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1. 发明授权

US10416310B2 Integrated positioning solution for global navigation satellite systems 有权
公开(公告)号：US10416310B2
公开(公告)日：2019-09-17
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： G01S19/02 , G01S19/05 , G01S19/08 , G01S19/33 , B64G1/36
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.

2. 发明授权

US08289153B2 Dissemination of critical atmospheric conditions within global and regional navigation satellite systems 有权
标题翻译：在全球和区域导航卫星系统内传播关键大气条件
公开(公告)号：US08289153B2
公开(公告)日：2012-10-16
申请号：US12138728
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： G08B1/08
CPC分类号： G01W1/00 , G01K2203/00 , G01S19/02 , G01S19/13 , G01S19/40
摘要： The invention relates to an apparatus for a regional or global navigation satellite system that includes an arrangement for receiving additional data or navigation messages from the navigation satellite system, and an arrangement for informing or alarming the user that critical atmospheric conditions occur, whereby the additional data or the navigation messages include atmospheric information.
摘要翻译：本发明涉及一种用于区域或全球导航卫星系统的装置，其包括用于从导航卫星系统接收附加数据或导航消息的装置，以及用于向用户通报或警告发生关键大气条件的装置，由此附加数据或导航信息包括大气信息。

3. 发明申请

US20090322602A1 INTEGRATED POSITIONING SOLUTION FOR GLOBAL NAVIGATION SATELLITE SYSTEMS 审中-公开
标题翻译：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。

4. 发明申请

US20090322515A1 DISSEMINATION OF CRITICAL ATMOSPHERIC CONDITIONS WITHIN GLOBAL AND REGIONAL NAVIGATION SATELLITE SYSTEMS 有权
标题翻译：全球和区域性导航卫星系统中的关键大气条件的揭示
公开(公告)号：US20090322515A1
公开(公告)日：2009-12-31
申请号：US12138728
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： G08B1/08 , G01W1/00
CPC分类号： G01W1/00 , G01K2203/00 , G01S19/02 , G01S19/13 , G01S19/40
摘要： The invention relates to an apparatus for a regional or global navigation satellite system that includes an arrangement for receiving additional data or navigation messages from the navigation satellite system, and an arrangement for informing or alarming the user that critical atmospheric conditions occur, whereby the additional data or the navigation messages include atmospheric information.
摘要翻译：本发明涉及一种用于区域或全球导航卫星系统的装置，其包括用于从导航卫星系统接收附加数据或导航消息的装置，以及用于向用户通报或警告发生关键大气条件的装置，由此附加数据或导航信息包括大气信息。

5. 发明申请

US20100141511A1 Method for Increasing the Availability of a Global Navigation System 失效
标题翻译：增加全球导航系统可用性的方法
公开(公告)号：US20100141511A1
公开(公告)日：2010-06-10
申请号：US12525964
申请日：2008-02-01
申请人： Tanja Rang , Hans L. Trautenberg
发明人： Tanja Rang , Hans L. Trautenberg
IPC分类号： G01S19/41
CPC分类号： G01S19/20
摘要： A process for increasing the availability of a global navigation system that includes a plurality of spacecraft, each of which transmits information for determining the position of a terminal. From the plurality of spacecraft, a first subset, with at least one spacecraft, and a second subset are determined. the second subset being constituted by those spacecraft that are not included in the first subset. The integrity risk is determined for the information transmitted only by the second spacecraft. The first and the second subsets of spacecraft are determined such that the integrity risk, for information transmitted by the second subset spacecraft minimized relative to the integrity risk for information of all spacecraft included in the plurality of spacecraft.
摘要翻译：一种用于增加包括多个航天器的全球导航系统的可用性的过程，每个航天器都发送用于确定终端的位置的信息。从多个航天器中确定具有至少一个航天器的第一子集和第二子集。第二子集由那些不包括在第一子集中的那些航天器构成。对于仅由第二航天器传送的信息确定完整性风险。确定航天器的第一和第二子集，使得由第二子集航天器传输的信息相对于包括在多个航天器中的所有航天器的信息的完整性风险最小化的完整性风险。

6. 发明授权

US07595749B2 Method and device for relative time and position determination for moving objects based on one-way and two-way measurements 失效
标题翻译：基于单向和双向测量的移动物体相对时间和位置确定的方法和装置
公开(公告)号：US07595749B2
公开(公告)日：2009-09-29
申请号：US11802074
申请日：2007-05-18
申请人： Tanja Rang , Hans L. Trautenberg
发明人： Tanja Rang , Hans L. Trautenberg
IPC分类号： G01S1/00 , G01C21/00 , G05D1/02 , H04B7/19
CPC分类号： G01S5/0289 , G01S19/02
摘要： In a method for relative time and position determinations for moving objects of a constellation, signals by the objects are isochronously transmitted, with each object transmitting a unique signal for that object. The received signals of each object of the constellation are transmitted to all other objects of the constellation after a predetermined waiting time.
摘要翻译：在用于移动星座运动对象的相对时间和位置确定的方法中，对象的信号被等时发送，每个对象传送该对象的唯一信号。在预定的等待时间之后，将星座的每个对象的接收信号发送到星座的所有其它对象。

7. 发明授权

US08094069B2 Method for increasing the availability of a global navigation system 失效
标题翻译：增加全球导航系统可用性的方法
公开(公告)号：US08094069B2
公开(公告)日：2012-01-10
申请号：US12525964
申请日：2008-02-01
申请人： Tanja Rang , Hans L. Trautenberg
发明人： Tanja Rang , Hans L. Trautenberg
IPC分类号： G01S19/20
CPC分类号： G01S19/20
摘要： A process for increasing the availability of a global navigation system that includes a plurality of spacecraft, each of which transmits information for determining the position of a terminal. From the plurality of spacecraft, a first subset, with at least one spacecraft, and a second subset are determined, the second subset being constituted by those spacecraft that are not included in the first subset. The integrity risk is determined for the information transmitted only by the second spacecraft. The first and the second subsets of spacecraft are determined such that the integrity risk, for information transmitted by the second subset spacecraft minimized relative to the integrity risk for information of all spacecraft included in the plurality of spacecraft.
摘要翻译：一种用于增加包括多个航天器的全球导航系统的可用性的过程，每个航天器都发送用于确定终端的位置的信息。从多个航天器确定具有至少一个航天器和第二子集的第一子集，第二子集由未包括在第一子集中的那些航天器构成。对于仅由第二航天器传送的信息确定完整性风险。确定航天器的第一和第二子集，使得由第二子集航天器传输的信息相对于包括在多个航天器中的所有航天器的信息的完整性风险最小化的完整性风险。

8. 发明申请

US20070273579A1 Method and device for relative time and position determination for moving objects based on one-way and two-way measurements 失效
标题翻译：基于单向和双向测量的移动物体相对时间和位置确定的方法和装置
公开(公告)号：US20070273579A1
公开(公告)日：2007-11-29
申请号：US11802074
申请日：2007-05-18
申请人： Tanja Rang , Hans L. Trautenberg
发明人： Tanja Rang , Hans L. Trautenberg
IPC分类号： H04B7/185 , G01C21/00
CPC分类号： G01S5/0289 , G01S19/02
摘要： In a method for relative time and position determinations for moving objects of a constellation, signals by the objects are isochronously transmitted, with each object transmitting a unique signal for that object. The received signals of each object of the constellation are transmitted to all other objects of the constellation after a predetermined waiting time.
摘要翻译：在用于移动星座运动对象的相对时间和位置确定的方法中，对象的信号被等时发送，每个对象传送该对象的唯一信号。在预定的等待时间之后，将星座的每个对象的接收信号发送到星座的所有其它对象。

9. 发明授权

US08095312B2 Device and method for orbit determination and prediction of satellites providing signals to users 失效
标题翻译：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。

10. 发明授权

US08610623B2 RAIM algorithm 有权
标题翻译： 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。

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