SYSTEM AND METHOD FOR HIGHLIGHTING AN AREA ENCOMPASSING AN AIRCRAFT THAT IS FREE OF HAZARDS
    11.
    发明申请
    SYSTEM AND METHOD FOR HIGHLIGHTING AN AREA ENCOMPASSING AN AIRCRAFT THAT IS FREE OF HAZARDS 有权
    用于强调无风险的飞机的区域的系统和方法

    公开(公告)号:US20150045994A1

    公开(公告)日:2015-02-12

    申请号:US13962669

    申请日:2013-08-08

    CPC classification number: G08G5/04 B64C25/44 G08G5/0021 G08G5/065

    Abstract: A system and method display a hazard free area around an aircraft that is modified to alert a pilot if a threshold distance between a detected object and the aircraft is reached. The modification may include, for example, altering the size of the hazard free area and its color. Additional information that may be displayed includes distance to the object, width of the hazard free area, stopping distance of the aircraft, and a route to avoid the object.

    Abstract translation: 系统和方法显示飞机周围的无危险区域,如果达到检测到的物体与飞行器之间的阈值距离,该飞机被修改以警告飞行员。 该修改可以包括例如改变无危险区域的尺寸及其颜色。 可能显示的附加信息包括到物体的距离,无危险区域的宽度,飞机的停止距离以及避开物体的路线。

    Systems and methods for providing obstacle information to aircraft operator displays

    公开(公告)号:US12094351B2

    公开(公告)日:2024-09-17

    申请号:US17485694

    申请日:2021-09-27

    CPC classification number: G08G5/0086 G06F16/29 G08G5/0026 G08G5/0069 G08G5/045

    Abstract: Disclosed are methods, systems, and non-transitory computer-readable media for transmitting obstacle information to one or more operator displays associated with an aircraft. For instance, the method may include obtaining aircraft flight information including a current position and altitude; retrieving obstacle information for a flight area; scanning the flight area with environment sensors to identify observed obstacles and generate observed obstacle information. The method may further include aggregating the obstacle information with the observed obstacle information of the observed obstacles identified by the environment sensors to generate aggregated obstacle information identifying obstacles in the flight area; determining obstacle characteristics of the obstacles located in the flight area; assigning visual characteristics to each of the obstacles based at least in part on the determined obstacle characteristics; determining a subset of the obstacles relevant to the aircraft; and transmitting information on the relevant subset of obstacles to a display of the aircraft.

    SYSTEM AND METHOD FOR A MISSION-BASED BATTERY STATUS DISPLAY FOR ELECTRIC VEHICLES

    公开(公告)号:US20220063431A1

    公开(公告)日:2022-03-03

    申请号:US17009466

    申请日:2020-09-01

    Abstract: Systems and methods are provided for displaying operating data for a re-chargeable battery for an electric vehicle. The system comprises a re-chargeable battery for powering components of an electrical vehicle, a sensor that detects a present level of charge in the battery and a display. The display receives the present level of charge of the battery from the monitor and displays the present level of charge in the battery, a required level of endurance for the battery that is based on a planned operational parameter for the vehicle, a minimum level of charge in the battery that meets the required level of endurance, and an amount of time needed to re-charge the battery to achieve the minimum level of charge.

    Aircraft systems and methods for displaying wind shear

    公开(公告)号:US10407179B2

    公开(公告)日:2019-09-10

    申请号:US15294978

    申请日:2016-10-17

    Abstract: A vehicle system includes a control unit with a weather module configured to receive weather data and to identify a wind shear zone at a location based on the weather data, the weather module further configured to generate wind shear coordinate data and wind shear characteristic data based on the weather data. The control unit further includes a display module configured to generate display commands based on the wind shear coordinate data and wind shear characteristic data from the weather module. The vehicle system further includes a display device coupled to receive the display commands from the control unit and configured to display a three-dimensional forward perspective view corresponding to a vehicle environment. The display device is further configured to display first wind shear symbology within the view at a position that indicates the location of the wind shear zone.

    AIRCRAFT SYSTEMS AND METHODS FOR DISPLAYING WIND SHEAR

    公开(公告)号:US20180105284A1

    公开(公告)日:2018-04-19

    申请号:US15294978

    申请日:2016-10-17

    Abstract: A vehicle system includes a control unit with a weather module configured to receive weather data and to identify a wind shear zone at a location based on the weather data, the weather module further configured to generate wind shear coordinate data and wind shear characteristic data based on the weather data. The control unit further includes a display module configured to generate display commands based on the wind shear coordinate data and wind shear characteristic data from the weather module. The vehicle system further includes a display device coupled to receive the display commands from the control unit and configured to display a three-dimensional forward perspective view corresponding to a vehicle environment. The display device is further configured to display first wind shear symbology within the view at a position that indicates the location of the wind shear zone.

    DISPLAY SYSTEMS AND METHODS FOR PROVIDING DISPLAYS HAVING AN ADAPTIVE COMBINED VISION SYSTEM
    17.
    发明申请
    DISPLAY SYSTEMS AND METHODS FOR PROVIDING DISPLAYS HAVING AN ADAPTIVE COMBINED VISION SYSTEM 审中-公开
    用于提供具有适应性组合视觉系统的显示器的显示系统和方法

    公开(公告)号:US20150019048A1

    公开(公告)日:2015-01-15

    申请号:US13942062

    申请日:2013-07-15

    CPC classification number: B64D45/00 G01C23/005 G08G5/04

    Abstract: A method for providing a display to a flight crew of an aircraft includes the steps of providing a synthetic image comprising a first field of view forward of a direction of travel of the aircraft and providing a sensory image overlaying at least a first portion of the synthetic image. The sensory image includes a second field of view forward of the direction of travel of the aircraft. At least a portion of the first field of view and a portion of the second field of view overlap one another. The sensory image is centered within the synthetic image with respect to a horizontal axis. The method further includes moving the sensory image so as to overlay at least a second portion of the synthetic image such that the sensory image is no longer centered with respect to the horizontal axis within the synthetic image.

    Abstract translation: 用于向飞行员的飞行机组提供显示器的方法包括以下步骤:提供合成图像,该合成图像包括飞行器的行进方向的前方的第一视场,并且提供覆盖合成的至少第一部分的感官图像 图片。 感官图像包括飞机前进方向的第二视场。 第一视野的至少一部分和第二视场的一部分彼此重叠。 感觉图像相对于水平轴在合成图像内居中。 该方法还包括移动感觉图像以覆盖合成图像的至少第二部分,使得感觉图像不再在合成图像内相对于水平轴居中。

    SLIDER CONTROL FOR GRAPHICAL USER INTERFACE AND METHOD FOR USE THEREOF
    18.
    发明申请
    SLIDER CONTROL FOR GRAPHICAL USER INTERFACE AND METHOD FOR USE THEREOF 审中-公开
    用于图形用户界面的滑块控制及其使用方法

    公开(公告)号:US20140229897A1

    公开(公告)日:2014-08-14

    申请号:US13767654

    申请日:2013-02-14

    CPC classification number: G06F3/04847 G01C23/00 G06F3/04855

    Abstract: A system and method are provided for varying a parameter graphically represented by a first control button on a display. The first control button is pressed either by contacting a touch screen or via a cursor control. Symbology is then generated on the display graphically representative of a slide control, which is dragged to vary the parameter to a desired value. Contact with the display, either by means of touch or cursor control, as the case may be, is then terminated.

    Abstract translation: 提供了一种用于改变由显示器上的第一控制按钮图形表示的参数的系统和方法。 通过联系触摸屏或通过光标控制按下第一个控制按钮。 然后在图形上代表幻灯片控制的显示器上生成符号学,其被拖动以将参数改变为期望值。 然后终止与显示器的接触,通过触摸或光标控制(视情况而定)。

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