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    AIRCRAFT SYSTEMS AND METHODS WITH ENHANCED NOTAMS
    3.
    发明申请
    AIRCRAFT SYSTEMS AND METHODS WITH ENHANCED NOTAMS 有权
    飞机系统及其增强方法

    公开(公告)号：US20160209234A1

    公开(公告)日：2016-07-21

    申请号：US14601641

    申请日：2015-01-21

    Applicant: Honeywell International Inc.

    Inventor： Bretislav Passinger ,  Petr Hornych ,  Dominik Vahala ,  Ivan Lacko

    IPC: G01C23/00 ,  G08G5/00 ,  B64D43/00

    CPC classification number: G08G5/0047 ,  B64D43/00 ,  G01C23/00

    Abstract: An aircraft system includes a processing unit configured to receive navigation data and notice to airmen (NOTAM) information and to generate display signals based on the navigation data and the NOTAM information. The system further includes a display device coupled to the processing unit and configured to render an image according to the display signals with a first area depicting a navigation display based on the navigation data and a second area depicting a list of NOTAM text messages.

    Abstract translation: 飞机系统包括：处理单元，被配置为接收导航数据并通知飞行员（NOTAM）信息，并且基于导航数据和NOTAM信息生成显示信号。 所述系统还包括耦合到所述处理单元并被配置为根据所述显示信号渲染图像的显示设备，所述显示信号具有基于所述导航数据描绘导航显示的第一区域和描绘NOTAM文本消息列表的第二区域。

    Systems and methods for generating a recapture path for an aircraft
    4.
    发明授权
    Systems and methods for generating a recapture path for an aircraft 有权

    公开(公告)号：US11043131B2

    公开(公告)日：2021-06-22

    申请号：US16285367

    申请日：2019-02-26

    Applicant: HONEYWELL INTERNATIONAL INC.

    Inventor： Dorothee De Villele ,  Marek Batelka ,  Rajesh Chaubey ,  Jim Rumbo ,  Kiran Mancheiah Venkataramana ,  Daniel Corbel ,  Zdenek Moravek ,  Ivan Lacko ,  Zdenek Jancik

    IPC: G08G5/00 ,  G08G5/04 ,  B64D45/00

    Abstract: Provided are enhanced flight guidance systems and methods for an aircraft. The method includes recognizing when the aircraft is in manual operation and an active flight path is different than the planned flight path. An interrupt is received and categorized as one of (i) obstacle, (ii) equipment/fuel, or (iii) pilot health monitor. A managed mode begins, including identifying a rejoining leg of the planned flight path at which to rejoin and a location on the rejoining leg at which to rejoin. A recapture path strategy is selected from (i) lateral, (ii) vertical, and (iii) mixed lateral and vertical. A recapture path to the location on the rejoining leg is computed. The computed recapture path includes speed targets and configuration requirements at dedicated points along the recapture path. Aircraft state data along the recapture path is predicted and guidance controls for the aircraft along the recapture path are generated.

    SYSTEMS AND METHODS FOR GENERATING A RECAPTURE PATH FOR AN AIRCRAFT
    5.
    发明申请
    SYSTEMS AND METHODS FOR GENERATING A RECAPTURE PATH FOR AN AIRCRAFT 审中-公开

    公开(公告)号：US20200273349A1

    公开(公告)日：2020-08-27

    申请号：US16285367

    申请日：2019-02-26

    Applicant: HONEYWELL INTERNATIONAL INC.

    Inventor： Dorothee De Villele ,  Marek Batelka ,  Rajesh Chaubey ,  Jim Rumbo ,  Kiran Mancheiah Venkataramana ,  Daniel Corbel ,  Zdenek Moravek ,  Ivan Lacko ,  Zdenek Jancik

    IPC: G08G5/00 ,  G08G5/04 ,  B64D45/00

    Abstract: Provided are enhanced flight guidance systems and methods for an aircraft. The method includes recognizing when the aircraft is in manual operation and an active flight path is different than the planned flight path. An interrupt is received and categorized as one of (i) obstacle, (ii) equipment/fuel, or (iii) pilot health monitor. A managed mode begins, including identifying a rejoining leg of the planned flight path at which to rejoin and a location on the rejoining leg at which to rejoin. A recapture path strategy is selected from (i) lateral, (ii) vertical, and (iii) mixed lateral and vertical. A recapture path to the location on the rejoining leg is computed. The computed recapture path includes speed targets and configuration requirements at dedicated points along the recapture path. Aircraft state data along the recapture path is predicted and guidance controls for the aircraft along the recapture path are generated.

    On-duty/off-duty work alternation planning based on sensed physiological and activity parameters
    6.
    发明授权
    On-duty/off-duty work alternation planning based on sensed physiological and activity parameters 有权

    公开(公告)号：US10055963B1

    公开(公告)日：2018-08-21

    申请号：US15426410

    申请日：2017-02-07

    Applicant: HONEYWELL INTERNATIONAL INC.

    Inventor： Zdenek Moravek ,  David Kunes ,  Ivan Lacko

    IPC: G08B21/00 ,  G08B21/04 ,  G08B7/06 ,  G08B21/18 ,  G06Q10/06

    Abstract: A system and method for alerting an on-duty operator of the need to transfer operational control to an off-duty operator includes processing first and second physiological and activity data from the on-duty operator and the off-duty operator, respectively. The processor compares the fatigue state of the on-duty operator to a predetermined fatigue state threshold, and the rest state of the off-duty operator to a predetermined rest state threshold. The processor will generate an alert signal indicating that the on-duty operator should transfer operational control to the off-duty operator when (i) the fatigue state of the on-duty operator exceeds the predetermined fatigue state threshold or (ii) the rest state of the off-duty operator exceeds the predetermined rest state threshold.

    Methods and systems facilitating stabilized descent to a diversion airport
    8.
    发明授权
    Methods and systems facilitating stabilized descent to a diversion airport 有权

    公开(公告)号：US10134289B2

    公开(公告)日：2018-11-20

    申请号：US15047355

    申请日：2016-02-18

    Applicant: HONEYWELL INTERNATIONAL INC.

    Inventor： Zdenek Moravek ,  Robert Sosovicka ,  Filip Magula ,  David Kunes ,  Katerina Sprinarova ,  Ivan Lacko

    IPC: G06F19/00 ,  G06G7/70 ,  G08G5/00 ,  B64C9/38 ,  G05D1/06 ,  G08G5/02

    Abstract: Methods and systems are provided for guiding or otherwise assisting operation of a vehicle to intersect a stabilized approach to a destination. One exemplary method of assisting an aircraft for landing at an airport involves obtaining, from a system onboard the aircraft, a current position of the aircraft and a current velocity of the aircraft, determining a descent strategy for the aircraft from the current position to an initialization point for a stable approach to the airport based at least in part on the current position and the current velocity, and providing indication of the descent strategy on a display device. The descent strategy is determined based on one or more validation criteria associated with the initialization point so that one or more predicted values for one or more characteristics of the aircraft satisfy the one or more validation criteria at the initialization point.

    Aircraft systems and methods for detecting non-compliant pilot action
    10.
    发明授权
    Aircraft systems and methods for detecting non-compliant pilot action 有权
    用于检测不符合标准的飞行员行动的飞机系统和方法

    公开(公告)号：US09446852B2

    公开(公告)日：2016-09-20

    申请号：US14030426

    申请日：2013-09-18

    Applicant: HONEYWELL INTERNATIONAL INC.

    Inventor： Ivan Lacko ,  Jiri Vasek ,  Petr Uhlir

    IPC: G08G5/00 ,  B64D45/00

    CPC classification number: B64D45/00 ,  G08G5/0013 ,  G08G5/0021

    Abstract: Aircraft systems and methods for detecting non-compliant pilot action are provided. The method includes analyzing an outbound communication from an aircraft to recognize a word or phrase corresponding to a parameter associated with a prior request for pilot action. If the word or phrase is recognized, the method further includes storing data corresponding to the outbound communication in a data storage device. The stored data and pilot action taken are compared to determine if there is a discrepancy between the pilot action and the stored data. A discrepancy alert is outputted if the discrepancy is determined to exist. A predetermined time interval is timed from the outbound communication. A timeout alert is outputted at a timeout of the predetermined time interval unless the requested pilot action is taken within the predetermined time interval.

    Abstract translation: 提供了用于检测不合规导频动作的飞行器系统和方法。 该方法包括分析来自飞行器的出站通信以识别与先前对先导动作请求相关联的参数相对应的单词或短语。 如果该单词或短语被识别，则该方法还包括将对应于出站通信的数据存储在数据存储设备中。 比较所存储的数据和导频操作，以确定导频操作和存储的数据之间是否存在差异。 如果确定存在差异，则输出差异警报。 从出站通信定时预定的时间间隔。 在预定时间间隔的超时时间内输出超时警报，除非在预定的时间间隔内进行所请求的导频操作。

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