公开(公告)号：US20110175765A1

公开(公告)日：2011-07-21

申请号：US12742884

申请日：2008-11-12

申请人： Claude Chekroun ,  Gilles Chekroun

发明人： Claude Chekroun ,  Gilles Chekroun

IPC分类号： G01S13/89

CPC分类号： G01S7/41 ,  G01S7/024 ,  G01S13/887 ,  G01S2013/9076 ,  G01S2013/9082

摘要： The present invention relates to a device for detecting objects. The device comprises at least one microwave-frequency transmitter and one microwave-frequency receiver. The receiver makes a relative rotary movement about the transmitter, a signal being transmitted toward an individual for several positions of the receiver on the circle of relative rotation, the signals reflected by points of an object and received by the receiver at the positions being supplied to processing means in order to form a radar image. The receiver and the transmitter can be installed on a disk with a very low moment of inertia. The invention applies notably for the detection of weapons or explosives carried by persons.

摘要翻译： 本发明涉及一种用于检测物体的装置。 该装置包括至少一个微波频率发射器和一个微波频率接收器。 接收器围绕发射器进行相对旋转运动，信号朝向相对于相对旋转的圆周上的接收器的几个位置的个体发送，由物体的点反射并由接收器在被提供给位置的位置处接收的信号 处理手段以形成雷达图像。 接收器和发射器可以安装在具有非常低的惯性矩的盘上。 本发明特别适用于检测人员携带的武器或爆炸物。

公开(公告)号：US5379041A

公开(公告)日：1995-01-03

申请号：US131634

申请日：1993-10-05

申请人： Helmut Klausing

发明人： Helmut Klausing

IPC分类号： G01S13/90

CPC分类号： G01S13/9035 ,  G01S2013/9082

摘要： A rotating antenna synthetic aperture radar apparatus having a module in the processor circuit in which are stored image definition values for reducing image errors. The module acts upon process circuits to subdivide the distance range illuminated by the antenna into individual distance intervals and to determine the reference functions in these distance intervals.

摘要翻译： 具有处理器电路中的模块的旋转天线合成孔径雷达装置存储有用于减少图像误差的图像定义值。 该模块作用于处理电路，将由天线照射的距离范围细分为单独的距离间隔，并确定这些距离间隔中的参考功能。

公开(公告)号：US4737788A

公开(公告)日：1988-04-12

申请号：US719854

申请日：1985-04-04

申请人： Peter D. Kennedy

发明人： Peter D. Kennedy

IPC分类号： G01S13/50 ,  G01S13/90 ,  G01S13/93

CPC分类号： G01S13/93 ,  G01S13/50 ,  G01S2013/9082

摘要： A pulsed Doppler radar mounted adjacent to the tip of a helicopter rotor blade for sensing obstacles in the helicopter path. The rotor tip velocity shifts the frequency of radar echos so that, through pulsed Doppler radar techniques, the echos from obstacles can be separated from clutter.

摘要翻译： 安装在直升机转子叶片尖端附近的脉冲多普勒雷达，用于感测直升机路径中的障碍物。 转子尖端速度使雷达回波频率发生变化，通过脉冲多普勒雷达技术，障碍物的回波可以与杂波分离。

公开(公告)号：US20170016988A1

公开(公告)日：2017-01-19

申请号：US15123787

申请日：2015-03-05

申请人： MITSUBISHI ELECTRIC CORPORATION

发明人： Kenichi NUMATA

IPC分类号： G01S13/90 ,  G01S7/36

CPC分类号： G01S13/9035 ,  G01S7/023 ,  G01S7/025 ,  G01S7/36 ,  G01S2013/0245 ,  G01S2013/9082 ,  H01Q1/281 ,  H01Q3/04 ,  H01Q3/10 ,  H01Q3/30

摘要： A radar device includes: an aperture surface including element antennas and phase shifters; an antenna phase control unit for calculating phase amounts based on a beam orientation direction and a rotation angle of the aperture surface; an antenna driving control unit for setting a rotation angle to a rotation mechanism; a signal processing unit for detecting a target with the use of the radar receiver, setting at least one of the rotation angle of the aperture surface or the beam orientation direction in the antenna driving control unit and the antenna phase control unit, and calculating the level of competing cluttering with the use of an antenna pattern, to thereby determine propriety of the rotation angle; and a pattern calculating unit for calculating the antenna pattern from the rotation angle of the aperture surface and from the beam orientation direction.

摘要翻译： 雷达装置包括：孔径表面，包括元件天线和移相器; 天线相位控制单元，用于基于光束定向方向和孔径表面的旋转角度来计算相位量; 用于设定与旋转机构的旋转角度的天线驱动控制单元; 信号处理单元，用于使用雷达接收器检测目标，设置天线驱动控制单元和天线相位控制单元中的孔径表面的旋转角度或光束定向方向中的至少一个，并且计算水平 与使用天线图案竞争混乱，从而确定旋转角度的合适性; 以及图案计算单元，用于根据孔表面的旋转角度和从光束定向方向计算天线图案。

公开(公告)号：US09128184B1

公开(公告)日：2015-09-08

申请号：US13803264

申请日：2013-03-14

申请人： Lockheed Martin Corporation

发明人： Svetlana M. Bachmann ,  Elliott Reitz

IPC分类号： F03D7/00 ,  F03D9/00 ,  G01S13/62 ,  G01S13/95 ,  F03D11/00 ,  F03D7/02 ,  H01Q1/12

CPC分类号： F03D7/0268 ,  F03D1/0675 ,  F03D7/022 ,  F03D7/0264 ,  F03D7/0276 ,  F03D7/042 ,  F03D9/255 ,  F03D13/20 ,  F05B2260/99 ,  G01S7/003 ,  G01S7/02 ,  G01S13/60 ,  G01S13/9035 ,  G01S13/95 ,  G01S13/951 ,  G01S13/956 ,  G01S2007/027 ,  G01S2013/9064 ,  G01S2013/9082 ,  H01Q1/12 ,  H01Q1/42 ,  H01Q1/44 ,  Y02A90/18 ,  Y02E10/721 ,  Y02E10/723 ,  Y02E10/725

摘要： A blade mounted radar system comprises a wind turbine having a hub and blades extending therefrom; a radar antenna configured to transmit and/or receive a radio frequency (RF) signal; and a processor in electrical communication with the radar antenna and configured to generate the RF signal for transmission and/or to process the received RF signal. The radar antenna is affixed to one of the blades of the wind turbine such that relative motion is defined between the radar antenna and a target within a line of sight of the radar antenna. The problem of the ground based radar line of sight being obscured by the wind turbine is mitigated in this setup, as radar and turbine coexist in the same structure. Improved performance and additional capability are enabled by elevated installation and vertical SAR imaging capability. Doppler capabilities are extended using known motion of the antenna relative to stationary objects.

摘要翻译： 一种安装有叶片的雷达系统，包括具有从其延伸的轮毂和叶片的风力涡轮机; 被配置为发射和/或接收射频（RF）信号的雷达天线; 以及处理器，与所述雷达天线电通信并被配置为产生用于传输和/或处理所接收的RF信号的RF信号。 雷达天线被固定在风力涡轮机的一个叶片上，使得在雷达天线和雷达天线的视线内的目标之间定义相对运动。 由于雷达和涡轮机在同一结构中共存，基于雷达和雷达的雷达视线被风力涡轮机遮蔽的问题在此设置中得到了缓解。 通过提高安装和垂直SAR成像能力，可以提高性能和附加功能。 使用天线相对于固定物体的已知运动来扩展多普勒能力。

公开(公告)号：US20090051585A1

公开(公告)日：2009-02-26

申请号：US11894069

申请日：2007-08-20

申请人： Kapriel V. Krikorian ,  Robert A. Rosen ,  Michael Gubala

发明人： Kapriel V. Krikorian ,  Robert A. Rosen ,  Michael Gubala

IPC分类号： G01S13/90 ,  B64C27/04

CPC分类号： G01S13/9035 ,  G01S2013/9082

摘要： A hovering helicopter has a radar transmitter/receiver for transmitting radar pulses for illuminating a target for SAR imaging, and rotor blades for generating lift. Radar reflectors are on the rotor blades. The radar reflectors are oriented to reflect the radar pulses from the transmitter to the target as the rotor blades rotate. The radar pulses reflected by the moving reflector from the transmitter are timed to generate the synthetic aperture image using radar returns from the target. The receiver also receives blade returns directly reflected from the moving reflectors attached to the lift rotor blades. The receiver analyzes the blade returns to extract motion details of the reflectors and uses the motion details for motion compensation of target returns for SAR imaging.

摘要翻译： 悬停的直升机具有雷达发射器/接收器，用于发射用于照射SAR成像目标的雷达脉冲，以及用于产生电梯的转子叶片。 雷达反射器位于转子叶片上。 当转子叶片旋转时，雷达反射器被定向以将发射器的雷达脉冲反射到目标。 来自发射机的移动反射器反射的雷达脉冲被定时以使用来自目标的雷达返回产生合成孔径图像。 接收器还接收从附接到提升转子叶片的运动反射器直接反射的叶片返回。 接收机分析刀片返回以提取反射器的运动细节，并使用运动细节进行SAR成像的目标返回的运动补偿。

公开(公告)号：US06577264B1

公开(公告)日：2003-06-10

申请号：US10088896

申请日：2002-03-25

申请人： Aribert Wolframm

发明人： Aribert Wolframm

IPC分类号： G01S1390

CPC分类号： G01S13/9035 ,  G01S2013/9082

摘要： A helicopter-borne radar system has a synthetic aperture with rotating antennae (ROSAR). The antennae for transmitting and receiving radar pulses are arranged at the end of each arm rotating with the rotor, and are connected with the radar system which has at least one transmitting module, one electronic module with a central control device and an image processor as well as a display. In order to align the imaging on the display of the radar system with an inertial axis of the helicopter, and to limit the influence of a change of the rotational rotor on the imaging, a signal generator arranged at the rotor of the helicopter generates signals indicative of rotating positions of the rotor. The latter signals are transmitted to an electronic module of the radar system, which marks the flank of an individual signal from the signal sequence for a rotation of the rotor. This flank of a signal is defined as a “basic position” and is counted. The invention permits azimuthally phase-accurate synchronization between the viewing angle of a helicopter-borne radar system and an inertial axis of the helicopter, as well as a defined alignment of the image on the video screen with respect to an inertial axis of the helicopter (and thus with respect to the flight direction of the helicopter). The viewing direction of the radar system (ROSAR) can be adjusted by means of an electric regulator wheel, so that the pilot can set a desired defined viewing direction of the radar image on the video screen.

摘要翻译： 直升机雷达系统具有带旋转天线（ROSAR）的合成孔径。 用于发送和接收雷达脉冲的天线布置在每个臂与转子一起旋转的末端，并且与具有至少一个发射模块的雷达系统，具有中央控制装置的一个电子模块和图像处理器 作为显示。 为了将雷达系统的显示器与直升机的惯性轴对准，并且限制旋转转子改变对成像的影响，布置在直升机转子处的信号发生器产生指示 转子的旋转位置。 后一种信号被传送到雷达系统的电子模块，其标记来自信号序列的单独信号的侧翼以转动转子。 信号的这个侧面被定义为“基本位置”并被计数。 本发明允许直升机雷达系统的视角与直升机的惯性轴之间的方位相位精确同步，以及相对于直升机的惯性轴在视频屏幕上定义的图像对准（ 因此相对于直升机的飞行方向）。 雷达系统（ROSAR）的观察方向可以通过电动调节轮进行调整，使飞行员可以在视频屏幕上设置所需的雷达图像观看方向。

公开(公告)号：US20020135506A1

公开(公告)日：2002-09-26

申请号：US10050895

申请日：2002-01-18

发明人： Helmut Klausing ,  Horst Kaltschmidt

IPC分类号： G01S013/90

CPC分类号： G01S13/9035 ,  G01S7/412 ,  G01S2013/9082

摘要： A ROSAR wire detection method is based upon ROSAR focusing of entire segments of wire. By generating a wire reference signal comprised of a sum of coherent reference signals, the basis for reliable wire detectability is provided.

摘要翻译： ROSAR线检测方法基于整个线段的ROSAR聚焦。 通过产生由相干参考信号之和构成的导线参考信号，提供了可靠的线检测性的基础。

公开(公告)号：US5381152A

公开(公告)日：1995-01-10

申请号：US131736

申请日：1993-10-05

申请人： Helmut Klausing

发明人： Helmut Klausing

IPC分类号： G01S13/02 ,  G01S13/90

CPC分类号： G01S13/9035 ,  G01S2013/9082

摘要： In a rotating antenna synthetic aperture radar, a method and apparatus for unfocussed signal processing for the correlation of the received signals by means of the reference functions. In unfocussed signal processing, only the main portion of the receiving signal S.sub.E is used, in which the phase shift is smaller than or equal to 90.degree. for the go-and return-path of the signal. A simplified window function is used as a reference function whose width also corresponds to the main portion of the received signal. Preferably, the in-phase and quadrature component (I.sub.r, Q.sub.r) of the window function r are selected to be identical.

摘要翻译： 在旋转天线合成孔径雷达中，用于通过参考功能对接收到的信号进行相关的用于未被聚焦的信号处理的方法和装置。 在未被聚焦的信号处理中，仅使用接收信号SE的主要部分，其中对于信号的去往和返回路径，相移小于或等于90°。 简化的窗口函数用作参考函数，其宽度也对应于接收信号的主要部分。 优选地，窗函数r的同相和正交分量（Ir，Qr）被选择为相同。

公开(公告)号：US09441610B1

公开(公告)日：2016-09-13

申请号：US14847242

申请日：2015-09-08

申请人： Lockheed Martin Corporation

发明人： Svetlana M. Bachmann ,  Elliott Reitz

IPC分类号： G01S13/95 ,  F03D7/02 ,  F03D11/04 ,  F03D1/06 ,  F03D7/04 ,  G01S13/60 ,  G01S7/00 ,  G01S13/90

CPC分类号： F03D7/0268 ,  F03D1/0675 ,  F03D7/022 ,  F03D7/0264 ,  F03D7/0276 ,  F03D7/042 ,  F03D9/255 ,  F03D13/20 ,  F05B2260/99 ,  G01S7/003 ,  G01S7/02 ,  G01S13/60 ,  G01S13/9035 ,  G01S13/95 ,  G01S13/951 ,  G01S13/956 ,  G01S2007/027 ,  G01S2013/9064 ,  G01S2013/9082 ,  H01Q1/12 ,  H01Q1/42 ,  H01Q1/44 ,  Y02A90/18 ,  Y02E10/721 ,  Y02E10/723 ,  Y02E10/725

摘要： A blade mounted radar system comprises a wind turbine having a hub and blades extending therefrom; a radar antenna configured to transmit and/or receive a radio frequency (RF) signal; and a processor in electrical communication with the radar antenna and configured to generate the RF signal for transmission and/or to process the received RF signal. The radar antenna is affixed to one of the blades of the wind turbine such that relative motion is defined between the radar antenna and a target within a line of sight of the radar antenna. The problem of the ground based radar line of sight being obscured by the wind turbine is mitigated in this setup, as radar and turbine coexist in the same structure. Improved performance and additional capability are enabled by elevated installation and vertical SAR imaging capability. Doppler capabilities are extended using known motion of the antenna relative to stationary objects.

摘要翻译： 一种安装有叶片的雷达系统，包括具有从其延伸的轮毂和叶片的风力涡轮机; 被配置为发射和/或接收射频（RF）信号的雷达天线; 以及处理器，与所述雷达天线电通信并被配置为产生用于传输和/或处理所接收的RF信号的RF信号。 雷达天线被固定在风力涡轮机的一个叶片上，使得在雷达天线和雷达天线的视线内的目标之间定义相对运动。 由于雷达和涡轮机在同一结构中共存，基于雷达和雷达的雷达视线被风力涡轮机遮蔽的问题在此设置中得到了缓解。 通过提高安装和垂直SAR成像能力，可以提高性能和附加功能。 使用天线相对于固定物体的已知运动来扩展多普勒能力。