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Patent Agency Ranking
1.发明授权Systems and methods for providing a visualization of satellite sightline obstructions 有权提供卫星视线障碍物可视化的系统和方法公开(公告)号：US09235923B1
公开(公告)日：2016-01-12
申请号：US14039777
申请日：2013-09-27
Applicant: Google Inc.
Inventor： Craig Lewin Robinson , James Brian Roseborough , Daniel Joseph Filip
CPC classification number: G06T11/60 , G06T17/05 , G06T19/006 , H04B7/18519 , H04B7/18554 , H04N5/23238 , H04W16/22
Abstract: Systems and methods for providing a visualization of satellite sightline obstructions are provided. An example method includes identifying an approximate position of a receiver antenna. The method further includes providing a rendering of a physical environment surrounding the receiver antenna for display within a user interface. The user interface can be provided on a display. Satellite positional data associated with the position of a satellite is accessed and a sightline between the approximate position of the receiver antenna and the position of the satellite is determined. The method further includes presenting the sightline within the user interface in association with the rendering. An example system includes a data capture system and a computing device to provide a visualization of satellite sightline obstructions.
Abstract translation: 提供了提供卫星视线障碍物可视化的系统和方法。 示例性方法包括识别接收机天线的近似位置。 该方法还包括提供围绕接收机天线的物理环境的渲染，以在用户界面内显示。 可以在显示器上提供用户界面。 与卫星的位置相关联的卫星位置数据被访问，并且确定接收机天线的近似位置与卫星的位置之间的视线。 所述方法还包括在所述呈现的关联下在所述用户界面内呈现所述视线。 示例系统包括数据捕获系统和计算设备，以提供卫星视线障碍物的可视化。
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2.发明授权Systems and methods for estimating attitude using double differenced GPS carrier phase measurements 有权使用双差分GPS载波相位测量估计姿态的系统和方法公开(公告)号：US09529093B2
公开(公告)日：2016-12-27
申请号：US14054396
申请日：2013-10-15
Applicant: Google Inc.
CPC classification number: G01S19/54
Abstract: Systems and methods for estimating attitude using double differenced GPS carrier phase measurements are provided. An exemplary computer-implemented method includes obtaining, by one or more computing devices, an initial candidate attitude. The method includes determining, by the one or more computing devices, a plurality of expected double differenced carrier phase values based on the initial candidate attitude. The method includes inputting, by the one or more computing devices, the plurality of expected double differenced carrier phase values into a cost function. The cost function respectively compares the plurality of expected double differenced carrier phase values to a plurality of measured double differenced carrier phase values. The method includes minimizing, by the one or more computing devices, the cost function. The method includes selecting, by the one or more computing devices, a final candidate attitude associated with the minimized cost function as the attitude of the device.
Abstract translation: 提供了使用双差分GPS载波相位测量来估计姿态的系统和方法。 示例性的计算机实现的方法包括由一个或多个计算设备获得初始候选姿态。 该方法包括由一个或多个计算设备基于初始候选姿态来确定多个预期的双差分载波相位值。 该方法包括通过一个或多个计算设备将多个预期的双差分载波相位值输入到成本函数中。 成本函数分别将多个预期双差分载波相位值与多个测量的双差分载波相位值相比较。 该方法包括通过一个或多个计算设备来最小化成本函数。 该方法包括由一个或多个计算设备选择与最小化成本函数相关联的最终候选姿势作为设备的姿态。
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公开(公告)号：US09679406B2
公开(公告)日：2017-06-13
申请号：US14991380
申请日：2016-01-08
Applicant: Google Inc.
Inventor： Craig Lewin Robinson , James Brian Roseborough , Daniel Joseph Filip
CPC classification number: G06T11/60 , G06T17/05 , G06T19/006 , H04B7/18519 , H04B7/18554 , H04N5/23238 , H04W16/22
Abstract: Systems and methods for providing a visualization of satellite sightline obstructions are provided. An example method includes identifying an approximate position of a receiver antenna. The method further includes providing a rendering of a physical environment surrounding the receiver antenna for display within a user interface. The user interface can be provided on a display. Satellite positional data associated with the position of a satellite is accessed and a sightline between the approximate position of the receiver antenna and the position of the satellite is determined. The method further includes presenting the sightline within the user interface in association with the rendering. An example system includes a data capture system and a computing device to provide a visualization of satellite sightline obstructions.
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4.发明申请Systems and Methods for Estimating Attitude Using Double Differenced GPS Carrier Phase Measurements 有权使用双差分GPS载波相位测量估计姿态的系统和方法公开(公告)号：US20150168562A1
公开(公告)日：2015-06-18
申请号：US14054396
申请日：2013-10-15
Applicant: Google Inc.
IPC: G01S19/54
CPC classification number: G01S19/54
Abstract: Systems and methods for estimating attitude using double differenced GPS carrier phase measurements are provided. An exemplary computer-implemented method includes obtaining, by one or more computing devices, an initial candidate attitude. The method includes determining, by the one or more computing devices, a plurality of expected double differenced carrier phase values based on the initial candidate attitude. The method includes inputting, by the one or more computing devices, the plurality of expected double differenced carrier phase values into a cost function. The cost function respectively compares the plurality of expected double differenced carrier phase values to a plurality of measured double differenced carrier phase values. The method includes minimizing, by the one or more computing devices, the cost function. The method includes selecting, by the one or more computing devices, a final candidate attitude associated with the minimized cost function as the attitude of the device.
Abstract translation: 提供了使用双差分GPS载波相位测量来估计姿态的系统和方法。 示例性的计算机实现的方法包括由一个或多个计算设备获得初始候选姿态。 该方法包括由一个或多个计算设备基于初始候选姿态来确定多个预期的双差分载波相位值。 该方法包括通过一个或多个计算设备将多个预期的双差分载波相位值输入到成本函数中。 成本函数分别将多个预期双差分载波相位值与多个测量的双差分载波相位值相比较。 该方法包括通过一个或多个计算设备来最小化成本函数。 该方法包括由一个或多个计算设备选择与最小化成本函数相关联的最终候选姿势作为设备的姿态。
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5.发明申请公开(公告)号：US20160125634A1
公开(公告)日：2016-05-05
申请号：US14991380
申请日：2016-01-08
Applicant: Google Inc.
Inventor： Craig Lewin Robinson , James Brian Roseborough , Daniel Joseph Filip
CPC classification number: G06T11/60 , G06T17/05 , G06T19/006 , H04B7/18519 , H04B7/18554 , H04N5/23238 , H04W16/22
Abstract: Systems and methods for providing a visualization of satellite sightline obstructions are provided. An example method includes identifying an approximate position of a receiver antenna. The method further includes providing a rendering of a physical environment surrounding the receiver antenna for display within a user interface. The user interface can be provided on a display. Satellite positional data associated with the position of a satellite is accessed and a sightline between the approximate position of the receiver antenna and the position of the satellite is determined. The method further includes presenting the sightline within the user interface in association with the rendering. An example system includes a data capture system and a computing device to provide a visualization of satellite sightline obstructions.
Abstract translation: 提供了提供卫星视线障碍物可视化的系统和方法。 示例性方法包括识别接收机天线的近似位置。 该方法还包括提供围绕接收机天线的物理环境的渲染，以在用户界面内显示。 可以在显示器上提供用户界面。 与卫星的位置相关联的卫星位置数据被访问，并且确定接收机天线的近似位置与卫星的位置之间的视线。 所述方法还包括在所述呈现的关联下在所述用户界面内呈现所述视线。 示例系统包括数据捕获系统和计算设备，以提供卫星视线障碍物的可视化。
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