公开(公告)号：US09070283B2

公开(公告)日：2015-06-30

申请号：US13752782

申请日：2013-01-29

Applicant: HONEYWELL INTERNATIONAL INC.

Inventor： Subash Samuthirapandian ,  Fazurudheen A ,  Markus Johnson

IPC: G08G5/04 ,  G08G5/00

CPC classification number: G08G5/0008 ,  G08G5/0021 ,  G08G5/0078

Abstract: Embodiments of a flight deck display system for deployment onboard a host aircraft are provided, as are embodiments of a method carried-out by a flight deck display system. In one embodiment, the flight deck display system includes a cockpit display, a wireless communication module, and a controller operatively coupled to the cockpit display and to the wireless communication module. The controller is configured to generate a vertical In-Trail Procedure (ITP) window on the cockpit display, which includes graphics representative of the current position of the host aircraft, the current position of an intruder aircraft when present within a predetermined distance of the host aircraft, and a plurality of flight levels. The controller is further configured to receive data from which the current flight path of the intruder aircraft can be derived; and periodically update the vertical ITP window to include flight path symbology indicative of the current flight path of the intruder aircraft.

Abstract translation: 提供了用于部署在主机上的飞行甲板显示系统的实施例，由飞行甲板显示系统执行的方法的实施例。 在一个实施例中，驾驶舱显示系统包括驾驶舱显示器，无线通信模块和可操作地耦合到驾驶舱显示器和无线通信模块的控制器。 控制器被配置为在驾驶舱显示器上生成垂直行进步骤（ITP）窗口，该窗口包括代表主机飞行器当前位置的图形，当存在于主机的预定距离内时入侵者飞行器的当前位置 飞机和多个飞行高度。 所述控制器还被配置为接收可从其导出入侵者飞行器的当前飞行路径的数据; 并定期更新垂直ITP窗口，以包括指示入侵者飞机当前飞行路径的飞行路线符号系统。

公开(公告)号：US20140210648A1

公开(公告)日：2014-07-31

申请号：US13752782

申请日：2013-01-29

Applicant: HONEYWELL INTERNATIONAL INC.

Inventor： Subash Samuthirapandian ,  Fazurudheen A ,  Markus Johnson

IPC: G08G5/00

CPC classification number: G08G5/0008 ,  G08G5/0021 ,  G08G5/0078

Abstract: Embodiments of a flight deck display system for deployment onboard a host aircraft are provided, as are embodiments of a method carried-out by a flight deck display system. In one embodiment, the flight deck display system includes a cockpit display, a wireless communication module, and a controller operatively coupled to the cockpit display and to the wireless communication module. The controller is configured to generate a vertical In-Trail Procedure (ITP) window on the cockpit display, which includes graphics representative of the current position of the host aircraft, the current position of an intruder aircraft when present within a predetermined distance of the host aircraft, and a plurality of flight levels. The controller is further configured to receive data from which the current flight path of the intruder aircraft can be derived; and periodically update the vertical ITP window to include flight path symbology indicative of the current flight path of the intruder aircraft.

Abstract translation: 提供了用于部署在主机上的飞行甲板显示系统的实施例，由飞行甲板显示系统执行的方法的实施例。 在一个实施例中，驾驶舱显示系统包括驾驶舱显示器，无线通信模块和可操作地耦合到驾驶舱显示器和无线通信模块的控制器。 控制器被配置为在驾驶舱显示器上生成垂直行进步骤（ITP）窗口，该窗口包括代表主机飞行器当前位置的图形，当存在于主机的预定距离内时入侵者飞行器的当前位置 飞机和多个飞行高度。 所述控制器还被配置为接收可从其导出入侵者飞行器的当前飞行路径的数据; 并定期更新垂直ITP窗口，以包括指示入侵者飞机当前飞行路径的飞行路线符号系统。

公开(公告)号：US20150212782A1

公开(公告)日：2015-07-30

申请号：US14163263

申请日：2014-01-24

Applicant: HONEYWELL INTERNATIONAL INC.

Inventor： Subash Samuthirapandian ,  Markus Alan Johnson ,  Fazurudheen A

IPC: G06F3/14 ,  G08G5/04 ,  G06T1/00 ,  G08G5/00

CPC classification number: G06F3/1407 ,  G01C23/00 ,  G06T1/0007 ,  G08G5/0008 ,  G08G5/0021 ,  G08G5/0078 ,  G08G5/045

Abstract: Presented herein is a system and method for graphically displaying intruder aircraft symbology on an avionics display system onboard a host aircraft. The method comprises receiving data from the intruder aircraft, determining the reference altitude of the intruder aircraft, displaying intruder symbology on the display, and generating symbology on the display to visually distinguish the intruder symbology when the barosetting of the intruder is not substantially equal to the barosetting of the host aircraft.

Abstract translation: 这里提出的是用于在主机上的航空电子显示系统上图形地显示入侵者飞行器符号系统的系统和方法。 该方法包括从入侵飞行器接收数据，确定入侵者飞机的参考高度，在显示器上显示入侵者符号系统，并且在入侵者的撞击力基本不等于 主机飞机的轰轰烈烈