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    • 13. 发明申请
    • AIRBORNE RECONNAISSANCE SYSTEM
    • AIRBORNE重新建立系统
    • WO2003102505A1
    • 2003-12-11
    • PCT/IL2003/000422
    • 2003-05-22
    • RAFAEL - ARMAMENT DEVELOPMENT AUTHORITY LTD.GREENFELD, IsraelYAVIN, ZviUHL, Bernd
    • GREENFELD, IsraelYAVIN, ZviUHL, Bernd
    • G01C11/02
    • G01S3/7864F41G5/14F41G7/2213F41G7/2253F41G7/2293G01C11/025G01C21/005G01C21/165
    • An airborne reconnaissance system comprising: (1) Gimbals having at least two degrees of freedom; (2) At least one array of light sensors positioned on the gimbals, for being directed by the same within at least two degrees of freedom; (3) Map storage means for storing at least one Digital Elevation Map of an area of interest, divided into portions; (4) Inertial Navigation System for real-time providing to a gimbals control unit navigation and orientation data of the aircraft with respect to a predefined global axes system;(5) Portion selection unit for selecting, one at a time, another area portion from the area of interest; and (6) servo means for directing the gimbals. The system uses data from the inertial navigation system and from the digital elevation map for real-time calculating direction to selected area portions, and for maintaining the direction during integration of light from the terrain, and for producing corresponding images of area portions.
    • 一种机载侦察系统,包括:(1)具有至少两个自由度的万用表; (2)定位在万向面上的至少一组光传感器,由至少两个自由度引导; (3)地图存储装置,用于存储感兴趣区域的至少一个数字高程图,被分成多个部分; (4)惯性导航系统,用于相对于预定义的全局轴系统实时提供飞行器的万向节控制单元导航和取向数据;(5)部分选择单元,用于一次一个地从另一个区域部分 感兴趣的领域 和(6)用于引导万向架的伺服装置。 该系统使用来自惯性导航系统的数据和数字高程图的实时计算方向的数据,并且用于在来自地形的光的集成期间保持方向,并且用于产生区域部分的相应图像。
    • 16. 发明申请
    • DUAL FIELD OF VIEW OPTICS
    • 双视场光学
    • WO2007015236A1
    • 2007-02-08
    • PCT/IL2006/000885
    • 2006-07-31
    • RAFAEL-ARMAMENT DEVELOPMENT AUTHORITY LTD.NIZANI, Zvi
    • NIZANI, Zvi
    • G02B17/08H04N1/48H01L27/00
    • H04N5/2254G02B13/146G02B17/0896H04N9/045
    • The invention is an optical system, which simultaneously captures two images of a scene. The system has no moving parts and each image has a different field of view. The system of the invention comprises a dichroic filter, a single detector, and additional optical elements. The dichroic filter divides the light entering the system into a first spectral range and a second spectral range. The additional optical elements focus the light that enters the system onto the planar surface of the detector, which has a surface comprising a matrix of pixels, each of which comprises at least two subpixels. One of the subpixels is sensitive to light in the first spectral range and the other is sensitive to light in the second spectral range. The first image is captured on the set of subpixels sensitive to the first spectral range and the second image is simultaneously captured on the other set of subpixels.
    • 本发明是同时捕获场景的两个图像的光学系统。 该系统没有移动部件,每个图像具有不同的视野。 本发明的系统包括二向色滤光器,单个检测器和附加的光学元件。 二向色滤光器将进入系统的光分成第一光谱范围和第二光谱范围。 附加的光学元件将进入系统的光聚焦到检测器的平面表面上,其具有包括像素矩阵的表面,每个像素包括至少两个子像素。 其中一个子像素对第一光谱范围内的光敏感,另一个对第二光谱范围内的光敏感。 在对第一光谱范围敏感的子像素组上捕获第一图像,并且在另一组子像素上同时捕获第二图像。
    • 18. 发明申请
    • AIRBORNE LASER IMAGE CAPTURING SYSTEM AND METHOD
    • AIRBORNE激光图像捕获系统和方法
    • WO2005076036A1
    • 2005-08-18
    • PCT/IL2005/000127
    • 2005-02-03
    • RAFAEL-ARMAMENT DEVELOPMENT AUTHORITY LTD.LANDAU, Uzi
    • LANDAU, Uzi
    • G01S17/89
    • G01S17/89G01S7/4811G01S17/107
    • The present invention relates to an airborne laser image capturing system which comprises: (a) A laser source and laser focal plan array, both being mounted on a same gimbals platform; (b) A pulse generator for providing a series of pulses to said laser source during a scanning period, thereby activating laser illumination by said laser source during each of said pulses, the laser source being characterized in that its illumination beam is so concentrated that each pulse provides illumination of only a portion of the expected target; (c) A scanning unit for receiving a line of sight direction to a target, and for providing to the gimbals a scanning signal for effecting a sequential stepping-scanning movement in such a manner as to scan an area in which the target is included; (d) A motion compensation unit for providing to said gimbals, in addition to said scanning signal a motion compensation signal for compensating for the aircraft motion and for the aircraft vibrations; (e) A timing unit for: (e.i) Activating, in coordination with the said scanning unit, said pulse generator during the scanning period, in order to produce over the target a series of illumination spots, each relating to one of said laser pulses, and wherein each of said spots overlaps at least a portion of one or more adjacent spots; and (e.ii) Activating said laser focal plan array during the illumination of the target by each specific pulse in order to capture many of distinct spot-images, each relating to one illumination pulse; (f) A memory unit for receiving from said focal plan array the captured spot-images, and for storing them; (g) A correlating unit for correlating images stored in said memory by finding similarity between features of overlapping portions of neighboring spot-images; and (h) A combining unit receiving information from said correlating unit for combining the spot-images to form a complete image of the scanned area.
    • 本发明涉及一种机载激光图像拍摄系统,包括:(a)激光源和激光焦点计划阵列,两者都安装在相同的万向台上; (b)脉冲发生器,用于在扫描周期期间向所述激光源提供一系列脉冲,从而在每个所述脉冲期间激活所述激光源的激光照明,其特征在于,其照明光束如此集中,使得每个 脉冲仅提供预期目标的一部分的照明; (c)用于接收目标方向的扫描单元,用于向万用表提供扫描信号,以进行顺序的步进扫描运动,以扫描包含目标的区域; (d)运动补偿单元,除了所述扫描信号之外还向所述万向节提供用于补偿飞行器运动和飞行器振动的运动补偿信号; (e)定时单元,用于:(ei)在扫描周期期间与所述扫描单元协调地激活所述脉冲发生器,以便在目标上产生一系列照明点,每个照明点与所述激光脉冲之一 ,并且其中每个所述斑点与一个或多个相邻斑点的至少一部分重叠; 和(e.ii)在每个特定脉冲的目标照射期间激活所述激光焦点计划阵列,以便捕获许多与一个照明脉冲相关的不同的斑点图像; (f)存储单元,用于从所述焦点计划阵列接收捕获的斑点图像并存储它们; (g)相关单元,用于通过发现相邻斑点图像的重叠部分的特征之间的相似性来使存储在所述存储器中的图像相关; 以及(h)组合单元,从所述相关单元接收用于组合所述点图像以形成所述扫描区域的完整图像的信息。