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    SYSTEM AND METHOD FOR DISPLAYING CONSTRAINT INFORMATION ON A GRAPHICAL AIRCRAFT INSTRUMENT TAPE ELEMENT
    1.
    发明申请
    SYSTEM AND METHOD FOR DISPLAYING CONSTRAINT INFORMATION ON A GRAPHICAL AIRCRAFT INSTRUMENT TAPE ELEMENT 审中-公开
    用于在图形飞行器仪表带元件上显示约束信息的系统和方法

    公开(公告)号：US20100023187A1

    公开(公告)日：2010-01-28

    申请号：US12181096

    申请日：2008-07-28

    申请人： Aaron Gannon ,  Gang He ,  Thea L. Feyereisen ,  Ivan S. Wyatt

    发明人： Aaron Gannon ,  Gang He ,  Thea L. Feyereisen ,  Ivan S. Wyatt

    IPC分类号： G06F17/00 ,  G01C21/00

    CPC分类号： G01C23/00

    摘要： A flight deck display system for an aircraft includes a processor architecture configured to receive aircraft instrument data (e.g., altimeter or airspeed) and position data for the aircraft and, based upon the instrument data and the position data, generate image rendering display commands. The system also includes a display element configured to receive the image rendering display commands and, in response thereto, to render a graphical instrument tape. The instrument tape includes a graphical representation of a scrolling altitude or airspeed range that dynamically scrolls in response to changes in the altitude/airspeed data, along with a graphical representation of a position-dependent altitude/airspeed clearance element that conveys an altitude/airspeed restriction for an approaching geographic position of the aircraft. The content of the position-dependent clearance element is influenced by the position data.

    摘要翻译： 用于飞行器的飞行甲板显示系统包括被配置为接收飞行器仪表数据（例如，高度计或空速）和用于飞机的位置数据的处理器架构，并且基于仪器数据和位置数据，生成图像渲染显示命令。 该系统还包括被配置为接收图像呈现显示命令的显示元件，并且响应于此，呈现图形化的仪器带。 仪表带包括响应于高度/空速数据的变化动态滚动的滚动高度或空速范围的图形表示，以及传达高度/空速限制的位置相关高度/空速间隙元件的图形表示 为飞机接近的地理位置。 位置相关的间隙元素的内容受位置数据的影响。

    System and method for increasing visibility of critical flight information on aircraft displays
    2.
    发明申请
    System and method for increasing visibility of critical flight information on aircraft displays 有权
    提高航空器显示屏上关键航班信息可见度的系统和方法

    公开(公告)号：US20090207048A1

    公开(公告)日：2009-08-20

    申请号：US11170498

    申请日：2005-06-29

    申请人： Gang He ,  Thea L. Feyereisen ,  Aaron J. Gannon ,  Blake W. Wilson ,  Jary E. Engels ,  Ivan S. Wyatt

    发明人： Gang He ,  Thea L. Feyereisen ,  Aaron J. Gannon ,  Blake W. Wilson ,  Jary E. Engels ,  Ivan S. Wyatt

    IPC分类号： G01C23/00

    CPC分类号： G01C23/00

    摘要： System and method increase the visibility of critical flight information on electronic displays. An aircraft display system includes a processing unit, a flight management system, a navigation system, a database for storing target data and terrain data, a graphics display generator, and a visual display. The flight management system and/or the navigation system provide real-time aircraft operational and flight control information. The processing unit directs the graphics display generator to generate graphic control signals for the visual display, which increase the transparency of a segment of a zero pitch reference line in the vicinity of a flight path marker on the display.

    摘要翻译： 系统和方法提高了电子显示屏上关键航班信息的可见度。 飞机显示系统包括处理单元，飞行管理系统，导航系统，用于存储目标数据和地形数据的数据库，图形显示生成器和视觉显示器。 飞行管理系统和/或导航系统提供实时飞机操作和飞行控制信息。 处理单元引导图形显示发生器产生用于视觉显示的图形控制信号，这增加了显示器上的飞行路径标记附近的零俯仰参考线段的透明度。

    Perspective view primary flight display with terrain-tracing lines and method
    3.
    发明授权
    Perspective view primary flight display with terrain-tracing lines and method 有权
    透视图主要飞行显示与地形跟踪线和方法

    公开(公告)号：US07212216B2

    公开(公告)日：2007-05-01

    申请号：US11174271

    申请日：2005-06-29

    申请人： Gang He ,  Thea L. Feyereisen ,  Ivan S. Wyatt

    发明人： Gang He ,  Thea L. Feyereisen ,  Ivan S. Wyatt

    IPC分类号： G06T17/00

    CPC分类号： G01C23/00

    摘要： A display system and method are provided for a vehicle that includes a processor and a display. The processor is adapted to receive terrain data and navigation data operable, in response thereto, to supply one or more image rendering display commands. The display device is coupled to receive the image rendering display commands and operable, in response thereto, to simultaneously render (i) a perspective view image representative of the terrain data and the navigation data and (ii) one or more terrain-tracing lines.

    摘要翻译： 为包括处理器和显示器的车辆提供显示系统和方法。 该处理器适于接收地面数据和导航数据，响应于此可提供一个或多个图像呈现显示命令。 显示设备被耦合以接收图像呈现显示命令，并且响应于此可同时呈现（i）表示地形数据和导航数据的透视图像，以及（ii）一个或多个地形跟踪线。

    Displaying obstacles in perspective view
    6.
    发明授权
    Displaying obstacles in perspective view 有权
    在透视图中显示障碍物

    公开(公告)号：US07375678B2

    公开(公告)日：2008-05-20

    申请号：US11169515

    申请日：2005-06-29

    申请人： Thea L. Feyereisen ,  Gang He ,  Blake W. Wilson ,  John G. Suddreth ,  Ivan S. Wyatt

    发明人： Thea L. Feyereisen ,  Gang He ,  Blake W. Wilson ,  John G. Suddreth ,  Ivan S. Wyatt

    IPC分类号： G01S7/04 ,  G06T15/10

    CPC分类号： G01S7/20 ,  G01C23/00 ,  G01S7/22 ,  G08G5/0021 ,  G08G5/0078

    摘要： A system and method for displaying obstacles in a conformal perspective view. The system comprises a display screen for graphical display of data, at least one obstacle data source, one or more graphics processors for receiving obstacle data from the at least one obstacle data source, and for providing input to the display screen. The display screen displays obstacles in a 3-dimensional graphical representation of real space. The display size of the obstacles varies based on the distance to the obstacles. Obstacles located beyond a selected distance are displayed as semi-transparent line objects and obstacles located within the selected distance are displayed as semi-transparent polygons.

    摘要翻译： 用于在保形透视图中显示障碍物的系统和方法。 该系统包括用于图形显示数据的显示屏幕，至少一个障碍物数据源，用于从至少一个障碍物数据源接收障碍物数据的一个或多个图形处理器，以及用于向显示屏幕提供输入。 显示屏幕显示实际空间的三维图形表示中的障碍物。 障碍物的显示尺寸根据与障碍物的距离而变化。 位于选定距离之外的障碍显示为半透明线对象，位于所选距离内的障碍物显示为半透明多边形。

    System and method for increasing visibility of critical flight information on aircraft displays
    8.
    发明授权
    System and method for increasing visibility of critical flight information on aircraft displays 有权
    提高航空器显示屏上关键航班信息可见度的系统和方法

    公开(公告)号：US07834779B2

    公开(公告)日：2010-11-16

    申请号：US11170498

    申请日：2005-06-29

    申请人： Gang He ,  Thea L. Feyereisen ,  Aaron J. Gannon ,  Blake W. Wilson ,  Jary E. Engels ,  Ivan S Wyatt

    发明人： Gang He ,  Thea L. Feyereisen ,  Aaron J. Gannon ,  Blake W. Wilson ,  Jary E. Engels ,  Ivan S Wyatt

    IPC分类号： G01C23/00

    CPC分类号： G01C23/00

    摘要： System and method increase the visibility of critical flight information on electronic displays. An aircraft display system includes a processing unit, a flight management system, a navigation system, a database for storing target data and terrain data, a graphics display generator, and a visual display. The flight management system and/or the navigation system provide real-time aircraft operational and flight control information. The processing unit directs the graphics display generator to generate graphic control signals for the visual display, which increase the transparency of a segment of a zero pitch reference line in the vicinity of a flight path marker on the display.

    摘要翻译： 系统和方法提高了电子显示屏上关键航班信息的可见度。 飞机显示系统包括处理单元，飞行管理系统，导航系统，用于存储目标数据和地形数据的数据库，图形显示生成器和视觉显示器。 飞行管理系统和/或导航系统提供实时飞机操作和飞行控制信息。 处理单元引导图形显示发生器产生用于视觉显示的图形控制信号，这增加了显示器上的飞行路径标记附近的零俯仰参考线段的透明度。

    AUTOMATED LANDING AREA DETECTION FOR AIRCRAFT
    9.
    发明申请
    AUTOMATED LANDING AREA DETECTION FOR AIRCRAFT 审中-公开
    用于飞机的自动登陆区域检测

    公开(公告)号：US20100039294A1

    公开(公告)日：2010-02-18

    申请号：US12191491

    申请日：2008-08-14

    申请人： Thea L. Feyereisen ,  Ivan S. Wyatt ,  Gang He

    发明人： Thea L. Feyereisen ,  Ivan S. Wyatt ,  Gang He

    IPC分类号： G01C23/00

    CPC分类号： G08G5/025 ,  G01S7/412 ,  G06K9/0063 ,  G06K9/6202 ,  G08G5/0086

    摘要： A system for detecting a landing area or runway for an aircraft includes a detection subsystem, a processor architecture, flight deck instrumentation, and a runway feature template database. The system is operated to perform an automated method for visually confirming the presence of a runway on approach. The method obtains sensor data indicative of an approach area of the aircraft, and extracts visually distinguishable features of the approach area from the sensor data. The method also accesses the runway feature template corresponding to the intended approach runway for the aircraft, fits the visually distinguishable features to the runway feature template, and provides flight crew feedback in response to the fitting step.

    摘要翻译： 用于检测飞行器的着陆区域或跑道的系统包括检测子系统，处理器架构，飞行甲板仪表和跑道特征模板数据库。 该系统被操作以执行自动化方法，用于在逼近时视觉上确认跑道的存在。 该方法获得指示飞行器的接近区域的传感器数据，并且从传感器数据中提取接近区域的视觉上可区分的特征。 该方法还访问与飞机的预期进近跑道相对应的跑道特征模板，将视觉上可区分的特征适合跑道特征模板，并响应于装配步骤提供飞行机组反馈。

    System and method for rendering a primary flight display having a conformal terrain avoidance guidance element
    10.
    发明授权
    System and method for rendering a primary flight display having a conformal terrain avoidance guidance element 有权
    用于渲染具有共形地形避免引导元件的主飞行显示的系统和方法

    公开(公告)号：US08068038B2

    公开(公告)日：2011-11-29

    申请号：US12366448

    申请日：2009-02-05

    申请人： Jary Engels ,  Thea L. Feyereisen ,  Aaron Gannon ,  Gang He ,  Ivan Sandy Wyatt

    发明人： Jary Engels ,  Thea L. Feyereisen ,  Aaron Gannon ,  Gang He ,  Ivan Sandy Wyatt

    IPC分类号： G08B23/00

    CPC分类号： G01C23/00 ,  G08G5/045

    摘要： A flight deck display system and related operating methods for an aircraft are provided. The system includes a processor architecture and a display element coupled to the processor architecture. The processor architecture is configured to receive real-time aircraft data and terrain data for the aircraft and, based upon the real-time aircraft data and the terrain data, generate image rendering display commands. The display element receives the image rendering display commands and, in response thereto, renders a primary flight display that includes a conformal view of terrain corresponding to a flight deck viewpoint. The primary flight display also includes a conformal terrain avoidance guidance (TAG) element on the view of terrain. The TAG element includes visual indicia of a desired navigation path that is intended to avoid terrain that obstructs a current flight path of the aircraft.

    摘要翻译： 提供飞机甲板显示系统及飞机的相关操作方法。 该系统包括耦合到处理器架构的处理器架构和显示元件。 处理器架构被配置为接收飞机的实时飞行器数据和地形数据，并且基于实时飞行器数据和地形数据，生成图像渲染显示命令。 显示元件接收图像渲染显示命令，并且响应于此，呈现包括对应于飞行甲板视点的地形的保形视图的主飞行显示。 主飞行显示还包括地形视图上的保形地形避免指导（TAG）元素。 TAG元件包括期望的导航路径的视觉标记，其旨在避免妨碍飞行器的当前飞行路径的地形。