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公开(公告)号：US11120694B2
公开(公告)日：2021-09-14
申请号：US16672096
申请日：2019-11-01
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Luis Melendez , Philip Sin , John Koenig , Michael Mast
Abstract: Technologically improved flight guidance systems and methods that generate thrust guidance related to a potential flight path angle are provided. The thrust guidance is provided as acceleration commands that may be communicated to the pilot in an intuitive manner, such as with an acceleration cue on a primary flight display (PFD) system. The provided acceleration cues are uniform across the flight envelope and present consistently for two basic thrust guidance modes.
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公开(公告)号：US20240274018A1
公开(公告)日：2024-08-15
申请号：US18646203
申请日：2024-04-25
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Michael Mast , Yuta Morioka , Jeffrey Glenn
Abstract: Flight guidance methods, systems, and aircraft systems providing assist-to-land and emergency land (EL) functions. The method includes generating a visual indication of the availability and status of an assist-to-land function and an EL function when the current altitude of the aircraft exceeds an altitude threshold. When in assist-to-land, visual and audible flight guidance can be generated to guide the pilot to a safe landing at a selected runway or at a best runway for the conditions. Functions can be activated by user manipulations of interface objects and/or by software determinations. Software determinations to enter the EL function can automatically control the flying of the aircraft along an approach profile to a safe landing at a nearest suitable airport. EL determinations can be made based on pilot incapacitation.
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公开(公告)号：US20210287560A1
公开(公告)日：2021-09-16
申请号：US17180954
申请日：2021-02-22
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Michael Mast , Yuta Morioka , Jeffrey Glenn
Abstract: Flight guidance methods, systems, and aircraft systems providing assist-to-land and emergency land (EL) functions. The method includes generating a visual indication of the availability and status of an assist-to-land function and an EL function when the current altitude of the aircraft exceeds an altitude threshold. When in assist-to-land, visual and audible flight guidance can be generated to guide the pilot to a safe landing at a selected runway or at a best runway for the conditions. Functions can be activated by user manipulations of interface objects and/or by software determinations. Software determinations to enter the EL function can automatically control the flying of the aircraft along an approach profile to a safe landing at a nearest suitable airport. EL determinations can be made based on pilot incapacitation.
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公开(公告)号：US20240420582A1
公开(公告)日：2024-12-19
申请号：US18815130
申请日：2024-08-26
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Michael Blaine Johnson , Michael Mast , Jan Urbanec , Emmanuel Letsu-Dake , Nichola Lubold
Abstract: Methods and systems are provided for assisting operation of a vehicle by automatically initiating activation of an automated functionality, such as autoland functionality of an aircraft, in the absence of user input within one or more monitoring periods. One method involves identifying a triggering event, identifying a monitoring period associated with the triggering event, monitoring one or more components for user input within the monitoring period associated with the triggering event, and automatically initiating activation of an automated functionality associated with the vehicle in the absence of user input within the monitoring period associated with the triggering event. In some implementations, the monitoring period adaptively and dynamically varies during operation.
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公开(公告)号：US11745896B2
公开(公告)日：2023-09-05
申请号：US17930124
申请日：2022-09-07
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Michael Mast , Yuta Morioka , Martin Jezek , Jeffrey Glenn
CPC classification number: B64D45/00 , B64D43/02 , B64D45/08 , G05D1/105 , G08G5/0047 , G08G5/025 , B64D2045/0085
Abstract: Flight guidance systems and methods that provide an airport selection in response to an EO condition in a single engine plane. The airport selection takes into consideration factors such as optimal approach type, runway length, weather, terrain, remaining battery time, and the like. Additionally, various also generate and display a visual indication of a remaining glide range when the EO condition is happening; the remaining glide range determination is based, at least in part, on terrain.
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Patent Agency Ranking
公开(公告)号：US11511883B2
公开(公告)日：2022-11-29
申请号：US17179957
申请日：2021-02-19
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Michael Mast , Yuta Morioka , Martin Jezek , Jeffrey Glenn
Abstract: Flight guidance systems and methods that provide an airport selection in response to an EO condition in a single engine plane. The airport selection takes into consideration factors such as optimal approach type, runway length, weather, terrain, remaining battery time, and the like. Additionally, various also generate and display a visual indication of a remaining glide range when the EO condition is happening; the remaining glide range determination is based, at least in part, on terrain.
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公开(公告)号：US20210065558A1
公开(公告)日：2021-03-04
申请号：US16672096
申请日：2019-11-01
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Luis Melendez , Philip Sin , John Koenig , Michael Mast
Abstract: Technologically improved flight guidance systems and methods that generate thrust guidance related to a potential flight path angle are provided. The thrust guidance is provided as acceleration commands that may be communicated to the pilot in an intuitive manner, such as with an acceleration cue on a primary flight display (PFD) system. The provided acceleration cues are uniform across the flight envelope and present consistently for two basic thrust guidance modes.
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公开(公告)号：US12112649B2
公开(公告)日：2024-10-08
申请号：US17411957
申请日：2021-08-25
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Michael Blaine Johnson , Michael Mast , Jan Urbanec , Emmanuel Letsu-Dake , Nichola Lubold
CPC classification number: G08G5/025 , G08G5/0021 , G08G5/0039 , G08G5/0056
Abstract: Methods and systems are provided for assisting operation of a vehicle by automatically initiating activation of an automated functionality, such as autoland functionality of an aircraft, in the absence of user input within one or more monitoring periods. One method involves identifying a triggering event, identifying a monitoring period associated with the triggering event, monitoring one or more components for user input within the monitoring period associated with the triggering event, and automatically initiating activation of an automated functionality associated with the vehicle in the absence of user input within the monitoring period associated with the triggering event. In some implementations, the monitoring period adaptively and dynamically varies during operation.
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公开(公告)号：US12020583B2
公开(公告)日：2024-06-25
申请号：US17180954
申请日：2021-02-22
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Michael Mast , Yuta Morioka , Jeffrey Glenn
CPC classification number: G08G5/025 , B64C9/00 , B64C13/16 , B64D43/00 , B64D45/08 , G05D1/042 , G05D1/101 , G08G5/0013
Abstract: Flight guidance methods, systems, and aircraft systems providing assist-to-land and emergency land (EL) functions. The method includes generating a visual indication of the availability and status of an assist-to-land function and an EL function when the current altitude of the aircraft exceeds an altitude threshold. When in assist-to-land, visual and audible flight guidance can be generated to guide the pilot to a safe landing at a selected runway or at a best runway for the conditions. Functions can be activated by user manipulations of interface objects and/or by software determinations. Software determinations to enter the EL function can automatically control the flying of the aircraft along an approach profile to a safe landing at a nearest suitable airport. EL determinations can be made based on pilot incapacitation.
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10.发明申请公开(公告)号：US20230002071A1
公开(公告)日：2023-01-05
申请号：US17930124
申请日：2022-09-07
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： Michael Mast , Yuta Morioka , Martin Jezek , Jeffrey Glenn
Abstract: Flight guidance systems and methods that provide an airport selection in response to an EO condition in a single engine plane. The airport selection takes into consideration factors such as optimal approach type, runway length, weather, terrain, remaining battery time, and the like. Additionally, various also generate and display a visual indication of a remaining glide range when the EO condition is happening; the remaining glide range determination is based, at least in part, on terrain.
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