公开(公告)号：US09734729B2

公开(公告)日：2017-08-15

申请号：US13860699

申请日：2013-04-11

Applicant: HONEYWELL INTERNATIONAL INC.

Inventor： Tomas Beda ,  Ondrej Koukol ,  Ondrej Pokorny

IPC: G08G5/06 ,  G08G5/00 ,  G06K9/00 ,  G06T7/73 ,  G01C23/00

CPC classification number: G08G5/065 ,  G01C23/00 ,  G06K9/00791 ,  G06T7/73 ,  G06T2207/10048 ,  G06T2207/30256 ,  G08G5/0021 ,  G08G5/0026

Abstract: A method for displaying stop bar information to an aircrew member of an aircraft includes the steps of capturing a light signature emitted from an area surrounding the aircraft, processing the captured light signature to detect a lighted stop bar, and providing information to the aircrew member regarding the detection of the lighted stop bar.

公开(公告)号：US20140309915A1

公开(公告)日：2014-10-16

申请号：US13860699

申请日：2013-04-11

Applicant: HONEYWELL INTERNATIONAL INC.

Inventor： Tomas Beda ,  Ondrej Koukol ,  Ondrej Pokorny

IPC: G08G5/06

CPC classification number: G08G5/065 ,  G01C23/00 ,  G06K9/00791 ,  G06T7/73 ,  G06T2207/10048 ,  G06T2207/30256 ,  G08G5/0021 ,  G08G5/0026

Abstract: A method for displaying stop bar information to an aircrew member of an aircraft includes the steps of capturing a light signature emitted from an area surrounding the aircraft, processing the captured light signature to detect a lighted stop bar, and providing information to the aircrew member regarding the detection of the lighted stop bar.

Abstract translation: 用于向飞机的空勤人员显示停止条信息的方法包括以下步骤：捕获从飞行器周围的区域发射的光签名，处理所捕获的光签名以检测点燃的停止条，以及向机组成员提供关于 检测点火停止杆。

公开(公告)号：US09269272B2

公开(公告)日：2016-02-23

申请号：US14227613

申请日：2014-03-27

Applicant: HONEYWELL INTERNATIONAL INC.

Inventor： Ondrej Koukol ,  Gang He ,  Simon Innocent

IPC: G06F19/00 ,  G08G5/02 ,  G01S19/15 ,  G01S19/42 ,  B64D45/04

CPC classification number: G08G5/02 ,  B64D45/04 ,  G01S1/022 ,  G01S1/024 ,  G01S1/14 ,  G01S19/15 ,  G01S19/42 ,  G01S19/48

Abstract: A system and method of monitoring received instrument landing system (ILS) signals onboard an aircraft includes performing a pre-approach sampling of the received ILS signals to thereby generate pre-approach phase ILS data. A statistical approach course of the aircraft is determined based at least in part on the pre-approach phase ILS data. A determination is made as to when the aircraft is below a predetermined activation altitude and, when it is, approach sampling of the received ILS signals is performed to generate approach phase ILS data. The approach phase ILS data is compared to the statistical approach course to determine a course deviation. An alert signal is selectively generated when the course deviation exceeds a predetermined magnitude.

Abstract translation: 监测飞机上接收的仪表着陆系统（ILS）信号的系统和方法包括对所接收的ILS信号进行预先进行采样，从而产生预进入阶段ILS数据。 至少部分地基于前进阶段ILS数据确定飞行器的统计学方法。 确定飞行时间何时低于预定的激活高度，并且当它被接收到接收的ILS信号的接近采样以产生接近阶段ILS数据时。 将接近阶段的ILS数据与统计学方法进行比较，以确定课程偏差。 当行程偏差超过预定幅度时，选择性地产生报警信号。

公开(公告)号：US20160012735A1

公开(公告)日：2016-01-14

申请号：US14227613

申请日：2014-03-27

Applicant: HONEYWELL INTERNATIONAL INC.

Inventor： Ondrej Koukol ,  Gang He ,  Simon Innocent

IPC: G08G5/02 ,  G01S19/42 ,  B64D45/04 ,  G01S19/15

CPC classification number: G08G5/02 ,  B64D45/04 ,  G01S1/022 ,  G01S1/024 ,  G01S1/14 ,  G01S19/15 ,  G01S19/42 ,  G01S19/48

Abstract: A system and method of monitoring received instrument landing system (ILS) signals onboard an aircraft includes performing a pre-approach sampling of the received ILS signals to thereby generate pre-approach phase ILS data. A statistical approach course of the aircraft is determined based at least in part on the pre-approach phase ILS data. A determination is made as to when the aircraft is below a predetermined activation altitude and, when it is, approach sampling of the received ILS signals is performed to generate approach phase ILS data. The approach phase ILS data is compared to the statistical approach course to determine a course deviation. An alert signal is selectively generated when the course deviation exceeds a predetermined magnitude.

Abstract translation: 监测飞机上接收的仪表着陆系统（ILS）信号的系统和方法包括对所接收的ILS信号进行预先进行采样，从而产生预进入阶段ILS数据。 至少部分地基于前进阶段ILS数据确定飞行器的统计学方法。 确定飞行时间何时低于预定的激活高度，并且当它被接收到接收的ILS信号的接近采样以产生接近阶段ILS数据时。 将接近阶段的ILS数据与统计学方法进行比较，以确定课程偏差。 当行程偏差超过预定幅度时，选择性地产生报警信号。

公开(公告)号：US20140249736A1

公开(公告)日：2014-09-04

申请号：US13783611

申请日：2013-03-04

Applicant: HONEYWELL INTERNATIONAL INC.

Inventor： Tomas Beda ,  Ondrej Koukol ,  Tomas Marczi

IPC: G08G5/06

CPC classification number: G08G5/065 ,  G05D1/0083 ,  G05D1/0274 ,  G05D1/0278 ,  G05D1/0297

Abstract: Embodiments of the subject application provide methods and systems for an autonomous aircraft guiding mobile unit (GMU). The GMU includes one or more light modules, one or more processing units, and one or more data storage mediums. The one or more data storage mediums include instructions which, when executed by the one or more processing units, cause the one or more processing units to receive control messages from a traffic control ground station (TCGS), the control messages assigning the GMU to an aircraft and controlling movement of the GMU and its assigned aircraft, and to provide light commands to a pilot of the assigned aircraft with the one or more light modules, the light commands directing movement of the assigned aircraft during taxiing.

Abstract translation: 本申请的实施例提供了用于自主飞行器引导移动单元（GMU）的方法和系统。 GMU包括一个或多个光模块，一个或多个处理单元和一个或多个数据存储介质。 所述一个或多个数据存储介质包括指令，当所述一个或多个处理单元执行时，使所述一个或多个处理单元从交通控制地面站（TCGS）接收控制消息，所述控制消息将所述GMU分配给 飞机和控制GMU及其指定飞机的运动，并且向所指定的飞机的飞行员提供具有所述一个或多个光模块的轻型指令，所述指令指示所述飞机在滑行期间的运动。