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：US20150073628A1

公开(公告)日：2015-03-12

申请号：US14021046

申请日：2013-09-09

Applicant: Honeywell International Inc.

Inventor： James Alexander Nicholls ,  Patricia May Ververs ,  Gang He ,  Marc Lajeunesse ,  Mark Sutter

IPC: B64D45/00

CPC classification number: B64D45/00 ,  G01C23/005

Abstract: A system and method are provided for integrating and displaying the collective cue and the pitch and roll cue of a helicopter display with a flight path marker providing a moving reference showing the aircraft flight path.

Abstract translation: 提供了一种系统和方法，用于整合和显示直升机展示的集体提示和俯仰和滚动提示，其中具有提供显示飞行器飞行路径的移动参考的飞行路径标记。

公开(公告)号：US20140207315A1

公开(公告)日：2014-07-24

申请号：US13747539

申请日：2013-01-23

Applicant: HONEYWELL INTERNATIONAL INC.

Inventor： Gang He

IPC: B64D45/08

CPC classification number: G01C23/005

Abstract: A system and method displays an intercept point on a synthetic vision display that conforms to the flight path intercepting the terrain when the nose of the helicopter is pitched up during landing. A steep approach during landing may be detected by an evaluation of, for example, attitude of the helicopter, rate of descent, and airspeed.

Abstract translation: 一种系统和方法在合成视觉显示屏上显示一个截距点，该拦截点符合在着陆期间直升机的鼻子俯仰时拦截地形的飞行路径。 通过对直升机的姿态，下降速率和空速进行评估可以检测着陆时的陡峭方法。

公开(公告)号：US20140058675A1

公开(公告)日：2014-02-27

申请号：US14077266

申请日：2013-11-12

Applicant: Honeywell International Inc.

Inventor： Gang He ,  John G. Suddreth ,  Thea L. Feyereisen

IPC: G01C21/00

CPC classification number: G01C23/005 ,  G01C21/00 ,  G01C23/00 ,  G06T7/70 ,  G06T11/20 ,  G06T19/003 ,  G08G5/0021

Abstract: A flight deck display system for an aircraft includes a processor architecture configured to receive aircraft instrument data, waypoint restriction information, and position data for the aircraft and, based upon the received 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 display that includes a perspective view of terrain and at least one waypoint marker corresponding to an approaching waypoint. The waypoint marker includes visually distinguishable characteristics that convey waypoint restriction information (e.g., altitude or airspeed constraint information that governs the waypoint).

Abstract translation: 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，航路点限制信息和飞机的位置数据的处理器架构，并且基于接收的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，呈现包括地形的透视图和至少一个对应于接近航点的航路点标记的显示。 航路点标记包括传达路点限制信息（例如，管理航点的高度或空速约束信息）的视觉上可区分的特征。