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    Device and method for orbit determination and prediction of satellites providing signals to users
    1.
    发明授权
    Device and method for orbit determination and prediction of satellites providing signals to users 失效
    用于向使用者提供信号的卫星的轨道确定和预测的装置和方法

    公开(公告)号：US08095312B2

    公开(公告)日：2012-01-10

    申请号：US12181750

    申请日：2008-07-29

    申请人： Hans L. Trautenberg ,  Michael Kirchner

    发明人： Hans L. Trautenberg ,  Michael Kirchner

    IPC分类号： G01C21/00 ,  G01S19/01

    CPC分类号： B64G1/24 ,  B64G1/1014 ,  B64G1/36 ,  G01S19/02

    摘要： A device and method for orbit prediction of satellites are provided. An accelerometer measures non-gravity forces acting on a satellite. A processor receives measured non-gravity forces from the accelerometer, estimates the contributions of the measured non-gravity forces to the movement of the satellite, and predicts the orbit of the satellite based on the estimated contributions of the non-gravity forces to the movement of the satellite.

    摘要翻译： 提供了一种用于卫星轨道预测的装置和方法。 加速度计测量作用在卫星上的非重力。 处理器从加速度计接收测量的非重力，估计测量的非重力对卫星运动的贡献，并根据非重力对运动的估计贡献预测卫星的轨道 的卫星。

    INTEGRATED POSITIONING SOLUTION FOR GLOBAL NAVIGATION SATELLITE SYSTEMS
    4.
    发明申请
    INTEGRATED POSITIONING SOLUTION FOR GLOBAL NAVIGATION SATELLITE SYSTEMS 审中-公开
    用于全球导航卫星系统的集成定位解决方案

    公开(公告)号：US20090322602A1

    公开(公告)日：2009-12-31

    申请号：US12138722

    申请日：2008-06-13

    申请人： Michael KIRCHNER ,  Tanja Rang ,  Hans L. Trautenberg

    发明人： Michael KIRCHNER ,  Tanja Rang ,  Hans L. Trautenberg

    IPC分类号： G01S1/00

    CPC分类号： G01S19/02 ,  B64G1/36 ,  G01S19/05 ,  G01S19/08 ,  G01S19/33

    摘要： The invention includes a process for one's own global navigation satellite system and at least one other global navigation satellite system including the following: Receiving ranging signals and navigation messages or ranging signals only from the at least one other global navigation satellite system, and processing the received ranging signals and navigation messages in a similar way as the ranging signals and navigation messages of the owned global navigation satellite system.

    摘要翻译： 本发明包括一个用于自己的全球导航卫星系统和至少一个其它全球导航卫星系统的方法，该系统包括以下：仅从至少一个其它全球导航卫星系统接收测距信号和导航消息或测距信号，并处理所接收的 测距信号和导航消息的方式与所属全球导航卫星系统的测距信号和导航信息相似。

    RAIM algorithm
    6.
    发明授权
    RAIM algorithm 有权
    RAIM算法

    公开(公告)号：US08610623B2

    公开(公告)日：2013-12-17

    申请号：US13165950

    申请日：2011-06-22

    申请人： Hans L. Trautenberg

    发明人： Hans L. Trautenberg

    IPC分类号： G01S19/19

    CPC分类号： G01S19/20

    摘要： Methods and apparatus for implementing a receiver autonomous integrity monitoring (RAIM) algorithm are provided. The RAIM algorithm is for determining an integrity risk in a global navigation satellite system (GNSS) by processing several ranging signals received from satellites of the GNSS. The algorithm involves determining several integrity risks at an alert limit for different fault conditions of the ranging signals, and determining an overall integrity risk at the alert limit from the determined several integrity risks.

    摘要翻译： 提供了一种用于实现接收机自主完整性监控（RAIM）算法的方法和装置。 RAIM算法用于通过处理从GNSS的卫星接收的多个测距信号来确定全球导航卫星系统（GNSS）中的完整性风险。 该算法涉及在测距信号的不同故障状况的警报极限下确定几个完整性风险，以及从确定的几个完整性风险确定警报极限处的整体完整性风险。

    Method for the transmission of additional data along with navigation messages in a satellite navigation system
    7.
    发明授权
    Method for the transmission of additional data along with navigation messages in a satellite navigation system 失效
    用于在卫星导航系统中传输附加数据以及导航消息的方法

    公开(公告)号：US08473210B2

    公开(公告)日：2013-06-25

    申请号：US12808096

    申请日：2008-12-15

    申请人： Hans L. Trautenberg

    发明人： Hans L. Trautenberg

    IPC分类号： G01C21/24

    CPC分类号： G01S19/39 ,  G01S19/02

    摘要： A method for transmitting additional information in a satellite navigation system includes providing a navigation message having a plurality of parameters, selecting at least one parameter from the plurality of parameters for the transmitting of the additional information, replacing the at least one parameter, at least partially, by the additional information so as to form a changed navigation message, and sending the changed navigation message.

    摘要翻译： 一种用于在卫星导航系统中发送附加信息的方法包括提供具有多个参数的导航消息，从多个参数中选择至少一个参数来传送附加信息，至少部分替换至少一个参数 ，通过附加信息形成改变的导航消息，并发送改变的导航消息。

    RAIM Algorithm
    8.
    发明申请
    RAIM Algorithm 有权
    RAIM算法

    公开(公告)号：US20110316737A1

    公开(公告)日：2011-12-29

    申请号：US13165950

    申请日：2011-06-22

    申请人： Hans L. Trautenberg

    发明人： Hans L. Trautenberg

    IPC分类号： G01S19/20

    CPC分类号： G01S19/20

    摘要： Methods and apparatus for implementing a receiver autonomous integrity monitoring (RAIM) algorithm are provided. The RAIM algorithm is for determining an integrity risk in a global navigation satellite system (GNSS) by processing several ranging signals received from satellites of the GNSS. The algorithm involves determining several integrity risks at an alert limit for different fault conditions of the ranging signals, and determining an overall integrity risk at the alert limit from the determined several integrity risks.

    摘要翻译： 提供了一种用于实现接收机自主完整性监控（RAIM）算法的方法和装置。 RAIM算法用于通过处理从GNSS的卫星接收的多个测距信号来确定全球导航卫星系统（GNSS）中的完整性风险。 该算法涉及在测距信号的不同故障状况的警报极限下确定几个完整性风险，以及从确定的几个完整性风险确定警报极限处的整体完整性风险。

    Method and apparatus for integrity communication in a navigation satellite system
    9.
    发明授权
    Method and apparatus for integrity communication in a navigation satellite system 失效
    导航卫星系统完整性通信的方法和装置

    公开(公告)号：US08072375B2

    公开(公告)日：2011-12-06

    申请号：US12634295

    申请日：2009-12-09

    申请人： Hans L. Trautenberg

    发明人： Hans L. Trautenberg

    IPC分类号： G01S19/02

    CPC分类号： G01S19/08 ,  G01S19/02

    摘要： For integrity communication, a navigation satellite system has a space segment with satellites that emit navigation signals for reception and analysis by user systems, and a ground segment with observation stations that monitor the satellites. The ground segment controls cause distribution of integrity information concerning the satellites to user systems with the navigation signals. The integrity information has a first SISMA value and a second broadcast SISMA value for the accuracy of the satellite monitored by the ground segment. The second broadcast SISMA value takes into account a failure of an observation station of the ground segment, and a threshold value for the second broadcast SISMA value is provided. The threshold value with the integrity information for a satellite is transmitted instead of the second broadcast SISMA value when the latter exceeds the threshold value and the first SISMA value is lower than the threshold value for the satellite. The integrity information to be transmitted when the second broadcast SISMA value and the first SISMA value for the satellite each exceed the threshold value.

    摘要翻译： 对于完整性通信，导航卫星系统具有卫星的空间段，其发射用于用户系统的接收和分析的导航信号，以及具有监测卫星的观测站的地面段。 地面段控制导致有关卫星的完整性信息分配给具有导航信号的用户系统。 完整性信息具有第一SISMA值和第二广播SISMA值，用于由地面段监视的卫星的精度。 第二广播SISMA值考虑到地面段的观测站的故障，并且提供第二广播SISMA值的阈值。 当后者超过阈值并且第一SISMA值低于卫星的阈值时，发送具有用于卫星的完整性信息的阈值而不是第二广播SISMA值。 当卫星的第二广播SISMA值和第一SISMA值都超过阈值时要发送的完整性信息。

    Method and apparatus for monitoring the integrity of satellite navigation signals
    10.
    发明授权
    Method and apparatus for monitoring the integrity of satellite navigation signals 失效
    监测卫星导航信号完整性的方法和装置

    公开(公告)号：US07924221B2

    公开(公告)日：2011-04-12

    申请号：US12252944

    申请日：2008-10-16

    申请人： Hans L. Trautenberg

    发明人： Hans L. Trautenberg

    IPC分类号： G01S19/08 ,  G01S5/04

    CPC分类号： G01S19/08 ,  G01S19/20

    摘要： A method for monitoring the integrity of satellite navigation system includes a first detection of integrity problems, in which the same entity of a navigation signal from a particular satellite is received at different sites, and evaluated to estimate the error of the entity and the error made during the error estimation process. In a second detection, navigation signals received from a specific satellite are measured and evaluated to estimate the error of the entity and the error in the error estimation process. Finally, in a third detection, several navigation signals from different satellites are measured, and evaluated to estimate the error of the entity and the error made in the error estimation process. Integrity problems which are detectable in the first and second detections are taken into account only if it is probable that they occur during the third detection, and have not been discovered during the first and second detection.

    摘要翻译： 一种用于监测卫星导航系统完整性的方法包括对完整性问题的第一次检测，其中来自特定卫星的导航信号的相同实体在不同地点被接收，并被评估以估计实体的误差和所做出的误差 在错误估计过程中。 在第二检测中，测量并评估从特定卫星接收的导航信号，以估计实体的误差和误差估计过程中的误差。 最后，在第三次检测中，测量了来自不同卫星的若干导航信号，并对该实体的误差和误差估计过程中产生的误差进行了估计。 只有在第三次检测期间可能出现第一次检测和第二次检测时才能检测到的完整性问题，并且在第一次检测和第二次检测期间尚未发现完整性问题。