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    • 41. 发明申请
    • DME GROUND APPARATUS
    • DME地面设备
    • US20080297398A1
    • 2008-12-04
    • US12129032
    • 2008-05-29
    • Yukihiro Kamimura
    • Yukihiro Kamimura
    • G01S13/74G01S13/08
    • G01S13/785
    • In a DME ground apparatus, under the control of a transmission-rate monitoring control unit, the transponder unit decodes an interrogation signal it has received and generates a response signal. The transmission rate at which to transmit the response signal is monitored. If the result of the monitoring indicates that the transmission rate has reached a preset value, the response signal is transmitted from the DME ground apparatus. If the result of the monitoring indicates that the transmission rate has not reached a preset value, squitter pulses are transmitted from the DME ground apparatus.
    • 在DME地面装置中,在传输速率监视控制单元的控制下,应答器单元对接收到的询问信号进行解码并产生响应信号。 监视发送响应信号的传输速率。 如果监视结果表明传输速率已达到预设值,则响应信号从DME地面设备发送。 如果监视结果表明传输速率尚未达到预设值,则从DME地面设备传送脉冲脉冲。
    • 42. 发明授权
    • System for the relative navigation of aircraft and spacecraft using a phased array antenna
    • 使用相控阵天线的飞机和航天器的相对导航系统
    • US07280072B2
    • 2007-10-09
    • US11104851
    • 2005-04-13
    • Brian Mallick
    • Brian Mallick
    • G01S1/08
    • G01S1/12G01S11/06G01S13/785
    • 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.
    • 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。
    • 43. 发明授权
    • Single receiver wireless tracking system
    • 单接收机无线跟踪系统
    • US06683567B2
    • 2004-01-27
    • US10316860
    • 2002-12-12
    • Brian De ChamplainFrank Gerlach
    • Brian De ChamplainFrank Gerlach
    • G01S100
    • H01R13/6273G01S3/18G01S13/767G01S13/785G01S13/788H01Q3/242H01Q9/32H01Q21/205
    • A wireless tracking system consists of a wireless target including a wireless communication system for transmitting a data packet over a communication path, and a locating station for determining a position of the target. The data packet transmitted from the target includes an identification code uniquely associated with the target. The locating station includes a configurable directional antenna, a communication interval processing system, a direction processing system, and a position processing system. The communication interval processing system is in communication with the directional antenna and determines the transmission interval of the transmitted data packet over the communication path. The direction processing system determines the transmission angle of the communication path, and is in communication with the directional antenna for controlling the configuration of the directional antenna so as to facilitate the determination of the transmission angle. The position processing system is in communication with the interval processing system and the direction processing system, and determines the target position from the identification code, the transmission interval and the transmission angle.
    • 无线跟踪系统由包括用于通过通信路径发送数据分组的无线通信系统的无线目标以及用于确定目标位置的定位站组成。 从目标发送的数据分组包括与目标唯一相关联的识别码。 定位站包括可配置定向天线,通信间隔处理系统,方向处理系统和位置处理系统。 通信间隔处理系统与定向天线通信,并且确定通过通信路径发送的数据分组的传输间隔。 方向处理系统确定通信路径的传输角度,并且与用于控制定向天线的配置的定向天线通信,以便于确定传输角度。 位置处理系统与间隔处理系统和方向处理系统通信,并且从识别码,发送间隔和发送角度确定目标位置。
    • 44. 发明授权
    • DME system with broadcasting function
    • 具有广播功能的DME系统
    • US06366233B1
    • 2002-04-02
    • US09412911
    • 1999-10-05
    • Naohito Oshida
    • Naohito Oshida
    • G01S1387
    • G01S13/785G01S13/765G01S13/788
    • Frequency resources of a DME/TACAN band specified for the aircraft band are effectively utilized, and a GPS reinforcing data is overlapped onto distance information to be broadcast. A header is added to a DGPS reinforcing data, and the transmitting pulse level of a conventional ground DME system is modulated, and the data is broadcast to an airborne system. In the airborne system, a threshold value of “1” and “0” is generated by a level detecting device (5), and the start point of the data is detected by a header detecting device (6), and the reinforcing data is supplied to the airborne system. Consequently, the function of broadcasting a data by overlapping the data onto the distance information of the DME is achieved. Since the DME uses the L band, the radio interference with the existing ILS, VOR, aircraft radio transmission, and broadcasting station can be avoided.
    • 有效利用为飞机频带指定的DME / TACAN频段的频率资源,并将GPS加强数据重叠到待广播的距离信息上。 一个头部被添加到DGPS加强数据中,传统的地面DME系统的发射脉冲电平被调制,数据被广播到机载系统。 在机载系统中,由电平检测装置(5)产生阈值“1”和“0”,由标题检测装置(6)检测数据的起始点,加强数据为 提供给机载系统。 因此,实现了通过将数据重叠到DME的距离信息上来广播数据的功能。 由于DME使用L波段,因此可以避免对现有ILS,VOR,飞机无线电传输和广播电台的无线电干扰。
    • 46. 发明授权
    • Arrangement for comparing two temporally separated bursts of signal at
two different frequencies
    • 用于比较两个不同频率处的两个时间上分离的信号脉冲串的装置
    • US5532701A
    • 1996-07-02
    • US65591
    • 1993-05-21
    • Daniele Biella
    • Daniele Biella
    • G01S7/40G01S13/78G01S1/04
    • G01S13/785G01S7/4008
    • A comparator circuit compares two temporally separated input bursts of signals which occur at two different frequencies. The first burst is an interrogation pulse and the second burst is a reply pulse in a DME system. The comparator circuit includes a first frequency converter (CO1) for receiving at an input thereof the two input bursts, and a comparing device (DC) connected to receive an output of the first frequency converter (CO1). In order to reduce the measurement errors, the first frequency converter (CO1) receives at the input thereof the two input bursts and converts them into two new bursts of signals that have a common frequency so that the comparing device (DC) can carry out the comparison at the common frequency.
    • 比较器电路比较两个在两个不同频率处出现的时间上分离的输入信号脉冲串。 第一个脉冲串是一个询问脉冲,第二个脉冲串是DME系统中的一个应答脉冲。 比较器电路包括用于在其输入处接收两个输入脉冲串的第一频率转换器(CO1)和连接以接收第一频率转换器(CO1)的输出的比较装置(DC)。 为了减少测量误差,第一变频器(CO1)在其输入处接收两个输入脉冲串,并将它们转换为具有共同频率的两个新的信号脉冲串,使得比较装置(DC)可以执行 比较在共同频率。
    • 49. 发明授权
    • Range reply search apparatus
    • 范围回复搜索装置
    • US4555704A
    • 1985-11-26
    • US441454
    • 1982-11-15
    • Jan E. Treise
    • Jan E. Treise
    • G01S13/70G01S13/78G01S13/00
    • G01S13/70G01S13/785
    • Apparatus for searching for range indicating pulse signals received as part of distance measuring equipment which first form a list of distance indications in a first search time. The distance indications obtained in a second search time are then logically combined with those indications in the first list and any combination that results in a difference value of less than a prescribed amount is retained for list updating purposes until there is only a single distance indication left in the list. The apparatus can then change to a track mode by placing a search window around the single distance indication thereby reducing the amount of extraneous information to be manipulated by the receiving apparatus.
    • 用于搜索指示作为距离测量设备的一部分接收的脉冲信号的范围的设备,其首先在第一搜索时间形成距离指示列表。 然后在第二搜索时间中获得的距离指示与第一列表中的那些指示逻辑组合,并且保留导致小于规定量的差值的任何组合以用于列表更新目的,直到仅剩下一个距离指示为止 在列表中。 然后,可以通过将搜索窗放置在单个距离指示周围,从而减少由接收设备操纵的无关信息的数量,该设备可以改变为轨迹模式。