢量网络分析仪的参数进行设置,如测试频率、测试电平等,矢量网络分析仪采集的射频信息通过LAN接口传输至终端显控系统存储。测试探头固定在测试伺服系统的扫描架上。随着扫描架的运动,测试探头可在指定位置对空间电场进行采样。The radio frequency detection system is responsible for completing the data collection of the test antenna, including: vector network analyzer, test probe, test interconnection cable, etc. The vector network analyzer and test interconnect cable interface is SMA. Port 1 of the vector network analyzer is connected to the test probe through a test interconnection cable, and port 2 is connected to the antenna under test through a test interconnection cable. In order to adapt to the interface of different types of antennas, the test interconnection cable can use a special adapter to transform the SMA connector. Through the terminal display and control system, the parameters of the vector network analyzer can be set, such as test frequency, test level, etc., and the radio frequency information collected by the vector network analyzer is transmitted to the terminal display and control system through the LAN interface for storage. The test probe is fixed on the scanning frame of the test servo system. With the movement of the scanning frame, the test probe can sample the space electric field at the specified position.
天线安装定位系统,负责完成待测天线的安装固定和位置校准,包括待测天线安装设备和光学定位设备。首先将待测天线安装到待测天线安装设备上。该设备预留有安装定位孔,可保证每个子阵安装位置的恒定。光学定位设备是为了保证每个子阵的测试相位中心恒定。在子阵方向图测试前,可将光学定位设备安装在扫描架上,通过发射激光点照射到待测天线上。移动扫描架,直至激光束照射到待测天线安装定位孔上,则该位置为测试探头的标准起始位置。将光学定位设备拆下,更换为测试探头即可开始测试。The antenna installation and positioning system is responsible for completing the installation, fixing and position calibration of the antenna under test, including the installation equipment of the antenna under test and the optical positioning equipment. First, install the antenna to be tested on the antenna installation device to be tested. The equipment is reserved with installation positioning holes, which can ensure the constant installation position of each sub-array. The optical positioning equipment is to ensure that the test phase center of each sub-array is constant. Before the sub-array pattern test, the optical positioning device can be installed on the scanning frame, and the laser spot can be irradiated on the antenna to be tested. Move the scanning frame until the laser beam is irradiated on the installation positioning hole of the antenna to be tested, then this position is the standard starting position of the test probe. Remove the optical positioning device and replace it with a test probe to start the test.
至此,已经结合附图对本发明大口径相控阵天线分块测试方法及测试系统进行了详细描述。依据以上描述,本领域技术人员应当对本发明有了清楚的认识。So far, the large-aperture phased array antenna block test method and test system of the present invention have been described in detail with reference to the accompanying drawings. Based on the above description, those skilled in the art should have a clear understanding of the present invention.
以上所述,仅为本发明最佳的具体实施方式,但本发明的保护范围并不局限于此,任何熟悉本技术领域的技术人员在本发明揭露的技术范围内,可轻易想到的变化或替换,都应涵盖在本发明的保护范围之内。The above description is only the best specific implementation mode of the present invention, but the scope of protection of the present invention is not limited thereto. Any person skilled in the art can easily conceive of changes or modifications within the technical scope disclosed in the present invention. Replacement should be covered within the protection scope of the present invention.
本发明说明书中未作详细描述的内容属于本领域专业技术人员的公知技术。The content that is not described in detail in the specification of the present invention belongs to the well-known technology of those skilled in the art.
Claims (10)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN202210938154.XA CN115542268A (en) | 2022-08-05 | 2022-08-05 | Large-aperture phased array antenna block testing method and system |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN202210938154.XA CN115542268A (en) | 2022-08-05 | 2022-08-05 | Large-aperture phased array antenna block testing method and system |
Publications (1)
Publication Number | Publication Date |
---|---|
CN115542268A true CN115542268A (en) | 2022-12-30 |
Family
ID=84724075
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN202210938154.XA Pending CN115542268A (en) | 2022-08-05 | 2022-08-05 | Large-aperture phased array antenna block testing method and system |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN115542268A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN117080759A (en) * | 2023-09-01 | 2023-11-17 | 中国电子科技集团公司第五十四研究所 | Large-scale ellipsoidal phased array antenna |
CN117289037A (en) * | 2023-11-23 | 2023-12-26 | 南京华成微波技术有限公司 | Method and system for testing plane near field of high-power phased array antenna |
Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN104833863A (en) * | 2015-05-21 | 2015-08-12 | 中国电子科技集团公司第三十八研究所 | Far-field dark room testing system and method for high-frequency phased-array antenna |
CN107340434A (en) * | 2017-05-16 | 2017-11-10 | 上海卫星工程研究所 | Satellite-borne synthetic aperture radar antenna direction picture capturing method based on internal calibration data |
CN111175583A (en) * | 2020-01-10 | 2020-05-19 | 中国电子科技集团公司第十四研究所 | High-speed high-precision desktop type small near-field tester |
CN111707877A (en) * | 2020-07-20 | 2020-09-25 | 广东圣大电子有限公司 | A radio frequency transmitter stray radiation test system and test method |
CN113281576A (en) * | 2021-05-20 | 2021-08-20 | 中国电子科技集团公司第十四研究所 | Antenna directional pattern testing method based on internal calibration multi-wave-position testing |
-
2022
- 2022-08-05 CN CN202210938154.XA patent/CN115542268A/en active Pending
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN104833863A (en) * | 2015-05-21 | 2015-08-12 | 中国电子科技集团公司第三十八研究所 | Far-field dark room testing system and method for high-frequency phased-array antenna |
CN107340434A (en) * | 2017-05-16 | 2017-11-10 | 上海卫星工程研究所 | Satellite-borne synthetic aperture radar antenna direction picture capturing method based on internal calibration data |
CN111175583A (en) * | 2020-01-10 | 2020-05-19 | 中国电子科技集团公司第十四研究所 | High-speed high-precision desktop type small near-field tester |
CN111707877A (en) * | 2020-07-20 | 2020-09-25 | 广东圣大电子有限公司 | A radio frequency transmitter stray radiation test system and test method |
CN113281576A (en) * | 2021-05-20 | 2021-08-20 | 中国电子科技集团公司第十四研究所 | Antenna directional pattern testing method based on internal calibration multi-wave-position testing |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN117080759A (en) * | 2023-09-01 | 2023-11-17 | 中国电子科技集团公司第五十四研究所 | Large-scale ellipsoidal phased array antenna |
CN117289037A (en) * | 2023-11-23 | 2023-12-26 | 南京华成微波技术有限公司 | Method and system for testing plane near field of high-power phased array antenna |
CN117289037B (en) * | 2023-11-23 | 2024-02-09 | 南京华成微波技术有限公司 | Method and system for testing plane near field of high-power phased array antenna |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CN113447730B (en) | Spherical antenna near-field calibration and scanning method, system and terminal | |
CN116047436A (en) | Near-field amplitude-phase calibration method, system and equipment for active phased array radar antenna | |
CN103064089B (en) | Method for calibrating satellite navigation digital multi-beam launching array antenna phase center | |
CN103616569A (en) | Method for correcting near-field test phases of millimeter wave plane | |
CN113252999B (en) | Antenna plane near field test method | |
CN113225147A (en) | Method, device and system for measuring total radiation power of array antenna | |
CN111965438A (en) | Multi-task antenna testing system, method and device based on mechanical arm | |
CN116208265B (en) | Calibration method, device and medium for active phased array antenna | |
CN111381112B (en) | Phase center far-field calibration method of satellite navigation array antenna | |
CN112505435B (en) | Equivalent far field testing device and method for large cylindrical phased array antenna | |
CN209841969U (en) | Compact range antenna test system | |
CN115542268A (en) | Large-aperture phased array antenna block testing method and system | |
CN107632210A (en) | A kind of Terahertz antenna plane near-field measurement system | |
CN109765437B (en) | System and method for calibrating simulated curved surface of full-space phased array antenna | |
CN112083234A (en) | Array antenna total radiation power measuring method, device and computer storage medium | |
CN112034264A (en) | Multi-probe compact range antenna test system and generation method | |
CN116520035A (en) | Two-dimensional pattern testing method adopting plane near-field rapid inversion method | |
CN113253000A (en) | Antenna field calibration system and method | |
CN117518207A (en) | Outfield test system and method for multi-beam phased array antenna | |
CN117092416A (en) | Testing system of active antenna | |
CN114994420A (en) | Phased Array Antenna Element Channel Phase Deflection Characteristics Test Method | |
CN210294411U (en) | A Terahertz Constricted Field Test System Based on Electronically Scanned Antenna | |
CN109975620A (en) | A kind of full airspace phased array is tested antenna rotary simulation calibration system and method | |
CN108761220A (en) | A kind of three-in-one test system in Terahertz antenna robot near field | |
CN113917241B (en) | Method, system, device and terminal for fast measurement and estimation of antenna pattern |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
PB01 | Publication | ||
PB01 | Publication | ||
SE01 | Entry into force of request for substantive examination | ||
SE01 | Entry into force of request for substantive examination |