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    SYSTEM AND METHOD FOR MANAGING SPEED CONSTRAINTS DURING REQUIRED TIME OF ARRIVAL OPERATIONS
    2.
    发明申请
    SYSTEM AND METHOD FOR MANAGING SPEED CONSTRAINTS DURING REQUIRED TIME OF ARRIVAL OPERATIONS 有权
    在需要运行的时间内管理速度限制的系统和方法

    公开(公告)号：US20160069688A1

    公开(公告)日：2016-03-10

    申请号：US14477476

    申请日：2014-09-04

    Applicant: HONEYWELL INTERNATIONAL INC.

    Inventor： Michal Polansky ,  Erwan Paricaud ,  Dorothee De Villele ,  Zdenek Jancik

    IPC: G01C21/00

    CPC classification number: G01C21/00 ,  G05D1/0005 ,  G05D1/0202 ,  G05D1/101 ,  G08G5/00 ,  G08G5/0021 ,  G08G5/0052

    Abstract: A method and apparatus includes strategies for improving required time of arrival reliability by an aircraft comprising determining a speed correction for one of AT speed constraints or an AT or ABOVE speed constraints, wherein the determining is selected from one or more of the mechanisms from the group consisting of continuous RTA speed management between constraints, padding of the AT speed constraints and the AT or ABOVE speed constraints; decelerating proactively; and using a variable guidance margin, wherein the guidance margin is a speed change not reflected in a flight plan prediction.

    Abstract translation: 一种方法和装置包括用于改进飞机所需的到达时间可靠性的策略，包括确定AT速度约束或AT或上述速度约束之一的速度校正，其中所述确定是从所述组中的一个或多个机构中选择的 包括连续的RTA速度管理约束，AT速度限制的填充和AT或ABOVE速度约束; 主动减速 并且使用可变引导边缘，其中所述引导边距是未被反映在飞行计划预测中的速度变化。

    SYSTEM AND METHOD FOR ENABLING AUTOMATIC DIVERSION MANAGEMENT
    3.
    发明申请
    SYSTEM AND METHOD FOR ENABLING AUTOMATIC DIVERSION MANAGEMENT 审中-公开

    公开(公告)号：US20200273350A1

    公开(公告)日：2020-08-27

    申请号：US16286792

    申请日：2019-02-27

    Applicant: HONEYWELL INTERNATIONAL INC.

    Inventor： Monika Litvova ,  Zdenek Jancik ,  Dorothee De Villele ,  Rajesh Chaubey

    IPC: G08G5/00 ,  B64D43/00

    Abstract: An automatic diversion management system on-board an aircraft is provided. The diversion management system is configured to automatically detect a need for the aircraft to divert from a primary airport to a diversion airport; automatically initiate diversion planning to a suitable diversion airport responsive to detecting conditions that can cause a need for diversion; automatically create a diversion flight plan; automatically send a clearance request to air traffic control (ATC) for a first type of conditions causing a need for diversion and send a clearance request to ATC, responsive to flight crew action, for a second type of conditions causing a need for diversion; and automatically activate the diversion flight plan after receipt of ATC clearance for the first type of conditions causing a need for diversion and activate the diversion flight plan, responsive to flight crew action, for the second type of conditions causing a need for diversion.

    System and method for determining and displaying optimized aircraft energy level
    4.
    发明授权
    System and method for determining and displaying optimized aircraft energy level 有权

    公开(公告)号：US11113978B2

    公开(公告)日：2021-09-07

    申请号：US15265330

    申请日：2016-09-14

    Applicant: HONEYWELL INTERNATIONAL INC.

    Inventor： Dorothee De Villele ,  Erwan Paricaud ,  Daniel Corbel ,  Michal Polansky ,  Zdenek Jancik

    IPC: G08G5/02 ,  B64D43/02 ,  G01C23/00 ,  G08G5/00 ,  B64D45/08

    Abstract: A system and method of displaying optimized aircraft energy level to a flight crew includes processing flight plan data, in a processor, to determine the optimized aircraft energy level along a descent profile of the aircraft from cruise altitude down to aircraft destination, and continuously processing aircraft data, in the processor, to continuously determine, in real-time, an actual aircraft energy level. The actual aircraft energy level of the aircraft is continuously compared, in the processor, to the optimized aircraft energy level. The processor is use to command a display device to render an image that indicates: (i) the optimized aircraft energy level, (ii) how the actual aircraft energy level differs from the optimized aircraft energy level, and (iii) how the actual aircraft energy level is trending relative to the optimized aircraft energy level.

    Systems and methods for generating a recapture path for an aircraft
    5.
    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
    6.
    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.

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