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公开(公告)号：EP2602778B1
公开(公告)日：2014-03-19
申请号：EP12195179.2
申请日：2012-11-30
CPC分类号： G08G5/0082 , G01S5/0027 , G01S2205/003 , G08G5/0008 , G08G5/0013 , G08G5/0078
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公开(公告)号：EP2503708B1
公开(公告)日：2015-04-15
申请号：EP12160651.1
申请日：2012-03-21
CPC分类号： H04B7/0857 , H04B7/0808 , H04B7/12
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公开(公告)号：EP2503707A1
公开(公告)日：2012-09-26
申请号：EP12160455.7
申请日：2012-03-20
IPC分类号： H04B7/12
CPC分类号： H04B7/12 , H04B7/068 , H04B7/0814 , H04B7/082 , H04B7/0874
摘要： A system comprises an outer shell having an inner spherical cavity and an inner sphere located in the spherical cavity. The inner sphere comprises a sensor; at least three transmit antennas; and at least three transmitters each coupled to the sensor and to a respective one of the at least three transmit antennas. The system comprises at least three receive antennas each located in the spherical cavity, wherein each of the at least three receive antennas is frequency matched to a transmit frequency of a respective one of the at least one transmit antennas. The system also comprises at least three receivers each coupled to a respective one of the at least three receive antennas and a data selection logic circuit configured to select at least one signal from the signals received from each of the at least three receivers based on the respective signal quality of the received signals.
摘要翻译： 系统包括具有内球面腔和位于球形空腔内的内球的外壳。 内球包括传感器; 至少三个发射天线; 以及至少三个发射机，每个发射机分别耦合到所述传感器和所述至少三个发射天线中的相应一个发射天线。 该系统包括至少三个接收天线，每个接收天线各自位于球形腔中，其中至少三个接收天线中的每一个接收天线与至少一个发射天线中的相应一个发射天线的发射频率频率匹配。 所述系统还包括至少三个接收器，每个接收器分别耦合到所述至少三个接收天线中的相应一个接收天线;以及数据选择逻辑电路，被配置为基于从所述至少三个接收机中的每一个接收的信号从所接收的信号中选择至少一个信号 接收信号的信号质量。
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4.发明公开Systems and methods for receiving aircraft position reports 有权Systeme und Verfahren zum Empfangen von Flugzeugpositionsberichten
公开(公告)号：EP2602778A1
公开(公告)日：2013-06-12
申请号：EP12195179.2
申请日：2012-11-30
CPC分类号： G08G5/0082 , G01S5/0027 , G01S2205/003 , G08G5/0008 , G08G5/0013 , G08G5/0078
摘要： One embodiment is directed to an aircraft position report system. The system comprises a satellite, an aircraft position reporting receiver mounted on the satellite, an antenna element mounted on the satellite, and an antenna interface mounted on the satellite. The aircraft position reporting receiver receives aircraft position reports through the antenna element by associating a spot beam with a narrow coverage area. The aircraft position reports are derived from a signal produced by the antenna element. The antenna interface changes the narrow coverage area associated with the spot beam to receive aircraft position reports from a wide coverage region within a reporting period. In one exemplary embodiment, the antenna interface mechanically steers the spot beam for each receiver to one of the narrow coverage areas. In another exemplary embodiment, the antenna interface electronically steers the spot beam for each receiver to one of the narrow coverage areas.
摘要翻译： 一个实施例涉及飞机位置报告系统。 该系统包括卫星，安装在卫星上的飞机位置报告接收器，安装在卫星上的天线元件和安装在卫星上的天线接口。 飞机位置报告接收机通过将点波束与窄覆盖区域相关联而通过天线元件接收飞机位置报告。 飞机位置报告是由天线元件产生的信号导出的。 天线接口改变与点波束相关联的窄覆盖区域，以在报告周期内从宽覆盖区域接收飞机位置报告。 在一个示例性实施例中，天线接口将每个接收机的点波束机械地引导到窄覆盖区域之一。 在另一个示例性实施例中，天线接口将每个接收机的点波束电子地引导到窄覆盖区域之一。
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公开(公告)号：EP2503708A1
公开(公告)日：2012-09-26
申请号：EP12160651.1
申请日：2012-03-21
CPC分类号： H04B7/0857 , H04B7/0808 , H04B7/12
摘要： A system comprises an outer shell having an inner spherical cavity and an inner sphere located in the spherical cavity. The inner sphere comprises a sensor; at least one transmit antenna; and at least one transmitter coupled to the sensor and to a respective one of the at least one transmit antenna. The system also comprises a first receive antenna located in the spherical cavity; a second receive antenna located in the spherical cavity; and a receiver located outside of the outer shell. The receiver is configured to determine the signal to noise ratio of a first signal received at the first receive antenna and the signal to noise ratio of a second signal received at the second receive antenna; and to combine the first and second signals based on the respective signal to noise ratios such that interference due to multi-path signals in the spherical cavity is reduced.
摘要翻译： 系统包括具有内球面腔和位于球形空腔内的内球的外壳。 内球包括传感器; 至少一个发射天线; 以及耦合到所述传感器和所述至少一个发射天线中的相应一个的至少一个发射机。 该系统还包括位于球形腔中的第一接收天线; 位于球形腔中的第二接收天线; 以及位于外壳外部的接收器。 接收机被配置为确定在第一接收天线处接收的第一信号的信噪比和在第二接收天线处接收的第二信号的信噪比; 并且基于相应的信噪比来组合第一和第二信号，使得减小了由于球形腔中的多径信号引起的干扰。
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