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1.发明授权公开(公告)号：US09244280B1
公开(公告)日：2016-01-26
申请号：US14225062
申请日：2014-03-25
CPC分类号： G02B27/0172 , G02B27/0093 , G02B27/01 , G02B27/0101 , G02B27/0149 , G02B27/017 , G02B27/14 , G02B2027/011 , G02B2027/0138 , G02B2027/014 , G02B2027/0141 , G02B2027/0165 , G02B2027/0187 , G06F3/147 , G09G5/00 , G09G2330/08 , G09G2340/12 , G09G2380/12
摘要： An apparatus provides a virtual display in an environment for various applications including avionic, naval, military, remote control, medical and other applications. The apparatus can be a near eye display, such as, a head up display (HUD) or head worn display (e.g., helmet mounted display (HMD), glasses-based, goggle-based, visor-based, etc.). The near eye display can include a combiner for providing one or more of: an image for a failed display, an image between two or more head down displays, or an image to direct attention to warnings or locations in the field-of-view of the combiner.
摘要翻译： 一种装置在包括航空电子，海军，军事，遥控，医疗和其他应用在内的各种应用的环境中提供虚拟显示。 该装置可以是近眼显示器，例如头部显示器（HUD）或头戴式显示器（例如，头盔安装显示器（HMD），基于眼镜的护目镜，基于面罩的等）。 近眼显示器可以包括用于提供以下各项中的一个或多个的组合器：用于故障显示的图像，两个或更多头下显示之间的图像，或者用于引导注意视场中的警告或位置的图像 组合器。
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公开(公告)号：US09785231B1
公开(公告)日：2017-10-10
申请号：US14038597
申请日：2013-09-26
CPC分类号： G06F3/012 , G02B27/0093 , G02B27/01 , G02B27/017 , G02B2027/0187 , G02B2027/0198 , G06F3/0346 , G06F11/1637
摘要： A head worn display system (e.g., helmet mounted (HMD) display system, and an eye wear mounted display system,) can include a combiner, a head position sensor and a computer. The computer provides symbology in response to first sensor input values associated with the head position. The symbology can be conformal with a real world scene. A monitoring system includes a redundant head position sensor for providing second sensor input values associated with head position. The computer monitors for positional accuracy of the symbology by comparing symbology calculated using the first and second input sensor values or by using an inverse function to compare sensor values.
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公开(公告)号：US09244281B1
公开(公告)日：2016-01-26
申请号：US14038400
申请日：2013-09-26
IPC分类号： G02B27/01
CPC分类号： G02B27/0176 , G02B27/01 , G02B2027/0154
摘要： An apparatus provides a virtual display in an environment for various applications including avionic, naval, military, remote control, medical and other applications. The apparatus can be a head up display (HUD) or head worn display (e.g., helmet mounted display (HMD) and can include image sources disposed at a respective image source position, and a combiner detached from the image sources. The combiner is movable to a respective combiner position for receiving light from a respective image source of the image sources. The combiner provides an image from the respective image source to a user.
摘要翻译： 一种装置在包括航空电子，海军，军事，遥控，医疗和其他应用在内的各种应用的环境中提供虚拟显示。 该装置可以是头部显示器（HUD）或头戴式显示器（例如头戴式显示器（HMD）），并且可以包括设置在相应图像源位置处的图像源和从图像源分离的组合器，组合器可移动 到相应的组合器位置，用于接收来自图像源的相应图像源的光。组合器从相应的图像源向用户提供图像。
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公开(公告)号：US10001376B1
公开(公告)日：2018-06-19
申请号：US14626073
申请日：2015-02-19
申请人： Carlo L. Tiana , Sarah Barber
发明人： Carlo L. Tiana , Sarah Barber
CPC分类号： G01C21/005 , B64D43/00 , B64D47/08 , G01C21/20 , G01C23/005
摘要： An apparatus monitors position for an aircraft. The aircraft includes a display, a position system, a vision system and a database comprising terrain data associated with an environment at a location of the aircraft. The apparatus includes a monitoring processor configured to perform character recognition or structure recognition on the image data to identify a structure or a character in the image data, correlate a position of the structure or character in the environment using a position from the position system and the terrain data, and cause the display to provide a confirmation in response to the position of the structure or character in the terrain data matches the position of the structure or character in the image data.
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5.发明授权System, module, and method for presenting a flight director-dependent hits pathway on an aircraft display unit 有权用于在飞行器显示单元上呈现飞行指导器相关命中路径的系统，模块和方法公开(公告)号：US08965601B1
公开(公告)日：2015-02-24
申请号：US12284561
申请日：2008-09-23
申请人： Sarah Barber
发明人： Sarah Barber
IPC分类号： G06F7/70
CPC分类号： G01C23/005
摘要： A present novel and non-trivial system, apparatus, and method is disclosed for presenting a flight director-dependent highway in the sky (“HITS”) pathway on an aircraft display unit. A processor receives flight plan data and flight director data, generates HITS data set representative of a flight director-dependent HITS pathway using flight plan data and flight director data, and provides the HITS data set to a display system for presentation of the flight director-dependent HITS pathway on a tactical display unit. Flight plan data provided to the processor may comprise of data sourced by a navigation system or HITS pathway data generated independently of flight director data. When presented on a tactical display unit, the flight director-dependent HITS pathway may be depicted with the flight director, where the proximal end of the HITS pathway aligns with the flight director.
摘要翻译： 公开了一种目前的小型和非平凡的系统，装置和方法，用于在飞行器显示单元上的天空（“HITS”）路径中呈现飞行指导器相关高速公路。 处理器接收飞行计划数据和飞行总监数据，使用飞行计划数据和飞行总监数据生成代表飞行导向器相关HITS路径的HITS数据集，并将HITS数据集提供给显示系统以呈现飞行总监 - 依赖的HITS通路在战术显示单元上。 提供给处理器的飞行计划数据可以包括由导航系统提供的数据或独立于飞行总监数据产生的HITS路径数据。 当在战术显示单元上呈现时，可以用飞行总监描绘与飞行指导相关的HITS通道，其中HITS通道的近端与飞行主任对齐。
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6.发明授权Systems and methods for positioning a heading-based image within a track-based image and for generating steering commands to a steerable forward-looking image capture device of an enhanced vision system 有权用于在基于轨迹的图像中定位基于标题的图像并且用于向增强视觉系统的可操纵的前瞻性图像捕获装置产生转向命令的系统和方法公开(公告)号：US08831798B1
公开(公告)日：2014-09-09
申请号：US13246239
申请日：2011-09-27
申请人： Sarah Barber
发明人： Sarah Barber
CPC分类号： G01C23/00 , G01C21/00 , G06T7/00 , G06T7/38 , G06T15/30 , G06T19/003 , G06T2207/10016 , G06T2207/10032 , G06T2207/20221 , G06T2207/30252
摘要： Present novel and non-trivial systems and methods for positioning a heading-based image within a track-based image and for generating steering commands for a forward-looking image capture device of an enhanced vision system (“EVS”). The positioning system is comprised of a source of navigation data, a source of first image data representative of a track-based image, a source of second image data representative of a heading-based image, and an avionics system processor (“ASP”) configured to receive the navigation data, the first image data, and the second image data, determine image positioning data, and merge the first image data with the second image data as a function of the image positioning data. The steering commands generating system is comprised of a source of navigation data, the ASP configured to generate steering command data commensurate to a wind correction angle, and the EVS configured to receive the steering data.
摘要翻译： 目前用于在基于轨迹的图像中定位基于标题的图像并用于为增强的视觉系统（“EVS”）的前瞻性图像捕获装置生成转向命令的新型和非平凡的系统和方法。 该定位系统包括导航数据源，表示基于轨迹的图像的第一图像数据的源，代表基于标题的图像的第二图像数据的源和航空电子系统处理器（“ASP”）， 被配置为接收导航数据，第一图像数据和第二图像数据，确定图像定位数据，并且根据图像定位数据将第一图像数据与第二图像数据合并。 所述转向指令生成系统包括导航数据源，所述ASP被配置为生成与风修正角度相称的转向命令数据，并且所述EVS被配置为接收所述转向数据。
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7.发明授权System supporting flight operations under instrument meteorological conditions using precision course guidance 有权系统使用精准课程指导，在仪表气象条件下支持飞行运行公开(公告)号：US08615337B1
公开(公告)日：2013-12-24
申请号：US12284787
申请日：2008-09-25
申请人： Patrick D. McCusker , Sarah Barber , Felix B. Turcios , Douglas A. Bell , Richard D. Jinkins , Timothy J. Etherington , Michael J. Krenz , Charles B. Dirks
发明人： Patrick D. McCusker , Sarah Barber , Felix B. Turcios , Douglas A. Bell , Richard D. Jinkins , Timothy J. Etherington , Michael J. Krenz , Charles B. Dirks
CPC分类号： G01C21/20
摘要： The present examples provide circuits, systems, processes, and the like for providing precision course guidance, typically for improved positive course guidance below published minimum descent altitude or decision altitude, including just in time calculations of obstacle free flight paths. The calculated flight path may be presented in the context of a synthetic scene of the environment surrounding the aircraft. To provide precision course guidance, exemplary avionics systems, processes and the like, as described below may be utilized.
摘要翻译： 本示例提供电路，系统，过程等，用于提供精确的课程指导，通常用于在公开的最低下降高度或决策高度以下的改进的积极课程指导，包括刚刚在无障碍飞行路径的时间计算中。 计算的飞行路线可以在飞机周围的环境的合成场景的背景下呈现。 为了提供精确的课程指导，可以使用如下所述的示例性航空电子系统，过程等。
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8.发明授权Required navigation performance (RNP) scales for indicating permissible flight technical error (FTE) 有权所需的导航性能（RNP）表示允许的飞行技术误差（FTE）公开(公告)号：US07782229B1
公开(公告)日：2010-08-24
申请号：US11824140
申请日：2007-06-28
申请人： Sarah Barber
发明人： Sarah Barber
IPC分类号： G01C21/00
CPC分类号： G01C23/005
摘要： The present invention is a flight deck system for promoting accurate navigation of an aircraft. The system includes a memory configured for storing position information for the aircraft. The system further includes a processor which is configured for being communicatively coupled with the memory, the processor also being configured for receiving the aircraft position information stored in the memory. The system also includes a display which is configured for being communicatively coupled with the processor. The display is further configured for displaying a scaled indicator, the scaled indicator having been output to the display by the processor, the scaled indicator being based upon the received aircraft position information. The scaled indicator includes: a current position indicator for indicating an estimated current position of the aircraft, a desired position indicator for indicating a desired navigational position for the aircraft, and an allowable Flight Technical Error (FTE) indicator for indicating allowable Flight Technical Error (FTE) for the aircraft. Further, the current position indicator, the desired position indicator, and the FTE indicator are suitable for use by a pilot of the aircraft in maintaining the aircraft within established navigational boundaries.
摘要翻译： 本发明是用于促进飞行器的精确导航的驾驶舱系统。 该系统包括被配置用于存储飞行器的位置信息的存储器。 该系统还包括被配置为与存储器通信耦合的处理器，该处理器还被配置为接收存储在存储器中的飞行器位置信息。 该系统还包括被配置为与处理器通信耦合的显示器。 显示器还被配置为显示缩放的指示器，缩放的指示器已经被处理器输出到显示器，缩放的指示器基于接收的飞行器位置信息。 缩放的指示器包括：用于指示飞机的估计当前位置的当前位置指示器，用于指示飞机的期望导航位置的期望位置指示器和用于指示允许的飞行技术错误的允许的飞行技术错误（FTE）指示符 FTE）。 此外，当前位置指示器，期望位置指示器和FTE指示符适用于飞机的飞行员将飞机维持在已建立的导航边界内。
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公开(公告)号：US07724155B1
公开(公告)日：2010-05-25
申请号：US11517101
申请日：2006-09-07
IPC分类号： G01C23/00
CPC分类号： G01C23/00
摘要： An avionics display is disclosed. A synthetic rendering of terrain is created using stored terrain data. A horizon line is overlaid upon the synthetic rendering of terrain. The horizon line represents zero degrees pitch attitude in a direction of travel of an aircraft in which the avionics display is installed. The horizon line is configured to move in response to attitude-changing movement of the aircraft. An attitude cue is overlaid upon the synthetic rendering of terrain and depicted on first and second sides of the horizon line such that the synthetic rendering of terrain remains substantially visible. The attitude cue has a first appearance on the first side of the horizon line and a second appearance on the second side of the horizon line. The first appearance is visually contrasted from the second appearance.
摘要翻译： 公开了一种航空电子显示器。 使用存储的地形数据创建地形的合成渲染。 地平线被叠加在地形的合成渲染上。 地平线表示在其中安装航空电子显示器的飞行器的行进方向上的零度俯仰姿态。 地平线配置为响应飞行器的姿态改变运动而移动。 姿态提示覆盖在地形的合成渲染上，并在地平线的第一和第二侧上描绘，使得地形的合成渲染基本上可见。 姿态提示在地平线的第一侧具有第一外观，在地平线的第二侧具有第二外观。 第一个外观与第二个外观形成鲜明对比。
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公开(公告)号：US07696955B1
公开(公告)日：2010-04-13
申请号：US11357327
申请日：2006-02-17
IPC分类号： G09G5/00
CPC分类号： G08G5/0021 , G01C23/00
摘要： An information magnification system for providing enhanced display information for a display system for a vehicle. The display system is of a type that includes a first display and a second display. The information magnification system includes a user interface for providing the capability for a user to select a magnification zone of interest on the first display of the vehicle. An information magnification electronics subsystem is associated with the user interface and with the first and second displays to enable the selected magnification zone to be presented on the second display appearing to be behind the physical surface of the second display at a selected distance, thus providing the capability for the user to maintain a far field of focus.
摘要翻译： 一种用于为车辆的显示系统提供增强的显示信息的信息放大系统。 显示系统是包括第一显示器和第二显示器的类型。 信息放大系统包括用户界面，用于提供用户在车辆的第一显示器上选择感兴趣的放大区域的能力。 信息放大电子系统与用户接口相关联，并且与第一和第二显示器相关联，以使得所选择的放大区域能够以显示在第二显示器的物理表面之后的第二显示器上呈现出选定距离，从而提供 用户能够保持远方的焦点。
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