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    • 52. 发明申请
    • Ranging system for determining ranging information of a spacecraft
    • 用于确定航天器测距信息的测距系统
    • US20040140930A1
    • 2004-07-22
    • US10675408
    • 2003-09-29
    • Guy Harles
    • G01S001/24H04L007/00
    • H04B7/18597G01S5/14G01S13/46G01S13/878G01S2013/466
    • The invention refers to a ranging system for determining ranging information of a spacecraft carrying a component of a communication channel. In order to provide a ranging system for determining ranging information of a satellite carrying a transponder as well as to provide a method thereof which yield a sufficient accuracy without causing further costs when narrow spot beams by the transponder are used, a ranging system according to the invention comprises a plurality of receiving stations at different locations on earth, wherein each receiving station is arranged for receiving a reference signal from said component; synchronisation means for providing a synchronised time base between the plurality of receiving stations; calculation means for calculating said ranging information in accordance with the propagation time of each received reference signal and with the synchronised time base; wherein at least one receiving station comprises a correlation receiver for receiving the reference signal.
    • 本发明涉及一种用于确定携带通信信道的分量的航天器的测距信息的测距系统。 为了提供一种用于确定承载应答器的卫星的测距信息的测距系统,并且提供其方法,其产生足够的精度,而不会在使用应答器的窄点波束时导致进一步的成本,根据 本发明包括在地球上不同位置处的多个接收站,其中每个接收站被布置为从所述组件接收参考信号; 同步装置,用于在所述多个接收站之间提供同步的时基; 计算装置,用于根据每个接收到的参考信号的传播时间和同步的时基来计算所述测距信息; 其中至少一个接收站包括用于接收参考信号的相关接收器。
    • 53. 发明申请
    • Method and apparatus for estimating velocity of a terminal in a wireless communication system
    • 用于估计无线通信系统中的终端的速度的方法和装置
    • US20020177450A1
    • 2002-11-28
    • US10044194
    • 2001-10-26
    • Alkinoos Vayanos
    • H04Q007/20
    • G01S19/52G01S11/10G01S2013/466
    • Techniques to estimate the velocity of a terminal in a wireless communication system. Movement by the terminal results in a Doppler shift in the frequency of each transmitted signal received at the terminal. In one method, the positions of the terminal, a base station, and each of two or more satellites are initially determined. A residual rate of change of pseudo-range may also be determined for each satellite, e.g., based on (1) an estimated baseband frequency error that includes the Doppler frequency shift due to the terminal's movement and (2) an estimated Doppler frequency shift due to movement by the satellite. A set of equations is then formed based on the determined positions of the terminal, the base station, and the satellites and the determined residual rates of change of pseudo-ranges for the satellites. The velocity of the terminal may thereafter be estimated based on the set of equations.
    • 估计无线通信系统中终端速度的技术。 由终端的移动导致在终端处接收的每个发送信号的频率的多普勒频移。 在一种方法中,首先确定终端,基站和两个或更多个卫星中的每一个的位置。 也可以针对每个卫星确定残差的残差率,例如,基于(1)由于终端的运动而包括多普勒频移的估计的基带频率误差,以及(2)估计的多普勒频移 由卫星运动。 然后基于确定的终端,基站和卫星的位置以及所确定的用于卫星的伪距变化的剩余速率来形成一组方程式。 此后可以基于方程组来估计终端的速度。
    • 54. 发明申请
    • Method and apparatus for determining the position of a mobile communication device
    • 用于确定移动通信设备的位置的方法和装置
    • US20010053699A1
    • 2001-12-20
    • US09777625
    • 2001-02-06
    • Dennis D. McCradyPeter CummiskeyLawrence J. DoyleHoward Forstrom
    • H04Q007/20
    • H04W64/00G01S5/021G01S5/0215G01S5/0221G01S5/0294G01S5/14G01S13/46G01S2013/466
    • A position location communication system determines the position of a mobile master radio using a round-trip messaging scheme in which the time of arrive (TOA) of ranging signals is accurately determined to yield the range estimates required to calculate the position of the mobile radio. The master radio transmits ranging signals to plural reference radios which respond by transmitting reply ranging signals. Upon reception of the reply ranging signal, the master radio determines the range to the reference radio from the signal propagation time. Any combination of fixed or mobile radios having known positions can be used as the reference radios for another mobile radio in the system. Individual radios do not need to be synchronized to a common time reference, thereby eliminating the need for highly accurate system clocks. Errors in TOA estimates are minimized by performing internal delay calibration, Doppler compensation, leading-edge-of-the-signal curve fitting and frequency diversity techniques.
    • 位置定位通信系统使用其中准确地确定测距信号的到达时间(TOA)的往返消息方式来确定移动主控无线电的位置,以产生计算移动无线电的位置所需的范围估计。 主无线电发送测距信号到通过发送应答测距信号进行响应的多个参考无线电。 在接收到应答测距信号时,主无线电从信号传播时间确定到参考无线电的范围。 具有已知位置的固定或移动无线电的任何组合可用作系统中另一移动无线电的参考无线电。 单个无线电不需要与公共时间参考同步,从而不需要高精度的系统时钟。 通过执行内部延迟校准,多普勒补偿,信号前沿曲线拟合和频率分集技术,TOA估计的误差被最小化。
    • 57. 发明授权
    • Method and apparatus for radar measurement of ball in play
    • 雷达测量球的方法和装置
    • US5138322A
    • 1992-08-11
    • US747380
    • 1991-08-20
    • Jerry A. Nuttall
    • Jerry A. Nuttall
    • A63B43/00A63B71/06G01S13/38G01S13/46G01S13/87G01S13/88
    • G01S13/87A63B71/0605G01S13/46A63B2071/0611A63B2225/54A63B43/00G01S2013/466
    • A system for continuously and precisely measuring the positions of a generally symmetrical object, e.g., a tennis ball, in motion in a predefined three-dimensional region, e.g., a tennis court, which transmits multiple radar signals from first, second, and third, spaced antenna devices, respectively, into the three-dimensional region. Multiple return signals are sensed and are compared with the transmitted signals to determine the phases of the return signals, to thereby obtain ambiguous ranges of the object. Ambiguities are removed by using the Chinese Remainder Theorem to obtain less-ambiguous ranges. Time-of-arrival range information is used in conjuction with the less-ambiguous ranges to provide unambiguous ranges over the range of interest. The unambiguous ranges are used to compute three-dimensional coordinates of the object that are accurate to within approximately 0.1 inches. A mathematical model defining boundaries of the three-dimensional region is completed by placing signal reflector devices on various boundary points of the three-dimensional region, and transmitting the radar signals when the object is not in the three-dimensional region. Coordinates of a projected trajectory are computed and compared with the actual coordinatres of the object, and certain characteristics are computed therefrom. Calibration of the system is maintained by placing signal reflector devices at various fixed locations within the region of interest and the return signals are processed to obtain an initial survey of the region and then to periodically resurvey the region.
    • 一种用于在预定义的三维区域(例如,从第一,第二和第三传送多个雷达信号的网球场)连续且精确地测量大致对称的物体(例如网球)的位置的系统, 间隔天线装置分别进入三维区域。 感测多个返回信号并将其与所发送的信号进行比较以确定返回信号的相位,从而获得对象的不明确的范围。 通过使用中国剩余定理来获取不太明确的范围来消除歧义。 到达时间范围信息与较不明确的范围结合使用,以在感兴趣的范围内提供明确的范围。 使用明确的范围来计算准确到大约0.1英寸内的物体的三维坐标。 通过将信号反射器装置放置在三维区域的各个边界点上,并且当物体不在三维区域时传输雷达信号,从而完成定义三维区域边界的数学模型。 计算投影轨迹的坐标,并与对象的实际坐标进行比较,并从中计算出某些特征。 通过将信号反射器装置放置在感兴趣的区域内的各个固定位置来维持系统的校准,并处理返回信号以获得该区域的初始调查,然后周期性地重新调整该区域。
    • 58. 发明授权
    • Dual satellite navigation system
    • 双卫星导航系统
    • US5017926A
    • 1991-05-21
    • US446979
    • 1989-12-05
    • William G. AmesIrwin M. JacobsLindsay A. Weaver, Jr.Klein S. Gilhousen
    • William G. AmesIrwin M. JacobsLindsay A. Weaver, Jr.Klein S. Gilhousen
    • G01S5/12G01S5/14G01S13/87G01S19/00G01S19/01G01S19/38G01S19/48H04B7/185
    • G01S19/00G01S13/46G01S13/876G01S19/38G01S5/14G01S2013/466
    • A method and system for determining the position of an object using a fixed station and a plurality of earth orbit satellites whose positions are known. Separate periodic signals are transmitted from the fixed station via first and second satellites to the object whose postion is to be determined. The phase offset in periodic characteristics of the periodic signals as received from the first and second satellites is measured at the object. The phase offset corresponds to a relative time difference in propagation of the signals traveling two different paths to the object. The object transmits via the first satellite a return signal indicative of the measured relative time difference. This return signal is activated some time in the future according to the object local time, which is slaved to receipt of the periodic signal sent through the first satellite. This future time is the start of the particular time period as decided by the fixed station's schedule. At the fixed station, an instantaneous round trip delay, determined by the time offset of the current transmission clock time relative to the receive clock time of reception of the return signal, along with the measured relative time difference sent back on the return signal, is used to calculate the distances between the first and second satellites to the object. From these distances the position of the object is calculated.
    • 一种用于使用固定站和位置已知的多个地球轨道卫星来确定物体的位置的方法和系统。 分离的周期信号从固定站经由第一和第二卫星发送到要确定位置的对象。 在物体处测量从第一和第二卫星接收的周期性信号的周期特性中的相位偏移。 相位偏移对应于传播到对象的两个不同路径的信号的传播的相对时间差。 物体经由第一卫星发送指示所测量的相对时间差的返回信号。 该返回信号在将来根据对象本地时间被激活一段时间,该对象本地时间被接收通过第一卫星发送的周期信号。 这个未来时间是由固定电台的时间表决定的特定时间段的开始。 在固定站,由当前传输时钟时间相对于接收返回信号的接收时钟时间的时间偏移确定的瞬时往返延迟以及在返回信号上发回的测量的相对时间差是 用于计算第一和第二卫星与物体之间的距离。 从这些距离计算物体的位置。
    • 59. 发明授权
    • Short range ranging system
    • 短程测距系统
    • US4833480A
    • 1989-05-23
    • US916696
    • 1986-10-08
    • Ronald J. PalmerLeonard Fischer
    • Ronald J. PalmerLeonard Fischer
    • G01S13/87
    • G01S13/876G01S13/46G01S2013/466
    • An accurate ranging system for position determination of a mobile unit using trilateralization. A pair of active reflectors return signals transmitted by the mobile unit in phase at the reflectors, after compensating for interval circuit delay. The mobile unit compares the phases and determines mutual distances and thus its position. The invention includes a two frequency technique for compensating for inaccuracies introduced at distances in excess of one wavelength and for inaccuracies observed at a large multiple of wavelengths, and also includes means for dynamically compensating for drift.
    • 一种使用三边移动单元进行位置确定的精确测距系统。 一对有源反射器在补偿间隔电路延迟之后,在移动单元同时返回在反射器处相位发送的信号。 移动单元比较相位并确定相互距离并因此确定其位置。 本发明包括用于补偿在超过一个波长的距离处引入的不准确性的两频技术,以及用于在大的多个波长处观察到的不准确性,并且还包括用于动态补偿漂移的装置。
    • 60. 发明授权
    • Radar selective interrogation system
    • 雷达选择询问系统
    • US4137531A
    • 1979-01-30
    • US796336
    • 1977-05-12
    • Christopher Pell
    • Christopher Pell
    • G01S5/14G01S19/48G01S9/56
    • G01S5/14G01S13/46G01S13/782G01S2013/466
    • An aircraft ground movement monitoring system is provided similar to that described in co-pending U.S. patent application Ser. No. 608,214, now U.S. Pat. No. 4,109,248, that makes use of an aircraft's existing SSR transponder in a hyperbolic selective interrogation technique to monitor an aircraft's position on an airfield in which, in order to overcome the problems particularly involving spurious mode C (height) interrogations that arise in long base-line systems, it is arranged that transponders that would be spuriously interrogated are interrogated first and that the required transponder is interrogated before the already interrogated transponders have finished replying.
    • 飞机地面运动监测系统的提供类似于共同未决的美国专利申请 第608,214号,现为美国专利 第4,109,248号文件,利用飞机现有的双相选择性询问技术中的SSR转发器来监控飞机在机场上的位置,其中为了克服特别涉及在长基地中产生的杂散模式C(高度)询问的问题 在线系统中,首先询问将被询问的转发器,并且在已经询问的应答器完成应答之前询问所需的应答器。