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    • 1. 发明授权
    • Location system for a flying craft
    • 飞行器的定位系统
    • US09348011B2
    • 2016-05-24
    • US13607739
    • 2012-09-09
    • Pascal CornicPatrick GarrecJean-Paul Artis
    • Pascal CornicPatrick GarrecJean-Paul Artis
    • G01S5/02G01S1/14F41G7/30
    • G01S5/0247F41G7/301F41G7/305G01S1/14
    • A location and guidance system including a flying craft and a reception device. The flying craft includes a plurality of antennas distributed around its fuselage and emitting rearwards with rectilinear polarization, the emitted signals being specific to each antenna, the positions and the dimensions of the antennas being configured such that the body of the flying craft avoids by masking for at least one antenna the reflections of the signal emitted by this antenna off the ground or off lateral obstacles whatever the position of the flying craft. The reception device is placed substantially on a trajectory axis of the flying craft and configured to be oriented to sight the rear thereof and includes at least two single-pulse antennas operating in orthogonal planes determines a position of the flying craft by analyzing the emitted signals received by the antennas of the reception device.
    • 包括飞行器和接收装置的位置和引导系统。 飞行器包括分布在其机身周围并以直线偏振向后发射的多个天线,所发射的信号是特定于每个天线的,天线的位置和尺寸被配置为使得飞行器的主体通过屏蔽来避免 至少有一个天线,由天线发射的信号离开地面或侧向障碍物的反射,无论飞行器的位置如何。 接收装置基本上放置在飞行器的轨迹轴上并且被配置为朝向其后方瞄准,并且包括在正交平面中操作的至少两个单脉冲天线通过分析所接收到的发射信号来确定飞行器的位置 通过接收设备的天线。
    • 3. 发明申请
    • DEVICE AND METHOD FOR LOCATING A MOBILE APPROACHING A SURFACE REFLECTING ELECTROMAGNETIC WAVES
    • 用于定位移动面反射电磁波的装置和方法
    • US20100085237A1
    • 2010-04-08
    • US12531657
    • 2008-03-14
    • Pascal CornicEric BarrauxPatrick Garrec
    • Pascal CornicEric BarrauxPatrick Garrec
    • G01S13/91
    • G01S13/913G01S13/685
    • Device and a method for locating a mobile object approaching a surface reflecting electromagnetic waves. The location device includes an emission antenna and a reception antenna. The emission antenna has one or more emission positions emitting a detection signal toward the mobile object. The reception antenna has at least one column of one or more reception positions, receiving a signal transmitted by the mobile object. An emission of the detection signal is activated on each emission position. An emission position that produces a detection by the reception antenna, of the signal of maximum energy transmitted by the mobile object, is selected to track the mobile object. One or more signals of maximum energy, received by one or more reception positions, are used to angularly locate the mobile object. The invention can be used to determine the position of an aircraft in the final landing phase for a guidance device.
    • 用于定位接近反射电磁波的表面的移动物体的装置和方法。 定位装置包括发射天线和接收天线。 发射天线具有朝向移动物体发射检测信号的一个或多个发射位置。 接收天线具有至少一列一个或多个接收位置,接收由移动对象发送的信号。 在每个发射位置激活检测信号的发射。 选择由接收天线产生由移动对象发送的最大能量的信号的发射位置,以跟踪移动对象。 使用由一个或多个接收位置接收的最大能量的一个或多个信号来角度地定位移动对象。 本发明可以用于确定飞机在用于引导装置的最终着陆阶段中的位置。
    • 4. 发明申请
    • AUTONOMOUS AND AUTOMATIC LANDING SYSTEM FOR DRONES
    • 自动和自动登陆系统
    • US20090055038A1
    • 2009-02-26
    • US12095768
    • 2006-12-01
    • Patrick GarrecPascal Cornic
    • Patrick GarrecPascal Cornic
    • G05D1/00
    • G01S13/825G01S11/10G01S13/003G01S13/88G01S13/913G05D1/0676
    • The invention relates to an automatic aircraft landing guidance system having an electromagnetic detecting and locating device, positioned on the ground and a first multifunction transmitting/receiving radiofrequency beacon, on board each guided aircraft and transmitting in particular a continuous wave. The detecting and locating device uses the continuous wave transmitted by the beacon to perform a passive locating intended to improve the accuracy of the measurement of the angular position of the aircraft. It also comprises means for generating and periodically transmitting to the aircraft, via the beacon, information enabling said aircraft to rejoin an optimum landing path from its position. The invention applies more particularly to the guidance of autonomous and automatic aircraft such as drones in the approach and landing phase.
    • 本发明涉及一种自动飞机着陆引导系统,其具有位于地面上的电磁检测和定位装置,以及在每个引导的飞行器上的第一多功能发射/接收射频信标,并且特别地传输连续波。 检测和定位装置使用由信标发射的连续波来执行被动定位,旨在提高飞行器的角位置的测量精度。 它还包括用于通过信标产生和周期性地向飞机发送信息,使得所述飞机能够从其位置重新加入最佳着陆路径的信息。 本发明更具体地适用于自主和自动飞机如进近和着陆阶段的无人机的指导。
    • 8. 发明授权
    • System for measuring the radial speed of a moving body
    • 用于测量移动体的径向速度的系统
    • US08902106B2
    • 2014-12-02
    • US13309322
    • 2011-12-01
    • Patrick GarrecPascal CornicStéphane Kemkemian
    • Patrick GarrecPascal CornicStéphane Kemkemian
    • G01S3/02G01S1/44G01P3/36G01S11/10
    • G01P3/36G01S11/10
    • A system for measuring the radial speed of a moving body in a line of sight determined for a referential position is disclosed. The system includes an emitter assembly for emitting a signal and a referential receiver assembly dedicated to reception of the signal. The emitter assembly is disposed on a first of the elements of a group formed by the moving body and the referential position. The receiver assembly is disposed on a second of the elements of the group. The emitter assembly is able to emit a signal on at least two emission frequencies, where the emission frequencies are separated by a chosen emission frequency gap. The system also includes an analyzer configured to analyze the signal received by the receiver assembly, and to measure the reception frequency gap separating the signal reception frequencies to calculate the radial speed of the moving body according to a function of the reception frequency gap and emission frequency gap.
    • 公开了一种用于测量在参考位置确定的视线中的移动体的径向速度的系统。 该系统包括用于发射信号的发射器组件和专用于接收信号的参考接收器组件。 发射器组件设置在由移动体和参考位置形成的组中的第一元件上。 接收器组件设置在组中的第二个元件上。 发射器组件能够发射至少两个发射频率的信号,其中发射频率被选择的发射频率间隙分开。 该系统还包括分析器,其被配置为分析由接收器组件接收的信号,并且测量分离信号接收频率的接收频率间隙,以根据接收频率间隙和发射频率的函数来计算移动体的径向速度 间隙。
    • 10. 发明授权
    • Method and system for assisting in the landing or the decking of a light aircraft
    • 辅助轻型飞机着陆或甲板的方法和系统
    • US08768542B2
    • 2014-07-01
    • US12783972
    • 2010-05-20
    • Patrick GarrecPascal Cornic
    • Patrick GarrecPascal Cornic
    • G06F7/70
    • G01S13/913B64F1/20G01C23/005G01S13/825G01S13/86G05D1/0676G08G5/0013G08G5/0021G08G5/025
    • The present invention relates to a method and a system for assisting in the landing or the decking of a light aircraft, the method being implemented by a system comprising a device on the ground for locating the aircraft, the aircraft having an onboard signal sender, the method comprising at least the following steps: the locating device on the ground uses signals sent by the sender to determine the position and/or movement of the aircraft; said device transmits the previously determined aircraft position and/or movement data to the aircraft; display means show at least some of said data made accessible to the pilot of the aircraft. The invention applies in particular to the field of civil light aeronautics, notably for facilitating the landing of pleasure aeroplanes, small transport aeroplanes and helicopters.
    • 本发明涉及一种用于辅助轻型飞机着陆或甲板的方法和系统,该方法由包括在地面上用于定位飞行器的设备的系统来实现,飞行器具有车载信号发送器, 方法至少包括以下步骤:地面上的定位装置使用由发送者发送的信号来确定飞机的位置和/或移动; 所述设备将先前确定的飞机位置和/或移动数据传输到飞行器; 显示装置显示飞机的飞行员可访问的至少一些所述数据。 本发明尤其适用于民用轻型航空领域,特别是为了便利着陆飞机,小型运输飞机和直升机。