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21. 发明申请

US20060250304A1 System and method for fast initialization of navigational satellite signal receivers 有权
标题翻译：导航卫星信号接收机快速初始化的系统和方法
公开(公告)号：US20060250304A1
公开(公告)日：2006-11-09
申请号：US11124413
申请日：2005-05-06
申请人： Jun Mo , Hansheng Wang , Chi-Shin Wang , Shaowei Han , Kudrethaya Shridhara
发明人： Jun Mo , Hansheng Wang , Chi-Shin Wang , Shaowei Han , Kudrethaya Shridhara
IPC分类号： G01S5/14
CPC分类号： G01S19/28
摘要： The present invention provides a method and apparatus for a satellite navigation receiver to lock onto satellite signals in the cold start mode with no information on the receiver position, the satellite position, or time estimates stored in the receiver's memory. All satellites in a positioning system are divided into groups based on the satellite constellation structure. In an embodiment, the positioning system is the Global Positioning System (GPS) and all GPS satellites are divided into three groups. During initialization of the receiver, the satellites are searched per group to lock onto at least one satellite signal. Other satellites are then searched in a given order based on their respective distance or proximity to the first satellite acquired. This method reduces the Time-to-First-Fix (TTFF) ordinarily required by conventional receivers in the cold start mode.
摘要翻译：本发明提供了一种用于卫星导航接收机在冷启动模式下锁定卫星信号的方法和装置，其中没有关于存储在接收机的存储器中的接收机位置，卫星位置或时间估计的信息。基于卫星星座结构将定位系统中的所有卫星分成几组。在一个实施例中，定位系统是全球定位系统（GPS），所有GPS卫星分为三组。在接收机的初始化期间，每组搜索卫星以锁定至少一个卫星信号。然后根据其相应的距离或与所获取的第一卫星的距离，以给定的顺序搜索其他卫星。这种方法减少了常规接收机在冷启动模式下通常要求的首次固定时间（TTFF）。

22. 发明申请

US20050001762A1 Enhanced real time kinematics determination method and apparatus 有权
标题翻译：增强型实时运动学测定方法及装置
公开(公告)号：US20050001762A1
公开(公告)日：2005-01-06
申请号：US10610541
申请日：2003-07-02
申请人： Shaowei Han , Kevin Chin
发明人： Shaowei Han , Kevin Chin
IPC分类号： G01S19/21 , G01S5/14 , G01S19/26
CPC分类号： G01S19/44
摘要： A method of and computer-readable medium containing instructions for high accuracy, reliable position determination. A high precision GPS-RTK system using the present novel techniques is initialized instantaneously or near instantaneously. To improve the computational efficiency and to improve the reliability of the procedure, advances in data functional and stochastic modeling, validation criteria, adaptation and system design were achieved. A position estimate using an integrated method is determined. Ambiguity resolution of the position estinate is enhanced by applying a quality control procedure using derived validation criteria. A second position estimate based on the enhanced ambiguity resolution is derived.
摘要翻译：包含用于高精度，可靠位置确定的指令的方法和计算机可读介质。使用本新技术的高精度GPS-RTK系统被瞬时或接近地初始化。为了提高计算效率和提高程序的可靠性，实现了数据功能和随机建模，验证标准，适应和系统设计的进步。确定使用积分方法的位置估计。通过使用衍生的验证标准应用质量控制程序来增强位置估计的模糊度分辨率。导出基于增强的模糊度分辨率的第二位置估计。

23. 发明授权

US07567208B2 Position and time determination under weak signal conditions 有权
标题翻译：弱信号条件下的位置和时间确定
公开(公告)号：US07567208B2
公开(公告)日：2009-07-28
申请号：US11771845
申请日：2007-06-29
申请人： Jun Mo , Shaowei Han
发明人： Jun Mo , Shaowei Han
IPC分类号： G01S1/00
CPC分类号： G01S19/24 , G01S19/42
摘要： Described herein are systems and methods that are capable of determining receiver position and system time under weak signal conditions. When the receiver is unable to accurately determine the satellite signal travel time, e.g., due to weak signal reception or some other condition, the receiver can still estimate the pseudo-range for the satellite based on an initial receiver position and system time. In this case, the system and methods described herein provide the necessary initial receiver position and system time with enough accuracy to estimate the pseudo-range, even under weak signal conditions. The receiver can then use the estimated pseudo-range to determine a more accurate receiver position.
摘要翻译：这里描述的是能够在弱信号条件下确定接收机位置和系统时间的系统和方法。当接收机不能准确地确定卫星信号传播时间时，例如由于信号接收弱或某种其他条件，接收机仍然可以基于初始的接收机位置和系统时间来估计卫星的伪距离。在这种情况下，即使在弱信号条件下，本文所述的系统和方法也提供了足够准确的必要的初始接收机位置和系统时间来估计伪距离。然后，接收机可以使用估计的伪距来确定更准确的接收机位置。

24. 发明授权

US07545317B2 Method and apparatus for navigation data downloads from weak signals 失效
标题翻译：从弱信号下载导航数据的方法和装置
公开(公告)号：US07545317B2
公开(公告)日：2009-06-09
申请号：US11558611
申请日：2006-11-10
申请人： Shaowei Han
发明人： Shaowei Han
IPC分类号： G01S1/00 , H03K9/00
CPC分类号： G01S19/252
摘要： The present invention provides systems and methods that enable a standalone receiver capable of downloading navigation data under weak signal conditions. In an embodiment, a standalone navigation receiver generates predicted satellite orbits based on the tracking history of the satellites stored in the receiver. The tracking history comprises historical navigation data previously received from the satellites. The receiver uses the predicted satellite orbit to generate navigation data such as ephemeris and almanac. Since the predicted satellite is accurate, the generated navigation data is similar to the navigation data transmitted by the navigation satellites, and can therefore be used by the receiver to correct the downloaded navigation data bits. Thus many of the bits of a downloaded navigation word, especially the higher order significant bits of the word can be corrected. The remaining bit errors can be resolved based on a parity check of the word.
摘要翻译：本发明提供了能够在弱信号条件下能够下载导航数据的独立接收机的系统和方法。在一个实施例中，独立导航接收机基于存储在接收机中的卫星的跟踪历史来生成预测的卫星轨道。跟踪历史包括先前从卫星接收的历史导航数据。接收机使用预测的卫星轨道来生成导航数据，如星历和年历。由于预测的卫星是准确的，因此所生成的导航数据与由导航卫星发送的导航数据相似，因此可由接收机使用以校正下载的导航数据比特。因此，可以校正下载的导航字的许多位，特别是该字的高阶有效位。可以基于字的奇偶校验来解决剩余的位错误。

25. 发明授权

US07535414B2 Navigational positioning without timing information 有权
标题翻译：导航定位无定时信息
公开(公告)号：US07535414B2
公开(公告)日：2009-05-19
申请号：US11759769
申请日：2007-06-07
申请人： Shaowei Han
发明人： Shaowei Han
IPC分类号： G01S1/02 , G01S5/14
CPC分类号： G01S19/256 , G01S19/45
摘要： Provided herein are systems and methods that enable a navigation receiver to determine receiver position using a low ppm (Parts Per Million) Real Time Clock (RTC) under weak satellite signal reception conditions without the need for timing information from navigation satellites or aiding systems. Under weak signal conditions, the receiver is unable to demodulate navigation data bits but may be able to synchronize with the one ms PN sequences and 20 ms data bit edges of a received signal. In this case, the receiver is unable to determine the signal travel time from the navigation data bits resulting in one ms and/or 20 ms integer ambiguities in the travel time. Systems and methods are provided for resolving these one ms and/or 20 ms integer ambiguities and correct or reconstruct the pseudorange measurements accordingly. The reconstructed pseudorange measurements are used to accurately determine the receiver position.
摘要翻译：本文提供的系统和方法使得导航接收机能够在弱卫星信号接收条件下使用低ppm（百万分之几）实时时钟（RTC）来确定接收机位置，而不需要来自导航卫星或辅助系统的定时信息。在弱信号条件下，接收机不能解调导航数据位，但是可能能够与接收到的信号的1ms PN序列和20ms数据比特边沿同步。在这种情况下，接收机不能从导航数据位确定信号行进时间，导致行进时间中的一毫秒和/或20毫秒的整数模糊度。提供了用于解决这些1ms和/或20ms整数模糊度的系统和方法，并相应地校正或重构伪距测量。重建的伪距测量用于准确地确定接收机的位置。

26. 发明申请

US20080270026A1 METHOD AND APPARATUS IN POSITIONING WITHOUT BROADCAST EPHEMERIS 有权
标题翻译：没有广泛的EPHEMERIS的定位方法和设备
公开(公告)号：US20080270026A1
公开(公告)日：2008-10-30
申请号：US11741448
申请日：2007-04-27
申请人： Shaowei Han
发明人： Shaowei Han
IPC分类号： G01C21/20
CPC分类号： G01S19/25 , G01S19/27
摘要： 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.
摘要翻译：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。

27. 发明申请

US20080111738A1 METHOD AND APPARATUS IN STANDALONE POSITIONING WITHOUT BROADCAST EPHEMERIS 有权
标题翻译：没有广泛的EPHEMERIS的STANDALONE定位的方法和装置
公开(公告)号：US20080111738A1
公开(公告)日：2008-05-15
申请号：US11558614
申请日：2006-11-10
申请人： Shaowei Han
发明人： Shaowei Han
IPC分类号： G01S5/14
CPC分类号： G01S19/27
摘要： The present invention provides methods and system for enabling a standalone navigation receiver capable of generating receiver specific predicted satellite orbits based on historical navigation data collected by and stored in the receiver. Thus, the navigation receiver is able to use the predicted satellite orbits to obtain better Time-To-First-Fix (TTFF) and position accuracy without the need of connecting to a remote server and the associated communications system. In an embodiment, a standalone navigation receiver having sufficient memory collects navigation data from navigation satellites and generates predicted satellite orbits using the collected navigation data. Under weak signal conditions when decoding of the navigation data is not possible, the receiver uses the predicted satellite orbits to predict the accurate satellite positions or the set of ephemeris and the associated pseudoranges. The predicted orbits may be accurate for several days without the reception of broadcast ephemeris.
摘要翻译：本发明提供了能够基于由接收机收集和存储的历史导航数据产生能够产生接收机专用预测卫星轨道的独立导航接收机的方法和系统。因此，导航接收机能够使用预测的卫星轨道来获得更好的时间优先（TTFF）和位置精度，而不需要连接到远程服务器和相关联的通信系统。在一个实施例中，具有足够存储器的独立导航接收器从导航卫星收集导航数据并使用所收集的导航数据产生预测的卫星轨道。在导航数据解码不可能的弱信号条件下，接收机使用预测的卫星轨道来预测精确的卫星位置或星历集和相关联的伪距。预测的轨道可能准确几天而没有接收广播星历。

28. 发明授权

US07324045B2 System and method for fast initialization of navigational satellite signal receivers 有权
标题翻译：导航卫星信号接收机快速初始化的系统和方法
公开(公告)号：US07324045B2
公开(公告)日：2008-01-29
申请号：US11124413
申请日：2005-05-06
申请人： Jun Mo , Hansheng Wang , Chi-Shin Wang , Shaowei Han , Kudrethaya A. Shridhara
发明人： Jun Mo , Hansheng Wang , Chi-Shin Wang , Shaowei Han , Kudrethaya A. Shridhara
IPC分类号： G01S1/00 , H04B7/185 , H04B1/00
CPC分类号： G01S19/28
摘要： The present invention provides a method and apparatus for a satellite navigation receiver to lock onto satellite signals in the cold start mode with no information on the receiver position, the satellite position, or time estimates stored in the receiver's memory. All satellites in a positioning system are divided into groups based on the satellite constellation structure. In an embodiment, the positioning system is the Global Positioning System (GPS) and all GPS satellites are divided into three groups. During initialization of the receiver, the satellites are searched per group to lock onto at least one satellite signal. Other satellites are then searched in a given order based on their respective distance or proximity to the first satellite acquired. This method reduces the Time-to-First-Fix (TTFF) ordinarily required by conventional receivers in the cold start mode.
摘要翻译：本发明提供了一种用于卫星导航接收机在冷启动模式下锁定卫星信号的方法和装置，其中没有关于存储在接收机的存储器中的接收机位置，卫星位置或时间估计的信息。基于卫星星座结构将定位系统中的所有卫星分成几组。在一个实施例中，定位系统是全球定位系统（GPS），所有GPS卫星分为三组。在接收机的初始化期间，每组搜索卫星以锁定至少一个卫星信号。然后根据其相应的距离或与所获取的第一卫星的距离，以给定的顺序搜索其他卫星。这种方法减少了常规接收机在冷启动模式下通常要求的首次固定时间（TTFF）。

29. 发明授权

US07298319B2 Automatic decorrelation and parameter tuning real-time kinematic method and apparatus 有权
标题翻译：自动去相关和参数调整实时运动学方法和装置
公开(公告)号：US07298319B2
公开(公告)日：2007-11-20
申请号：US10826270
申请日：2004-04-19
申请人： Shaowei Han , Liwen Dai
发明人： Shaowei Han , Liwen Dai
IPC分类号： G01S5/14 , G01C21/20
CPC分类号： G01S19/44
摘要： A method of and computer-readable medium containing instructions for high accuracy, reliable position determination. The ADAPT-RTK Technology (Automatic Decorrelation and Parameter Tuning Real-Time Kinematic technology) is described using an innovative decorrelation algorithm to decorrelate the correlation between L1 and L2 measurements through a functional model and a stochastic model reducing the impact on performance of distance dependent biases.
摘要翻译：包含用于高精度，可靠位置确定的指令的方法和计算机可读介质。使用创新的去相关算法描述ADAPT-RTK技术（自动相关和参数调谐实时运动技术），通过功能模型和随机模型去除关联L1和L2测量之间的相关性，从而降低对距离相关偏差的影响。

30. 发明申请

US20070211793A1 Multipath error estimation in satellite navigation receivers 有权
标题翻译：卫星导航接收机中的多径误差估计
公开(公告)号：US20070211793A1
公开(公告)日：2007-09-13
申请号：US11372739
申请日：2006-03-09
申请人： Shaowei Han
发明人： Shaowei Han
IPC分类号： H04B1/00
CPC分类号： G01S19/37 , G01S19/22 , G01S19/24 , H04B1/709 , H04B1/7117
摘要： The invention presented in this disclosure gives methods to estimate and compensate for the multi-path in a typical navigational or spread spectrum receiver. The multi-path delay is estimated based on the outputs of different correlators of the receiver. Unlike three correlators normally used, the present disclosure uses five correlators, namely, Early2 (E2), Early1 (E1), Prompt (P), Late1 (L1) and Late2 (L2). The possible multi-path scenarios are classified into six different cases depending upon the reflected signal delay and the errors are computed. Further, the algorithm in the present disclosure can be extended to any correlators spacing.
摘要翻译：在本公开中呈现的本发明提供了估计和补偿典型导航或扩频接收机中的多路径的方法。基于接收机的不同相关器的输出来估计多径延迟。不同于通常使用的三个相关器，本公开使用五个相关器，即早期2（E 2），早期1（E 1），提示（P），延迟1（L 1）和后期2（L 2）。根据反射的信号延迟，可能的多路径情景分为六种不同的情况，并计算出误差。此外，本公开中的算法可以扩展到任何相关器间隔。

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