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    PROVIDING EPHEMERIS DATA AND CLOCK CORRECTIONS TO A SATELLITE NAVIGATION SYSTEM RECEIVER
    81.
    发明申请
    PROVIDING EPHEMERIS DATA AND CLOCK CORRECTIONS TO A SATELLITE NAVIGATION SYSTEM RECEIVER 审中-公开
    向卫星导航系统接收机提供EPHEMERIS数据和时钟校正

    公开(公告)号：WO2011112211A1

    公开(公告)日：2011-09-15

    申请号：PCT/US2010/046388

    申请日：2010-08-23

    Applicant: ATHEROS COMMUNICATIONS, INC. ,  VENKATRAMAN, Sai ,  JARPENVAA, Janne ,  SUN, Qinfang

    Inventor： VENKATRAMAN, Sai ,  JARPENVAA, Janne ,  SUN, Qinfang

    IPC: H04B7/185

    CPC classification number: G01S19/05 ,  G01S19/258 ,  G01S19/27

    Abstract: A device can access scaled values and scaling factors, which are used to convert the scaled values into coefficients and residuals. The coefficients and residuals can in turn be used with time- dependent functions to reconstruct predicted ephemeris data, including clock correction data, for satellite navigation system satellites. Ephemeris data that is broadcast from any of the satellites can be used to update the calculated ephemeris data.

    Abstract translation: 设备可以访问缩放的值和缩放因子，用于将缩放的值转换为系数和残差。 系数和残差又可以与时间相关函数一起使用，以重建卫星导航系统卫星的预测星历数据，包括时钟校正数据。 可以使用从任何卫星广播的星历数据来更新计算出的星历数据。

    PREFERENCE LISTS FOR ASSISTANCE DATA REQUESTS IN GLOBAL NAVIGATION SATELLITE SYSTEMS
    83.
    发明申请
    PREFERENCE LISTS FOR ASSISTANCE DATA REQUESTS IN GLOBAL NAVIGATION SATELLITE SYSTEMS 审中-公开
    全球导航卫星系统中辅助数据要求的优先级

    公开(公告)号：WO2010142857A1

    公开(公告)日：2010-12-16

    申请号：PCT/FI2010/050485

    申请日：2010-06-11

    Applicant: NOKIA CORPORATION ,  WIROLA, Lauri ,  HALIVAARA, Ismo ,  LAINE, Tommi

    Inventor： WIROLA, Lauri ,  HALIVAARA, Ismo ,  LAINE, Tommi

    IPC: G01S1/00 ,  G01S19/05 ,  G01S19/25

    CPC classification number: G01S19/05 ,  G01S5/0063 ,  G01S19/258

    Abstract: Methods and devices may request and provide assistance data from an assistance server to a receiver in a global navigation satellite system. A request for assistance data may include a preference list of navigation models suitable for the requesting receiver. Multiple preference lists for different navigation model types (e.g., orbit model, clock model, almanac model) may be included in a single list and/or data structure, or as multiple lists and/or data structures. An assistance server may receive and process the preference list, for example, by parsing and traversing the ordered list(s) for different navigation model types, in order to provide satellite navigation data to the receiver in accordance with suitable navigation models that are available at both the receiver and the assistance server.

    Abstract translation: 方法和设备可以从全球导航卫星系统向辅助服务器请求和提供辅助数据到接收机。 对辅助数据的请求可以包括适合于请求接收者的导航模型的偏好列表。 可以将不同导航模型类型（例如，轨道模型，时钟模型，历书模型）的多个偏好列表包括在单个列表和/或数据结构中，或者作为多个列表和/或数据结构。 辅助服务器可以例如通过解析和遍历用于不同导航模型类型的有序列表来接收和处理偏好列表，以便根据可用的适当的导航模型向接收机提供卫星导航数据 接收器和辅助服务器。

    SPOOFING DETECTION FOR CIVILIAN GNSS SIGNALS
    84.
    发明申请
    SPOOFING DETECTION FOR CIVILIAN GNSS SIGNALS 审中-公开
    民用GNSS信号的检测

    公开(公告)号：WO2010105136A2

    公开(公告)日：2010-09-16

    申请号：PCT/US2010027106

    申请日：2010-03-12

    Applicant: UNIV CORNELL ,  PSIAKI MARK L

    Inventor： PSIAKI MARK L

    IPC: G01S19/20 ,  G01S19/01

    CPC classification number: G01S19/215 ,  G01S19/05

    Abstract: A system and method for detecting spoofing of signals by processing intermittent bursts of encrypted Global Navigation Satellite System (GNSS) signals in order to determine whether unencrypted signals are being spoofed.

    Abstract translation: 一种用于通过处理加密的全球导航卫星系统（GNSS）信号的间歇性突发来检测信号的欺骗的系统和方法，以便确定未加密的信号是否被欺骗。

    HIGH-RELIABILITY PRODUCT/ACTIVITY TRACKING SYSTEM
    85.
    发明申请
    HIGH-RELIABILITY PRODUCT/ACTIVITY TRACKING SYSTEM 审中-公开
    高可靠性产品/活动跟踪系统

    公开(公告)号：WO2010072272A1

    公开(公告)日：2010-07-01

    申请号：PCT/EP2008/068281

    申请日：2008-12-23

    Applicant: TELESPAZIO S.P.A. ,  MUSMECI, Mario

    Inventor： MUSMECI, Mario

    IPC: G01S5/00 ,  G01S5/14 ,  G06Q10/00

    CPC classification number: G01S19/05 ,  G01S5/0027 ,  G01S5/0036 ,  G01S19/09 ,  G01S19/14 ,  G01S19/258

    Abstract: Disclosed herein is a tracking system (10; 10') configured to track a product and/or an activity. The tracking system (10; 10') comprises a tracing device (11) and a verification server (12). The tracing device (11) is coupled with the verification server (12) by means of communication means (13) configured to allow exchange of data between the tracing device (11) and the verification server (12). The tracing device (11) is coupled with a first satellite localization receiver which is configured to receive signals from a satellite localization system, process the received signals to obtain satellite localization observables, and compute locations based on the satellite localization observables. The tracing device (11) is configured to acquire from the first satellite localization receiver positioning data (21; 31). The positioning data (21; 31) comprise a location computed by the first satellite localization receiver, and a location time which represents time and data at which the location is computed by the first satellite localization receiver. The positioning data (21; 31) are related to a product and/or an activity to be tracked. The tracing device (11) is further configured to select a satellite localization observable based on which the location is computed by the first satellite localization receiver, and to acquire from the satellite localization receiver the selected satellite localization observable. The tracing device (11) is further configured to provide the verification server (12) with the positioning data (21; 31) and the satellite localization observable acquired from the satellite localization receiver. Moreover, the verification server (12), in turn, is configured to perform a location consistency check based on the location comprised in the positioning data (21; 31) provided by the tracing device (11), and on the satellite localization observable provided by the tracing device (11). The verification server (12) is further configured to generate a validation code (23; 33) on the basis of an outcome of the location consistency check, and on the basis of the positioning data (21; 31) provided by the tracing device (11). The verification server is further configured to provide the tracing device (11) with the generated validation code (23; 33). Furthermore, the tracing device (11) is further configured to store the positioning data (21; 31) and the validation code (23; 33) provided by the verification server (12) on tracking means (50) associated with the product and/or the activity to be tracked.

    Abstract translation: 本文公开了一种被配置为跟踪产品和/或活动的跟踪系统（10; 10'）。 跟踪系统（10; 10'）包括跟踪设备（11）和验证服务器（12）。 跟踪设备（11）通过被配置为允许跟踪设备（11）和验证服务器（12）之间的数据交换的通信装置（13）与验证服务器（12）耦合。 跟踪装置（11）与第一卫星定位接收器耦合，其被配置为从卫星定位系统接收信号，处理接收的信号以获得卫星定位可观测量，并且基于卫星定位可观测量来计算位置。 跟踪装置（11）被配置为从第一卫星定位接收机定位数据（21; 31）获取。 定位数据（21; 31）包括由第一卫星定位接收机计算的位置和表示由第一卫星定位接收机计算位置的时间和数据的位置时间。 定位数据（21; 31）与要跟踪的产品和/或活动相关。 跟踪设备（11）还被配置为选择可观测的卫星定位，基于该卫星定位由第一卫星定位接收机计算位置，并且从卫星定位接收机获取所选择的卫星定位可观测。 跟踪设备（11）还被配置为向验证服务器（12）提供定位数据（21; 31）和从卫星定位接收器获取的卫星定位可观测信号。 此外，验证服务器（12）又被配置为基于由跟踪设备（11）提供的定位数据（21; 31）中包括的位置以及所提供的卫星定位可观察地执行位置一致性检查 通过跟踪装置（11）。 验证服务器（12）还被配置为基于位置一致性检查的结果并且基于由跟踪设备提供的定位数据（21; 31）来生成验证码（23; 33） 11）。 验证服务器还被配置为向跟踪设备（11）提供生成的验证码（23; 33）。 此外，跟踪装置（11）还被配置为将由验证服务器（12）提供的定位数据（21; 31）和与产品相关联的跟踪装置（50）和/ 或要跟踪的活动。

    DGNSS CORRECTION FOR POSITIONING
    86.
    发明申请
    DGNSS CORRECTION FOR POSITIONING 审中-公开
    DGNSS定位校正

    公开(公告)号：WO2010057149A1

    公开(公告)日：2010-05-20

    申请号：PCT/US2009/064700

    申请日：2009-11-17

    Applicant: QUALCOMM INCORPORATED ,  FARMER, Dominic, Gerard ,  LIN, le-Hong ,  PON, Rayman Wai

    Inventor： FARMER, Dominic, Gerard ,  LIN, le-Hong ,  PON, Rayman Wai

    IPC: G01S1/00

    CPC classification number: G01S19/05 ,  G01S19/25 ,  G01S19/27

    Abstract: Techniques for supporting positioning with differential corrections are described. In an aspect, differential correction for a satellite may include (i) a user differential range error (UDRE) indicating an uncertainty in a pseudo-range correction for the satellite, (ii) a UDRE growth rate, which may be a scaling factor for the UDRE, and (iii) a time of validity for UDRE growth rate, which may be a time unit used to apply the scaling factor. In one design, a terminal may send a request message to ask for differential correction information and may receive a response message. The terminal may obtain differential correction ( e.g. , a UDRE, a UDRE growth rate, and a time of validity for UDRE growth rate) for each of at least one satellite from the response message. The terminal may derive a location estimate for itself based on the differential correction for each satellite.

    Abstract translation: 描述用于支持差分校正定位的技术。 在一方面，卫星的差分校正可以包括（i）指示卫星的伪距校正中的不确定性的用户差分范围误差（UDRE），（ii）UDRE增长率，其可以是用于 UDRE，以及（iii）UDRE增长率的有效期，可能是用于应用比例因子的时间单位。 在一种设计中，终端可以发送请求消息来请求差分校正信息，并且可以接收响应消息。 终端可以从响应消息中获得至少一个卫星中的每一个的差分校正（例如，UDRE，UDRE增长率和UDRE增长率的有效时间）。 终端可以基于每个卫星的差分校正导出其自身的位置估计。

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