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    • 3. 发明申请
    • METHOD FOR DESPECKLING OF SINGLE-LOOK DUAL-POLARIZATION SYNTHETIC APERTURE RADAR (SAR) DATA
    • 单点双极化合成孔径雷达(SAR)数据剔除方法
    • WO2011070538A3
    • 2011-12-01
    • PCT/IB2010055729
    • 2010-12-10
    • EADS SINGAPORE PTE LTDLEE KEN-YOONGBRETSCHNEIDER TIMO
    • LEE KEN-YOONGBRETSCHNEIDER TIMO
    • G01S13/90
    • G01S13/90G01S2013/9076
    • The application discloses a method for despeckling synthetic aperture radar (SAR) images. An SAR image is received. The SAR image comprises pixels which are represented by two dimensional complex valued input vectors. Each input vector comprises a horizontal and a vertical polarization value. For each pixel of a multitude of the pixels, at least one feature strength parameter is calculated. For each pixel of the multitude of the pixels, a dual polarization output matrix Z out is calculated from at least one input vector. If at least one of a predetermined subset of the feature strength parameters has its maximum value, the dual polarization output matrix Z_out is set equal to a dual polarization input matrix Z_in of a corresponding input vector. Otherwise, the dual polarization output matrix Z_out is set equal to a weighted average of dual polarization matrices, the dual polarization matrices comprising a first dual polarization matrix Z struct and a second dual polarization matrix Z_radius. The calculated dual polarization output matrix Z_out is output to an output destination.
    • 该申请公开了一种用于去合成孔径雷达(SAR)图像的方法。 SAR图像被接收。 SAR图像包括由二维复数值输入向量表示的像素。 每个输入矢量包括水平和垂直极化值。 对于多个像素中的每个像素,计算至少一个特征强度参数。 对于多个像素中的每个像素,从至少一个输入矢量计算双偏振输出矩阵Z out。 如果特征强度参数的预定子集中的至少一个具有其最大值,则将双偏振输出矩阵Z_out设置为等于对应输入矢量的双偏振输入矩阵Z_in。 否则,双偏振输出矩阵Z_out被设置为等于双偏振矩阵的加权平均,双偏振矩阵包括第一双偏振矩阵Z struct和第二双偏振矩阵Z_radius。 计算出的双偏振输出矩阵Z_out被输出到输出目的地。
    • 4. 发明申请
    • METHOD AND SYSTEM FOR AUTOMATIC LOGGING OF FLIGHT-HOUR DATA OF COMPONENTS IN AIRCRAFTS
    • 航空器组件航空数据自动登录的方法和系统
    • WO2011070536A2
    • 2011-06-16
    • PCT/IB2010055726
    • 2010-12-10
    • EADS SINGAPORE PTE LTDEADS DEUTSCHLAND GMBHNEUBAUER FRANKKRISHNA ANOOP KUMAR
    • NEUBAUER FRANKKRISHNA ANOOP KUMAR
    • B64D45/00B64C13/18G01C23/00G06F17/00
    • G07C5/02G07C5/008
    • The application provides a component flight-hour updating module (10) of an aircraft. The module comprises at least one Radio Frequency Identifier (RFID) tag (16; 54) being attached to at least one component (15) and a component flight-hour updating device. The RFID tag (16; 54) stores component flight-hour information. The component flight-hour updating device (21) comprises an RFID antenna, a first port, a memory unit, a processor unit, and a second port. The RFID antenna is communicatively connected to the RFID tag (16; 54) to retrieve the component flight-hour information. The first port is for communicatively connecting to an onboard flight-hour measurement device to retrieve aircraft flight-hour information. The memory unit stores the component flight-hour information and the aircraft flight- hour information. The processor unit determines updated component flight-hour information using the stored component flight-hour information and the stored aircraft flight-hour information. The RFID antenna also stores the updated component flight-hour information in the RFID tag (16; 54). The second port is communicatively connected to a device for displaying the at least one updated component flight-hour information.
    • 该应用程序提供飞行器的组件飞行小时更新模块(10)。 所述模块包括附接到至少一个组件(15)和组件飞行小时更新设备的至少一个射频识别器(RFID)标签(16; 54)。 RFID标签(16; 54)存储组件飞行时间信息。 部件飞行小时更新装置(21)包括RFID天线,第一端口,存储单元,处理器单元和第二端口。 RFID天线通信地连接到RFID标签(16; 54)以检索组件飞行小时信息。 第一个端口用于通信地连接到车载飞行小时测量装置以检索飞行器飞行小时信息。 存储单元存储组件飞行时间信息和飞行器飞行时间信息。 处理器单元使用所存储的组件飞行小时信息和所存储的飞机飞行小时信息来确定更新的组件飞行小时信息。 RFID天线还将更新的组件飞行小时信息存储在RFID标签中(16; 54)。 第二端口通信地连接到用于显示至少一个更新的组件飞行小时信息的设备。