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    • 111. 发明授权
    • Antenna field tester
    • 天线现场测试仪
    • US06285330B1
    • 2001-09-04
    • US09244954
    • 1999-02-04
    • Elyahu Perl
    • Elyahu Perl
    • H01Q300
    • G01R29/10
    • An apparatus and method for testing of rotating surface based antennas arrays (regardless of their shape), with the capability of fully diagnosing and locating a failure on the face of the antenna by coherently sampling and storing the radiation in the near field and imaging the fully array complex excitation from the stored data. The rotation of the antenna is used in order to collect data for the full azimuth span required for high resolution imaging of excitation in the horizontal domain. Excitation in the vertical domain can be preformed in two ways depending on the type of antenna used. For electronically scanning antennas in elevation (phased array antennas), the phase shifter in the desired row is toggled and the row is isolated by subtracting the complex data from pairs of adjacent samples. The sampling probe is moved vertically while the antenna is rotating horizontally. The vertical movement of the probe provides the aperture necessary to resolve the vertical excitation of the array to a degree of accuracy sufficient for fault detection and isolation.
    • 一种用于测试基于旋转表面的天线阵列(不管其形状)的装置和方法,具有通过在近场中相干采样和存储辐射来完全诊断和定位天线表面上的故障的能力,并对其进行成像 阵列复数激励从存储的数据。 使用天线的旋转以便收集水平域中激发的高分辨率成像所需的完整方位角的数据。 根据使用的天线类型,垂直领域的激励可以以两种方式进行。 对于电子扫描天线仰角(相控阵天线),期望行中的移相器被切换,并且通过从相邻采样对中减去复数数据来隔离该行。 当天线水平旋转时,采样探头垂直移动。 探头的垂直运动提供了将阵列的垂直激励解决到足以用于故障检测和隔离的精度的必要孔径。
    • 112. 发明授权
    • Global positioning system satellite selection method
    • 全球定位系统卫星选择方法
    • US06278404B1
    • 2001-08-21
    • US09348875
    • 1999-07-07
    • Frederick A. Niles
    • Frederick A. Niles
    • H01Q300
    • G01S19/14G01S19/28G01S19/36G01S19/37G01S19/426G01S19/53
    • The satellite selection method as utilized by the spaceborne Global Positioning System receiver provides navigational solutions and is designed for use in low Earth orbit. The satellite selection method is a robust algorithm that can be used a GPS receiver to select appropriate GPS satellites for use in calculating point solutions or attitude solutions. The method is takes into account the difficulty of finding a particular GPS satellite phase code, especially when the search range in greatly increased due to Doppler shifts introduced into the carrier frequency. The method starts with an update of the antenna pointing and spacecraft vectors to determine the antenna backplane direction. Next, the GPS satellites that will potentially be in view of the antenna are ranked on a list, whereby the list is generated based on the estimated attitude and position of each GPS satellite. Satellites blocked by the Earth are not entered on this list. A second list is created, whereby the GPS satellites are ranked according to their desirability for use in attitude determination. GPS satellites are ranked according to their orthogonality to the antenna backplane, and according to geometric dilution of precision considerations. After the lists are created, the channels of the spaceborne GPS receiver are assigned to various GPS satellites for acquisition and lock. Preliminary Doppler frequencies for searching are assigned to the various channels.
    • 由空间全球定位系统接收机使用的卫星选择方法提供导航解决方案,并设计用于低地球轨道。 卫星选择方法是一种鲁棒的算法,可以使用GPS接收机选择合适的GPS卫星,用于计算点解或姿态解。 该方法考虑到寻找特定的GPS卫星相位码的难度,特别是当由于多普勒频移引入载波频率而大大增加的搜索范围时。 该方法从天线指向和航天器向量的更新开始,以确定天线背板方向。 接下来,将潜在地考虑天线的GPS卫星列在列表中,由此基于每个GPS卫星的估计姿态和位置来生成该列表。 卫星被地球阻挡的卫星没有输入到这个列表中。 创建了第二个列表,其中GPS卫星根据其在姿态确定中的使用性能进行排名。 GPS卫星根据其与天线底板的正交性进行排序,并根据精度考虑的几何稀释。 在创建列表之后,空间GPS接收机的信道被分配给各种GPS卫星用于采集和锁定。 用于搜索的初步多普勒频率被分配给各种信道。
    • 114. 发明授权
    • Scanning apparatus
    • 扫描仪
    • US06259414B1
    • 2001-07-10
    • US09403201
    • 1999-10-15
    • Alan H. Lettington
    • Alan H. Lettington
    • H01Q300
    • H01Q15/246G01S7/02G01S7/024G01S13/89G01V8/005G02B26/101H01Q3/20
    • Scanning apparatus which scans input radiation from a scene and output radiation is transmitted to a receiver system, for example a millimetre wave imaging camera or a radar receiver by a rotatable reflective plate having an axis of rotation passing through the centre of its surface, secondary reflector and static reflector, wherein the secondary reflector is a second rotatable reflective plate having a common axis of rotation with the first rotatable reflective plate, wherein the common axis of rotation is inclined at a non-zero zero angle &thgr;b to the normal to the second reflective plate. The normal to the first rotatable plate is inclined at a small angle to the common axis of rotation, typically a few degrees and forms the secondary reflector. The static reflector may be a polarising roof reflector through which radiation is input to and output from the apparatus. The apparatus also includes a 45° Faraday rotator or a birefringent surface such as a Meander-line. An additional Faraday rotator and an inclined polariser may be included in the apparatus and arranged such that radiation output to the receiver system may be separated from the path of input radiation. Alternatively, the scanning apparatus may include a reflector lens arrangement, such that focused output radiation may be output directly to the receiver system.
    • 扫描来自场景的输入辐射和输出辐射的扫描装置通过具有穿过其表面中心的旋转轴线的可旋转反射板传送到接收机系统,例如毫米波成像照相机或雷达接收器,辅助反射器 和静态反射器,其中所述次级反射器是具有与所述第一可旋转反射板的公共旋转轴线的第二可旋转反射板,其中所述公共旋转轴线以非零零角度倾斜到所述第二反射板的法线 盘子。 第一可旋转板的法线倾斜与公共旋转轴线成小角度,通常为几度,并形成辅助反射器。 静态反射器可以是偏振屋顶反射器,辐射通过该反射器输入到设备并从设备输出。 该装置还包括45°法拉第旋转器或诸如弯曲线的双折射表面。 附加的法拉第旋转器和倾斜偏振器可以被包括在装置中并且被布置成使得输出到接收器系统的辐射可以与输入辐射的路径分离。 或者,扫描装置可以包括反射镜透镜装置,使得聚焦的输出辐射可以直接输出到接收器系统。
    • 115. 发明授权
    • Radio wave visualizing method and apparatus
    • 无线电波可视化方法和装置
    • US06249248B1
    • 2001-06-19
    • US09287660
    • 1999-04-07
    • Hitoshi Kitayoshi
    • Hitoshi Kitayoshi
    • H01Q300
    • G01R29/10G01R29/0814
    • An object shape distribution of an antenna intergral-type communication device to be observed with a sensor for measuring a three-dimensional shape is measured and recorded, and a scanning distribution of an interference complex data between a detected signal with a scanning probe antenna measuring a two-dimensional distribution of an electromagnetic wave and a detected signal with a fixed probe antenna, a relative position of which does not change against a measured object, as a two-dimensional electric field distribution or a two-dimensional magnetic field distribution is measured and recorded, based on movement with a predetermined step as a minimum movement unit. The object shape distribution and the two-dimensional electric field distribution or the two-dimensional magnetic field distribution are displayed in a superimposed state on a screen. A line area and a plane area of the antenna integral-type communication device are specified for the display screen. A complex current distribution of the specified line area and plane area is derived from the object shape distribution and the two-dimensional electric field distribution or the two-dimensional magnetic field distribution. Directivity is derived from the object shape distribution and the complex current distribution of the line area or the plane area. The derived directivity is displayed.
    • 测量和记录用于测量三维形状的传感器观察的天线整体式通信装置的对象形状分布,并且将检测信号与检测信号与扫描探针天线测量的扫描分布 测量作为二维电场分布或二维磁场分布的电磁波的二维分布和具有固定的探针天线的检测信号(其相对位置对测量对象不改变),并且 基于作为最小移动单位的预定步长的移动来记录。 物体形状分布和二维电场分布或二维磁场分布以叠加状态显示在屏幕上。 为显示画面指定天线整体式通信装置的线路面积和平面面积。 从物体形状分布和二维电场分布或二维磁场分布导出指定线面积和平面面积的复电流分布。 方向性是从对象形状分布和线区域或平面区域的复电流分布导出的。 显示派生方向性。
    • 116. 发明授权
    • Precision beacon tracking system
    • 精密信标跟踪系统
    • US06236361B1
    • 2001-05-22
    • US09301966
    • 1999-04-29
    • Harold A. Rosen
    • Harold A. Rosen
    • H01Q300
    • H01Q3/267H01Q1/288H01Q19/17
    • A system and method for eliminating pointing error in a beacon tracking system due to uncontrolled differences in passive loss or in amplification of the separate signals involved in creating a pilot signal. A locally generated reference signal (30) is radiated onto a set of feed horns (14), at least three (20, 22, 24) of which are used to track a pilot signal (18). The reference signal (30) is detected and used in an automatic gain control feedback loop (44, 46, 48) to maintain equal gain on the separate feed horn channels. The equalized signal is processed (62) to produce precision tracking signals.
    • 一种用于消除信标跟踪系统中的指向误差的系统和方法,这是由于在产生导频信号中涉及的单独信号的被动丢失或放大中的不受控制的差异。 本地产生的参考信号(30)被辐射到一组馈电喇叭(14)上,其中至少三(20,22,24)用于跟踪导频信号(18)。 在自动增益控制反馈回路(44,46,48)中检测并使用参考信号(30),以在单独的馈送喇叭通道上保持相等的增益。 处理均衡信号(62)以产生精确跟踪信号。
    • 117. 发明授权
    • Antenna configuration
    • 天线配置
    • US06198452B1
    • 2001-03-06
    • US09307313
    • 1999-05-07
    • Carl M. BehelerWilliam H. Grona
    • Carl M. BehelerWilliam H. Grona
    • H01Q300
    • H01Q1/18H01Q1/34H01Q3/08
    • A positioner (or gimbal assembly) for a compact antenna assembly is disclosed. The positioner provides accurate pointing of the antenna assembly (typically a narrow beam radio frequency (RF) radiating assembly) mounted on a rapidly moving platform. The positioner is comprised of a first, second, and third axis assemblies which support the antenna assembly and allow rotation of the antenna assembly about first, second, and third axis. The axis assemblies are arranged so the first, second and third axis are non-orthogonal and intersect at the approximate geometric center of the antenna assembly allowing continuous and independent rotation of the antenna assembly about each axis within a confined volume.
    • 公开了一种用于小型天线组件的定位器(或万向节组件)。 定位器提供安装在快速移动的平台上的天线组件(通常是窄射束射频(RF)辐射组件)的精确指向。 定位器由支撑天线组件并允许天线组件围绕第一轴,第二轴和第三轴旋转的第一,第二和第三轴组件组成。 轴组件布置成使得第一,第二和第三轴线不正交并且在天线组件的大致几何中心处相交,允许天线组件围绕限制体积内的每个轴线连续且独立地旋转。