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    • 4. 发明授权
    • System and method for rendering a primary flight display having a conformal terrain avoidance guidance element
    • 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
    • US08068038B2
    • 2011-11-29
    • US12366448
    • 2009-02-05
    • Jary EngelsThea L. FeyereisenAaron GannonGang HeIvan Sandy Wyatt
    • Jary EngelsThea L. FeyereisenAaron GannonGang HeIvan Sandy Wyatt
    • G08B23/00
    • G01C23/00G08G5/045
    • 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.
    • 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。
    • 5. 发明授权
    • Perspective view primary flight display system and method with range lines
    • 透视图主要飞行显示系统和方法与范围线
    • US07917289B2
    • 2011-03-29
    • US11929027
    • 2007-10-30
    • Thea L. FeyereisenGang HeSandy Wyatt
    • Thea L. FeyereisenGang HeSandy Wyatt
    • G08G5/04G01C23/00
    • G08G5/0086G01C23/005G08G5/0021
    • A display system for a vehicle includes a navigation database storing navigation data; a terrain sensor configured to gather terrain data; a processor adapted to receive the navigation data and the terrain data and operable to supply one or more image rendering display commands based upon the navigation data and the terrain data; and a display device. The display device is coupled to receive the image rendering display commands and operable, in response thereto, to render (i) a perspective view image representative of the terrain data and the navigation data and including terrain and (ii) at least one line on the perspective view image that extends at least partially across the terrain and represents at least one of a ground-referenced range to a fixed location on the terrain and a vehicle-referenced range from the vehicle to a fixed range away from the vehicle.
    • 一种用于车辆的显示系统包括存储导航数据的导航数据; 地形传感器,用于收集地形数据; 处理器,适于接收导航数据和地形数据,并且可操作以基于导航数据和地形数据提供一个或多个图像呈现显示命令; 和显示装置。 显示设备被耦合以接收图像呈现显示命令,并且响应于此可操作地渲染(i)表示地形数据和导航数据并包括地形的透视图,以及(ii)至少一条线 透视图图像,其至少部分地跨过地形延伸,并且表示地面上的固定位置的地面参考范围中的至少一个以及从车辆到从车辆到固定范围的车辆参考范围。
    • 6. 发明授权
    • Aircraft synthetic vision system for approach and landing
    • 飞机合成视觉系统的接近和着陆
    • US07852236B2
    • 2010-12-14
    • US12183693
    • 2008-07-31
    • Thea L. FeyereisenIvan Sandy WyattGang He
    • Thea L. FeyereisenIvan Sandy WyattGang He
    • G01C21/00G01C23/00
    • G01C23/005G01C5/005G08G5/0021G08G5/006G08G5/025
    • An aircraft synthetic vision system (100) is provided for increasing data input to a pilot (109) during approach and landing flight operations, and includes a runway assistance landing system (114) and a plurality of databases (106, 108, 110, 112) which may include, for example, a terrain database (106), an obstacle database (112); and a validated runway database (110). The processor (104) detects the likelihood of an error in determining the altitude from at least one of the runway assistance landing system (114), the plurality of databases (106, 108, 110, 112), and identifies the error. The processor (104) further determines augmented coordinates, and a processor (104) generates symbology commands to a first display (116) for displaying a runway environment in response to data provided to the processor (104) from each of the runway assistance landing system (114), the plurality of databases (106, 108, 110, 112), and the processor (104).
    • 提供一种飞机合成视觉系统(100),用于在接近和着陆飞行操作期间增加输入到飞行员(109)的数据,并且包括跑道辅助着陆系统(114)和多个数据库(106,108,110,112 ),其可以包括例如地形数据库(106),障碍物数据库(112); 和经验证的跑道数据库(110)。 处理器(104)检测从跑道辅助着陆系统(114),多个数据库(106,108,110,112)中的至少一个确定高度的错误的可能性,并且识别错误。 处理器(104)进一步确定增强的坐标,并且处理器(104)产生符号体系命令给第一显示器(116),用于响应从每个跑道辅助着陆系统提供给处理器(104)的数据来显示跑道环境 (114),所述多个数据库(106,108,110,112)和所述处理器(104)。
    • 8. 发明申请
    • PERSPECTIVE VIEW PRIMARY FLIGHT DISPLAY SYSTEM AND METHOD WITH RANGE LINES
    • 主观视图主要飞行显示系统和方法与范围线
    • US20100070176A1
    • 2010-03-18
    • US11929027
    • 2007-10-30
    • Thea L. FeyereisenGang HeSandy Wyatt
    • Thea L. FeyereisenGang HeSandy Wyatt
    • G01C21/00
    • G08G5/0086G01C23/005G08G5/0021
    • A display system for a vehicle includes a navigation database storing navigation data; a terrain sensor configured to gather terrain data; a processor adapted to receive the navigation data and the terrain data and operable to supply one or more image rendering display commands based upon the navigation data and the terrain data; and a display device. The display device is coupled to receive the image rendering display commands and operable, in response thereto, to render (i) a perspective view image representative of the terrain data and the navigation data and including terrain and (ii) at least one line on the perspective view image that extends at least partially across the terrain and represents at least one of a ground-referenced range to a fixed location on the terrain and a vehicle-referenced range from the vehicle to a fixed range away from the vehicle.
    • 一种用于车辆的显示系统包括存储导航数据的导航数据; 地形传感器,用于收集地形数据; 处理器,适于接收导航数据和地形数据,并且可操作以基于导航数据和地形数据提供一个或多个图像呈现显示命令; 和显示装置。 显示设备被耦合以接收图像呈现显示命令,并且响应于此可操作地渲染(i)表示地形数据和导航数据并包括地形的透视图,以及(ii)至少一条线 透视图图像,其至少部分地跨过地形延伸,并且表示地面上的固定位置的地面参考范围中的至少一个以及从车辆到从车辆到固定范围的车辆参考范围。
    • 9. 发明申请
    • AIRCRAFT SYNTHETIC VISION SYSTEM FOR APPROACH AND LANDING
    • 用于方法和陆地的飞机综合视觉系统
    • US20100026525A1
    • 2010-02-04
    • US12183693
    • 2008-07-31
    • Thea L. FeyereisenIvan Sandy WyattGang He
    • Thea L. FeyereisenIvan Sandy WyattGang He
    • G01C23/00G08G5/00G06F19/00
    • G01C23/005G01C5/005G08G5/0021G08G5/006G08G5/025
    • An aircraft synthetic vision system (100) is provided for increasing data input to a pilot (109) during approach and landing flight operations, and includes a runway assistance landing system (114) and a plurality of databases (106, 108, 110, 112) which may include, for example, a terrain database (106), an obstacle database (112); and a validated runway database (110). The processor (104) detects the likelihood of an error in determining the altitude from at least one of the runway assistance landing system (114), the plurality of databases (106, 108, 110, 112), and identifies the error. The processor (104) further determines augmented coordinates, and a processor (104) generates symbology commands to a first display (116) for displaying a runway environment in response to data provided to the processor (104) from each of the runway assistance landing system (114), the plurality of databases (106, 108, 110, 112), and the processor (104).
    • 提供一种飞机合成视觉系统(100),用于在接近和着陆飞行操作期间增加输入到飞行员(109)的数据,并且包括跑道辅助着陆系统(114)和多个数据库(106,108,110,112 ),其可以包括例如地形数据库(106),障碍物数据库(112); 和经验证的跑道数据库(110)。 处理器(104)检测从跑道辅助着陆系统(114),多个数据库(106,108,110,112)中的至少一个确定高度的错误的可能性,并且识别错误。 处理器(104)进一步确定增强坐标,并且处理器(104)产生符号体系命令给第一显示器(116),用于响应于从跑道辅助着陆系统中的每一个提供给处理器(104)的数据来显示跑道环境 (114),所述多个数据库(106,108,110,112)和所述处理器(104)。
    • 10. 发明授权
    • Aircraft display with potential thrust indicator
    • 飞机显示与潜在的推力指示器
    • US06469640B2
    • 2002-10-22
    • US09863214
    • 2001-05-21
    • Ivan Sandy Wyatt
    • Ivan Sandy Wyatt
    • G01C2300
    • G01C23/00
    • An aircraft display apparatus combines a flight path vector group with a potential thrust indicator. The display apparatus comprises a display screen and a pitch ladder symbol, a horizontal line and a flight path vector group displayed on the display screen. The flight path vector group comprises a flight path vector symbol, a potential flight path vector symbol, and a potential thrust symbol. The potential thrust symbol further comprises a thrust and drag limit symbol and at least one throttle symbol. The flight path vector group is oriented on the display screen in relation to the pitch ladder and the horizontal line. The position of the potential thrust symbol relative to the pitch ladder, flight path vector symbol and the potential flight path vector symbol represents current engine power and power limits of the aircraft.
    • 飞行器显示装置将飞行路径矢量组与潜在推力指示器组合。 显示装置包括在显示画面上显示的显示画面和俯仰梯符号,水平线和飞行路线矢量组。 飞行路径矢量组包括飞行路径矢量符号,潜在飞行路径矢量符号和潜在推力符号。 潜在推力符号还包括推力和阻力极限符号和至少一个节气门符号。 飞行路径矢量组相对于俯仰梯和水平线在显示屏上取向。 潜在推力符号相对于俯仰梯,飞行路径矢量符号和潜在飞行路径矢量符号的位置表示飞机的当前发动机功率和功率极限。