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    • 1. 发明申请
    • Systems and Methods of Communication in an Assisted Navigation System
    • 辅助导航系统中的通信系统和方法
    • US20130021202A1
    • 2013-01-24
    • US13564468
    • 2012-08-01
    • Shaowei HANWentao ZHANG
    • Shaowei HANWentao ZHANG
    • G01S19/25
    • G01S19/25G01S19/05G01S19/27
    • Provided herein are methods and systems for efficient communication between a server and a client in an assisted navigation system. In one or more embodiments, the server transmits a set of parameters for a satellite to the client, e.g., a GPS receiver, via a wireless or wired connection. The set of parameters includes a force parameter, initial condition parameters and time correction coefficients for the satellite. The receiver uses the received parameters in a numerical integration to compute the position of the satellite at a desired time. The set of parameters needed for the integration is small. To further reduce the amount of data transmitted, reference parameters may be subtracted from the original parameters before transmission from the server. The receiver is able to reconstruct the original parameters from the received parameters and the identically computed reference parameters. The parameters may be further compressed using data compression techniques.
    • 这里提供了用于在辅助导航系统中的服务器和客户端之间的有效通信的方法和系统。 在一个或多个实施例中,服务器经由无线或有线连接向卫星发送一组用于卫星的参数,例如GPS接收机。 该组参数包括一个力参数,初始条件参数和卫星的时间校正系数。 接收机使用数字积分中接收到的参数来计算卫星在所需时间的位置。 集成所需的一组参数很小。 为了进一步减少发送的数据量,可以在从服务器发送之前从原始参数中减去参考参数。 接收机能够从接收的参数和相同计算的参考参数重建原始参数。 可以使用数据压缩技术来进一步压缩参数。
    • 2. 发明授权
    • Narrow correlator technique for multipath mitigation
    • 用于多径缓解的窄相关器技术
    • US08000378B2
    • 2011-08-16
    • US11615704
    • 2006-12-22
    • Jun MoShaowei Han
    • Jun MoShaowei Han
    • H04B1/00H04L27/06
    • H04B1/7085H04B1/709H04B2201/70715
    • The present invention provides systems and methods for implementing narrowly spaced correlators to mitigate multipath error, and systems and methods for adaptively changing the correlator spacing for varying multipath conditions. In an embodiment, two sets of correlators with the same code frequency but different code phases are used to implement an adjustable correlator spacing. The correlator spacing is determined by the code phase difference between the two sets of correlators, which can be adjusted, e.g., by adjusting the code phase values of Numerically Controlled Oscillators (NCOs). An advantage of embodiments of the present invention is that they can achieve much narrower correlator spacings than conventional techniques, e.g., by making the code phase difference between the two sets of correlators very small. Further, the correlator spacing can be adjusted for varying multipath conditions, whereas the correlator spacing in conventional techniques is fixed.
    • 本发明提供了用于实现窄间隔相关器以减轻多路径误差的系统和方法,以及用于自适应地改变相关器间隔以用于变化的多径条件的系统和方法。 在一个实施例中,使用具有相同代码频率但不同代码阶段的两组相关器来实现可调整的相关器间隔。 相关器间距由两组相关器之间的码相位差确定,这可以通过例如调节数控振荡器(NCO)的码相位值来调整。 本发明的实施例的优点在于,它们可以实现比常规技术更窄的相关器间隔,例如通过使两组相关器之间的码相位差非常小。 此外,可以针对变化的多径条件来调整相关器间距,而常规技术中的相关器间隔是固定的。
    • 3. 发明授权
    • Systems and methods of communication in an assisted navigation system
    • 辅助导航系统中的通信系统和方法
    • US08635016B2
    • 2014-01-21
    • US13564468
    • 2012-08-01
    • Shaowei HanWentao Zhang
    • Shaowei HanWentao Zhang
    • G01C21/00
    • G01S19/25G01S19/05G01S19/27
    • Provided herein are methods and systems for efficient communication between a server and a client in an assisted navigation system. In one or more embodiments, the server transmits a set of parameters for a satellite to the client, e.g., a GPS receiver, via a wireless or wired connection. The set of parameters includes a force parameter, initial condition parameters and time correction coefficients for the satellite. The receiver uses the received parameters in a numerical integration to compute the position of the satellite at a desired time. The set of parameters needed for the integration is small. To further reduce the amount of data transmitted, reference parameters may be subtracted from the original parameters before transmission from the server. The receiver is able to reconstruct the original parameters from the received parameters and the identically computed reference parameters. The parameters may be further compressed using data compression techniques.
    • 这里提供了用于在辅助导航系统中的服务器和客户端之间的有效通信的方法和系统。 在一个或多个实施例中,服务器经由无线或有线连接向卫星发送一组用于卫星的参数,例如GPS接收机。 该组参数包括一个力参数,初始条件参数和卫星的时间校正系数。 接收机使用数字积分中接收到的参数来计算卫星在所需时间的位置。 集成所需的一组参数很小。 为了进一步减少发送的数据量,可以在从服务器发送之前从原始参数中减去参考参数。 接收机能够从接收的参数和相同计算的参考参数重建原始参数。 可以使用数据压缩技术来进一步压缩参数。
    • 6. 发明申请
    • SYSTEMS AND METHODS OF COMMUNICATION IN AN ASSISTED NAVIGATION SYSTEM
    • 辅助导航系统中的通信系统和通信方法
    • US20090237300A1
    • 2009-09-24
    • US12476458
    • 2009-06-02
    • Shaowei HANWentao Zhang
    • Shaowei HANWentao Zhang
    • G01S1/00
    • G01S19/25G01S19/05G01S19/27
    • Provided herein are methods and systems for efficient communication between a server and a client in an assisted navigation system. In one or more embodiments, the client, e.g., a GPS receiver, receives a set of parameters for a satellite from the server via a wireless or wired connection. The set of parameters includes a force parameter, initial condition parameters and time correction coefficients for the satellite. The receiver uses the received parameters in a numerical integration to compute the position of the satellite at a desired time. The set of parameters needed for the integration is small compared to current methods which require sending more data to the client. Thus these parameters require less communication resources to transmit. To further reduce the amount of data that needs to be transmitted, reference parameters may be subtracted from the original parameters before transmission from the server. The receiver is able to reconstruct the original parameters from the received parameters and the identically computed reference parameters. The parameters may be further compressed using data compression techniques.
    • 这里提供了用于在辅助导航系统中的服务器和客户端之间的有效通信的方法和系统。 在一个或多个实施例中,客户端,例如GPS接收器经由无线或有线连接从服务器接收卫星的一组参数。 该组参数包括一个力参数,初始条件参数和卫星的时间校正系数。 接收机使用数字积分中接收到的参数来计算卫星在所需时间的位置。 与需要向客户端发送更多数据的当前方法相比,集成所需的一组参数较小。 因此,这些参数需要更少的通信资源进行传输。 为了进一步减少需要传输的数据量,可以在从服务器发送之前从原始参数中减去参考参数。 接收机能够从接收的参数和相同计算的参考参数重建原始参数。 可以使用数据压缩技术来进一步压缩参数。
    • 7. 发明授权
    • Method and apparatus for self-calibration and adaptive temperature compensation in GPS receivers
    • GPS接收机中自校准和自适应温度补偿的方法和装置
    • US07459984B2
    • 2008-12-02
    • US11140492
    • 2005-05-26
    • Chi-Shin WangKudrethaya A. ShridharaJun MoShaowei HanHansheng Wang
    • Chi-Shin WangKudrethaya A. ShridharaJun MoShaowei HanHansheng Wang
    • H03L1/00G01S1/00
    • H03L1/026G01S19/235
    • The invention provides a method and apparatus to optimally estimate and adaptively compensate the temperature-induced frequency drift of a crystal oscillator in a navigational signal receiver. A Read-Write memory encodes two tables, one for looking up frequency drift values versus temperature readings and another one for valid data confirmation on the first table. The initially empty look-up table is gradually populated with frequency drift values while the receiver computes the frequency drift along with its position. During initial start of the receiver or re-acquisition of satellite signals, the stored frequency drift value corresponding to the current temperature is used. If no valid frequency drift value is available, the frequency drift value is computed based on the existing frequency drift values in the table. This invention reduces the Time-To-First-Fix (TTFF) of the receiver and enables the receiver to self-calibrate, thus no additional factory calibration would be necessary.
    • 本发明提供了一种方法和装置,用于对导航信号接收机中的晶体振荡器的温度感应频率漂移进行最佳估计和自适应补偿。 读写存储器编码两个表,一个用于查找频率漂移值与温度读数,另一个用于在第一个表上进行有效数据确认。 初始空的查找表逐渐填充频率漂移值,而接收器计算频率漂移及其位置。 在接收机初始启动或重新采集卫星信号时,使用与当前温度对应的存储频率漂移值。 如果没有有效的频率漂移值可用,则基于表中现有的频率漂移值来计算频率漂移值。 本发明减少了接收机的首次定时(TTFF),使得接收机能够自校准,因此不需要额外的工厂校准。
    • 8. 发明申请
    • NARROW CORRELATOR TECHNIQUE FOR MULTIPATH MITIGATION
    • 用于多路减速的NARROW CORRERATOR技术
    • US20080151971A1
    • 2008-06-26
    • US11615704
    • 2006-12-22
    • Jun MoShaowei Han
    • Jun MoShaowei Han
    • H04B1/707
    • H04B1/7085H04B1/709H04B2201/70715
    • The present invention provides systems and methods for implementing narrowly spaced correlators to mitigate multipath error, and systems and methods for adaptively changing the correlator spacing for varying multipath conditions. In an embodiment, two sets of correlators with the same code frequency but different code phases are used to implement an adjustable correlator spacing. The correlator spacing is determined by the code phase difference between the two sets of correlators, which can be adjusted, e.g., by adjusting the code phase values of Numerically Controlled Oscillators (NCOs). An advantage of embodiments of the present invention is that they can achieve much narrower correlator spacings than conventional techniques, e.g., by making the code phase difference between the two sets of correlators very small. Further, the correlator spacing can be adjusted for varying multipath conditions, whereas the correlator spacing in conventional techniques is fixed.
    • 本发明提供了用于实现窄间隔相关器以减轻多路径误差的系统和方法,以及用于自适应地改变相关器间隔以用于变化的多径条件的系统和方法。 在一个实施例中,使用具有相同代码频率但不同代码阶段的两组相关器来实现可调整的相关器间隔。 相关器间距由两组相关器之间的码相位差确定,这可以通过例如调节数控振荡器(NCO)的码相位值来调整。 本发明的实施例的优点在于,它们可以实现比常规技术更窄的相关器间隔,例如通过使两组相关器之间的码相位差非常小。 此外,可以针对变化的多径条件来调整相关器间距,而常规技术中的相关器间隔是固定的。
    • 10. 发明授权
    • Method and apparatus in positioning without broadcast ephemeris
    • 无广播星历的定位方法和设备
    • US07869948B2
    • 2011-01-11
    • US11741448
    • 2007-04-27
    • Shaowei Han
    • Shaowei Han
    • G01C21/20
    • G01S19/25G01S19/27
    • Provided herein are methods and system for enabling a navigation receiver to generate receiver specific satellite orbital models based on relatively small sets of parameters obtained from a server. In an embodiment, a set of parameters for a satellite includes a force parameter (e.g., solar radiation pressure), initial condition parameters (e.g., satellite position and velocity at a time instance) and time correction coefficients, which the receiver uses in a numerical integration to predict the position of the satellite. The set of parameters needed for the integration is small compared to current methods which require transmission of a complete set of ephemeris and other parameters for each satellite. Since the set of parameters is relatively small, it requires less communication resources to transmit compared to current methods. Further, the integration based on the small set of parameters enables the receiver to predict satellite orbits with low computational load.
    • 本文提供的方法和系统使得导航接收机能够基于从服务器获得的相对小的参数集合来生成接收机专用卫星轨道模型。 在一个实施例中,用于卫星的一组参数包括力参数(例如,太阳辐射压力),初始条件参数(例如,时间上的卫星位置和速度)和时间校正系数,接收器使用数字 整合以预测卫星的位置。 与需要传输一组完整的星历和每个卫星的其他参数的当前方法相比,集成所需的一组参数较小。 由于该组参数相对较小,因此与当前方法相比,传输资源要少。 此外,基于小的参数集合的集成使得接收机能够以低计算负荷来预测卫星轨道。