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    • 43. 发明专利
    • Satellite payload for augmentation system
    • 卫星系统的卫星付费
    • JP2013036995A
    • 2013-02-21
    • JP2012172038
    • 2012-08-02
    • Thalesテールズ
    • PEYLOTT CHRISTIAN
    • G01S19/02G01S19/08
    • G01S19/02G01S19/08
    • PROBLEM TO BE SOLVED: To provide a satellite payload for an augmentation system.SOLUTION: A payload for an augmentation satellite (600) comprises: input channels (201, 202 and 503) suitable for receiving navigation signals transmitted by at least one navigation land earth station (NLES) in a first frequency band; a plurality of output channels (206, 207, 208, 216, 217 and 218) each suitable for broadcasting navigation signals in a frequency band different from the first band and other broadcasting bands; and also a navigation processor (501). A satellite comprising such a payload and an augmentation system comprising such a satellite are also provided.
    • 要解决的问题:为增强系统提供卫星有效载荷。 解决方案:用于增强卫星(600)的有效载荷包括:适于接收由第一频带中的至少一个导航陆地地球站(NLES)发送的导航信号的输入信道(201,202和503) 多个输出通道(206,207,208,216,217和218),每个输出通道适于在与第一频带和其他广播频带不同的频带中广播导航信号; 以及导航处理器(501)。 还提供了包括这种有效载荷的卫星和包括这种卫星的增强系统。 版权所有(C)2013,JPO&INPIT
    • 44. 发明专利
    • Device for controlling light emitting diode with very high luminance dynamic range for display screen
    • 用于显示屏幕的非常高的亮度动态范围控制发光二极管的装置
    • JP2012253022A
    • 2012-12-20
    • JP2012125568
    • 2012-06-01
    • Thalesテールズ
    • GUY SCHOURENAULT FREDERIC
    • H05B37/02G02F1/13357
    • H05B33/0845H05B33/0818
    • PROBLEM TO BE SOLVED: To provide a device for controlling a light emitting diode with a very high luminance dynamic range for a display screen.SOLUTION: The general field of the present invention relates to a device for controlling luminance of a lighting system including a light emitting diode. A control device (10) is driven by a cyclic input signal (S) of a predetermined period, and each period includes an activation time (TA) representing a predetermined luminance level. The control device includes an analog electronic means (11) generating a second control signal (S) for the intensity of an electric current passing through the light emitting diode. The amplitude of the second control signal is an increasing function of the activation time in such a way that the combination of the cyclic input signal and the second signal applied to the light emitting diode gives a luminance dynamic range greater than the dynamic range of the cyclic input signal.
    • 要解决的问题:提供一种用于控制用于显示屏的非常高的亮度动态范围的发光二极管的装置。 解决方案:本发明的一般领域涉及一种用于控制包括发光二极管的照明系统的亮度的装置。 控制装置(10)由预定周期的循环输入信号(S PWM )驱动,并且每个周期包括表示预定亮度级的激活时间(TA)。 控制装置包括对通过发光二极管的电流的强度产生第二控制信号(S A-A )的模拟电子装置(11)。 第二控制信号的振幅是激活时间的增加函数,使得施加到发光二极管的循环输入信号和第二信号的组合给出大于循环输入信号的动态范围的亮度动态范围 输入信号。 版权所有(C)2013,JPO&INPIT
    • 45. 发明专利
    • System for geographical position measurement of radio signal transmitter positioned on surface and relevant distributed interference method
    • 无线电信号发射器位置表面和相关分布干扰方法的地理位置测量系统
    • JP2012252005A
    • 2012-12-20
    • JP2012125566
    • 2012-06-01
    • Thalesテールズ
    • PEYLOTT CHRISTIANMARTINURIE FRANCISTEBNE JEAN BAPTISTE
    • G01S5/02G01S5/14G01S19/14
    • G01S5/02B64G1/1085B64G1/66G01S5/06
    • PROBLEM TO BE SOLVED: To provide a system of the geometrical position measurement of a radio signal transmitter positioned on a surface and a relevant distributed interference method.SOLUTION: A system includes: artificial satellites (SAT1, SAT2, SAT3) equipped with reception antennas (ANT1, ANT2, ANT3) forming an extended interference method device; an inter-satellite relative measurement device including at least one exclusive sensor (CAPTd_1, CAPTd_2, CAPTd_3) and inter-satellite communication means (COMM1, COMM2, COMM3) for each satellite; devices (DAT1, DAT2, DAT3) for date determination of a reception signal to be distributed by the inter-satellite relative measurement device, and to be obtained on the basis of the determination of the mutual relative positions of those satellites; a second interference method device including at least one set of the antennas of the satellites; a ground base station (SBS); a device for transmitting measurement values obtained on the satellites to the ground base station; and means (DPA) for determining the absolute position of at least one of the satellites.
    • 要解决的问题:提供位于表面上的无线电信号发射器的几何位置测量系统和相关的分布式干扰方法。 解决方案:系统包括:配备有形成扩展干扰方法装置的接收天线(ANT1,ANT2,ANT3)的人造卫星(SAT1,SAT2,SAT3) 卫星间相关测量装置,其包括用于每个卫星的至少一个专用传感器(CAPTd_1,CAPTd_2,CAPTd_3)和卫星间通信装置(COMM1,COMM2,COMM3) 用于由卫星间相对测量装置分配的接收信号的日期确定的装置(DAT1,DAT2,DAT3),并且基于这些卫星的相对相对位置的确定而获得; 包括卫星的至少一组天线的第二干扰方法装置; 地面基站(SBS); 用于将在卫星上获得的测量值传送到地面基站的装置; 以及用于确定至少一个卫星的绝对位置的装置(DPA)。 版权所有(C)2013,JPO&INPIT
    • 46. 发明专利
    • Retractable planar structure, and satellite comprising the structure
    • 可收缩的平面结构和包含结构的卫星
    • JP2012192917A
    • 2012-10-11
    • JP2012057394
    • 2012-03-14
    • Thalesテールズ
    • KRAWCZYK RODOLPHE
    • B64G1/22
    • B64G1/222B64G1/407
    • PROBLEM TO BE SOLVED: To provide a retractable planar structure and a satellite comprising the structure.SOLUTION: The retractable planar structure (SPE) includes an expandable membrane (MD) anchored to N-sets of main assemblies (EP1, EP2, ..., EPK, ..., EPN) of n pieces of main rods (EPK_TP1, EPK_TP2, ..., EPK_TPn) each of which comprises an expansion means and which are joined to each other at the ends using n-1 pieces of joints (EPK_A1, EPK_A2, ..., EPK_An-1) and at least one set of intermediate assemblies (EI1, EI2, ..., EIK, ..., EIN) of n-pieces of intermediate rods (EIK_TI1, EIK_TI2, ..., EIK_TIn) which are joined to each other at ends using n-1 pieces of joints (EIK_A1, EIK_A2, ..., EIK_An-1) and which are smaller in volume than those of the main rods.
    • 要解决的问题:提供一种可缩回的平面结构和包括该结构的卫星。 解决方案:可伸缩平面结构(SPE)包括锚定在N组主杆(EP1,EP2,...,EPK,...,EPN)上的n组主杆的可膨胀膜(MD) (EPK_A1,EPK_A2,...,EPK_An-1)的端部使用扩展装置(EPK_TP1,EPK_TP2,...,EPK_TPn) 至少一组中间组件(EI1,EI2,...,EIK,...,EIN)的n个中间棒(EIK_TI1,EIK_TI2,...,EIK_TIn)在端部彼此连接使用 n-1个接头(EIK_A1,EIK_A2,...,EIK_An-1),体积小于主杆。 版权所有(C)2013,JPO&INPIT
    • 47. 发明专利
    • Simplified test bench for telescope, and telescope allowing autotesting
    • 简化的TELESCUTE测试台,以及允许自动化的TELESCOPE
    • JP2012177920A
    • 2012-09-13
    • JP2012035408
    • 2012-02-21
    • Thalesテールズ
    • PERRIN GUILLAUMELYOTARD ARNAUDBENARD HERB
    • G02B23/16
    • G01M11/005G02B17/061G02B23/02
    • PROBLEM TO BE SOLVED: To provide a simplified test bench for a telescope, and a telescope allowing autotesting.SOLUTION: The general field of this invention relates to the optical test of a telescope type optical instrument. An instrument (100) includes an optical lens (110), a photo-detecting case (120) arranged at the focus of an optical objective lens, and at least one light source (121) disposed adjacent to the photo-detecting case, and an optical pupil of the optical objective lens has a first diameter. Testing means fundamentally comprises: a plane mirror (130) having a second diameter smaller than the first diameter; means which allows the plane mirror to be disposed so that an image of light of the light source, which is given by the optical objective lens and is reflected by the plane mirror, is focused on the photo-detecting case; and means which analyzes the received image to allow determination of the optical quality of a telescope. The plane mirror may be combined with an autonomous test bench. The plane mirror may also be part of the telescope and be incorporated in a protective hood (140) for the lens.
    • 要解决的问题:为望远镜提供简化的测试台,以及允许自动测试的望远镜。 解决方案:本发明的一般领域涉及望远镜型光学仪器的光学测试。 仪器(100)包括光学透镜(110),布置在光学物镜的焦点处的光检测壳体(120)和邻近光检测器壳体设置的至少一个光源(121),以及 光学物镜的光瞳具有第一直径。 测试手段基本上包括:具有小于第一直径的第二直径的平面镜(130) 能够使平面镜配置为使得由光学物镜给出并被平面镜反射的光源的图像聚焦在光检测壳体上的装置; 以及分析接收到的图像以允许确定望远镜的光学质量的装置。 平面镜可以与自主测试台组合。 平面镜也可以是望远镜的一部分,并且被结合在用于透镜的保护罩(140)中。 版权所有(C)2012,JPO&INPIT