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    METHOD AND APPARATUS FOR DETERMINING A POSITION OF USER EQUIPMENT, AND AN ANTENNA SET THEREFOR
    2.
    发明申请
    METHOD AND APPARATUS FOR DETERMINING A POSITION OF USER EQUIPMENT, AND AN ANTENNA SET THEREFOR 有权
    用于确定用户设备位置的方法和装置及其天线组

    公开(公告)号：US20140320337A1

    公开(公告)日：2014-10-30

    申请号：US13872025

    申请日：2013-04-26

    申请人： TELEFONAKTIEBOLAGET L M ERICSSON (PUBL)

    发明人： Lee Jihoon ,  Kim Junghoon ,  Lee Konju

    IPC分类号： G01S1/44

    CPC分类号： G01S5/0252 ,  G01S1/12 ,  G01S1/14 ,  G01S1/44 ,  G01S1/58 ,  G01S3/58

    摘要： There is provided a method for positioning of user equipment. The method for positioning of user equipment, includes: receiving, by the user equipment, a signal from an external antenna, the signal being radiated in a cyclic pattern; measuring, by the user equipment, strength of the received signal, characterizing, by the user equipment, the measured strength to form a signal pattern over a time period; and determining a position of the user equipment based on the signal pattern.

    摘要翻译： 提供了一种用于定位用户设备的方法。 用户设备的定位方法包括：由用户设备接收来自外部天线的信号，所述信号以循环模式辐射; 由用户设备测量接收信号的强度，由用户设备表征测量的强度以在一段时间内形成信号模式; 以及基于所述信号模式确定所述用户设备的位置。

    SYSTEM FOR THE RELATIVE NAVIGATION OF AIRCRAFT AND SPACECRAFT USING A PHASED ARRAY ANTENNA
    4.
    发明申请
    SYSTEM FOR THE RELATIVE NAVIGATION OF AIRCRAFT AND SPACECRAFT USING A PHASED ARRAY ANTENNA 有权
    使用平面阵列天线进行飞机相关导航系统

    公开(公告)号：US20060232470A1

    公开(公告)日：2006-10-19

    申请号：US11104851

    申请日：2005-04-13

    申请人： Brian Mallick

    发明人： Brian Mallick

    IPC分类号： G01S1/08

    CPC分类号： G01S1/12 ,  G01S11/06 ,  G01S13/785

    摘要： A system for the relative navigation of aircraft and spacecraft is disclosed which uses a series of short duration, unmodulated radio pulses transmitted from a phased array antenna. The aircraft or spacecraft whose position is to be determined from another is called as the local station, whereas the other craft with the phased array antenna system is called as the transmitting station. The local station transmits a radio query pulse to the transmitting station. In response to the radio query pulse, the transmitting station transmits a series of unmodulated radio pulses, where each radio pulse is transmitted with a three dimensional radiation pattern that is different than the three dimensional radiation patterns of the other radio pulses transmitted by the transmitting station. A receiver attached to the local station aircraft or spacecraft receives each radio pulse, generates a signal that describes the radio signal strength of the received signal and sends that signal strength number to a stored program processor which stores that signal strength number into memory. After a series of radio signals are received at the local station and at least two radio signal strength measurements are stored in memory, the stored program processor calculates the power ratio or ratios of each received radio signal strength from each radio pulse transmitted by the transmitting location. Bearing is then determined by comparing the calculated radio signal power ratios with a library of angles that correspond to specific power ratios for all radio radiation patterns transmitted. The local station also records the time elapsed from when the first radio pulse is received from the transmitting station after the radio query pulse is sent. Range is determined by dividing that elapsed time by two and multiplying that time with the speed of light.

    摘要翻译： 公开了一种用于飞机和航天器的相对导航的系统，其使用从相控阵列天线发送的一系列短持续时间，未调制的无线电脉冲。 将其位置从另一个确定的飞机或航天器称为本地站，而具有相控阵天线系统的其他飞机称为发射台。 本地站向发射台发送无线电查询脉冲。 响应于无线电查询脉冲，发射站发送一系列未调制的无线电脉冲，其中每个无线电脉冲以与由发射站发送的其他无线电脉冲的三维辐射模式不同的三维辐射模式发射 。 连接到本地飞机或航天器的接收器接收每个无线电脉冲，产生描述接收信号的无线电信号强度的信号，并将该信号强度号发送到存储该存储器的存储程序处理器。 在本地站接收到一系列无线电信号并且至少两个无线电信号强度测量值存储在存储器中之后，存储的程序处理器计算由发送位置发送的每个无线电脉冲的每个接收的无线电信号强度的功率比或比率 。 然后通过将计算的无线电信号功率比与对应于所发送的所有无线电辐射图的特定功率比的角度库进行比较来确定轴承。 本地站还记录在发送无线电查询脉冲之后从发送站接收到第一无线电脉冲之后经过的时间。 范围通过将经过的时间除以2并将该时间与光速相乘来确定。

    METHOD AND APPARATUS FOR RECOGNITION OF DEVICES
    6.
    发明申请
    METHOD AND APPARATUS FOR RECOGNITION OF DEVICES 审中-公开
    用于识别设备的方法和装置

    公开(公告)号：US20110287789A1

    公开(公告)日：2011-11-24

    申请号：US13131898

    申请日：2009-11-26

    申请人： Daiqin Yang ,  Yong Liu ,  Lei Feng ,  Zhigang Chen

    发明人： Daiqin Yang ,  Yong Liu ,  Lei Feng ,  Zhigang Chen

    IPC分类号： H04W4/00

    CPC分类号： G01S1/12 ,  H04B17/24 ,  H04B17/318

    摘要： The present invention aims to provide a technical solution for recognizing a target device from a plurality of devices as follows: sending a first and second wireless signal to a plurality of devices and determining the target device according to the signal strength differences between the first and second signal strengths. By using the technical solutions of the present invention, the “near-far-effect” caused by a single antenna can be overcome, and different offsets in the measured received signal strengths caused by the diversity of the receiving antennas can also be eliminated, and thus the accuracy of recognition is improved efficiently.

    摘要翻译： 本发明旨在提供一种用于从多个设备识别目标设备的技术方案，如下：向多个设备发送第一和第二无线信号，并根据第一和第二设备之间的信号强度差确定目标设备 信号强度。 通过使用本发明的技术方案，可以克服由单个天线引起的“近远效应”，并且也可以消除由接收天线的分集引起的测量的接收信号强度的不同偏移，并且 从而有效地提高了识别的准确性。

    Independent landing monitoring system
    7.
    发明授权
    Independent landing monitoring system 失效
    独立着陆监控系统

    公开(公告)号：US4429312A

    公开(公告)日：1984-01-31

    申请号：US286312

    申请日：1981-07-24

    申请人： John P. Chisholm

    发明人： John P. Chisholm

    IPC分类号： G01S1/12 ,  G01S13/86 ,  G01S1/16

    CPC分类号： G01S13/86 ,  G01S1/12

    摘要： An independent landing monitoring system (ILM) for guiding airborne vehicles on final approach to a landing using a ground-based beacon which transmits a sequence of pulse signals including an omnidirectional signal coded to identify its location and used for initial approach, followed by time spaced directionally radiated right/left and up/down signals used for precision guidance along the final approach path. The time spacing of the various beacon signals and their order of succession in the sequence identify the signals, and the relative intensities of paired precision guidance signals as received by the aircraft is used to provide precision indications of the location of the aircraft on the path. The beacon can be either triggered by the weather radar in the aircraft which then receives the beacon signals on its beacon mode receiver, and/or it can be triggered randomly by a noise jittered oscillator in the beacon for use by approaching aircraft equipped only with a beacon receiver but no weather radar.

    摘要翻译： 一个独立的着陆监控系统（ILM），用于引导机载车辆使用基于地面的信标最终接近着陆点，该地面信标传送一系列脉冲信号，包括编码的全向信号，以识别其位置并用于初始逼近，其次是时间间隔 定向辐射右/左和上/下信号，用于沿着最终进近路径的精确引导。 各种信标信号的时间间隔及其顺序的顺序识别信号，并且使用由飞机接收的成对的精确引导信号的相对强度来提供飞行器在路径上的位置的精确指示。 信标可以由飞机中的天气雷达触发，然后在其信标模式接收机上接收信标信号，和/或可以由信标中的噪声抖动振荡器随机触发，以便通过接近仅配备 信标接收机，但没有天气雷达。

    System for the relative navigation of aircraft and spacecraft using a phased array antenna
    9.
    发明授权
    System for the relative navigation of aircraft and spacecraft using a phased array antenna 有权
    使用相控阵天线的飞机和航天器的相对导航系统

    公开(公告)号：US07280072B2

    公开(公告)日：2007-10-09

    申请号：US11104851

    申请日：2005-04-13

    申请人： Brian Mallick

    发明人： Brian Mallick

    IPC分类号： G01S1/08

    CPC分类号： G01S1/12 ,  G01S11/06 ,  G01S13/785

    摘要： A system for the relative navigation of aircraft and spacecraft is disclosed which uses a series of short duration, unmodulated radio pulses transmitted from a phased array antenna. The aircraft or spacecraft whose position is to be determined from another is called as the local station, whereas the other craft with the phased array antenna system is called as the transmitting station. The local station transmits a radio query pulse to the transmitting station. In response to the radio query pulse, the transmitting station transmits a series of unmodulated radio pulses, where each radio pulse is transmitted with a three dimensional radiation pattern that is different than the three dimensional radiation patterns of the other radio pulses transmitted by the transmitting station. A receiver attached to the local station aircraft or spacecraft receives each radio pulse, generates a signal that describes the radio signal strength of the received signal and sends that signal strength number to a stored program processor which stores that signal strength number into memory. After a series of radio signals are received at the local station and at least two radio signal strength measurements are stored in memory, the stored program processor calculates the power ratio or ratios of each received radio signal strength from each radio pulse transmitted by the transmitting location. Bearing is then determined by comparing the calculated radio signal power ratios with a library of angles that correspond to specific power ratios for all radio radiation patterns transmitted. The local station also records the time elapsed from when the first radio pulse is received from the transmitting station after the radio query pulse is sent. Range is determined by dividing that elapsed time by two and multiplying that time with the speed of light.

    摘要翻译： 公开了一种用于飞机和航天器的相对导航的系统，其使用从相控阵列天线发送的一系列短持续时间，未调制的无线电脉冲。 将其位置从另一个确定的飞机或航天器称为本地站，而具有相控阵天线系统的其他飞机称为发射台。 本地站向发射台发送无线电查询脉冲。 响应于无线电查询脉冲，发射站发送一系列未调制的无线电脉冲，其中每个无线电脉冲以与由发射站发送的其他无线电脉冲的三维辐射模式不同的三维辐射模式发射 。 连接到本地飞机或航天器的接收器接收每个无线电脉冲，产生描述接收信号的无线电信号强度的信号，并将该信号强度号发送到存储该存储器的存储程序处理器。 在本地站接收到一系列无线电信号并且至少两个无线电信号强度测量值存储在存储器中之后，存储的程序处理器计算由发送位置发送的每个无线电脉冲的每个接收的无线电信号强度的功率比或比率 。 然后通过将计算的无线电信号功率比与对应于所发送的所有无线电辐射图的特定功率比的角度库进行比较来确定轴承。 本地站还记录在发送无线电查询脉冲之后从发送站接收到第一无线电脉冲之后经过的时间。 范围通过将经过的时间除以2并将该时间与光速相乘来确定。

    Method of directing an aerial to a receiver according to a main direction
    10.
    发明授权
    Method of directing an aerial to a receiver according to a main direction 失效
    根据主要方向将天线引导到接收机的方法

    公开(公告)号：US3997901A

    公开(公告)日：1976-12-14

    申请号：US537691

    申请日：1974-12-31

    申请人： Jacques Claude Cayzac

    发明人： Jacques Claude Cayzac

    IPC分类号： G01S1/02 ,  G01S1/12 ,  H04B7/155 ,  G01S1/14

    CPC分类号： G01S1/12 ,  G01S1/02

    摘要： An apparatus for directing an antenna has an information signal being emitted in a main direction from the antenna. Two auxiliary signals are transmitted symmetrically about the antenna, from which an error signal can be derived for alignment of the antenna.

    摘要翻译： 用于引导天线的装置具有从天线沿主方向发射的信息信号。 两个辅助信号关于天线对称地传输，由此可以导出用于对准天线的误差信号。