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11.
公开(公告)号:US20180225945A1
公开(公告)日:2018-08-09
申请号:US15426410
申请日:2017-02-07
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor: Zdenek Moravek , David Kunes , Ivan Lacko
CPC classification number: G08B21/0453 , A61B5/18 , G06Q10/0631 , G06Q10/063114 , G06Q10/06312 , G06Q10/0639 , G06Q10/06398 , G08B7/06 , G08B21/0476 , G08B21/182
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.
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公开(公告)号:US20180059907A1
公开(公告)日:2018-03-01
申请号:US15245317
申请日:2016-08-24
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor: David Kunes , Zdenek Moravek , Katerina Chmelarova , Ivan Lacko
IPC: G06F3/0484 , G08G5/02
CPC classification number: G06F3/04842 , G06F3/0482 , G06F3/04892 , G08G5/0013 , G08G5/0021 , G08G5/0039 , G08G5/0091 , G08G5/025
Abstract: A system and method for an improved aircraft information display is provided. The provided embodiments integrate and analyze relevant data from on-board and external sources to render airport availability and suitability information on the aircraft information display. The airport availability and suitability information displayed on the aircraft information display incorporates links between related information, is intuitively arranged on the aircraft information display, and dynamically updates responsive to changes in data and to user interaction.
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公开(公告)号:US09640079B1
公开(公告)日:2017-05-02
申请号:US15019675
申请日:2016-02-09
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor: Zdenek Moravek , Robert Sosovicka , Filip Magula , David Kunes , Katerina Sprinarova
CPC classification number: G08G5/0013 , G01C21/00 , G01C21/20 , G08G5/0021 , G08G5/0039 , G08G5/0052 , G08G5/0091 , G08G5/025
Abstract: Methods and systems are provided for generating an interim route that facilitates navigating a vehicle to an intended destination. One exemplary method facilitating an aircraft landing at an intended destination involves obtaining a current position of the aircraft, obtaining one or more time constraints for the intended destination, determining an interim route from the current aircraft position to the intended destination that veers towards a conditional diversion destination based at least in part on the one or more time constraints for the intended destination, and providing indication of the interim route to an aircraft operator, for example, by displaying a graphical representation of the interim route on a navigational map on a display device.
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公开(公告)号:US10854091B2
公开(公告)日:2020-12-01
申请号:US16026423
申请日:2018-07-03
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor: Zdenek Moravek , Ivan Lacko
Abstract: Methods and systems are provided for guiding or otherwise assisting a stabilized approach to a destination by presenting an energy state associated with an aircraft with respect to a target energy state for the stabilized approach. One method involves providing a graphical indication of a targeted energy state at a first position, a second graphical indication of a current energy state at a second position, and a third graphical indication of a configuration change at a third position. The distance with respect to a reference axis between the first position and the second position corresponds to a difference between a target parameter value associated with the targeted energy state and a current parameter value associated with the current energy state, and while a second distance between the first position and the third position with respect to the reference axis corresponds to an estimated amount of time before the configuration change.
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公开(公告)号:US20190307385A1
公开(公告)日:2019-10-10
申请号:US15949615
申请日:2018-04-10
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor: Zdenek Moravek , Pavel Badin
Abstract: Methods and systems for classifying a subject's cognitive state are provided. The method receives and stores sensor signals comprising a first sensor signal (SS_1) from a first sensor configured to sense a first aspect of the subject, and a second sensor signal (SS_2) from a second sensor configured to sense a second aspect of the subject. The validity of SS_1 and SS_2 are determined using a binary signal validity methodology and a weighted signal validity methodology. SS_1 and SS_2 are analyzed to identify patterns therein, and the patterns are defined as either an objective marker or a subjective marker. A subject profile is referenced and updated through multiple iterations. The subject's cognitive state is subsequently classified based on both adjusted subjective and objective markers.
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公开(公告)号:US10152195B2
公开(公告)日:2018-12-11
申请号:US14967557
申请日:2015-12-14
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor: Ivan Lacko , Yujia Cao , Zdenek Moravek , Stepan Dopita
IPC: G06F3/048 , G06F3/0481 , G01C23/00 , G08G5/00 , G08G5/02
Abstract: A computer-implemented flight display system including a computer processor that is capable of determining a current energy situation of an aircraft, an electronic display device, and a graphical user interface (GUI) provided on the electronic display device. The GUI includes a current aircraft position symbol, an optimal aircraft position symbol, and at least one symbol indicating a position for changing aircraft configuration. Relative positioning on the GUI of the optimal aircraft position system and the at least one symbol indicating a position for changing aircraft configuration is based at least in part on the determined current energy situation of the aircraft.
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公开(公告)号:US10086950B1
公开(公告)日:2018-10-02
申请号:US15473966
申请日:2017-03-30
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor: Zdenek Moravek , David Kunes , Katerina Chmelarova
Abstract: A method for presenting an alert onboard an aircraft, by a computing device comprising at least system memory, a processor, and a plurality of sensors, is provided. The method identifies a status of the aircraft, by the processor, from a plurality of avionics communicatively coupled to the computing device via a wireless data connection; determines that attention of a flight crew member is required by one of the plurality of avionics, based on the status; determines that the computing device is in a state of current use, based on user input data received by the plurality of sensors; and presents an alert associated with the status and the one of the plurality of avionics, via a display device communicatively coupled to the processor, wherein the alert comprises an indication to direct the attention toward the one of the plurality of avionics and details associated with the status.
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公开(公告)号:US20180068569A1
公开(公告)日:2018-03-08
申请号:US15258400
申请日:2016-09-07
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor: Katerina Chmelarova , Zdenek Moravek , David Kunes
CPC classification number: G08G5/0039 , B64D45/00 , G01C21/20 , G01C23/00 , G08G5/0021 , G08G5/0056 , G08G5/025
Abstract: Methods and systems are provided for indicating suggested or recommended diversion destinations with respect to segments of a planned route of travel. One exemplary method of presenting potential diversion airports for an aircraft involves identifying a flight path segment of a plurality of flight path segments between a departure location and a destination location based on a flight plan from the departure location to the destination location and identifying a subset of airports satisfying one or more filtering criteria with respect to the flight path segment. From among that subset, a recommended diversion airport is identified based on a viability ranking of the subset of airports with respect to the flight path segment and indication of the recommended diversion airport for the flight path segment is provided to a pilot or other user.
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公开(公告)号:US20170168658A1
公开(公告)日:2017-06-15
申请号:US14967557
申请日:2015-12-14
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor: Ivan Lacko , Yujia Cao , Zdenek Moravek , Stepan Dopita
IPC: G06F3/0481 , G08G5/02 , G08G5/00 , G01C23/00
CPC classification number: G06F3/0481 , G01C23/005 , G08G5/0021 , G08G5/025
Abstract: A computer-implemented flight display system including a computer processor that is capable of determining a current energy situation of an aircraft, an electronic display device, and a graphical user interface (GUI) provided on the electronic display device. The GUI includes a current aircraft position symbol, an optimal aircraft position symbol, and at least one symbol indicating a position for changing aircraft configuration. Relative positioning on the GUI of the optimal aircraft position system and the at least one symbol indicating a position for changing aircraft configuration is based at least in part on the determined current energy situation of the aircraft.
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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
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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