公开(公告)号：US11585942B2

公开(公告)日：2023-02-21

申请号：US17080419

申请日：2020-10-26

Applicant: Honeywell International Inc.

Inventor： Guoqing Wang ,  Xiao Cao ,  Ping Ye

IPC: G01S19/21

Abstract: In some examples, a system includes a transceiver configured to receive surveillance messages from Y target vehicles, where Y is an integer greater than two. The system includes processing circuitry configured to determine predicted positions of the Y target vehicles based on the surveillance messages. The processing circuitry is also configured to determine reported positions of the Y target vehicles based on later received surveillance messages. The processing circuitry is further configured to determine that respective differences between the respective predicted position and the respective reported position for X of the Y target vehicles is greater than a threshold distance. The processing circuitry is configured to determine that Global Navigation Satellite System interference has occurred in response to determining that X divided by Y is greater than a threshold level.

公开(公告)号：US20230017616A1

公开(公告)日：2023-01-19

申请号：US17080419

申请日：2020-10-26

Applicant: Honeywell International Inc.

Inventor： Guoqing Wang ,  Xiao Cao ,  Ping Ye

IPC: G01S19/21 ,  G08G5/00 ,  G01S19/51

Abstract: In some examples, a system includes a transceiver configured to receive surveillance messages from Y target vehicles, where Y is an integer greater than two. The system includes processing circuitry configured to determine predicted positions of the Y target vehicles based on the surveillance messages. The processing circuitry is also configured to determine reported positions of the Y target vehicles based on later received surveillance messages. The processing circuitry is further configured to determine that respective differences between the respective predicted position and the respective reported position for X of the Y target vehicles is greater than a threshold distance. The processing circuitry is configured to determine that Global Navigation Satellite System interference has occurred in response to determining that X divided by Y is greater than a threshold level.

公开(公告)号：US10700767B2

公开(公告)日：2020-06-30

申请号：US15072210

申请日：2016-03-16

Applicant: Honeywell International Inc.

Inventor： Guoqing Wang ,  Haiming Wang ,  Haifeng Wang ,  Danhua Liang

IPC: H04B7/185 ,  G01W1/02 ,  G01C21/20 ,  G01W1/00 ,  G08G5/00 ,  G01S13/95 ,  G01S7/00

Abstract: A ground weather center may transmit information requests that carry at least one meteorological specific triggering command. An airborne system may translate the triggering command into detectable meteorological conditions and may arm the trigger(s) for specific weather sensors accordingly and downlink information upon the airborne system detects the triggering conditions. By using such a triggering command, the airborne system may be able transmit the same amount of valuable information with less bandwidth by reducing the number of redundant downlinked packets.

公开(公告)号：US10562642B2

公开(公告)日：2020-02-18

申请号：US15381926

申请日：2016-12-16

Applicant: Honeywell International Inc.

Inventor： Guoqing Wang ,  Ruy C. Brandao ,  Rong Zhang ,  Zhong Chen ,  Ray Zhang

IPC: B64D45/00 ,  G01D7/08 ,  G01S5/02 ,  G08G5/04 ,  G01S19/03

Abstract: A system for tracking a vehicle includes a transceiver configured to receive a first signal including first surveillance data from the vehicle at a first time, and receive a second signal from the vehicle at a second time. The system further includes processing circuitry configured to determine a first location and a first course of the vehicle at the first time based on the first surveillance data, and determine a change in power level from the first signal to the second signal. The processing circuitry is further configured to predict a maneuver for the vehicle based on the first location, the first course, and the change in power level from the first signal to the second signal.

公开(公告)号：US20180170573A1

公开(公告)日：2018-06-21

申请号：US15381926

申请日：2016-12-16

Applicant: Honeywell International Inc.

Inventor： Guoqing Wang ,  Ruy C. Brandao ,  Rong Zhang ,  Zhong Chen ,  Ray Zhang

IPC: B64D45/00 ,  G08G5/04 ,  G01S5/02 ,  G01D7/08

Abstract: A system for tracking a vehicle includes a transceiver configured to receive a first signal including first surveillance data from the vehicle at a first time, and receive a second signal from the vehicle at a second time. The system further includes processing circuitry configured to determine a first location and a first course of the vehicle at the first time based on the first surveillance data, and determine a change in power level from the first signal to the second signal. The processing circuitry is further configured to predict a maneuver for the vehicle based on the first location, the first course, and the change in power level from the first signal to the second signal.

公开(公告)号：US09773421B2

公开(公告)日：2017-09-26

申请号：US14886982

申请日：2015-10-19

Applicant: Honeywell International Inc.

Inventor： Guoqing Wang ,  Rong Zhang ,  Kevin J Conner ,  Ruy C. Brandao ,  Zhong Chen

IPC: G08G5/00

CPC classification number: G08G5/0078 ,  G08G5/0008 ,  G08G5/0021 ,  G08G5/0065

Abstract: This disclosure is directed to systems and methods for generating outputs based on collected aircraft maneuver data. In one example, a system is configured to collect surveillance data from one or more aircraft. The system is further configured to identify, from the collected surveillance data, aircraft maneuver data indicative of maneuvers of the one or more aircraft. The system is further configured to store the aircraft maneuver data in a data store. The system is further configured to perform one or more analyses of the stored aircraft maneuver data in the data store. The system is further configured to generate an output based on the one or more analyses of the stored aircraft maneuver data.

公开(公告)号：US20170110018A1

公开(公告)日：2017-04-20

申请号：US14886982

申请日：2015-10-19

Applicant: Honeywell International Inc.

Inventor： Guoqing Wang ,  Rong Zhang ,  Kevin J. Conner ,  Ruy C. Brandao ,  Zhong Chen

IPC: G08G5/00

CPC classification number: G08G5/0078 ,  G08G5/0008 ,  G08G5/0021 ,  G08G5/0065

Abstract: This disclosure is directed to systems and methods for generating outputs based on collected aircraft maneuver data. In one example, a system is configured to collect surveillance data from one or more aircraft. The system is further configured to identify, from the collected surveillance data, aircraft maneuver data indicative of maneuvers of the one or more aircraft. The system is further configured to store the aircraft maneuver data in a data store. The system is further configured to perform one or more analyses of the stored aircraft maneuver data in the data store. The system is further configured to generate an output based on the one or more analyses of the stored aircraft maneuver data.

公开(公告)号：US20190266814A1

公开(公告)日：2019-08-29

申请号：US15907487

申请日：2018-02-28

Applicant: HONEYWELL INTERNATIONAL INC.

Inventor： Haidong Huang ,  Guoqing Wang ,  Chuanbo Liang ,  Jianfeng Guo

IPC: G07C5/08 ,  G06F3/0482 ,  G06F17/30 ,  B64D45/00 ,  B64F5/40

Abstract: A method for providing Electronic Circuit Breaker (ECB) data onboard an aircraft is provided. The method obtains a current checklist applicable to current operations of the aircraft, by a processor communicatively coupled to an ECB system associated with the aircraft; obtains mapping data comprising mappings of aviation checklists mapped to associated ECB data, by the processor; identifies a subset of the ECB data associated with the current checklist, based on the mapping data, by the processor, wherein the current checklist includes a plurality of checklist tasks, and wherein the subset comprises at least one of the plurality of ECL tasks that includes an ECB instruction; filters the current checklist to create a filtered ECB list of the at least one of the plurality of checklist tasks, by the processor; and presents the filtered ECB list, via an ECB display onboard the aircraft.

公开(公告)号：US20170039858A1

公开(公告)日：2017-02-09

申请号：US14819635

申请日：2015-08-06

Applicant: HONEYWELL INTERNATIONAL INC.

Inventor： Guoqing Wang ,  Chuan Jiang ,  Robert E. De Mers

IPC: G08G5/00 ,  G10L25/72 ,  G10L25/51

CPC classification number: G08G5/0013 ,  G06F3/16 ,  G06F3/167 ,  G06F11/00 ,  G08G5/0021 ,  G08G5/0052 ,  G08G5/006 ,  G10L15/08 ,  G10L25/51 ,  G10L25/72 ,  G10L2015/085 ,  G10L2015/221

Abstract: A method for detecting noncompliance with aviation regulations and operating procedures is disclosed herein. The method analyzes communication associated with a host aircraft to identify key information, stores the identified key information in a data storage device, and determines whether a particular aviation regulation or operating procedure applies to the host aircraft. After determining that a regulation or operating procedure applies, the stored key information is compared against reference information maintained in a database in association with the regulation or operating procedure. An alert is generated when the comparing detects a discrepancy between the stored key information and the reference information.

Abstract translation: 本文公开了一种检测不符合航空规章和操作程序的方法。 该方法分析与主机相关联的通信以识别密钥信息，将所识别的密钥信息存储在数据存储设备中，并且确定特定航空规则或操作过程是否适用于主机。 在确定适用规则或操作程序之后，将存储的密钥信息与与规则或操作过程相关联的数据库中保存的参考信息进行比较。 当比较检测到存储的密钥信息和参考信息之间的差异时，生成警报。

公开(公告)号：US20160282120A1

公开(公告)日：2016-09-29

申请号：US14669143

申请日：2015-03-26

Applicant: HONEYWELL INTERNATIONAL INC.

Inventor： Guoqing Wang ,  Bin Zhang ,  Lin Du

IPC: G01C21/00 ,  G01S19/42 ,  G08G5/00 ,  G01C21/20 ,  G01C23/00

CPC classification number: G01C21/005 ,  G01C21/20 ,  G01C23/00 ,  G01S19/42 ,  G08G5/0013 ,  G08G5/0021 ,  G08G5/0078 ,  G08G5/0086 ,  G08G5/025

Abstract: An aircraft synthetic vision display system (SVS) includes a topographical database including topographical information relating to an airport, a global positioning system receiver that receives a satellite signal from a global positioning satellite to determine a geographical position of the aircraft, and a ground-based augmentation system receiver that receives a ground-based signal from a ground-based transmitter associated with the airport, wherein the ground-based signal includes geographical information associated with the airport. The SVS further includes a computer processor that retrieves the topographical information from the topographical database based on the geographical position of the aircraft, that retrieves the geographical information associated with the airport, and that corrects the topographical information using the geographical information associated with the airport to generate corrected topographical information. Still further, the SVS includes a display device that renders three-dimensional synthetic imagery of environs of the aircraft based on the corrected topographical information.

Abstract translation: 飞机合成视觉显示系统（SVS）包括一个地形数据库，其中包括与机场有关的地形信息，一个从全球定位卫星接收卫星信号以确定飞机地理位置的全球定位系统接收机，以及基于地面 增强系统接收器，其从与机场相关联的基于地面的发射器接收基于地面的信号，其中所述基于地面的信号包括与所述机场相关联的地理信息。 SVS还包括计算机处理器，其基于飞行器的地理位置从地形数据库检索地形信息，其检索与机场相关联的地理信息，并且使用与机场相关联的地理信息来校正地形信息 生成更正的地形信息。 此外，SVS包括显示装置，其基于校正的地形信息来呈现飞行器的环境的三维合成图像。