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1. 发明授权

US08068038B2 System and method for rendering a primary flight display having a conformal terrain avoidance guidance element 有权
标题翻译：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。

2. 发明申请

US20100161158A1 SYSTEMS AND METHODS FOR ENHANCING TERRAIN ELEVATION AWARENESS 审中-公开
标题翻译：用于增强TERRAIN ELEVATION AWARENESS的系统和方法
公开(公告)号：US20100161158A1
公开(公告)日：2010-06-24
申请号：US12338708
申请日：2008-12-18
申请人： Aaron Gannon , Thea L. Feyereisen , Gang He
发明人： Aaron Gannon , Thea L. Feyereisen , Gang He
IPC分类号： G06F19/00
CPC分类号： G01C23/00 , G08G5/0021
摘要： A display system for an aircraft is provided. The display includes a processing unit configured to receive terrain data and navigation data and to supply display commands with symbology based on the terrain data and navigation data; and a display device coupled the processing unit and configured to receive the display commands and operable to render a three-dimensional view with the symbology. The symbology includes terrain, a zero pitch line, and elevation symbology indicating a relative elevation between the zero pitch line and a position in the view.
摘要翻译：提供了一种用于飞行器的显示系统。显示器包括：处理单元，被配置为接收地形数据和导航数据，并且基于地形数据和导航数据提供具有符号系统的显示命令; 以及耦合所述处理单元并被配置为接收所述显示命令并且可操作以用所述符号体系呈现三维视图的显示设备。符号系统包括地形，零间距线和高程符号，表示零间距线和视图中的位置之间的相对高程。

3. 发明申请

US20100030405A1 AIRCRAFT DISPLAY SYSTEMS AND METHODS FOR ENHANCED DISPLAY OF FLIGHT PATH INFORMATION 有权
标题翻译：飞机显示系统和方法，用于增强航行信息的显示
公开(公告)号：US20100030405A1
公开(公告)日：2010-02-04
申请号：US12182904
申请日：2008-07-30
申请人： Gang He , Thea L. Feyereisen , Aaron Gannon
发明人： Gang He , Thea L. Feyereisen , Aaron Gannon
IPC分类号： G06F19/00
CPC分类号： G01C23/00
摘要： A display system for a vehicle includes a processing unit configured to receive data representative of flight path information and terrain and to supply display commands associated with the flight path information and the terrain; and a display device coupled the processing unit and configured to receive the display commands and operable to render a three-dimensional view, including symbology representing the flight path information on the terrain.
摘要翻译：车辆的显示系统包括：处理单元，被配置为接收表示飞行路径信息和地形的数据，并提供与飞行路径信息和地形相关联的显示命令; 以及耦合所述处理单元并被配置为接收所述显示命令并且可操作以呈现三维视图的显示设备，所述三维视图包括表示所述地形上的飞行路径信息的符号系统。

4. 发明授权

US09389097B2 Aircraft display systems and methods for enhanced display of flight path information 有权
标题翻译：飞机显示系统和方法，用于增强飞行路径信息的显示
公开(公告)号：US09389097B2
公开(公告)日：2016-07-12
申请号：US12182904
申请日：2008-07-30
申请人： Gang He , Thea L. Feyereisen , Aaron Gannon
发明人： Gang He , Thea L. Feyereisen , Aaron Gannon
IPC分类号： B64C13/20 , G05D1/00 , G01C23/00
CPC分类号： G01C23/00
摘要： A display system for a vehicle includes a processing unit configured to receive data representative of flight path information and terrain and to supply display commands associated with the flight path information and the terrain; and a display device coupled the processing unit and configured to receive the display commands and operable to render a three-dimensional view, including symbology representing the flight path information on the terrain.
摘要翻译：车辆的显示系统包括：处理单元，被配置为接收表示飞行路径信息和地形的数据，并提供与飞行路径信息和地形相关联的显示命令; 以及耦合所述处理单元并被配置为接收所述显示命令并且可操作以呈现三维视图的显示设备，所述三维视图包括表示所述地形上的飞行路径信息的符号系统。

5. 发明申请

US20100023187A1 SYSTEM AND METHOD FOR DISPLAYING CONSTRAINT INFORMATION ON A GRAPHICAL AIRCRAFT INSTRUMENT TAPE ELEMENT 审中-公开
标题翻译：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。

6. 发明申请

US20100194602A1 SYSTEM AND METHOD FOR RENDERING A PRIMARY FLIGHT DISPLAY HAVING A CONFORMAL TERRAIN AVOIDANCE GUIDANCE ELEMENT 有权
标题翻译：提供具有一致的三角洲避风指导要素的主要飞行显示系统和方法
公开(公告)号：US20100194602A1
公开(公告)日：2010-08-05
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： G01C21/00
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。

7. 发明申请

US20070001874A1 Perspective view conformal traffic targets display 有权
公开(公告)号：US20070001874A1
公开(公告)日：2007-01-04
申请号：US11170356
申请日：2005-06-29
申请人： Thea Feyereisen , Aaron Gannon , Gang He , David Shirley , Blake Wilson
发明人： Thea Feyereisen , Aaron Gannon , Gang He , David Shirley , Blake Wilson
IPC分类号： G08G1/123
CPC分类号： G01D7/02 , G01C23/00 , G08G5/0021 , G08G5/0078
摘要： A system and method for displaying traffic targets in a conformal perspective view. The system comprises a display screen for graphical display of data, one or more sensors for obtaining traffic data regarding traffic targets, and one or more processors for receiving traffic data from the one or more sensors and providing input to the display screen. The display screen displays traffic targets as icons in a 3-dimensional graphical representation of real space. The display size of the icons is selected from a finite set of sizes which correspond to a finite set of distance ranges based on the distance to the traffic targets.

8. 发明申请

US20070085705A1 Dynamic primary flight displays for unusual attitude conditions 有权
标题翻译：动态主飞行显示异常态度条件
公开(公告)号：US20070085705A1
公开(公告)日：2007-04-19
申请号：US11250124
申请日：2005-10-13
申请人： Gang He , Ivan Wyatt , Jary Engels , Thea Feyereisen , Aaron Gannon , Blake Wilson
发明人： Gang He , Ivan Wyatt , Jary Engels , Thea Feyereisen , Aaron Gannon , Blake Wilson
IPC分类号： G08B23/00 , G01C23/00
CPC分类号： G01C23/00
摘要： Embodiments of the present invention provide a method of dynamically transitioning into a distinct display format during unusual attitude conditions. In one embodiment, the method includes collecting attitude data, comparing current attitude to a first set attitude angle, and fading a distinct display format into a display for unusual attitude conditions when current attitude is at least equal to the first set attitude angle.
摘要翻译：本发明的实施例提供了一种在异常姿势条件下动态地转换成不同显示格式的方法。在一个实施例中，该方法包括当当前姿态至少等于第一设定姿态角度时，收集姿态数据，将当前姿态与第一设置姿势角进行比较，以及将不同显示格式衰减为用于异常姿势条件的显示。

9. 发明申请

US20070188350A1 Dynamic lateral deviation display 有权
标题翻译：动态横向偏差显示
公开(公告)号：US20070188350A1
公开(公告)日：2007-08-16
申请号：US11353555
申请日：2006-02-14
申请人： Gang He , Aaron Gannon
发明人： Gang He , Aaron Gannon
IPC分类号： G01C21/00 , G06F15/00 , G06F17/00
CPC分类号： G01C23/005
摘要： A method of dynamically displaying lateral deviation in formats on a display is provided. The method comprises assigning one or more positional boundaries for displaying the lateral deviation information, wherein the one or more positional boundaries define areas on a display. The method also comprises calculating display positions of a lateral deviation symbology and determining if each calculated display position is allowed based on where the lateral deviation display would be located, if displayed at each calculated position, in relation to the one or more positional boundaries. The method further comprises, displaying the lateral deviation symbology at the calculated positions when the calculated positions are allowed, and displaying a lateral deviation indicator when the calculated positions are not allowed.
摘要翻译：提供了一种在显示器上动态显示格式的横向偏差的方法。该方法包括分配用于显示横向偏差信息的一个或多个位置边界，其中所述一个或多个位置边界限定显示器上的区域。该方法还包括计算横向偏差符号系统的显示位置，并且相对于一个或多个位置边界，如果在每个计算位置显示，则基于横向偏差显示将位于哪里来确定是否允许每个计算的显示位置。该方法还包括：当允许计算的位置时，在所计算的位置处显示横向偏差符号，并且当不允许计算的位置时显示横向偏差指示符。

10. 发明申请

US20090302172A1 INPUT/STEERING MECHANISMS AND AIRCRAFT CONTROL SYSTEMS FOR USE ON AIRCRAFT 有权
标题翻译：用于飞机的输入/转向机构和飞机控制系统
公开(公告)号：US20090302172A1
公开(公告)日：2009-12-10
申请号：US12132964
申请日：2008-06-04
申请人： John G. Suddreth , Aaron Gannon
发明人： John G. Suddreth , Aaron Gannon
IPC分类号： B64C13/04 , H01H9/00
CPC分类号： B64C13/04 , B64D43/00 , B64D2045/0075
摘要： Input/steering mechanisms and aircraft control systems are provided. In an embodiment, by way of example only, an input/steering mechanism is provided for use with an aircraft control system. The input/steering mechanism includes a yoke that includes a hub, an alphanumeric keyboard, and a first grip surface. The alphanumeric keyboard is disposed on a face of the hub and is adapted to receive a manual input from a user and to transmit an output signal to the aircraft control system in response to the manual input. The first grip surface is formed on an outer periphery of the hub and is contoured to correspond with one or more fingers of the user, the first grip surface is formed such that a thumb of the user is positioned to rest in proximity to at least a portion of the alphanumeric keyboard when the one or more fingers grip the first grip surface.
摘要翻译：提供输入/转向机构和飞机控制系统。在一个实施例中，仅作为示例，提供用于飞机控制系统的输入/转向机构。输入/转向机构包括一个轭，它包括一个轮毂，一个字母数字键盘和一个第一把手表面。字母数字键盘设置在集线器的表面上，并且适于从用户接收手动输入，并且响应于手动输入将输出信号发送到飞行器控制系统。第一抓握表面形成在轮毂的外周上并且被轮廓化以对应于使用者的一个或多个手指，第一抓握表面形成为使得使用者的拇指定位成靠近至少一个当一个或多个手指握住第一抓握表面时，字母数字键盘的一部分。

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