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    • 1. 发明公开
    • TRACKING SYSTEM, TRACKING METHOD, AND PROGRAM
    • 追踪系统跟踪方法和程序
    • EP3018756A4
    • 2017-03-01
    • EP14820326
    • 2014-05-15
    • MITSUBISHI ELECTRIC CORP
    • UEGO NAOYASAKAI YUJISAITO MASAKAZU
    • H01Q3/08G01S3/42H01Q1/12
    • G01S3/42H01Q1/1257H01Q1/1264H01Q3/08
    • A rotation determiner (23) determines whether the azimuth (AZ) angle of an antenna (3) rotates beyond a rotation range within a predetermined duration of time on the basis of a predicted orbit value. When the AZ angle of the antenna (3) is determined to rotate beyond the rotation range, an orbit determiner (24) determines whether an estimated satellite position is within a drivable range in which the AZ angle rotates from a reference value beyond the rotation range, and in which an xEL axis can be driven in a state in which the AZ angle is set to a predetermined value that is permissible for the AZ angle. When the AZ angle rotates beyond the rotation range and while the estimated satellite position is within the drivable range, a determiner (22) sends a command to a switching section (17) to cause three-axis control, and a command to cause an AZ command operator (15) to output a command value that keeps the AZ angle at a predetermined value. When the AZ angle rotates beyond the rotation range and while the estimated satellite position is not within the drivable range, or when the AZ angle does not rotate beyond the rotation range, the determiner (22) sends a command to the switching section (17) to cause two-axis control.
    • 3. 发明公开
    • Satellite connection apparatus for transport means
    • SatmittitenverbindungsvorrichtungfürTransportmittel
    • EP2290390A1
    • 2011-03-02
    • EP09425324.2
    • 2009-08-07
    • Milano Teleport S.p.A.
    • Steiner, Carlo
    • G01S3/42H01Q1/34H01Q3/08H01Q1/12
    • G01S3/42H01Q1/125H01Q1/34H01Q3/08
    • A satellite connection apparatus (1) is provided for transport means (11) comprising: an antenna (2) of geostabilized type, suitable to track a first satellite (10) in coverage and of establishing a connection with said first satellite (10), a modem (3) capable of rendering the signal received by said antenna (2) usable by computers and the like, a position detection device (5) capable of determining the position of said transport means (11) on the globe and automatic actuator means capable of moving said antenna (2), wherein the antenna (2) is capable of automatically tracking a different satellite (10) in coverage, when the first satellite (10) is no longer in coverage following movements of the transport means.
    • 一种用于传输装置(11)的卫星连接装置(1),包括:适于跟踪覆盖范围内的第一卫星(10)并建立与所述第一卫星(10)的连接的地理稳定型天线(2) 能够呈现由计算机等可使用的所述天线(2)接收的信号的调制解调器(3),能够确定所述传送装置(11)在球形体上的位置的位置检测装置(5)和自动致动装置 能够移动所述天线(2),其中当所述第一卫星(10)在所述传送装置的移动之后不再处于覆盖状态时,所述天线(2)能够自动跟踪覆盖中的不同卫星(10)。
    • 4. 发明公开
    • VEHICLE LOCATION AND RECOVERY SYSTEMS
    • 车辆定位和恢复系统
    • EP1776599A1
    • 2007-04-25
    • EP04801286.8
    • 2004-12-02
    • LoJack Corporation
    • DUVALL, William
    • G01S5/00G01S5/02G08B25/00G08G1/123B60R25/00
    • G01S5/0027G01S3/42G01S5/0072G01S5/02G01S13/74
    • A system and technique for improving the speed and ease of missing vehicle location and recovery by vehicle-carried transponder periodic coded replies to radio interrogation by a network of (VHF) transmitting towers, by integrating a concealed GPS location receiver with the transponder and providing the GPS-obtained coordinate information through the VHF network to enable a preliminary initial recovery location from which to home-in for recovery by subsequent direction-finding from the periodic transponder responses. Other location-on-demand services are also readily operable through the use of this VHF network, including providing said GPS coordinate or location information on the Internet.
    • 一种系统和技术,用于通过车载应答器对由(VHF)发射塔网络进行的无线电询问的周期性编码答复,通过将隐藏的GPS定位接收器与发射机应答器集成在一起并提供 通过VHF网络获得的GPS获得的坐标信息,以使初始初始恢复位置能够从周期性转发器响应中通过随后的方向查找归位以恢复。 其他按需定位服务也可以通过使用该VHF网络容易地操作,包括在互联网上提供所述GPS坐标或位置信息。
    • 8. 发明公开
    • Direction tracking antenna system
    • 天线系统
    • EP0373604A1
    • 1990-06-20
    • EP89122957.7
    • 1989-12-12
    • Nippon Steel CorporationSYSTEM UNIQUES CORPORATION
    • Uematsu, MasahiroHiratsuka, RyuichiKato, Kazuro c/o SYSTEM UNIQUES CORPORATION
    • G01S3/46
    • H01Q1/3275G01S3/42G01S3/46
    • A satellite tracking antenna system comprises three or four plane antennas juxtaposed on a single plane. A first and a second antenna are juxtaposed in an azimuth direction, and a phase difference between signals received by these antennas is detected in order to determine a declination of an antenna unit with respect to the satellite as viewed in the azimuth direction. The first and a third antenna are juxtaposed in an elevation direction, and a phase difference between signals received by these antennas is detected to determine a declination of the antenna unit with respect to the satellite as viewed in the elevation direction. The antenna unit is driven so as to reduce these declinations to zero. Stated differently, values of a sine and a cosine function are extracted which have a phase difference between signals received by a pair of antennas as a parameter, and a tangent value representing the ratio therebetween is calculated and is then inversely converted to provide phase difference information.
    • 卫星跟踪天线系统包括并置在单个平面上的三个或四个平面天线。 第一和第二天线在方位方向并置,并且检测由这些天线接收的信号之间的相位差,以便在方位角方向上确定天线单元相对于卫星的偏角。 第一和第三天线在高度方向上并置,并且检测由这些天线接收的信号之间的相位差,以确定天线单元相对于卫星在仰角方向上的偏角。 天线单元被驱动以将这些偏差减小到零。 换句话说,提取具有由一对天线接收的信号之间的相位差作为参数的正弦和余弦函数的值,并且计算表示其之间的比值的正切值,然后逆向转换以提供相位差信息 。
    • 9. 发明公开
    • Tracking controller for three-axis mount antenna systems
    • Nachführungssteuervorrichtungfürdreiachsige Antennentragesysteme。
    • EP0246635A2
    • 1987-11-25
    • EP87107347.4
    • 1987-05-20
    • NEC CORPORATION
    • Nakayama, Makoto
    • H01Q3/08G01S3/42
    • G01S3/42H01Q3/08
    • In a satellite tracking control system, a receiver derirves a pair of elevation (EL) and cross-elevation (XEL) tracking error signals having a quadratic relationship in a coordinate system from a signal received from a polar-orbital satellite. Elevation and cross-elevation motors are respectively controlled in response to the elevation (EL) and cross-elevation (XEL) tracking error signals. An azimuth controller derives an azimuth control signal from angle data representing the angles of the antenna about the azimuth, elevation and cross-elevation axes detected by angle detectors. Preferably, the antenna is rotatable about the elevation (EL) axis in the range between zero and l80 degrees.
    • 在卫星跟踪控制系统中,接收机从从极轨道卫星接收的信号中减去坐标系中具有二次关系的一对高程(EL)和横坐标(XEL)跟踪误差信号。 高程和横高电机分别根据高程(EL)和横截面(XEL)跟踪误差信号进行控制。 方位角控制器从角度数据中得出方位角控制信号,该角度数据表示由角度检测器检测到的方位角,仰角和横截面轴的天线角度。 优选地,天线可以在高度(EL)轴之间在0和180度之间的范围内旋转。