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    • 8. 发明申请
    • AUTOMATED LANDING AREA DETECTION FOR AIRCRAFT
    • 用于飞机的自动登陆区域检测
    • US20100039294A1
    • 2010-02-18
    • US12191491
    • 2008-08-14
    • Thea L. FeyereisenIvan S. WyattGang He
    • Thea L. FeyereisenIvan S. WyattGang He
    • G01C23/00
    • G08G5/025G01S7/412G06K9/0063G06K9/6202G08G5/0086
    • 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.
    • 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。
    • 9. 发明申请
    • SYSTEM AND METHOD FOR DISPLAYING CONSTRAINT INFORMATION ON A GRAPHICAL AIRCRAFT INSTRUMENT TAPE ELEMENT
    • 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
    • US20100023187A1
    • 2010-01-28
    • US12181096
    • 2008-07-28
    • Aaron GannonGang HeThea L. FeyereisenIvan S. Wyatt
    • Aaron GannonGang HeThea L. FeyereisenIvan S. Wyatt
    • G06F17/00G01C21/00
    • G01C23/00
    • 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.
    • 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。