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    METHODS AND SYSTEMS FOR REPRESENTING TIME OF ARRIVAL INFORMATION ON A COCKPIT DISPLAY
    11.
    发明申请
    METHODS AND SYSTEMS FOR REPRESENTING TIME OF ARRIVAL INFORMATION ON A COCKPIT DISPLAY 有权
    用于表示COCKPIT显示的抵达时间的方法和系统

    公开(公告)号：US20140278069A1

    公开(公告)日：2014-09-18

    申请号：US13843634

    申请日：2013-03-15

    Applicant: HONEYWELL INTERNATIONAL INC.

    Inventor： Bretislav Passinger ,  Jiri Vasek ,  Jiri Svoboda ,  Michal Polansky

    IPC: G08G5/00

    CPC classification number: G08G5/0021 ,  G01C23/00 ,  G08G5/0052

    Abstract: A method is provided for displaying information on a display device of an aircraft. The method comprises receiving data indicating a point selected from a trajectory of a flight path; determining an estimated time of arrival minimum and an estimated time of arrival maximum based on the point; and displaying in a dialogue box associated with the trajectory of the flight path the estimated time of arrival minimum and the estimated time of arrival maximum for the point.

    Abstract translation: 提供一种用于在飞行器的显示装置上显示信息的方法。 该方法包括接收指示从飞行路径的轨迹中选择的点的数据; 基于该点确定估计的到达时间最小值和估计到达时间最大值; 并且在与飞行路径的轨迹相关联的对话框中显示估计的到达时间最小值和该点的估计到达时间最大值。

    AIRPORT SURFACE COLLISION-AVOIDANCE SYSTEM (ASCAS)
    12.
    发明申请
    AIRPORT SURFACE COLLISION-AVOIDANCE SYSTEM (ASCAS) 有权
    机场表面碰撞避免系统（ASCAS）

    公开(公告)号：US20140081567A1

    公开(公告)日：2014-03-20

    申请号：US13742688

    申请日：2013-01-16

    Applicant: HONEYWELL INTERNATIONAL INC.

    Inventor： James Christopher Kirk ,  Matej Dusik ,  Joseph Duval ,  Jiri Vasek ,  Andrew Fannon Lamkin

    IPC: G08G5/04 ,  G08G5/06

    CPC classification number: G08G5/06 ,  B64D47/08 ,  G01S13/93 ,  G08G5/0021 ,  G08G5/04 ,  G08G5/065

    Abstract: Systems and methods for performing airport surface collision-avoidance. A wingtip-mounted camera allows the pilot to positively ascertain that the wingtip will clear objects located in the video. An exemplary system implemented on an aircraft includes a wingtip module having a camera that generates a video stream and a communication device that transmits the generated video stream. A processor receives the video stream and generates a reticule for the video stream. A display device simultaneously presents the video stream and the reticule. The reticule includes a horizon line and is based on a focal length of a lens of the camera and height of the camera above ground. The reticule includes curved and/or straight distance lines and curved or straight travel lines. The travel line(s) correspond to at least one aircraft component or a zone of importance and are based on location of the camera and trajectory of the aircraft.

    Abstract translation: 执行机场防碰撞的系统和方法。 机翼安装的相机允许飞行员肯定地确定翼尖将清除位于视频中的物体。 在飞行器上实现的示例性系统包括具有生成视频流的摄像机的翼尖模块和发送生成的视频流的通信设备。 处理器接收视频流并生成视频流的网状。 显示装置同时呈现视频流和网状物。 网格包括水平线，并且基于相机的镜头的焦距和相机在地面上方的高度。 网状物包括弯曲和/或直线距离线和弯曲或直线行进线。 行驶线对应于至少一个飞行器部件或重要的区域，并且基于相机的位置和飞行器的轨迹。

    SYSTEMS AND METHODS FOR FILTERING WINGTIP SENSOR INFORMATION
    13.
    发明申请
    SYSTEMS AND METHODS FOR FILTERING WINGTIP SENSOR INFORMATION 有权
    过滤传感器信息的系统和方法

    公开(公告)号：US20130321193A1

    公开(公告)日：2013-12-05

    申请号：US13741291

    申请日：2013-01-14

    Applicant: HONEYWELL INTERNATIONAL INC.

    Inventor： Jiri Vasek ,  Pavel Kolcarek ,  Olukayode Olofinboba

    IPC: G01S13/93 ,  G01S7/04 ,  G01S13/04

    CPC classification number: G01S13/93 ,  G01S7/04 ,  G01S7/51 ,  G01S13/04 ,  G01S13/931 ,  G01S17/933 ,  G01S2013/9335 ,  G08G5/0021 ,  G08G5/0078 ,  G08G5/045 ,  G08G5/065

    Abstract: Systems and methods for providing improved situational awareness for an aircraft while taxiing. An exemplary method generates reflectivity data based on an associated emission at a transceiver located on an aircraft. At a processor, targets are determined if a portion of the generated reflectivity data is greater than a predefined threshold. Then, the analyzed targets are determined as to whether they are within a dynamically defined three-dimensional envelope. The envelope is based on wingtip light module speed and trajectory. On a display device, an indication of the nearest target is presented at the associated range to the nearest target.

    Abstract translation: 系统和方法，用于在滑行时为飞机提供改善的情境意识。 示例性方法基于位于飞机上的收发器处的相关发射产生反射率数据。 在处理器中，确定所生成的反射率数据的一部分是否大于预定阈值的目标。 然后，确定分析的目标是否在动态定义的三维包络内。 信封是基于机翼灯模块的速度和轨迹。 在显示设备上，将最近的目标的指示呈现在与最近的目标相关联的范围上。

    Software development kit for aircraft tablet device and airborne application server
    14.
    发明授权
    Software development kit for aircraft tablet device and airborne application server 有权

    公开(公告)号：US10666734B2

    公开(公告)日：2020-05-26

    申请号：US16254198

    申请日：2019-01-22

    Applicant: Honeywell International Inc.

    Inventor： Matej Dusik ,  John Beckwith ,  John Hajdukiewicz ,  Filip Magula ,  Frantisek Mikulu ,  Jiri Vasek

    IPC: H04L29/08 ,  G06F8/70 ,  H04W88/02 ,  B64D45/00

    Abstract: A server system for an aircraft is provided. In one embodiment, the server system comprises an aircraft server unit that is operative to receive data from one or more data sources, and a software development kit (SDK) application server in operative communication with the aircraft server unit. The SDK application server comprises one or more processing core modules configured to process the data from the one or more data sources, and one or more application modules including one or more aircraft tablet device logic modules that are configured to respectively execute one or more aircraft tablet device applications. The data processed by the one or more processing core modules is separated from the one or more aircraft tablet device logic modules. The SDK application server is configured to communicate with one or more external portable computing devices.

    Software development kit for aircraft tablet device and airborne application server
    15.
    发明授权
    Software development kit for aircraft tablet device and airborne application server 有权

    公开(公告)号：US10225349B2

    公开(公告)日：2019-03-05

    申请号：US15334822

    申请日：2016-10-26

    Applicant: Honeywell International Inc.

    Inventor： Matej Dusik ,  John Beckwith ,  John Hajdukiewicz ,  Filip Magula ,  Frantisek Mikulu ,  Jiri Vasek

    IPC: H04W80/04 ,  H04L29/08 ,  G06F8/70 ,  H04W88/02 ,  B64D45/00

    Abstract: A server system for an aircraft is provided. In one embodiment, the server system comprises an aircraft server unit that is operative to receive data from one or more data sources, and a software development kit (SDK) application server in operative communication with the aircraft server unit. The SDK application server comprises one or more processing core modules configured to process the data from the one or more data sources, and one or more application modules including one or more aircraft tablet device logic modules that are configured to respectively execute one or more aircraft tablet device applications. The data processed by the one or more processing core modules is separated from the one or more aircraft tablet device logic modules. The SDK application server is configured to communicate with one or more external portable computing devices.

    System and method for providing enhanced HMI navigation
    18.
    发明授权
    System and method for providing enhanced HMI navigation 有权
    提供增强HMI导航的系统和方法

    公开(公告)号：US09335917B2

    公开(公告)日：2016-05-10

    申请号：US14299197

    申请日：2014-06-09

    Applicant: HONEYWELL INTERNATIONAL INC.

    Inventor： Martin Dostal ,  Jiri Vasek ,  Matej Papp

    IPC: G01C23/00 ,  G06F3/0485 ,  G01C21/00 ,  G06F3/0484

    CPC classification number: G06F3/04855 ,  G01C21/00 ,  G01C23/00 ,  G06F3/04842 ,  G06F3/04847 ,  G08G5/0021 ,  G08G5/0052 ,  G08G5/006 ,  G08G5/0091

    Abstract: A method and apparatus is provided for enhancing an HMI (Human Machine Interface) mechanism to include continuous, sequential, and time-based navigation capabilities. Airspace data associated with a flight plan is received, and the airspace data associated with a region of the flight plan is displayed. A time scale substantially coextensive with the region is also displayed. To view a future region of the airspace, the time scale on the display is moved in a first direction, and to view a previous region, the time scale on the display is moved in a second, substantially opposite direction.

    Abstract translation: 提供了一种用于增强HMI（人机接口）机制以包括连续，顺序和基于时间的导航功能的方法和装置。 接收与飞行计划相关联的空域数据，并且显示与飞行计划的区域相关联的空域数据。 还显示了与该区域基本上共同延伸的时间尺度。 为了查看空域的未来区域，显示器上的时间尺度沿第一方向移动，并且为了查看前一区域，显示器上的时间刻度在第二基本上相反的方向上移动。

    SYSTEM AND METHOD FOR PROVIDING ENHANCED HMI NAVIGATION
    19.
    发明申请
    SYSTEM AND METHOD FOR PROVIDING ENHANCED HMI NAVIGATION 有权
    用于提供增强HMI导航的系统和方法

    公开(公告)号：US20150355832A1

    公开(公告)日：2015-12-10

    申请号：US14299197

    申请日：2014-06-09

    Applicant: HONEYWELL INTERNATIONAL INC.

    Inventor： Martin Dostal ,  Jiri Vasek ,  Matej Papp

    IPC: G06F3/0485 ,  G06F3/0484 ,  G01C21/00

    CPC classification number: G06F3/04855 ,  G01C21/00 ,  G01C23/00 ,  G06F3/04842 ,  G06F3/04847 ,  G08G5/0021 ,  G08G5/0052 ,  G08G5/006 ,  G08G5/0091

    Abstract: A method and apparatus is provided for enhancing an HMI (Human Machine Interface) mechanism to include continuous, sequential, and time-based navigation capabilities. Airspace data associated with a flight plan is received, and the airspace data associated with a region of the flight plan is displayed. A time scale substantially coextensive with the region is also displayed. To view a future region of the airspace, the time scale on the display is moved in a first direction, and to view a previous region, the time scale on the display is moved in a second, substantially opposite direction.

    Abstract translation: 提供了一种用于增强HMI（人机接口）机制以包括连续，顺序和基于时间的导航功能的方法和装置。 接收与飞行计划相关联的空域数据，并且显示与飞行计划的区域相关联的空域数据。 还显示了与该区域基本上共同延伸的时间尺度。 为了查看空域的未来区域，显示器上的时间尺度沿第一方向移动，并且为了查看前一区域，显示器上的时间刻度在第二基本上相反的方向上移动。

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