知搜-全球专利检索

  1. Login
  2. Sign Up

Search Results

218 records (took 0.02 seconds)

    SEEKER HAVING SCANNING-SNAPSHOT FPA
    11.
    发明申请
    SEEKER HAVING SCANNING-SNAPSHOT FPA 有权
    SEEKER有扫描-SNAPSHOT FPA

    公开(公告)号：US20150268345A1

    公开(公告)日：2015-09-24

    申请号：US13924028

    申请日：2013-06-21

    Applicant: Rosemount Aerospace, Inc.

    Inventor： Todd Ell

    IPC: G01S17/66 ,  F41G7/26 ,  G01S7/486

    CPC classification number: G01S17/66 ,  F41G7/008 ,  F41G7/2253 ,  F41G7/226 ,  F41G7/2293 ,  F41G7/26 ,  G01S3/784 ,  G01S7/4861 ,  G01S7/4865

    Abstract: A dual-mode laser-based and image-based seeker for projectiles, missiles, and other ordnance that persecute targets by detecting and tracking energy scattered from targets. The disclosed embodiments use a single digital imager having a single focal plane array (FPA) sensor to sense data in both the image-based and laser-based modes of operation. A control mechanism controls pixel scanning at a sub-window of the FPA to tightly control the imager's shuttering to detect, decode and localize in the imager's field-of-view a known pulse repetition frequency (PRF) from a known designator in the presence of ambient light and other confusing target designators, each having a different PRF.

    Abstract translation: 一种基于双模激光和基于图像的射弹探测器，用于通过检测和跟踪从目标散射的能量来迫害目标。 所公开的实施例使用具有单个焦平面阵列（FPA）传感器的单个数字成像器来在基于图像和基于激光的操作模式中感测数据。 控制机构控制FPA的子窗口处的像素扫描，以紧密地控制成像仪的快门，以在成像仪的视场中检测，解码和定位来自已知指示符的已知脉冲重复频率（PRF） 环境光和其他令人困惑的目标指示符，每个具有不同的PRF。

    DIGITALLY SCANNED MULTI-CELL ELECTRO-OPTIC SENSOR
    12.
    发明申请
    DIGITALLY SCANNED MULTI-CELL ELECTRO-OPTIC SENSOR 有权
    数字扫描多单元电光传感器

    公开(公告)号：US20140231650A1

    公开(公告)日：2014-08-21

    申请号：US13768778

    申请日：2013-02-15

    Applicant: RAYTHEON COMPANY

    Inventor： Casey T. Streuber ,  Kent P. Pflibsen ,  Michael P. Easton

    IPC: H01L27/146

    CPC classification number: H01L27/14625 ,  F41G7/008 ,  F41G7/2253 ,  F41G7/226 ,  F41G7/2293 ,  G01S3/781 ,  G01S3/784 ,  G02B26/0875 ,  G02B26/10 ,  H04N5/33 ,  H04N5/335

    Abstract: A digitally scanned multi-cell EO sensor comprises a low-resolution multi-cell imaging detector. An array of optical focusing elements decomposes the sensor's FOV into at least four sub-fields. A sub-field directing array and focusing optic direct the optical radiation onto the imaging detector. In a first tilt mode, the optical radiation from the sub-fields is directed into at least four spatially separated sub-regions that each map to a different detector cell. A high-resolution spatial light modulator (SLM) digitally scans the FOV to select different portions of the FOV to map onto the different detector cells to time demultiplex spatially overlapping portions of the FOV onto each detector cell to stitch together a sub-image of a selected area of the FOV up to the native resolution of the SLM.

    Abstract translation: 数字扫描多单元EO传感器包括低分辨率多单元成像检测器。 一组光聚焦元件将传感器的FOV分解成至少四个子场。 子场引导阵列和聚焦光学器件将光辐射引导到成像检测器上。 在第一倾斜模式中，来自子场的光辐射被引导到至少四个空间上分离的子区域，每个子区域映射到不同的检测器单元。 高分辨率空间光调制器（SLM）数字扫描FOV以选择FOV的不同部分以映射到不同的检测器单元上，以将FOV的空间重叠部分时间解复用到每个检测器单元上以将一个子图像 FOV的选定区域达到SLM的原始分辨率。

    Antenna/optics system and method
    13.
    发明授权
    Antenna/optics system and method 有权
    天线/光学系统和方法

    公开(公告)号：US08773300B2

    公开(公告)日：2014-07-08

    申请号：US13076836

    申请日：2011-03-31

    Applicant: Glafkos K. Stratis ,  Alphonso A. Samuel ,  Salvatore Bellofiore ,  David J. Knapp

    Inventor： Glafkos K. Stratis ,  Alphonso A. Samuel ,  Salvatore Bellofiore ,  David J. Knapp

    IPC: G01S7/41

    CPC classification number: H01Q1/281 ,  F41G3/145 ,  F41G7/008 ,  F41G7/2246 ,  F41G7/226 ,  F41G7/2286 ,  F41G7/2293 ,  H01Q1/42 ,  H01Q1/422

    Abstract: A missile includes a radar system that has a radome through which a main antenna sends and receives signals. The radome includes a radome body and a radome tip include different transmissive materials, with for example the radome body primarily made of a lossy optically nontransparent material, and the radome tip primarily made of a lossless (permittivity with low imaginary part) glass material that may also be optically transparent. A laser may be used in conjunction with the radome to send and receive encoded signals. The laser may be located behind (aft of) the main antenna, and one or more optical fibers may extend into and/or along the radome to guide laser signals to the radome tip. The laser may be used to emit encoded signals so as to allow multiple radar systems operating in the same area at the same time to discriminate between different targets.

    Abstract translation: 导弹包括雷达系统，其具有天线罩，主天线通过天线罩发送和接收信号。 雷达罩包括天线罩体，天线罩顶端包括不同的透射材料，例如天线罩体主要由有损光学上不透明的材料制成，并且天线罩顶端主要由无损（具有低虚部的介电常数）玻璃材料制成， 也是光学透明的。 激光器可以与天线罩结合使用以发送和接收编码信号。 激光器可以位于主天线的后面（后面），并且一个或多个光纤可以延伸到天线罩中和/或沿着天线罩，以将激光信号引导到天线罩顶端。 激光器可以用于发射编码信号，以允许在同一区域同时操作的多个雷达系统区分不同的目标。

    Dual-mode electro-optic sensor and method of using target designation as a guide star for wavefront error estimation
    16.
    发明授权
    Dual-mode electro-optic sensor and method of using target designation as a guide star for wavefront error estimation 有权
    双模电光传感器和使用目标指定作为波前误差估计的引导星的方法

    公开(公告)号：US08502128B1

    公开(公告)日：2013-08-06

    申请号：US13621047

    申请日：2012-09-15

    Applicant: Casey T. Streuber ,  Kent P. Pflibsen ,  Michael P. Easton

    Inventor： Casey T. Streuber ,  Kent P. Pflibsen ,  Michael P. Easton

    IPC: F41G7/20 ,  F42B15/01 ,  F41G7/00 ,  F42B15/00

    CPC classification number: F41G7/001 ,  F41G7/008 ,  F41G7/2253 ,  F41G7/226 ,  F41G7/2293 ,  F42B15/01

    Abstract: A dual-mode sensor uses the active guidance radiation as a “guide star” to generate a wavefront error estimate for the primary optical element in-situ without interfering with the generation of either the active guidance or passive imaging guidance signals. An array of optical focusing elements performs the normal function of spatially encoding an angle of incidence of the active guidance radiation at an entrance pupil onto an active imaging detector. The array also performs an additional function of spatially encoding wavefront tilt deviations emanating from sub-pupils of an exit pupil onto the active imaging detector. A processor processes the electrical signals from the imaging detector in accordance with the respective spatial encodings to generate an active guidance signal and the wavefront error estimate for the primary optical element.

    Abstract translation: 双模传感器使用主动引导辐射作为“导星”来原位生成主光学元件的波前误差估计，而不会干扰主动引导或无源成像引导信号的产生。 光学聚焦元件的阵列执行将入射光瞳上的主动引导辐射的入射角空间编码到有源成像检测器上的正常功能。 该阵列还执行空间编码从出射光瞳的子瞳孔发射到有源成像检测器上的波前倾斜偏差的附加功能。 处理器根据相应的空间编码处理来自成像检测器的电信号，以产生主要的光学元件的主动引导信号和波前误差估计。

    System and method for navigating an object
    17.
    发明授权
    System and method for navigating an object 有权
    用于导航对象的系统和方法

    公开(公告)号：US08502126B2

    公开(公告)日：2013-08-06

    申请号：US12789172

    申请日：2010-05-27

    Applicant: Anthony K. Tyree

    Inventor： Anthony K. Tyree

    IPC: F42B15/01 ,  F42B15/00

    CPC classification number: F42B15/01 ,  F41G7/008 ,  F41G7/22 ,  F41G7/36

    Abstract: One example embodiment relates to a navigation system for a guided projectile. The navigation system includes a detector within the guided projectile. The detector determines an actual amount of time it takes after launch for the guided projectile to accelerate through mach one. The navigation system further includes a guidance system within the object. The guidance system includes a projected flight plan for the guided projectile. The projected flight plan includes an estimated amount of time after launch it will take the object to accelerate through the speed of sound. The guidance system compares the actual amount of time and the estimated amount of time and adjusts the flight path of the guided projectile based on data received from the detector.

    Abstract translation: 一个示例性实施例涉及一种用于引导射弹的导航系统。 导航系统包括在引导的射弹内的探测器。 探测器确定发射后实际的引导时间。 导航系统还包括对象内的引导系统。 指导系统包括引导弹丸的预计飞行计划。 预计的飞行计划包括发射后的估计时间，将通过声速来加速对象。 引导系统比较实际的时间量和估计的时间量，并根据从检测器接收到的数据调整被引导弹体的飞行路径。

    Infrared Seeker Head
    18.
    发明申请
    Infrared Seeker Head 有权
    红外探头

    公开(公告)号：US20120248238A1

    公开(公告)日：2012-10-04

    申请号：US13433762

    申请日：2012-03-29

    Applicant: Roderich RUEGER ,  Juergen Zoz

    Inventor： Roderich RUEGER ,  Juergen Zoz

    IPC: F42B15/01

    CPC classification number: F41G7/008 ,  F41G7/2213 ,  F41G7/2253 ,  F41G7/226 ,  F41G7/2293

    Abstract: A mount for a seeker head includes a plane spanned by a holder frame in which the pitch motion of the device containing at least one detector can be performed with respect to the missile structure and within the holder frame, at right angles to the plane spanned by the holder frame, a rotating mechanism for the rotational yaw motion of the device containing at least one detector is arranged about a rotation axis lying in the plane spanned by the holder frame. The pitch and yaw motion of the device is possible in a range of much more than +/−90°.

    Abstract translation: 用于探针头的安装件包括由保持器框架跨过的平面，其中可以相对于导弹结构并且在保持器框架内与包含至少一个检测器的平面跨越的平面成直角地执行包含至少一个检测器的设备的俯仰运动 保持框架，用于包含至少一个检测器的装置的旋转偏转运动的旋转机构围绕位于由支架框架跨过的平面中的旋转轴布置。 装置的俯仰和偏航运动可以在远大于+/- 90°的范围内。

Patent Agency Ranking