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    Aircraft maneuver data management system
    1.
    发明授权
    Aircraft maneuver data management system 有权

    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.

    Runway location determination
    3.
    发明授权
    Runway location determination 有权
    跑道位置确定

    公开(公告)号：US09406235B2

    公开(公告)日：2016-08-02

    申请号：US14250022

    申请日：2014-04-10

    Applicant: Honeywell International Inc.

    Inventor： Kevin J Conner ,  Christine Marie Haissig ,  Ruy C. Brandao

    IPC: G01C21/00 ,  G08G5/00 ,  G01C21/30 ,  G08G5/06

    CPC classification number: G08G5/0017 ,  G01C21/00 ,  G01C21/30 ,  G08G5/0013 ,  G08G5/0082 ,  G08G5/065

    Abstract: In some examples described herein, a runway location is determined based on aircraft state information from at least one aircraft. For example, a processor may determine the coordinates of one or more points of a runway based on aircraft state information generated by one or more aircraft using the runway. In some examples, the processor may aggregate coordinates determined from the aircraft state information provided by a plurality of different aircraft in order to determine the location of the runway. The processor can be located onboard an aircraft providing the state information, onboard a different aircraft, or external to any aircraft.

    Abstract translation: 在本文描述的一些示例中，基于来自至少一架飞行器的飞机状态信息来确定跑道位置。 例如，处理器可以基于由使用跑道的一个或多个飞行器产生的飞行器状态信息来确定跑道的一个或多个点的坐标。 在一些示例中，处理器可以聚集由多个不同飞行器提供的飞行器状态信息确定的坐标，以便确定跑道的位置。 处理器可以位于提供状态信息的飞机上，在不同的飞机上或在任何飞机外部。

    System and method for modulating alerts for an intended runway
    4.
    发明授权
    System and method for modulating alerts for an intended runway 有权
    调整预期跑道的警报的系统和方法

    公开(公告)号：US09293052B2

    公开(公告)日：2016-03-22

    申请号：US14060768

    申请日：2013-10-23

    Applicant: HONEYWELL INTERNATIONAL INC.

    Inventor： Kevin J Conner ,  Yasuo Ishihara ,  Steve Johnson

    IPC: G08G5/02 ,  G08G5/00 ,  G05D1/00 ,  G05D1/06

    CPC classification number: G08G5/0021 ,  G05D1/0077 ,  G05D1/0676 ,  G08G5/0065 ,  G08G5/025

    Abstract: A system and method provide an alert to a pilot of an aircraft aurally with a given volume and inflection, and/or visually with a text message which includes color, font, and pitch (size). The alert is rendered in distinct fashion for the expected and unexpected cases, e.g., an intended runway and an unintended runway. In a preferred embodiment, the alert for the intended runway is changed to a confirmation level, or one that is less likely to interfere with other information flow, while the alert for the unintended runway would be provided in a more conspicuous manner.

    Abstract translation: 一种系统和方法向具有给定音量和拐点的声音的飞行员提供警报，和/或以视觉方式提供包括颜色，字体和音调（大小）的文本消息的警报。 对于预期和意想不到的情况，例如预期的跑道和非预期的跑道，警报以不同的方式呈现。 在优选实施例中，预期跑道的警报改变为确认级别，或者更不可能干扰其他信息流的警报，同时将以更显眼的方式提供非预期跑道的警报。

    Aircraft systems and methods for attitude recovery
    6.
    发明授权
    Aircraft systems and methods for attitude recovery 有权
    飞机系统和姿态恢复方法

    公开(公告)号：US09221552B2

    公开(公告)日：2015-12-29

    申请号：US13901022

    申请日：2013-05-23

    Applicant: HONEYWELL INTERNATIONAL INC.

    Inventor： Kevin J Conner ,  Yasuo Ishihara ,  Thea L. Feyereisen ,  John Allan Morgan

    IPC: G08B23/00 ,  B64D45/00 ,  G01C23/00

    CPC classification number: B64D45/00 ,  G01C23/005

    Abstract: A vehicle system is provided. The system includes a processor configured to receive data representative of a current attitude and a desired attitude and to generate display signals associated with the current attitude and the desired attitude. The system further includes a display device configured to receive the display signals and operable to selectively render an image including roll angle alert symbology. The roll angle alert symbology includes a first curved arrow.

    Abstract translation: 提供车辆系统。 该系统包括处理器，其被配置为接收表示当前姿态和期望姿势的数据，并且产生与当前姿态和期望姿态相关联的显示信号。 该系统还包括被配置为接收显示信号并且可操作以选择性地呈现包括滚转角警报符号系统的图像的显示装置。 滚角警报符号系统包括第一个弯曲的箭头。

    GROUND OBSTACLE COLLISION ALERT DEACTIVATION
    7.
    发明申请
    GROUND OBSTACLE COLLISION ALERT DEACTIVATION 有权
    接地障碍冲突警报消除

    公开(公告)号：US20150170525A1

    公开(公告)日：2015-06-18

    申请号：US14109093

    申请日：2013-12-17

    Applicant: Honeywell International Inc.

    Inventor： Kevin J Conner ,  Tomas Marczi ,  Christine Marie Haissig ,  John Howard Glover

    IPC: G08G5/00 ,  G08G5/06

    CPC classification number: G08G5/0021 ,  G08G5/0073 ,  G08G5/06 ,  G08G5/065

    Abstract: In some examples, a processor is configured to control a ground obstacle collision alerting system of an aircraft to deactivate delivery of ground obstacle collision alerts in response to determining the aircraft is in a designated ground area. In some examples, the processor is configured to determine the aircraft is in the designated ground area based on user input, based on a geographic location of the aircraft, or both. The processor is further configured to control the ground obstacle collision alerting system to automatically reactivate the delivery of the ground obstacle collision alerts in response to determining the aircraft is outside of the designated ground area. In some examples, the processor is configured to determine the aircraft is outside of the designated ground area based on a geographic location of the aircraft, a ground speed of the aircraft, or both.

    Abstract translation: 在一些示例中，处理器被配置为响应于确定飞行器在指定的地面区域来控制飞行器的地面障碍物碰撞警报系统以停用地面障碍物碰撞警报的传递。 在一些示例中，处理器被配置为基于飞行器的地理位置或两者来基于用户输入来确定飞行器在指定地面区域。 所述处理器还被配置为响应于确定所述飞机在所述指定的地面以外的区域来控制所述地面障碍物碰撞警报系统以自动地重新启动所述地面障碍物碰撞警报的传递。 在一些示例中，处理器被配置为基于飞机的地理位置，飞机的地面速度或两者来确定飞行器在指定的地面区域之外。

    Ground obstacle collision alert deactivation
    8.
    发明授权
    Ground obstacle collision alert deactivation 有权
    地面障碍物碰撞警报停用

    公开(公告)号：US09318025B2

    公开(公告)日：2016-04-19

    申请号：US14109093

    申请日：2013-12-17

    Applicant: Honeywell International Inc.

    Inventor： Kevin J Conner ,  Tomas Marczi ,  Christine Marie Haissig ,  John Howard Glover

    IPC: G08G5/00 ,  G08G5/06

    CPC classification number: G08G5/0021 ,  G08G5/0073 ,  G08G5/06 ,  G08G5/065

    Abstract: In some examples, a processor is configured to control a ground obstacle collision alerting system of an aircraft to deactivate delivery of ground obstacle collision alerts in response to determining the aircraft is in a designated ground area. In some examples, the processor is configured to determine the aircraft is in the designated ground area based on user input, based on a geographic location of the aircraft, or both. The processor is further configured to control the ground obstacle collision alerting system to automatically reactivate the delivery of the ground obstacle collision alerts in response to determining the aircraft is outside of the designated ground area. In some examples, the processor is configured to determine the aircraft is outside of the designated ground area based on a geographic location of the aircraft, a ground speed of the aircraft, or both.

    Abstract translation: 在一些示例中，处理器被配置为响应于确定飞行器在指定的地面区域来控制飞行器的地面障碍物碰撞警报系统以停用地面障碍物碰撞警报的传递。 在一些示例中，处理器被配置为基于飞行器的地理位置或两者来基于用户输入来确定飞行器在指定地面区域。 所述处理器还被配置为响应于确定所述飞机在所述指定的地面以外的区域来控制所述地面障碍物碰撞警报系统以自动地重新启动所述地面障碍物碰撞警报的传递。 在一些示例中，处理器被配置为基于飞机的地理位置，飞机的地面速度或两者来确定飞行器在指定的地面区域之外。

    System and method for providing model-based alerting of spatial disorientation to a pilot
    9.
    发明授权
    System and method for providing model-based alerting of spatial disorientation to a pilot 有权
    为飞行员提供基于模型的空间定向障碍警报的系统和方法

    公开(公告)号：US09205929B2

    公开(公告)日：2015-12-08

    申请号：US13943549

    申请日：2013-07-16

    Applicant: HONEYWELL INTERNATIONAL INC.

    Inventor： Kevin J Conner ,  Santosh Mathan ,  Steve Johnson

    IPC: G08B23/00 ,  B64D45/00 ,  A61B5/00 ,  G01C23/00 ,  G01C21/00 ,  G06F7/70

    CPC classification number: B64D45/00 ,  A61B5/00 ,  A61B5/4023 ,  A61B2503/22 ,  B64D2045/004

    Abstract: A system and method monitor aircraft state parameters, for example, aircraft movement and flight parameters, applies those inputs to a spatial disorientation model, and makes a prediction of when pilot may become spatially disoriented. Once the system predicts a potentially disoriented pilot, the sensitivity for alerting the pilot to conditions exceeding a threshold can be increased and allow for an earlier alert to mitigate the possibility of an incorrect control input.

    Abstract translation: 监视飞机状态参数（例如飞机运动和飞行参数）的系统和方法将这些输入应用于空间定向模型，并且对飞行员何时可能变得空间迷失方向进行预测。 一旦系统预测潜在迷失方向的飞行员，可以增加提醒飞行员超出阈值条件的灵敏度，并允许更早的警报来减轻错误的控制输入的可能性。

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