WO2009039693A1 - Testing method of the ota performances of a wireless communication product - Google Patents
Testing method of the ota performances of a wireless communication product Download PDFInfo
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- WO2009039693A1 WO2009039693A1 PCT/CN2007/003632 CN2007003632W WO2009039693A1 WO 2009039693 A1 WO2009039693 A1 WO 2009039693A1 CN 2007003632 W CN2007003632 W CN 2007003632W WO 2009039693 A1 WO2009039693 A1 WO 2009039693A1
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- H—ELECTRICITY
- H04—ELECTRIC COMMUNICATION TECHNIQUE
- H04B—TRANSMISSION
- H04B17/00—Monitoring; Testing
- H04B17/10—Monitoring; Testing of transmitters
- H04B17/15—Performance testing
- H04B17/16—Test equipment located at the transmitter
Definitions
- the present invention relates to the field of radio frequency test techniques for wireless communication products, and in particular to a method for testing spatial radio frequency performance of a wireless communication product (Over The Air, OTA).
- TRP Total Radiated Power
- TIS Total Isotropic Sensitivity
- the test standard for mobile terminal space RF performance is defined as "The test plan for mobile station OTA performance".
- the radio frequency performance of the mobile terminal space shall be tested in accordance with the requirements of the CTIA standard, and the TRP and TIS shall meet certain limit requirements.
- the measurement of TRP and TIS is performed on the spherical surface centered on the device under test. In order to accurately evaluate the transmitting and receiving performance of the device under test, it is necessary to select enough test points.
- the wireless communication product is placed on a first rotating shaft or a second rotating shaft of a testing device, the first rotating shaft rotating range is 0-180 degrees, and the second rotating shaft rotating range is 0-360 degrees. 15 degrees ⁇ (0-180 degrees) and ⁇ (0-360 degrees) take a test point, a total of 264 points need to be tested. TIS test needs to be every 30 degrees 0 (0-180 degrees) and ⁇ (0-360 degrees) Take a test point and test a total of 60 points. Since the test points are equally selected, they are non-uniformly distributed on the spherical surface. TRP, TIS need to calculate the ball area according to all test points.
- the test speed of RF performance depends largely on the number of test points, so too many test points will cause the test time to be too long.
- the calculation of TRP and TIS requires 4 spheres to be processed, and the calculation process is complicated.
- the two points on the spherical surface with angles of 0 degrees and 180 degrees are 0 in the calculation and do not work in the TRP or TIS calculation.
- a spatial RF performance testing method includes: "Spherical coordinate system establishing step, and establishing the spherical coordinate defined by the x, y, and z axes with the measured wireless communication product as the coordinate origin. ⁇ The angle is the angle between the i-type point and the positive direction of the z-axis.
- test path planning step test path planning is required to increase the difficulty of mechanical implementation. Rotate the first rotation axis and the second rotation axis of the test device, per The angle of the corner corresponding to a test point is tested in a certain order. The points with the same angle are tested according to the ⁇ size in a certain order.
- the data processing step is to linearly average the data measured at each test point to obtain the required TRP.
- TIS value the formula is as follows: N ⁇ 8 ⁇ ( ⁇ ⁇ where ⁇ is the number of measurement points obtained by triangulating L times, ⁇ is L times triangulation to obtain the number of test points with different ⁇ values, m is the same as the angle of the triangle obtained by triangulation of L times but ⁇ The number of test points with different angles.
- EiRP g ( , is the equivalent omnidirectional radiated power horizontal polarization component value of the test point at angle ⁇ >, , , in milliwatts.
- the equivalent omnidirectional radiated power of the test point is the value of the vertical polarization component' in milliwatts.
- EIS e ( ⁇ ⁇ ⁇ ) is the equivalent omnidirectional received power horizontal polarization component of the test point at an angle of / , in milliwatts.
- EIS e is the value of the equivalent omnidirectional received power vertical polarization component of the test point of angle ⁇ , ⁇ ., in milliwatts.
- the test system in the test step, is not increased in mechanical complexity, and the first rotation axis and the second rotation axis of the rotation test device measure each test point. For test points with equal corners, the test points are measured in the order of ⁇ angles. 3 ⁇ 4.
- the distribution of the test points on the sphere can be made as uniform as possible, which can meet the requirements of test accuracy. In this case, the number of test points is reduced, thereby saving test time, while simplifying the test result processing algorithm, and the test results at 0 and 180 degrees are meaningful for the evaluation of spatial performance.
- Other features and advantages of the present invention are possible for the evaluation of spatial performance.
- FIG. 1 is a flow chart of a method for testing a spatial RF performance according to an embodiment of the present invention
- FIG. 2 is a spherical coordinate system established with an origin of a wireless communication product under test
- FIG. 3 is a two rotation axis of the test device
- FIG. 4 is a schematic diagram of a normal icosahedral spherical surface treatment on a spherical surface according to an embodiment of the present invention
- FIG. 5 is a schematic diagram of a regular icosahedral spherical surface triangulation
- FIG. 6 is a three-dimensional triangulation using a regular icosahedron
- the obtained test point distribution map
- FIG. 7 is a test point distribution diagram obtained by performing two times of triangulation using a regular icosahedron
- FIG. 8A is a schematic diagram of a test apparatus according to an embodiment of the present invention
- FIG. 8B is a schematic diagram of a test apparatus according to an embodiment of the present invention
- FIG. 9 is a test point test path diagram obtained by using a regular icosahedron for three times of triangulation
- Fig. 10 is a test point test path diagram obtained by using a regular icosahedron for two times of triangulation
- a list of angular distributions of test points is planned twice in accordance with an embodiment of the present invention.
- Figure 12 is a list of angular distributions of planned test points for three times in accordance with an embodiment of the present invention.
- DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENT(S) The following is a description of the preferred embodiments of the present invention, Firstly, a spatial RF performance measurement method for a wireless communication product is provided. As shown in FIG.
- the method may generally include the following processes: a spherical coordinate system establishing step (S102), and a test point selecting step (S104) ), test step (S106), and data processing steps (S108). Each processing step will be further described in detail below.
- the spherical coordinate system defined by the x, y, and z axes is established with the measured wireless communication products as the origin.
- the ⁇ angle is the angle between the test point and the positive direction of the z-axis.
- the ⁇ angle is the angle between the positive X-axis and the projection point of the test point on the x and y planes. See Figure 2.
- the measured wireless communication product is placed on a first rotating shaft or a second rotating shaft of a testing device, and the corresponding relationship between the two rotating shafts of the testing device and the space spherical coordinates is shown in Fig. 3;
- Test point selection Use the normal N-facet to triangulate the entire sphere to obtain the test of the uniform hook on the spherical surface.
- the so-called triangulation means that the unit sphere is first divided into a regular tetrahedron, a regular octahedron, a regular dodecahedron, or a regular icosahedron. Each surface corresponds to a spherical triangle, and then the midpoint of the three sides of the spherical triangle is connected. A spherical triangle is divided into four spherical triangles, and the vertices of the triangular mesh are taken as test points. So recursively divide until the number of triangles required is the number of test points. The vertices of these triangles are distributed as evenly as possible over the entire sphere.
- test points are evenly distributed on the sphere, the number of test points required for TRP and TIS tests can be greatly reduced, thus reducing test time. For example, on the spherical surface as shown in Figure 2, select the test point by the following process: First, positive
- the icosahedron triangulates the entire sphere, and the purpose of the spherical triangulation is to evenly distribute the test points on the sphere.
- the unit sphere may be first divided into a regular tetrahedron or a regular octahedron, or a regular dodecahedron, a regular hexahedron or an icosahedron.
- the description is shown in Fig. 4 and Fig. 5.
- Fig. 4 the description is shown in Fig. 4 and Fig. 5.
- 1 and 12 are spherical vertices, 2-11 are respectively two regular pentagon vertices, and points 2 to X are respectively
- the positive angle is 26.565 degrees; in Figure 5, the triangles 1-2-3 are respectively triangle 4 1 1 -4-6, 4-2-5, 6-5-3, 4-5-6
- class 4 is divided to obtain the required number of measurement points, and the test points are selected at the vertices of each spherical triangle.
- 1 is the test point
- 2 is the triangle after triangulation.
- Each face corresponds to a spherical triangle, and then connects the midpoint of the three sides of the spherical triangle.
- Each of the spherical triangles is divided into four spherical triangles, so recursively divided until the required number of triangles is reached.
- Test points are selected at the vertices of each spherical triangle.
- Figure 6 shows the distribution of test points obtained by performing triangulation three times. 162 test points can be obtained. These test points are distributed as evenly as possible on the spherical surface with the device under test as the midpoint. The measurement of the point can accurately give the same TRP value as the method on CTIA. It can accurately evaluate the spatial RF performance TRP of the device under test, but the test point is reduced from 264 points specified by the CTIA standard to 162 points, thus reducing the measurement time by about 38%.
- the receiving performance of the test equipment can be fully evaluated.
- the measured result is the same as the TIS result obtained by the CTIA test method, and every 30 times specified by the CTIA.
- the degree angle test reduces the number of points by 18 points, which reduces the measurement time by 30%.
- the integral processing of the test results in the CTIA standard is avoided, and only the measurement results are linearly averaged, which simplifies the test result processing algorithm, thereby saving the result processing time. Since the results of the previous processing of the test are used, the measurement results for ⁇ equal to 0 and 180 degrees cannot be covered in the evaluation of the entire test result, but this is avoided by linear averaging.
- Fig. 8A is a test device
- 1 is a first rotating shaft
- the shaft rotation range is 0-180 degrees
- 2 is a second rotating shaft
- the rotation range is 0- 360 degrees
- 3 is the measuring antenna.
- Fig. 8B is another test device, 1 is a first rotating shaft, the shaft rotation range is 0-180 degrees
- 2 is a second rotating shaft
- the rotation range is 0-360 degrees.
- 3 is the measuring antenna.
- each test point is measured by sequentially rotating the test device rotation axis ⁇ axis ⁇ axis. After obtaining the test points on the spherical surface, the path planning of the test is required.
- the spatial RF performance indicators TRP and TIS of mobile terminal equipment or other wireless communication products can be obtained by linearly averaging the data measured at each test point. It does not require complicated integration operations, which simplifies the calculation method. Through the invention, the distribution of the test points on the space on the spherical surface can be made as uniform as possible, and the number of test points can be reduced under the condition of satisfying the test accuracy and the accuracy requirement, thereby saving test time.
- the above description is only the preferred embodiment of the present invention, and is not intended to limit the present invention, and various modifications and changes can be made to the present invention. Any modifications, equivalent substitutions, improvements, etc. made within the scope of the present invention are intended to be included within the scope of the present invention.
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Abstract
The present invention discloses a testing method of the OTA performances. The method includes following approaches: the step of setting up a spherical coordinate system, the step of selecting the testing points, the step of testing, and the step of dealing with the data. By using the present invention, OTA testing points can be distributed on the spherical surface equably, and the number of testing points is reduced while satisfying the testing precision, so as to save the testing time and simplify the disposal arithmetic of the testing results.
Description
无线通信产品空间射频性能测试方法 技术领域 本发明涉及无线通信产品的射频测试支术领域, 具体地, 涉及无线通信 产品 (Over The Air, OTA ) 的空间射频性能测试方法。 背景技术 随着现代工业的发展,各类无线通讯产品只有具备良好的发射和接收性 能才能保证通讯质量, 即, 总辐射功率 (Total Radiated Power, 下文中简称 为 TRP )要高于一定值, 全向接收灵敏度 ( Total Isotropic Sensitivity , TIS ) 要^ ί氐于一定值, 也就是空间射频性能 (Over The Air, 下文中简称为 OTA ) 测试指标要良好。 TECHNICAL FIELD The present invention relates to the field of radio frequency test techniques for wireless communication products, and in particular to a method for testing spatial radio frequency performance of a wireless communication product (Over The Air, OTA). BACKGROUND With the development of modern industry, all kinds of wireless communication products can only guarantee communication quality if they have good transmitting and receiving performance, that is, Total Radiated Power (hereinafter referred to as TRP) is higher than a certain value, The Total Isotropic Sensitivity (TIS) is required to be a certain value, that is, the spatial RF performance (Over The Air, hereinafter referred to as OTA).
CTIA (蜂窝通讯标准化协会) 为了保障移动终端设备在网络中正常使 用, 制定了移动终端空间射频性能的测试标准即 《The test plan for mobile station OTA performance)), 目前, 很多运营商都要求进入其网络的移动终端 空间射频性能要按照 CTIA标准要求进行测试, TRP、 TIS要满足一定的限值 要求。 在 CTIA标准中, 对于 TRP和 TIS的测量是在以被测设备为圓心的球 面上进 ^"取点测试。 为了准确评价被测设备的发射和接收性能, 需要选取足 够多的测试点。 被测无线通信产品放置于一测试装置的第一旋转轴或第二旋 转轴上, 第一旋转轴旋转范围为 0-180度, 第二旋转轴旋转范围为 0-360度。 其中 TRP测试需要每隔 15度 Θ ( 0-180度)和 Φ ( 0-360度)取一个测试点, 总共需要测试 264个点。 TIS测试需每隔 30度 Θ ( 0-180度)和 Φ ( 0-360度) 取一个测试点, 共需测试 60 个点。 由于测试点是等 度选取的 所以其在 球面上是非均匀分布的。 TRP、 TIS 需要 ·据所有的测试点进行球面积分计 算得出。 在积分运算中, 对位于 θ=0, θ=180的两个测试点, 其正弦值为零, 所以这两个点不进行测试。 随着信息技术的发展, 无线通信产品的空间性能测试越来越多, 同时也 越来越复杂, 测试所占用的时间是制约空间射频性能测试测试速度的一个瓶 颈, 随着多频段无线通信产品的增加, 完成其空间射频性能评估的时间也越
长, 目前, 对于现有的使用等角度进行球面取点测试方法, 测试点在球面命 -: 布不均匀, 为了能更加准确地评估 EUT ( Equipment Under Test, 被测设备) ' 的空间射频性能,需测量足够多的点, TRP测试 264个点, TIS测试 60个点。 射频性能的测试速度很大程度上取决于测试点的个数, 因此测试点过多会造 成测试时间过长。 另外, 在测试结果的处理上由于测试点在球面上非均匀分 布, 计算 TRP和 TIS时需要 4吏用球面积分进行处理, 计算过程比较复杂。 再 者, 这样球面上 Θ角为 0度和 180度的两个点在计算中为 0, 在 TRP或 TIS 计算中不起作用。 鉴于上述内容,如果能够提供一种既能够节省测试时间又可以简化测试 后的计算方法, 同时对于 Θ等于 0度和 180度时测试结果有意义的空间射频 性能测试方法无疑是理想的。 发明内容 考虑到相关技术中存在的上述问题而提出本发明, 为此, 本发明旨在提 供一种用于无线通信产品的空间射频性能测试方案。 根据本发明, 提供了一种空间射频性能测试方法。 该方法包 ^": 球面坐标系建立步骤, 以被测无线通讯产品为坐标原点建 立由 x、 y、 z轴所定义的球面坐标。 Θ 角为测 i式点与 z轴正方向的夹角, φ 角为 X轴正向与测试点在 x、 y平面上的投影点的夹角; 测试点选取步骤, 使用正 N 面体对整个球面进行三角化来获得尽可能 均匀分布在球面上的测试点; 其中正 N面体的一个顶点位于 θ=0度点处。 测 试路径规划步骤, 为不增加机械实现难度需进行测试路径规划。 旋转测试装 置的第一旋转轴和第二旋转轴, 按照每一测试点所对应的 Θ角大小按照一定 顺序进行测试, 对于 Θ角相等的点依据 φ大小按照一定顺序进行测试; 数据 处理步骤, 将在各个测试点所测量的数据进行线性平均得到需要的 TRP 及 TIS值, 公式如下:
N
ΕΙ8φ(θ φ 其中, Ν,为进行 L次三角化得到的测量点个数 ,η为 L次三角化得到 Θ 值不同的测试点个数, m为 L次三角化得到的 Θ角相同但 φ角不同的测试点 个数。 CTIA (Cellular Communication Standardization Association) In order to ensure the normal use of mobile terminal equipment in the network, the test standard for mobile terminal space RF performance is defined as "The test plan for mobile station OTA performance". Currently, many operators require access to their networks. The radio frequency performance of the mobile terminal space shall be tested in accordance with the requirements of the CTIA standard, and the TRP and TIS shall meet certain limit requirements. In the CTIA standard, the measurement of TRP and TIS is performed on the spherical surface centered on the device under test. In order to accurately evaluate the transmitting and receiving performance of the device under test, it is necessary to select enough test points. The wireless communication product is placed on a first rotating shaft or a second rotating shaft of a testing device, the first rotating shaft rotating range is 0-180 degrees, and the second rotating shaft rotating range is 0-360 degrees. 15 degrees Θ (0-180 degrees) and Φ (0-360 degrees) take a test point, a total of 264 points need to be tested. TIS test needs to be every 30 degrees 0 (0-180 degrees) and Φ (0-360 degrees) Take a test point and test a total of 60 points. Since the test points are equally selected, they are non-uniformly distributed on the spherical surface. TRP, TIS need to calculate the ball area according to all test points. In the operation, for two test points located at θ=0, θ=180, the sine value is zero, so these two points are not tested. With the development of information technology, the space performance test of wireless communication products is more and more More and more complex, testing The occupied time is a bottleneck that restricts the test speed of the space RF performance test. With the increase of multi-band wireless communication products, the time to complete the evaluation of the spatial RF performance is also higher. Long, at present, for the existing spherical angle test method, the test point is in the spherical life -: uneven cloth, in order to more accurately evaluate the spatial RF performance of the EUT (Equipment Under Test) Need to measure enough points, TRP test 264 points, TIS test 60 points. The test speed of RF performance depends largely on the number of test points, so too many test points will cause the test time to be too long. In addition, in the processing of the test results, because the test points are non-uniformly distributed on the spherical surface, the calculation of TRP and TIS requires 4 spheres to be processed, and the calculation process is complicated. Furthermore, the two points on the spherical surface with angles of 0 degrees and 180 degrees are 0 in the calculation and do not work in the TRP or TIS calculation. In view of the above, if a calculation method capable of saving test time and simplifying the test can be provided, it is undoubtedly ideal for a spatial RF performance test method which is meaningful for the test results when Θ is equal to 0 degrees and 180 degrees. SUMMARY OF THE INVENTION The present invention has been made in view of the above problems in the related art, and an object of the present invention is to provide a spatial radio frequency performance testing scheme for a wireless communication product. According to the present invention, a spatial RF performance testing method is provided. The method includes: "Spherical coordinate system establishing step, and establishing the spherical coordinate defined by the x, y, and z axes with the measured wireless communication product as the coordinate origin. Θ The angle is the angle between the i-type point and the positive direction of the z-axis. , φ angle is the angle between the positive X-axis and the projection point of the test point on the x and y planes; the test point selection step, using the normal N-plane to triangulate the entire sphere to obtain the test as evenly distributed as possible on the sphere Point; where a vertex of the positive N-face is located at θ = 0 degrees. In the test path planning step, test path planning is required to increase the difficulty of mechanical implementation. Rotate the first rotation axis and the second rotation axis of the test device, per The angle of the corner corresponding to a test point is tested in a certain order. The points with the same angle are tested according to the φ size in a certain order. The data processing step is to linearly average the data measured at each test point to obtain the required TRP. And the TIS value, the formula is as follows: N ΕΙ8φ(θ φ where Ν is the number of measurement points obtained by triangulating L times, η is L times triangulation to obtain the number of test points with different Θ values, m is the same as the angle of the triangle obtained by triangulation of L times but φ The number of test points with different angles.
EiRPg ( , 为角度为 έ>, , ,的测试点的等效全向辐射功率水平极化分量 值, 单位为毫瓦。 EiRP g ( , is the equivalent omnidirectional radiated power horizontal polarization component value of the test point at angle έ>, , , in milliwatts.
)为角度为 , ^的测试点的等效全向辐射功率垂直极化分量 值' 单位为毫瓦。 ) For the angle of , the equivalent omnidirectional radiated power of the test point is the value of the vertical polarization component' in milliwatts.
EISe (θ φΊ )为角度为 , /的测试点的等效全向接收功率水平极化分量 值, 单位为毫瓦。 EIS e (θ φ Ί ) is the equivalent omnidirectional received power horizontal polarization component of the test point at an angle of / , in milliwatts.
EISe 为角度为 Θ,, φ.的测试点的等效全向接收功率垂直极化分量 值, 单位为毫瓦。 在上述方法中, 在测试步骤中, 不增加测试系统机械复杂度, 旋转测试 装置的第一旋转轴和第二旋转轴测量各测试点。 对于 Θ角相等的测试点, 按 照 φ角大小顺序对各测试点进 4亍测 "¾。 通过本发明, 可以使得空间的测试点在球面上的分布尽量均勾, 能够在 满足测试精度要求的情况下减少测试点数, 从而节省测试时间, 同时简化了 测试结果处理算法, 以及在 Θ角为 0度和 180度时的测试结果对于空间性能 的评估是有意义的。 本发明的其它特征和优点将在随后的说明书中阐述, 并且, 部分地从说 明书中变得显而易见, 或者通过实施本发明而了解。 本发明的目的和其他优 点可通过在所写的说明书、 权利要求书、 以及附图中所特别指出的结构来实 现和获得。
附图说明 附图用来提供对本发明的进一步理解, 并且构成说明书的一部分, 与本 发明的实施例一起用于解释本发明, 并不构成对本发明的限制。 在附图中: 图 1是 居本发明实施例的空间射频性能测试方法的流程图; 图 2是以被测无线通讯产品为原点建立的球面坐标系; 图 3是测试装置两个旋转轴与空间球坐标对应关系图; 图 4是根据本发明实施例的在球面上进行正 20面体球面处理的示意图; 图 5是正 20面体球面三角化示意图; 图 6是使用正 20面体进行 3次三角化得到的测试点分布图; 图 7是使用正 20面体进行 2次三角化得到的测试点分布图; 图 8A是根据本发明实施例的一种测试装置示意图; 图 8B是根据本发明实施例的另一种测试装置示意图; 图 9是使用正 20面体进行 3次三角化得到的测试点测试路径图; 图 10是使用正 20面体进行 2次三角化得到的测试点测试路径图; 图 11是根据本发明实施例 2次规划测试点的角度分布列表。 图 12是根据本发明实施例 3次规划测试点的角度分布列表。 具体实施方式 以下结合附图对本发明的优选实施例进^"说明, 应当理解, 此处所描述 的优选实施例仅用于说明和解释本发明, 并不用于限定本发明。 根据本发明实施例,首先提供了一种用于无线通信产品的空间射频性能 测 i式方法。 如图 1所示, 该方法大致可以包括以下几项处理: 球面坐标系建立步骤 ( S102 ), 测试点选取步骤 (S104 ), 测试步骤 (S106 ), 以及数据处理步骤
( S108 )。 以下将进一步对各处理步骤进 4于详细描述。 EIS e is the value of the equivalent omnidirectional received power vertical polarization component of the test point of angle Θ, φ., in milliwatts. In the above method, in the test step, the test system is not increased in mechanical complexity, and the first rotation axis and the second rotation axis of the rotation test device measure each test point. For test points with equal corners, the test points are measured in the order of φ angles. 3⁄4. By the invention, the distribution of the test points on the sphere can be made as uniform as possible, which can meet the requirements of test accuracy. In this case, the number of test points is reduced, thereby saving test time, while simplifying the test result processing algorithm, and the test results at 0 and 180 degrees are meaningful for the evaluation of spatial performance. Other features and advantages of the present invention. BRIEF DESCRIPTION OF THE DRAWINGS The invention will be apparent from the description, or will be apparent from the <RTIgt; The structure specifically indicated is implemented and obtained. The drawings are intended to provide a further understanding of the invention, and are intended to be a part of the description of the invention. In the drawings: FIG. 1 is a flow chart of a method for testing a spatial RF performance according to an embodiment of the present invention; FIG. 2 is a spherical coordinate system established with an origin of a wireless communication product under test; FIG. 3 is a two rotation axis of the test device; FIG. 4 is a schematic diagram of a normal icosahedral spherical surface treatment on a spherical surface according to an embodiment of the present invention; FIG. 5 is a schematic diagram of a regular icosahedral spherical surface triangulation; FIG. 6 is a three-dimensional triangulation using a regular icosahedron; The obtained test point distribution map; FIG. 7 is a test point distribution diagram obtained by performing two times of triangulation using a regular icosahedron; FIG. 8A is a schematic diagram of a test apparatus according to an embodiment of the present invention; FIG. 8B is a schematic diagram of a test apparatus according to an embodiment of the present invention; Another test device schematic diagram; Fig. 9 is a test point test path diagram obtained by using a regular icosahedron for three times of triangulation; Fig. 10 is a test point test path diagram obtained by using a regular icosahedron for two times of triangulation; A list of angular distributions of test points is planned twice in accordance with an embodiment of the present invention. Figure 12 is a list of angular distributions of planned test points for three times in accordance with an embodiment of the present invention. DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENT(S) The following is a description of the preferred embodiments of the present invention, Firstly, a spatial RF performance measurement method for a wireless communication product is provided. As shown in FIG. 1, the method may generally include the following processes: a spherical coordinate system establishing step (S102), and a test point selecting step (S104) ), test step (S106), and data processing steps (S108). Each processing step will be further described in detail below.
(一 ) 球面坐标系建立 对于无线通信产品空间射频性能测试,以被测无线通信产品为原点建立 由 x、 y、 z轴所定义的球面坐标系。 Θ 角为测试点与 z轴正方向的夹角, φ 角为 X轴正向与测试点在 x、 y平面上的投影点的夹角, 参见图 2。 被测无线 通信产品放置于一测试装置的第一旋转轴或第二旋转轴上, 测试装置两个旋 转轴与空间球坐标对应关系见图 3; (I) Spherical coordinate system establishment For the wireless RF performance test of wireless communication products, the spherical coordinate system defined by the x, y, and z axes is established with the measured wireless communication products as the origin. The Θ angle is the angle between the test point and the positive direction of the z-axis. The φ angle is the angle between the positive X-axis and the projection point of the test point on the x and y planes. See Figure 2. The measured wireless communication product is placed on a first rotating shaft or a second rotating shaft of a testing device, and the corresponding relationship between the two rotating shafts of the testing device and the space spherical coordinates is shown in Fig. 3;
(二) 测试点选取 使用正 N 面体对整个球面进行三角化来获得均勾分布在球面上的测试 (II) Test point selection Use the normal N-facet to triangulate the entire sphere to obtain the test of the uniform hook on the spherical surface.
所谓三角化, 是指先将单位球面划分为正四面体、 正八面体、 正十二面 体、 或者正二十面体, 每一个面对应一个球面三角形, 然后连接球面三角形 三条边的中点, 把每一个球面三角形划分为四个球面三角形, 取三角网格的 顶点为测试点。 如此递归划分直到达到需要的三角形个数即测试点个数。 这 些三角形的顶点尽可能均匀的分布在整个球面上。 所以只要获得足够的测试 点数就可以评估移动终端或者其他的无线设备的空间射频性能总发射功率 ( TRP )、 全向接收灵敏度( TIS )。 因为测试点均匀分布在球面上, 所以可以 大大较少 TRP、 TIS测试需要的测试点数, 从而减少测试时间。 例如, 在如图 2 所示的球面上, 通过如下处理选取测式点: 首先以正The so-called triangulation means that the unit sphere is first divided into a regular tetrahedron, a regular octahedron, a regular dodecahedron, or a regular icosahedron. Each surface corresponds to a spherical triangle, and then the midpoint of the three sides of the spherical triangle is connected. A spherical triangle is divided into four spherical triangles, and the vertices of the triangular mesh are taken as test points. So recursively divide until the number of triangles required is the number of test points. The vertices of these triangles are distributed as evenly as possible over the entire sphere. Therefore, as long as sufficient test points are obtained, the spatial RF performance total transmit power (TRP) and omnidirectional receive sensitivity (TIS) of the mobile terminal or other wireless devices can be evaluated. Because the test points are evenly distributed on the sphere, the number of test points required for TRP and TIS tests can be greatly reduced, thus reducing test time. For example, on the spherical surface as shown in Figure 2, select the test point by the following process: First, positive
20面体对整个球面进行三角化,球面三角化的目的是使测试点均匀分布在球 面上。将球面均匀三角化时, 可以先将单位球面划分为正四面体或正八面体, 也可以是正十二面体、 正十六面体或者正二十面体。 此处以正 20 面体为例 进 ^"说明, 图 4、 图 5所示, 在图 4中, 1、 12为球面两顶点, 2-11 分别 两个正五边形顶点, 点 2到 X轴正向的角度为 26.565度; 在图 5中, 三角形 1-2-3 分别被三角 4匕为 1 -4-6、 4-2-5、 6-5-3、 4-5-6 四个三角形, 依次类 4体进 行划分得到需要的测量点数, 测试点选在各个球面三角形 顶点。在图 6中, 1是测试点, 2是三角化后的三角形。
每一个面对应一个球面三角形, 然后连接球面三角形三条边的中点, 4巴 每一个球面三角形划分为四个球面三角形, 如此递归划分直到达到需要的三 角形个数。 测试点选在各个球面三角形的顶点。 图 6所示是进行 3次三角化 得到的测试点的分布, 可以得到 162个测试点, 这些测试点尽可能均匀地分 布在以被测设备为中点的球面上, 经过 TRP测试证明, 这些点的测量能够准 确给出与 CTIA上的方法同样的 TRP值。 能够准确地评价被测设备的空间射 频性能 TRP, 但是测试点却由 CTIA标准规定的 264个点减少到 162个点, 这样, 测量时间就减少约 38%。 对于 TIS测试只需要进行 2次三角化, 测量 42个点,如图 7所示, 可以完全评估测试设备的接收性能,测量结果与 CTIA 的测试方法得到的 TIS结果相同,与 CTIA规定的每 30度角测试一个点相比 减少了 18 个点, 这样测量时间减少了 30%。 同时由于测试点均匀分布在球 面上, 所以避免了 CTIA标准中的测试结果的积分处理, 只需要对测量结果 进行线性平均, 这样简化了测试结果处理算法,从而也节省了结果处理时间。 由于以前采用积分处理测试结果, 因此对于 Θ等于 0度和 180度点的测量结 果不能涵盖在整个测试结果评估中, 但是采用线性平均就避免了这一点。 The icosahedron triangulates the entire sphere, and the purpose of the spherical triangulation is to evenly distribute the test points on the sphere. When the sphere is evenly triangulated, the unit sphere may be first divided into a regular tetrahedron or a regular octahedron, or a regular dodecahedron, a regular hexahedron or an icosahedron. Here, taking the regular 20-faced body as an example, the description is shown in Fig. 4 and Fig. 5. In Fig. 4, 1 and 12 are spherical vertices, 2-11 are respectively two regular pentagon vertices, and points 2 to X are respectively The positive angle is 26.565 degrees; in Figure 5, the triangles 1-2-3 are respectively triangle 4 1 1 -4-6, 4-2-5, 6-5-3, 4-5-6 The triangle, in turn, class 4 is divided to obtain the required number of measurement points, and the test points are selected at the vertices of each spherical triangle. In Fig. 6, 1 is the test point, and 2 is the triangle after triangulation. Each face corresponds to a spherical triangle, and then connects the midpoint of the three sides of the spherical triangle. Each of the spherical triangles is divided into four spherical triangles, so recursively divided until the required number of triangles is reached. Test points are selected at the vertices of each spherical triangle. Figure 6 shows the distribution of test points obtained by performing triangulation three times. 162 test points can be obtained. These test points are distributed as evenly as possible on the spherical surface with the device under test as the midpoint. The measurement of the point can accurately give the same TRP value as the method on CTIA. It can accurately evaluate the spatial RF performance TRP of the device under test, but the test point is reduced from 264 points specified by the CTIA standard to 162 points, thus reducing the measurement time by about 38%. For the TIS test, only two rounds of triangulation are required, and 42 points are measured. As shown in Fig. 7, the receiving performance of the test equipment can be fully evaluated. The measured result is the same as the TIS result obtained by the CTIA test method, and every 30 times specified by the CTIA. The degree angle test reduces the number of points by 18 points, which reduces the measurement time by 30%. At the same time, since the test points are evenly distributed on the spherical surface, the integral processing of the test results in the CTIA standard is avoided, and only the measurement results are linearly averaged, which simplifies the test result processing algorithm, thereby saving the result processing time. Since the results of the previous processing of the test are used, the measurement results for Θ equal to 0 and 180 degrees cannot be covered in the evaluation of the entire test result, but this is avoided by linear averaging.
(三) 测试步 4¾ 参见图 8A和 8B所示, 图 8A为一种测试装置, 1为第一旋转轴, 轴旋 转范围为 0-180度, 2为第二旋转轴, 旋转范围为 0-360度, 3为测量天线。 图 8B为另一种测试装置, 1为第一旋转轴, 轴旋转范围为 0-180度, 2为第 二旋转轴, 旋转范围为 0-360度。 3 为测量天线。 为不增加测试装置机械难 度, 依次旋转测试装置旋转轴 Θ轴 Φ轴测量各测试点。 取得了球面上的测试点以后, 就需要进行测试的路径规划, 经过对测试 点所对应的角度值进行分析, 在同一 Θ角上对应了几个 φ角不等的点。 越是 接近大圓, 需要测量的点数越多, 在两极附近需要的测试点减少, 这样避免 了 CTIA标准中的等角度测试方法在任何一个高度角 Θ上都需要测量等数量 的点。 为此, 按照测试点的 Θ ( 0-180 )的大小顺序依次测试每个角 Θ所对应的 平面上的对应于不同 φ ( 0-360 ) 的测试点; 对于 Θ角相等的测试点, 按照 φ 的大小顺序对各测试点进行测试。其中,图 9示出了 TRP测试点及路径规划, 图 10 示出了 TIS 测试点及路径规划。 首先将测试装置的两个轴都旋转到 0 度, 使被测设备的状态达到测试要求。 从 θ=0度的点开始测试, 测试完成后
旋转测试装置的第一旋转轴使 Θ角到下一个角度, 在此角度上对应着几个 φ 值不同的角, 旋转测试装置的第二旋转轴, 依次测试这些点, 以此类推测试 完成所有的点。 2次划分和 3次划分的测试点如图 11和图 12所示。 (3) Test step 43⁄4 Referring to Figs. 8A and 8B, Fig. 8A is a test device, 1 is a first rotating shaft, the shaft rotation range is 0-180 degrees, 2 is a second rotating shaft, and the rotation range is 0- 360 degrees, 3 is the measuring antenna. Fig. 8B is another test device, 1 is a first rotating shaft, the shaft rotation range is 0-180 degrees, 2 is a second rotating shaft, and the rotation range is 0-360 degrees. 3 is the measuring antenna. In order not to increase the mechanical difficulty of the test device, each test point is measured by sequentially rotating the test device rotation axis Θ axis Φ axis. After obtaining the test points on the spherical surface, the path planning of the test is required. After analyzing the angle values corresponding to the test points, a number of points with different φ angles are corresponding on the same corner. The closer to the big circle, the more points that need to be measured, and the fewer test points required near the poles, thus avoiding the equal angle test method in the CTIA standard that needs to measure the same number of points on any one of the height angles. To do this, test the test points corresponding to different φ ( 0-360 ) on the plane corresponding to each corner according to the order of the Θ ( 0-180 ) of the test points; Each test point is tested in the order of magnitude of φ. Among them, Figure 9 shows the TRP test points and path planning, and Figure 10 shows the TIS test points and path planning. First, rotate both axes of the test device to 0 degrees to make the state of the device under test meet the test requirements. Start the test from the point of θ = 0 degrees, after the test is completed Rotating the first axis of rotation of the test device to the next angle, corresponding to several angles of different values of φ, rotating the second axis of rotation of the test device, testing the points in turn, and so on. Point. The test points of the 2nd division and the 3rd division are shown in FIG. 11 and FIG.
(四) 数据处理 将在各个测试点所测量的数据进行线性平均,就可以得到移动终端设备 或者其他无线通信产品的空间射频性能指标 TRP、 TIS。 而不需要进行繁杂 的积分运算, 简化了计算方法。 通过本发明, 可以使得空间的测试点在球面上的分布尽量均勾, 能够在 满足测试精度及准确度要求的情况下减少测试点数, 从而节省测试时间。 以上所述仅为本发明的优选实施例而已, 并不用于限制本发明, 对于本 领域的技术人员来说, 本发明可以有各种更改和变化。 凡在本发明的 4青神和 原则之内, 所作的任何修改、 等同替换、 改进等, 均应包含在本发明的保护 范围之内。
(IV) Data Processing The spatial RF performance indicators TRP and TIS of mobile terminal equipment or other wireless communication products can be obtained by linearly averaging the data measured at each test point. It does not require complicated integration operations, which simplifies the calculation method. Through the invention, the distribution of the test points on the space on the spherical surface can be made as uniform as possible, and the number of test points can be reduced under the condition of satisfying the test accuracy and the accuracy requirement, thereby saving test time. The above description is only the preferred embodiment of the present invention, and is not intended to limit the present invention, and various modifications and changes can be made to the present invention. Any modifications, equivalent substitutions, improvements, etc. made within the scope of the present invention are intended to be included within the scope of the present invention.
Claims
1. 一种空间射频性能测试方法, 用于无线通信产品的空间射频性能测试, 被测无线通信产品放置于一测试装置的第一旋转轴或第二旋转轴上, 其 特征在于, 该方法包括: A spatial RF performance test method for spatial RF performance testing of a wireless communication product, wherein the measured wireless communication product is placed on a first rotating shaft or a second rotating shaft of a testing device, wherein the method comprises :
球面坐标系建立步骤, 以被测无线通信产品为原点建立由 x、 y、 z 轴所定义的球面坐标系; a spherical coordinate system establishing step of establishing a spherical coordinate system defined by the x, y, and z axes with the measured wireless communication product as an origin;
测试点选取步骤, 使用正 N 面体对整个球面进行三角化来获得均 匀分布在球面上的测试点; The test point selection step is to use the normal N-facet to triangulate the entire sphere to obtain a test point uniformly distributed on the spherical surface;
测试步骤, 旋转测试装置的第一旋转轴和第二旋转轴, 按照各测试 点的 Θ角大小依次测试每个 Θ角所对应的平面上的对应于不同 φ角的测 试点的空间射频性能数据,其中 Θ角为测试点与所述 ζ轴正方向的夹角, φ角为所述 X轴正向与测试点在所述 x、 y平面上的投影点的夹角; a test step of rotating the first rotating shaft and the second rotating shaft of the testing device, and sequentially testing the spatial RF performance data of the test points corresponding to different φ angles on the plane corresponding to each corner according to the corner angle of each test point Wherein the corner is the angle between the test point and the positive direction of the x-axis, and the angle φ is the angle between the forward direction of the X-axis and the projection point of the test point on the x, y plane;
数据处理步骤,将在各个测试点所测量的空间射频性能数据进行线 性平均计算得到总的测试结果。 In the data processing step, the spatial RF performance data measured at each test point is linearly averaged to obtain the total test result.
2. 根据权利要求 1 所述的方法, 其特征在于, 在所述测试步骤中, 对于 Θ 角相等的测试点, 按照 φ角大小顺序对各测试点进行测试。 2. The method according to claim 1, wherein in the testing step, for test points having the same angle, each test point is tested in order of magnitude of φ.
3. 根据权利要求 2所述的方法, 其特征在于, 所述测试步骤具体包括: 按 照测试点对应的 Θ值的大小进行排序, 对于 Θ值相同但 φ值不同的测试 点再按照 φ值大小进行排序, 按照排序后的测试点顺序依次测试各测试 点的空间射频性能数据。 The method according to claim 2, wherein the testing step comprises: sorting according to the size of the Θ value corresponding to the test point, and the test point having the same Θ value but different φ values according to the φ value Sorting, testing the spatial RF performance data of each test point in the order of the sorted test points.
4. 居权利要求 1 所述的方法, 其特征在于, 所述第一旋转轴的旋转范围 为 0- 180度, 第二旋转轴的旋转范围为 0-360度。 The method according to claim 1, wherein the first rotating shaft has a rotation range of 0-180 degrees, and the second rotating shaft has a rotation range of 0-360 degrees.
5. 根据权利要求 1 所述的方法, 其特征在于, 所述测试点选取步骤具体包 将球面划分为正四面体、 正^\面体、 正十二面体、 或者正二十面体, 每一个面对应一个球面三角形, 连接球面三角形三条边的中点, ■!巴每一 个球面三角形划分为四个球面三角形, 取三角网格的顶点为测试点。 The method according to claim 1, wherein the test point selecting step specifically divides the spherical surface into a regular tetrahedron, a positive ^\ plane, a dodecahedron, or an icosahedron, each surface Corresponding to a spherical triangle, connecting the midpoints of the three sides of the spherical triangle, ■! Each spherical triangle of the bar is divided into four spherical triangles, and the vertices of the triangular mesh are taken as test points.
6. 根据权利要求 1 所述的方法, 其特征在于, 所述各测试点的空间射频性 能数据包括以下数据中的至少一种: 发射功率、 接收灵敏度。
The method according to claim 1, wherein the spatial radio frequency performance data of each test point comprises at least one of the following data: transmit power, receive sensitivity.
7. 根据权利要求 6所述的方法, 其特征在于, 根据所述数据处理步骤计算 总的测试结果的步骤包 4舌: .· · -.. 根据以下公式计算总发射功率 (TRP ): 7. The method according to claim 6, wherein the step of calculating the total test result according to the data processing step is: .. -.. Calculating the total transmit power (TRP) according to the following formula:
TRP ≡^-∑∑ [EiRPe (θι , φί ) + EiRP* (θ, , } ) 和 /或根据以下公式计算全向接收灵敏度 ( TIS ):
TRP ≡^-∑∑ [EiRP e (θ ι , φ ί ) + EiRP* (θ, , } ) and/or calculate the omnidirectional receiving sensitivity (TIS) according to the following formula:
其中, 为进行 L次三角化得到的测量点个数, η为 L次三角化 得到 Θ值不同的测试点个数, m为 L次三角化得到的 Θ角相同但 φ角不 同的测 i式点个数; Wherein, for the number of measurement points obtained by tri-degree triangulation, η is the L-th-triangulation to obtain the number of test points with different Θ values, and m is the same as the Θ angle obtained by the L-th-triangulation. Count the number;
& ^ ( ,^ )为角度为 , ^的测试点的等效全向辐射功率水平极化 分量值, 单位为毫瓦; & ^ ( , ^ ) is the equivalent omnidirectional radiated power horizontal polarization component value of the test point of angle ^, in milliwatts;
EiRP^ (θί,φί )为角度为 θ( , φ}的测试点的等效全向辐射功率垂直极化 分量值, 单位为毫瓦; 为角度为 , ^的测试点的等效全向接收功率水平极化 分量值, 单位为毫瓦; EiRP^ (θ ί ,φ ί ) is the value of the equivalent omnidirectional radiated power vertical polarization component of the test point with angle θ( , φ } , in milliwatts; for the angle, the equivalent of the test point of ^ The value of the polarization component to the received power level, in milliwatts;
EISe (θί , )为角度为 θ , φί的测试点的等效全向接收功率垂直极化 分量值, 单位为毫瓦。
EIS e (θ ί , ) is the equivalent omnidirectional received power vertical polarization component of the test point with angles θ , φ ί , in milliwatts.
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