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    • 43. 发明授权
    • Covariance rotation with perspective projection for creating radar search volumes from remote cues
    • 协方差旋转与透视投影从远程提示创建雷达搜索量
    • US09081092B1
    • 2015-07-14
    • US13197572
    • 2011-08-03
    • Mark A. Friesel
    • Mark A. Friesel
    • G01S13/00G01S13/72G01S13/66
    • G01S13/726G01S7/003G01S13/426G01S13/66G01S13/87
    • A radar installation searches a limited volume within view, such as a covariance ellipsoid where a target is expected to be found based on a cue from a remote radar. The radar activates beams selected from an angularly diverging array of beams spanning the azimuth and elevation of an acquisition face whose area increases with range from the radar. A controller projects the search volume relative to the acquisition face, for selecting beam positions intersecting the search volume, and activates beams for a time interval that determines maximum range. A coordinate transformation is effected, so that with decreasing range, the angular divergence between projected points of the search volume is correspondingly increased, including points tangent to outer edges of the ellipsoid. The search volume accurately corresponds to the covariance ellipsoid by accounting for perspective in this way, reducing the time needed to examine the search volume for the target.
    • 雷达装置在视野内搜索有限的体积,例如根据来自远程雷达的提示预期找到目标的协方差椭球。 雷达激活从角度发散的波束阵列中选出的波束,横跨射频面积的方位角和仰角,其面积随雷达的范围而增加。 A控制器相对于采集面投影搜索量,用于选择与搜索卷相交的波束位置,并激活确定最大范围的时间间隔的波束。 实现坐标变换,使得随着范围的减小,搜索体积的投影点之间的角度发散度相应地增加,包括与椭圆体的外边缘相切的点。 通过以这种方式计算透视度,搜索量准确地对应于协方差椭球,减少了检查目标搜索量所需的时间。
    • 45. 发明申请
    • Real Aperture Radar System For Use On Board A Satellite And For Maritime Surveillance Applications
    • 用于卫星和海上监视应用的实际孔径雷达系统
    • US20140266899A1
    • 2014-09-18
    • US14208162
    • 2014-03-13
    • THALES ALENIA SPACE ITALIA S.p.A. CON UNICO SOCIO
    • Andrea Torre
    • G01S13/02
    • G01S13/02G01S13/24G01S13/426
    • The present invention regards a method of operation of a real aperture radar system for surveillance of the Earth's surface, said real aperture radar system being installed on a space vehicle/platform that moves in a direction of flight and comprising a transceiving antenna, or a transmitting antenna and a receiving antenna, which is/are electronically steerable. The method comprises: a) transmitting, via the transceiving/transmitting antenna, a series of M radar pulses towards a swath of the Earth's surface parallel to the direction of flight using an antenna beam pointed at said swath, wherein M is an integer greater than two; b) for each of the M radar pulses transmitted, receiving, via the transceiving/receiving antenna, a corresponding echo signal during the time interval that elapses between transmission of said radar pulse and transmission of the following radar pulse using the same antenna beam as the one used for transmitting the M radar pulses; c) carrying out elevation scanning cycles, wherein each elevation scanning cycle is carried out by repeating N times the operations a) and b) and by electronically changing, each time, the direction of pointing in elevation of the antenna beam so that, at each elevation scanning cycle, the radar pulses are transmitted towards, and the echo signals are received from, N swaths of the Earth's surface that are parallel to the direction of flight and are adjoining or partially overlapping, wherein N is an integer greater than one. All the radar pulses are transmitted: with a predefined pulse repetition frequency and a predefined timing of the scanning cycle such that to guarantee a complete coverage of each of the N swaths parallelly to the direction of flight; and by using a frequency agility technique.
    • 本发明涉及一种用于监视地球表面的实际孔径雷达系统的操作方法,所述实际孔径雷达系统安装在沿飞行方向移动并包括收发天线或发射天线的空中飞行器/平台上 天线和接收天线,其是电子可操纵的。 该方法包括:a)使用收发/发射天线,使用指向所述条带的天线波束,将平行于飞行方向的一系列M雷达脉冲发射到地球表面的一条线上,其中M是大于 二; b)对于发射的每个M雷达脉冲,经由收发/接收天线接收在所述雷达脉冲的传输和使用与所述雷达脉冲相同的天线波束的传输之后的时间间隔期间的对应的回波信号 用于发送M雷达脉冲的一个; c)进行仰角扫描循环,其中通过重复N次操作a)和b)来执行每个仰角扫描周期,并且每次通过电子地改变天线波束的仰角指向,使得在每个 仰角扫描周期,雷达脉冲被传送到地球表面的平行于飞行方向并且相邻或部分重叠的N条带中的回波信号,其中N是大于1的整数。 所有雷达脉冲都以预定义的脉冲重复频率和扫描周期的预定定时被传输,以便保证平行于飞行方向的N条中的每一条的完整覆盖; 并使用频率捷变技术。
    • 48. 发明授权
    • Electronic scanning type radar device and method for estimating direction of reception wave
    • 电子扫描型雷达装置及估计接收波方向的方法
    • US08730096B2
    • 2014-05-20
    • US13859492
    • 2013-04-09
    • Honda elesys Co., Ltd.
    • Junji KanamotoHiroyuki Akimoto
    • G01S13/00G01S13/58
    • G01S13/426G01S3/74G01S13/04G01S13/345G01S13/584G01S13/931G01S2013/9375
    • An electronic scanning type radar device mounted on a moving body includes: a transmission unit transmitting a transmission wave; a reception unit comprising a plurality of antennas receiving a reflection wave of the transmission wave from a target; a beat signal generation unit generating a beat signal from the transmission wave and the reflection wave; a frequency resolution processing unit frequency computing a complex number data; a target detection unit detecting an existence of the target; a correlation matrix computation unit computing a correlation matrix from each of a complex number data of a detected beat frequency; a target consolidation processing unit linking the target in a present detection cycle and a past detection cycle; a correlation matrix filtering unit generating an averaged correlation matrix by weighted averaging a correlation matrix of a target in the present detection cycle and a correlation matrix of a related target in the past detection cycle; and a direction detection unit computing an arrival direction of the reflection wave based on the averaged correlation matrix.
    • 安装在移动体上的电子扫描型雷达装置包括:传输单元,发送传输波; 接收单元,包括从目标接收所述传输波的反射波的多个天线; 拍子信号生成部,从发送波和反射波生成拍子信号; 频率分辨率处理单元对复数数据进行频率计算; 检测目标的存在的目标检测单元; 相关矩阵计算单元从检测到的拍频的复数数据中的每一个计算相关矩阵; 目标整合处理单元,其在当前检测周期和过去检测周期之间连接目标; 相关矩阵滤波单元,通过对当前检测周期中的目标的相关矩阵和过去检测周期中的相关目标的相关矩阵进行加权平均来生成平均相关矩阵; 以及方向检测单元,其基于所述平均相关矩阵来计算所述反射波的到达方向。
    • 50. 发明申请
    • ANTENNA DEVICE, AMPLIFIER AND RECEIVER CIRCUIT, AND RADAR CIRCUIT
    • 天线设备,放大器和接收器电路以及雷达电路
    • US20140035780A1
    • 2014-02-06
    • US14111821
    • 2011-04-20
    • Saverio Trotta
    • Saverio Trotta
    • H01Q3/34H01Q3/00
    • H01Q3/34G01S7/032G01S13/426G01S13/931G01S2013/9375H01Q1/3233H01Q3/00H01Q21/065
    • An antenna device comprises a first chain of at least two antenna components, wherein each of the antenna components comprises a transmit antenna having a line of antenna patches for emitting radar waves; and a receive antenna having a line of antenna patches for receiving radar response waves; wherein the line of antenna patches of the receive antenna is aligned with the line of antenna patches of the transmit antenna. An amplifier and receiver circuit for amplifying radar signals and for receiving radar re-sponse signals, the amplifier and receiver circuit comprises a phase shifter for shifting a phase of the radar signals to be amplified and for synchronously shifting the received radar response signals. A radar circuit comprises a first chain of at least two radar components, wherein each of the radar components comprises: an amplifier and receiver circuit as described above; and a transmit antenna for emitting radar waves; and a receive antenna for re-ceiving radar response waves.
    • 天线装置包括至少两个天线部件的第一链,其中每个天线部件包括具有用于发射雷达波的天线贴片线的发射天线; 以及具有用于接收雷达响应波的天线贴片线的接收天线; 其中所述接收天线的所述天线贴片线与所述发射天线的天线块的线对齐。 一种用于放大雷达信号并用于接收雷达反应信号的放大器和接收器电路,放大器和接收器电路包括用于移位要放大的雷达信号的相位的移相器,并用于同步地移位所接收的雷达响应信号。 雷达电路包括至少两个雷达组件的第一链,其中每个雷达组件包括:如上所述的放大器和接收器电路; 和用于发射雷达波的发射天线; 以及用于重新接收雷达响应波的接收天线。